Proposed Classification System for Smart Materials and Systems Category Fundamental Material Characteristics Fundamental System Behaviors Traditional materials: Materials have given prop
Trang 2Leadingedge
TrailingedgeDynamic pressure
Active aeroelastic wing: Blending ofleading and trailing edge effectiveness
Figure 22 Achievable roll performance by combining leading
and trailing edges.
for example, by an all-movable aerodynamic surface that
has adaptive rotational attachment stiffness This also
pro-vides high effectiveness at low speeds, and excessive loads
from diverging components or flutter instabilities at high
speeds can be avoided
The usable aeroelastic effectiveness for conventional
concepts is rather limited between take-off and cruise
speed Aileron reversal usually occurs between the cruise
speed and limit speed, and too high an effectiveness of
lead-ing edge surfaces must be avoided at the limit speed On
the other hand, adaptive all-movable concepts can provide
high effectiveness at all speeds and avoid excessive loads at
the high end of the speed envelope, as indicated in Figs 23
and 24 This means, for example, that a stabilizer surface
can be built smaller than would be required by “rigid”
aero-dynamic low-speed performance
NEED FOR ANALYZING AND OPTIMIZING THE DESIGN
OF ACTIVE STRUCTURAL CONCEPTS
Of course, active materials and structural components,
together with the stimulating forces, need a correct
Active aeroelastic conceptsRange of aeroelastic
1.0
Rigid aircraft
Figure 23 Aeroelastic effectiveness of conventional and
adaptive-all-movable active aeroelastic concepts.
For conventional activeaeroelastic concepts
Usable range of aeroelastic effectiveness byflight envelope
For advanced activeaeroelastic concept
Dynamic pressure Dynamic pressure
Figure 24 Usable range of aeroelastic effectiveness for
conven-tional and advanced active aeroelastic concepts.
description in theoretical structural or multidisciplinaryanalysis and optimization (MDAO) models and methods.Once this is provided, the actively deforming structureneeds another approach for static aeroelastic analysis Thedeflections of selected control surfaces of an aircraft thathas conventional control surfaces can be predescribed foraeroelastic analysis For an actively deformed structure,initial deformations without external loads first need to bedetermined, for example, by static analysis
As described before, the deformations achievable in junction with the distribution of external aerodynamicloads are essential for the effectiveness of active structuralconcepts for aircraft control This requires efficient toolsand methods for simultaneous, multidisciplinary analyti-cal design The best design involves optimizing
con-rexternal shape,
rarranging the passive structure (topology),
rsizing the passive structure,
rplacing and sizing the active elements, and
ra control concept for the active components.
The aims of this approach are the optimum result for theobjective function (minimum weight, aerodynamic perfor-mance), fulfillment of all constraints like strength, and alsooptimization of additional objectives, such as minimum en-ergy As depicted in Fig 25 for the optimization of a passivestructure that has different constraints for the requiredrolling moment effectiveness, the energy required to actu-ate the control surface can be considerably reduced, even
if the required (low) roll rate is already met
MDO does not mean combining single discipline lytic tools by formal computing processes It means first agood understanding of what is going on This is essentialfor a conventional design Only from this understandingcan the creative design of an active concept start
ana-It is also very important to choose the proper analyticmethods for individual disciplines Usually, not the high-est level of accuracy is suitable for the simulation of impor-tant effects for other disciplines This also refers to refin-ing the analytic models, where local details are usually not
Trang 3Structural weight
Rollingmoment
effectiveness
Baselinestaticdesign1.0
Aileronhinge moment [kNm]
Rigid
50.0
10.0
Figure 25 Optimization of the rolling moment and hinge
mo-ment of a trailing edge aileron of a low aspect ratio fighter wing.
interesting for interactions It is more important to keep
the models as versatile as possible for changes in the
de-sign concepts and to allow the simulation as many variants
as possible This also means an efficient process for
gener-ating models, including the knowledge of the user for this
process Fully automated model generators can create
ter-rible results, if the user cannot interpret or understand the
modeling process
Any improvement in a technical system is often referred
to as an optimization In structural design today, this
ex-pression is mainly used for formal analytic and numerical
methods Some years after the introduction of finite
ele-ment methods (FEM) for analyzing aircraft structures, the
first attempts were made to use these tools in an automated
design process Although the structural weight is usually
used as the objective function for optimization, the major
advantage of these tools is the fulfillment of aeroelastic
con-straints, not the weight saving Other than static strength
requirements, which can be met by adjusting the
dimen-sions of individual finite elements, the sensitivities of the
elements to aeroelastic constraints cannot be expressed so
easily
In the world of aerodynamics, the design of the required
twist and camber distribution for a desired lift at minimum
drag is also an optimization task Assuming that minimum
drag is achieved by an elliptical lift distribution along the
wingspan, this task can be solved by a closed formal
so-lution and potential flow theory More sophisticated
nu-merical methods are required for the 2-D airfoil design or
for Euler and Navier–Stokes CFD methods, which are now
maturing for practical use in aircraft design
Formal optimization methods have been used for
con-ceptual aircraft design for many years Here, quantities
such as direct operating costs (DOC) can be expressed by
rather simple equations, and the structural weight can be
derived from empirical data Formal methods such as
op-timum control theory are also available for designing the
flight control system
So, one might think that these individual optimization
tasks could easily be combined into one global aircraft
op-timization process The reasons that this task is not so
simple is the different natures of the design variables of dividual disciplines and their cross sensitivities with otherdisciplines The expression multidisciplinary optimization(MDO) summarizes all activities in this area, which haveintensified in recent years It must be admitted that todaymost existing tools and methods in this area are still singlediscipline optimization tasks that have multidisciplinaryconstraints
in-To design and analyze active aeroelastic aircraft cepts, especially when they are based on active materials
con-or other active structural members, new quantities are quired to describe their interaction with the structure, theflight control system, and the resulting aeroelastic effects
re-SUMMARY, CONCLUSIONS, AND PREDICTIONS
In the same way as it was wrong in the past to demandthat an aircraft design to be as rigid as possible, it’s wrongnow to demand a design that is as flexible as possible
It is sometimes said that smart structural concepts cancompletely replace conventional control surfaces But thislooks very unrealistic, at least at the moment The majordifficulties for successful application are the limited defor-mation capacity of active materials, as well as their strainallowables, which are usually below those of the passivestructure However, this can be resolved by proper design
of the interface between the passive and active structures.But the essential difficulties are the stiffness and strainlimitations of the passive structure itself It cannot be ex-pected that the material of the passive structure just needs
to be replaced by more flexible materials without an sive weight penalty It is also not correct to believe that
exces-an active aeroelastic concept becomes more effective, if theflexibility of the structure is increased Aeroelastic effec-tiveness depends on proper aeroelastic design, which needscertain rigidity of a structure to produce the desired loads
A very flexible structure would also not be desirable fromthe standpoints of aerodynamic shape, stability of the flightcontrol system, and transmission of static loads
Because large control surface deflections are required
at low speeds, where aeroelastic effects on a fixed surfaceare small, it is more realistic to use conventional controlsurfaces for this part of the flight envelope and use activeaeroelastic deformations only at higher speeds This wouldstill save weight on the control surfaces and their actua-tion system due to the reduced loads and actuation powerrequirements
To produce usable deformations of the structure also atlow speeds, all-movable aerodynamic surfaces that have
a variable attachment stiffness are an interesting option.This concept relies on development efforts for active de-vices that have a wide range of adjustable stiffness.The reasons that we have not seen more progress to date
in successfully demonstrating smart structural concepts inaeronautics may be that
rspecialists in aircraft design do not know enough
about the achievements in the area of smart rials and structures, and
mate-rsmart materials and actuation system specialists,
who try to find and demonstrate applications in
Trang 4aeronautics, do not know or care enough about world conditions for airplane structures.
real-What we need is more awareness on both sides, as well
as stronger efforts to learn from each other and work
together
Although there are strong doubts about useful
applica-tions of smart structures for aircraft control, it should
al-ways be remembered how often leading experts have been
wrong in the past in their predictions, in many cases even
on their own inventions Norman R Augustine quotes some
of them in his famous book “Augustine’s Laws” (46):
r“The [flying] machines will eventually be fast; they
will be used in sport but they should not be thought of
as commercial carriers.” – Octave Chanute, aviationpioneer, 1910
r“The energy produced by the breaking down of the
atom is a very poor kind of thing Anyone who expects
a source of power from the transformation of theseatoms is talking moonshine – Ernest Rutherford,physicist, ca 1910
r“Fooling around with alternative currents is just a
waste of time Nobody will use it, ever It’s too gerous it could kill a man as quick as a bolt of
dan-lightning Direct current is safe.” – Thomas Edison,inventor, ca 1880
Also quoted by Augustine (46), the eminent scientist Niels
Bohr remarked: “Prediction is very difficult, especially
about the future.”
At the moment it looks more realistic that new hybrid,
concentrated active devices, positioned between a passive
but properly aeroelastically tailored main aerodynamic
surface and the corresponding control surfaces are showing
the like Hopefully this article will inspire useful
applica-tions of smart structures and prevent some unnecessary
3 W Schwipps, Schwerer als Luft—die Fr ¨ uhzeit der
Flugtech-nik in Deutschland Bernhard & Graefe Verlag, Koblenz,
Germany, 1984.
4 M.I Woods, J.F Henderson, and G.D Lock, Aeronaut J.
(2001).
5 E Pendleton, B Sanders, P Flick, and O Sensburg Int Forum
Aeroelasticity Struct Dynamics, Madrid, Spain, 2001.
6 J.J Bertin and M.L Smith, Aerodynamics for Engineers.
Prentice-Hall, Englewood Cliffs, NJ,1979.
7 O Sensburg, H H¨onlinger, T.E Noll, L.J Huttsell, J Aircraft
19 (5): 1981.
8 C.R Larson, E Falanges, S.K Dobbs, SPIEs 5th Annu Int.
Symp Smart Struct Mater., San Diego, CA, 1998.
9 C.R Crowe and J.M Sater, AGARD Symp Future Aerosp.
Technol Serv Alliance, Paris, 1997, CP-600, Vol I.
10 A.R McGowan, J Heeg, and R.C Lake, Proc 37th AIAA/ ASME/ASCE/AHS/ASC Struct Struct Dynamics Mater Conf., Salt Lake City, UT, 1996.
11 O.L Skopik, Wie berechnet und konstruiert man selbst ein Flugzeug Vienna, Austria, 1917.
12 C.M Christensen, The Innovator’s Dilemma Harvard
Busi-ness School Press, Boston, 1997.
13 H.I Flomenhoft, The Revolution in Structural Dynamics
Dy-naflow Press, Palm Beach Gardens, FL, 1997.
14 A.R Collar, J R Aeronaut Soc 613–636, August 1946.
15 J Schweiger, J Simpson, F Weiss, E Coetzee, and Ch Boller,
SPIEs 6th Annu Int Symp Smart Structures Mater., Newport
Beach, CA, 1999.
16 T.A Weisshaar, RTO Meet Proc 36 (AC/323(AVT)TP/17) from the RTO AVT Specialists’ Meet Struct Aspects Flexible Aircraft Control, Ottawa, Canada, October 1999.
17 E.W Pendleton, D Bessette, P.B Field, G.D Miller, K.E.
Griffin, and J Aircraft 37(4), (2000).
18 J Aircraft 32(1), Special Section (1995).
19 O Sensburg, G.; Schneider, V.; Tischler, and V Venkayya, cialists’ Meet Struct Aspects Flexible Aircraft Control RTA Meet Design Issues, Ottawa, Canada; October 1999.
Spe-20 A.H.G Fokker and B Gould, Flying Dutchman The Life of Anthony Fokker Henry Holt, NY, year unknown.
21 T Noll, H H¨onlinger, O Sensburg, and K Schmidt, Active Flutter Suppression Design and Test, a Joint U:S.-F.R.G Pro- gram ICAS- CP 80-5.5 Munich, Germany, 1980.
22 K.B Lazarus, E Saarmaa, and G.S Agnes, Active Smart terial System for Buffet Load Alleviation Bellingham, WA,
Ma-1995, SPE Vol 22447/179.
23 R.M Hauch, J.H Jacobs, K Ravindra, and C Dima, Reduction
of Vertical Tail Buffet Response Using Active Control CP-95-1080, Washington, 1995.
AIAA-24 R.W Moses, 40th AIAA-SDM Con., St Louis, 1999.
25 J Simpson and J Schweiger, SPIE 5th Annu Int Symp Smart Struct and Mater., San Diego, CA, 1998.
26 T.A Weisshaar, J Aircraft 17(6), (1980).
27 J Schweiger, J Krammer, and H H¨ornlein, 6th AIAA/NASA/ ISSMO Symp Multidisciplinary Anal Optimization, Seattle,
WA, 1996, CP-4169.
28 N Khot, F Eastep, and R Kolonay, A Method for ment of the Rolling Maneuver of a Flexible Wing AIAA-CP-96- 1361.
Enhance-29 K Griffin and M Hopkins, 36th AIAA Struct Struct mics Mater Conf., New Orleans, 1995.
Dyna-30 C.L Giese, G.W Reich, M.A Hopkins, and K.E Griffin, An Investigation of the Aeroelastic Tailoring for Smart Structures Concept AIAA-96-1575-CP, 1996.
31 A.R McGowan, L.G Horta, J.S Harrison, and D.L Raney,
RTO Meet Proc 36 (AC/323(AVT)TP/17) RTO AVT ists’ Meet Struct Aspects Flexible Aircraft Control, Ottawa,
Special-Canada, October 1999.
32 S.L Padula, J.L Rogers, and D.L Raney,
Multidisci-plinary Techniques and Novel Aircraft Control Systems 8th AIAA/NASA/ISSMO Symp Multidisciplinary Anal Opti- mization, Long Beach, CA, 2000, AIAA-CP-2000-4848.
33 J Aircraft 32(1), Special Section (1995).
34 E Pendleton, K.E Griffin, M.W Kehoe, and B Perry, Conf Proc AIAA-96-1574-CP.
35 P.M Flick and M.H Love, Specialists’ Meet Struct Aspects Flexible Aircraft Control, RTA Meet Design Issues, Ottawa,
Canada, October 1999.
Trang 536 S.I Kuzmina, G.A Amiryants, F.Z Ishmuratov, V.A Mosunov,
and V.V Chedrik, Int Forum Aeroelasticity Struct Dynamics,
Madrid, Spain, 2001.
37 J Schweiger and O Sensburg, Int Forum Aeroelasticity
Struct Dynamics, Madrid, Spain, 2001.
38 R.W Moses, CP, 40th AIAA-SDM Conf., St Louis, 1999.
39 J Simpson and J Schweiger, Industrial Approach to
Piezo-electric Damping of Large Fighter Aircraft Components SPIE
6th Annu Int Symp Smart Struct Mater., San Diego, CA,
1998.
40 A.R McGowan, SPIE 5th Annu Int Symp Smart Struct.
Mater., Newport Beach, CA, 1999.
41 T.A Weisshaar, 41st Annu Isr Conf Aerosp Sci., Tel Aviv and
Haifa, February 2001.
42 R Barrett, in Smart Materials and Structures No 5, IOP, UK,
1996.
43 P Costa, P.A Moniz, and A Suleman, 42nd AIAA SDM Conf.,
Seattle, WA, 2001, AIAA-2001-1361.
44 H.P Monner, E Breitbach, Th Bein, and H Hanselka,
Aero-naut J 104(1032), (2000).
45 J Schweiger, F Weiss, T Kullrich, 8th AIAA/USAF/NASA/
ISSMO Symp Multidisciplinary Anal Optimization, Long
Beach, CA, September 2000.
46 N.R Augustine, Augustine’s Laws AIAA, Reston, VA, 1997.
An inextricable link has existed historically between
a building’s characteristics—form, appearance, and
function—and the characteristics of the different
materi-als that were available and suitable for construction As
exemplified by historical building traditions in stone and
wood, early architects sought to understand intuitively
the intrinsic physical behavior of commonly available
materials to exploit their properties in designing and
constructing buildings Conversely, later innovations in
the type and availability of materials strongly impacted
the development of new architectural forms as architects
began to respond to changing societal demands and new
building functions emerged This trend is illustrated by
the development of steel in the nineteenth century and
the related emergence of long-span and high-rise building
forms Today, architects are beginning to look forward to
using the developments in smart materials to bring new
solutions to long-standing problems and also to exploit the
potential of smart materials in developing new building
functions, forms, and responses The wide variety of smart
materials available has great potential for use within the
field, but, in this area, their applications remain only
marginally explored
MATERIAL CONSIDERATIONS IN ARCHITECTURE
Unlike materials used for specific applications or productssuch as in refractory linings or engine blocks that arefundamentally chosen on the basis of performance crite-ria and cost, the choice of materials for architectural usehas always been based on very different types of criteria.Performance and cost obviously play a role, but the finalselection is often based on appearance and aesthetics, ease
of constructability in terms of labor skill, local or regionalavailability, as well as the material used in nearby exist-ing buildings The multimodal nature of the selection pro-cess coupled with the wide-ranging array of building types,uses, and locales has resulted in a material palette that en-compasses all of the major material classes
TRADITIONAL MATERIAL CLASSIFICATIONS
IN ARCHITECTURE
The Construction Specification Institute (or CSI) devised
a classification system in 1948 that is used throughoutthe architectural design and building construction indus-tries The classification system is bipartite: the first half
is devoted to the broad classes of materials typically used
in buildings, including paint, laminate, and concrete, andthe second half categorizes standard building componentssuch as doors, windows, and insulation The emphasis inboth major groupings is on application, not on fundamentalbehavior or properties For example, in Division 6 the char-acteristics of wood are discussed in relationship to theirrelevance to the intended application: the grade of woodsuitable for load-bearing roof structures or the type of woodsuitable for finish flooring
The CSI index serves as a template for communicationamong architects, contractors, fabricators, and suppliers.After the preliminary design of a building is completedand approved, architects prepare construction documents(known as CDs) that will serve as the “instructions” forconstructing the building Accompanying each set of CDsare the “Construction Specifications”: a textual documentthat defines each building element documented in the CDsand specifies the material or component The ConstructionSpecifications serve as a binding contract that construc-tion professionals and contractors must follow Trade asso-ciations and manufacturers of building products routinelywrite their material and product specifications in CSI for-mat to streamline the specification process for architects,and many architectural firms maintain an internal set ofConstruction Specifications that is used as the baseline forall of their projects
TRADITIONAL TECHNOLOGY CLASSIFICATION
IN ARCHITECTURE
The CSI index also categorizes the technologies used inarchitectural design and construction Unlike the standardtechnology classifications used in engineering sciencesthat categorize according to process and product, theCSI specifications categorize by system As in the CSI
Trang 6material classes, the focus of the technology classes is
also on application The technologies are divided into
two major groups: the first is devoted to building
op-erational systems such as HVAC, lighting, and
plumb-ing systems, and the second is devoted to buildplumb-ing
con-struction systems such as structural, drainage, and
ver-tical circulation systems The specifications for the
build-ing operational systems are almost entirely supplied by
manufacturers
PROPOSED CLASSIFICATION SYSTEM
FOR SMART MATERIALS
The introduction of smart materials into architecture poses
a challenge to the normative classification system A smart
material may be considered as a replacement for a
con-ventional material in many components and applications,
but most smart materials have inherent “active” behaviors,
and, as such, are also potentially applicable as
technolo-gies For example, electrochromic glass can be
simultane-ously a glazing material, a window, a curtain wall system, a
lighting control system, or an automated shading system
The product would then fall into many separate categories,
rendering it particularly difficult for the architect to take
into consideration the multimodal character and
perfor-mance of the material Furthermore, many smart
mate-rials are introducing unprecedented technologies into the
field of design, and are also making more commonplace
many technologies, such as sensors, which previously had
only limited application in highly specialized functions
Table 1 describes a proposed organization in which smart
materials establish a sequential relationship between
ma-terials and technologies The proposed organization also
maintains the fundamental focus on application of the
traditional classification system
Table 1 Proposed Classification System for Smart Materials and Systems
Category Fundamental Material Characteristics Fundamental System Behaviors
Traditional materials: Materials have given properties Materials have no or limited
Natural materials (stone, wood) and are “acted upon” intrinsic active response
High performance materials: Material properties are designed
Polymers, composites for specific purposes
Property-changing and energy-exchanging respond intelligently to varying responses to external stimuli and materials external conditions or stimuli can serve as sensors and actuators
Intelligent components: Behaviors are designed to Complex behaviors can be
Smart assemblies, polyvalent walls respond intelligently to varying designed to respond intelligently
external conditions or stimuli in and directly to multimodal demands discrete locations
Intelligent environments Environments have designed Intelligent environments consist
interactive behaviors and of complex assemblies that often intelligent response—materials combine traditional materials and systems “act upon” the with smart materials and
characteristics are enabled via a computational domain
TAXONOMY OF SMART MATERIALS
Four fundamental characteristics are particularly relevant
in distinguishing a smart material from the traditionalmaterials used in architecture: (1) capability of propertychange (2) capability for energy exchange, (3) discretesize/location, and (4) reversibility These characteristicscan potentially be exploited either to optimize a materialproperty to match transient input conditions better or tooptimize certain behaviors to maintain steady-state condi-tions in the environment
Smart Material Characteristics Property Change The class of smart materials that has
the greatest volume of potential applications in ture is the property-changing class These materials un-dergo a change in a property or properties—chemical,thermal, mechanical, magnetic, optical, or electrical—inresponse to a change in the conditions of the material’senvironment The conditions of the environment may beambient or may be produced via a direct energy input In-cluded in this class are all color-changing materials, such
architec-as thermochromics, electrochromics, and photochromics,
in which the intrinsic surface property of the molecularspectral absorptivity of visible electromagnetic radiation
is modified by an environmental change (incident solarradiation, surface temperature) or an energy input to thematerial (current, voltage)
Energy Exchange The next class of materials predicted
to have a large penetration into architecture is the exchanging class These materials, which can also be called
energy-“first law” materials, change an input energy into other form to produce an output energy in accordancewith the first law of thermodynamics Although the energy
Trang 7an-converting efficiency of smart materials such as
photo-voltaics and thermoelectrics is typically much less than
those of conventional energy conversion technologies, the
potential utility of the energy is much greater For
exam-ple, the direct relationship between input energy and
out-put energy renders many of the energy-exchanging smart
materials, including piezoelectrics, pyroelectrics and
pho-tovoltaics, excellent environmental sensors The form of
the output energy can further add direct actuating
capa-bilities such as those currently demonstrated by
electrore-strictives, chemoluminescents and conducting polymers
Reversibility/Directionality Some of the materials in the
two previous classes also exhibit the characteristic of
ei-ther reversibility or bidirectionality Many of the electricity
converting materials can reverse their input and output
energy forms For example, some piezoelectric materials
can produce a current from an applied strain or can
de-form from an applied current Materials that have a
bi-directional property change or energy-exchange
behav-ior can often allow further exploitation of their transient
change rather than only of the input and output energies
and/or properties The energy absorption characteristics of
phase changing materials can be used either to stabilize an
environment or to release energy to the environment,
de-pending on the direction in which the phase change is
tak-ing place The bidirectional nature of shape-memory alloys
can be exploited to produce multiple or switchable outputs,
allowing the material to replace components composed of
many parts
Size/Location Regardless of the class of smart material,
one of the most fundamental characteristics that
differen-tiates smart materials from traditional materials is the
discrete size and direct action of the material The
elimi-nation or reduction in secondary transduction networks,
additional components, and, in some cases, even packaging
and power connections allows minimizing the size of the
active part of the material A component or element
com-posed of a smart material can be much smaller than a
simi-lar construction using traditional materials and also will
require less infrastructural support The resulting
compo-nent can then be deployed in the most efficacious location
The smaller size coupled with the directness of the
prop-erty change or energy exchange renders these materials
particularly effective as sensors: they are less likely to
in-terfere with the environment that they are measuring, and
they are less likely to require calibration
Relevant Properties and Behaviors
Architectural materials are generally deployed in very
large quantities, and building systems tend to be highly
integrated into the building to maintain homogeneous
in-terior conditions Materials and systems must also
with-stand very large ranges of transient exterior conditions
The combination of these two general requirements tends
to result in buildings of high thermal and mechanical
in-ertia Therefore, even though the typical building uses
several different materials for many functions, there areonly a few areas in which the characteristics of smart mate-rials can be useful The transient environmental conditionsexperienced by most buildings often results in oversizingsystems to accommodate the full range of the exterior en-vironmental swing The swings may be instantaneous, as
in the case of wind, diurnal, or seasonal These conditionsinclude those that affect both heat transfer and daylighttransmission through the building envelope (also known
as the building fac¸ade or exterior skin) as well as those thatcreate dynamic loading on the building’s structural supportsystem For the building envelope, the property-changingclass of smart materials has the most potential application,whereas the energy-exchanging class is already finding ap-plication in building structural systems
Buildings consume two-thirds of the electrical energygenerated in the United States, and the majority of thatelectrical energy is used to support the building’s ambi-ent environmental systems, primarily lighting and HVAC(heating, ventilating, and air conditioning) systems Theintent of these systems is to effect a desired state in theinterior That state may be defined by a specified illumi-nance level or by an optimum temperature and relativehumidity Because conditions are generally maintained at
a steady state, the primary need is for more efficaciouscontrol Energy-exchanging materials have potential ap-plication as discrete sources, particularly for lighting deliv-ery systems, and also as secondary energy supply sources.The most significant applications of smart materials inbuildings, however, has been and will continue to be assensors and actuators for the control systems of these am-bient environmental systems
Smart Material Mapping
The material properties and/or characteristics that aremost relevant to architectural requirements are mapped inTable 2 against examples of smart material applications
CATEGORIES OF APPLICATIONS
One of the major difficulties in incorporating smart rials into architectural design is the recognition that veryfew materials and systems are under single environmen-tal influences For example, the use of a smart material tocontrol conductive heat transfer through the building en-velope may adversely impact daylight transmission Fur-thermore, because most systems in a building are highlyintegrated, it is difficult to optimize performance withoutimpacting the other systems or disrupting control systembalancing As an example, many ambient lighting systemsinclude plenum returns through the luminaires (lightingfixtures) that make it particularly difficult to decoupleHVAC from lighting systems The following discussion es-tablishes four major categories of applications for smartmaterials and takes into account the material/behaviormapping described in Table 2 but also considers the com-plex systems that are affected The four categories—glazing materials, lighting systems, energy systems, and
Trang 8mate-Table 2 Mapping of Smart Materials to Architectural Needs
Architectural Need Relevant Material Characteristic Smart Material Application Control of solar radiation Spectral absorptivity/transmission Electrochromics
transmitting through the building of envelope material Photochromics
Suspended particle panels Relative position of envelope material Louver control systems
r exterior radiation sensors
transfer through the building envelope material Phase change materials Control of interior heat generation Heat capacity of interior material Phase change materials
Relative location of heat source Fiber-optic systems
Thermoelectrics Lumen/watt energy conversion ratio Photoluminescents
Light-emitting diodes Secondary energy supply systems Conversion of ambient energy to Photovoltaics
electrical energy
Illuminance measurements Photoelectrics Occupancy sensing
Relative location of source Fiber optics
Electroluminescents
CO 2 and chemical detection Biosensors Relative location of source Thermoelectrics
Electrorheological Shape-memory alloys
monitoring/control systems—are also intended to be
con-sistent with the more normative and identifiable
classifi-cation systems of architecture
Glazing Materials
Whether serving as windows or as glass curtain walls,
glazing materials are extensively used on the building
en-velope Originally incorporated and developed during the
twentieth century for aesthetic reasons, the current use
of glazing materials also considers the delivery of daylight
into the building’s interior The majority of developments in
high-performance glazing materials have focused on
ther-mal characteristics—spectral selectivity to reduce radiant
transmission to the interior or low emissivity to reduce
ra-diant loss to the exterior Glazing introduces the
problem-atic condition in which, depending on the exterior
envi-ronmental conditions, performance criteria that have been
optimized for one set of conditions may be undesirable in
a matter of hours or even moments later The ideal
glaz-ing material would be switchable—managglaz-ing the radiant
transmission between exterior to interior to transmit
so-lar radiation when the envelope is conducting heat out
(typical winter daytime condition) and reflect solar ation when the envelope is conducting heat into the build-ing (typical summer daytime condition) Photochromics,thermochromics and thermotropics have been proposed asswitchable glazing materials, although only thermotropicsare currently being developed commercially for this appli-cation The basic operation of these materials is that ei-ther high incident solar radiation (photochromic) or highexterior temperature (thermochromic or thermotropic)produces a property change in the material that increasesits opacity, thereby reducing radiant transmission to theinterior When incident solar radiation lessens or when theexterior temperature drops, the material reverts to a moretransparent quality, allowing more solar radiation to trans-mit to the interior
radi-There are numerous circumstances, however, for whichthis type of switching is neither desirable nor useful Di-rect solar radiation into the building can create over-heated zones in particular locations, even in the dead ofwinter Winter sun altitude is also much lower, therebysignificantly increasing the potential for glare if solarradiation is not controlled During the summer, reduc-ing the radiant transmission may increase the need for
Trang 9Human perceptionsand actions
External stimuli(Light level)
Direct user controle.g., switches
Liquid crystalfilm
Laminations(Film laminated betweenglass layers)
Sensor control(Light level sensor)
Interface
Building enclosure element (wall)with controllable transparency
Enablingtechnologies
Figure 1 Typical current use of a smart material in architecture Only a single behavior is
controlled.
interior lighting systems and, because all electrically
gen-erated light has a lower lumen/watt ratio than daylight,
might exacerbate the building’s internal heat gains As
a result, the majority of efforts to develop smart glazing
have focused on the electrically activated chromogenics—
electrochromics, liquid crystal panels, and suspended
particle panels (see Fig 1) By using an electrical
in-put to control transparency, these materials can be more
easily incorporated into the control schemes for energy
management systems and/or lighting control systems The
optimum balance among lighting needs, heating/cooling
re-quirements, and occupant comfort can be determined, and
the transparency can be adjusted to meet these demands
in highly transient conditions
Lighting Systems
Most high efficiency lighting systems—fluorescent, HID
(high intensity discharge)—are relatively unsuitable for
low-level lighting or task lighting Furthermore, the typical
ambient lighting system requires enormous infrastructure
for support: electronic control systems, ballasts, integrated
cooling, light diffusers/distributors (often part of the
lumi-naire or lighting fixture) The efficiency and economics of
these systems drop as the overall lighting requirements
be-come smaller or more discrete Ambient systems are also
difficult to dim and to focus, so that very low-efficiency
in-candescent/halogen systems are still widely used for task
or discrete lighting requirements The low efficiency of the
typical lighting system results in producing a substantial
amount of heat and can be responsible for as much as 30%
of a commercial building’s cooling load The development
of fiber-optic lighting systems allows decoupling the
deliv-ered light from the primary energy conversion processes for
generating light This has the dual advantage of allowing
light delivery to any location in a building, which is much
more efficacious than using ambient lighting systems to
de-liver light, as well as removing the heat source from the
oc-cupied space Current applications for fiber-optic systems
include many museums and retail display areas, where theremoval of the heat source can profoundly improve the en-vironmental conditions of the objects under display and thediscrete nature of the light allows better highlighting andfocusing
Ambient lighting systems are generally designed to vide a standard illuminance level throughout a space at aspecified height (usually three feet above the floor) Thehuman eye, however, responds to the relative luminancecontrast between surfaces in the field of vision A light-ing level of 100 footcandles may be too low for reading ifthe surrounding surfaces provide little contrast and may
pro-be too high if the surfaces provide high contrast The vision of light into smaller and more discrete sources al-lows optimizing contrast within the field of vision Fur-thermore, the design of lighting for managing contrastenables using lower levels of lighting Sources produced
di-by the various luminescents—chemo, photo, electro—arestarting to find application in architectural interiors, par-ticularly as emergency lighting systems, because they havelow and in some cases no input power requirements LED(light-emitting diode) systems are also being developed aslow energy lighting delivery systems The latest develop-ments in polymer LED technology have produced lightingfixtures that have precise color control They provide ex-cellent color rendition and also allow for color variation—features that are difficult to achieve in standard lightingsystems
Energy Systems
The majority of buildings in the United States are nected to a utility grid and as such have little need forprimary energy conversion on-site There are numerouscircumstances, however, where secondary energy conver-sion can be quite useful, including back-up power genera-tion, peak demand control, and discrete power for remoteneeds For these situations, photovoltaic energy systemsare increasingly becoming popular because they can be
Trang 10con-readily deployed on roofs or integrated directly into the
building envelope to take advantage of the incident
so-lar radiation Two other developments in smart materials
hold greater promise for managing energy needs within
a building The large interior heat loads of most
build-ings coupled with a diurnal exterior temperature swing
has encouraged investigation into thermal mass systems
for maximum exploitation of a building’s thermal
iner-tia Although theoretically sound, thermal mass systems
have three major problems: (1) very slow response time,
(2) the inability to switch off the phenomenon when it
is not desirable, and (3) the large embodied energy
re-quired to provide the necessary mass of material Phase
change materials offer the advantages of thermal mass
and very few of its disadvantages The materials can be
tuned to particular temperatures and can have very rapid
responses Much less mass is required, and therefore, the
materials can be packaged and distributed throughout the
building much more efficiently and strategically By
lay-ering phase change materials and other smart
materi-als, such as electrochromics or thermotropics, there may
be a potential to add switching capability that allows
ac-tivating or deacac-tivating of the inertial behavior of the
materials
The removal of heat generated in a building is
becom-ing an increasbecom-ing concern as point loads from lightbecom-ing,
computers, and other electrical equipment escalate
Am-bient HVAC systems do not distinguish between
human-generated and equipment-human-generated cooling needs The
ability to manage and remove the heat generated by a
point load without affecting the ambient environmental
system could improve the operation of the ambient system
and significantly reduce the energy requirements
Ther-moelectrics are currently being explored for their potential
to manage point loads discretely Already serving as heat
sinks in the majority of microprocessor cooling packages,
thermoelectrics could be incorporated into integrated
cool-ing for many other types of point sources Although the
devices are not practical for cooling air directly because of
their low coefficient of performance (COP), they are ideal
for managing the conjugate heat transfer that is
charac-teristic of most nonhuman heat sources encountered in a
building
Monitoring and Control Systems
The increasing push to reduce the energy used by
build-ing HVAC systems has led to tighter buildbuild-ings to reduce
infiltration and to larger resets for the control equipment
This combination of an impermeable building envelope and
more variable interior conditions has led to an increase
in occupant complaints and indoor air quality problems
Many of the strategies intended to reduce energy can
im-pact human health adversely, and much discussion of the
appropriate compromise between the two requirements
continues One solution that holds promise is DCV, or
“de-mand controlled ventilation.” DCV adjusts interior
venti-lation depending on the presence of occupants; it reduces
ventilation when no occupants are in a room or zone and
increases ventilation as more occupants enter Because the
human need for fresh air is linked to activity, simple pancy sensors are not enough The level of carbon dioxide
occu-in a room has been proposed as a good surrogate for theamount of fresh air needed in a space, but many concernshave arisen in regard to other chemical contamination,such as finish material outgassing, that is not connected
to occupancy Chemical sensing for building monitoringhas previously been too expensive to incorporate and tooslow to be useful New developments in smart sensors forenvironmental monitoring, particularly biosensors, holdgreat promise for optimizing the controls of ambient HVACsystems
The need to control various kinds of motions and,
in particular, vibrations in a structure appears in manyforms At the level of the whole building structure, ex-citations resulting from seismic or wind forces can re-sult in damage to both primary structural systems andnonstructural elements User discomfort can also result.Many pieces of delicate equipment in buildings also need
to be protected from external vibrations by using similarstrategies Alternatively, many pieces of equipment used inbuildings can produce unwanted vibrations that can prop-agate through buildings In response to these needs, meth-ods of mitigating structural damage have been proposedthat seek to control overall structural responses via con-trollable smart damping mechanisms used throughout astructure Several smart base isolation systems for miti-gating structural damage in buildings exposed to seismicexcitations have also been proposed These dampers arebased on various electro- or magnetorheological fluids orpiezoelectric phenomena Piezoelectric sensors and actua-tors, for example, have been tested for use in vibrationalcontrol of steel frame structures for semiconductor manu-facturing facilities
Active control can be used to modify the behavior ofspecific structural elements by stiffening or strengtheningthem Structures can adaptively modify their stiffnessproperties, so that they are either stiff or flexible as needed
In one project, microstrain sensors coupled with ceramic actuators were used to control linear buckling,thereby increasing the bucking load of the column several-fold
piezo-Several new technologies provide capabilities for age detection in structures Various kinds of optical-fibersensors have been developed for monitoring damage in ma-terials as diverse as concrete and fiber-reinforced plasticcomposite laminate structures Optical fibers are usuallyembedded in the material Strain levels can be measuredvia wavelength shifts and other techniques Crack devel-opment in structures made of concrete, for example, hasbeen monitored via optical-fiber sensors, and special dis-tributed systems have been developed for use in the struc-tural health monitoring of high-performance yachts Dis-tributed fiber-optic systems have also been proposed forleak detection in site applications involving infrastructuresystems Other site-related structural applications includeusing optical-fiber sensors for ground strain measurement
dam-in seismically active areas Other applications where smartmaterials serve as sensors include the use of embeddedtemperature sensors in carbon-fiber structures
Trang 11FUTURE DESIGN APPROACHES IN ARCHITECTURE
The previous sections have outlined and discussed smart
materials in conjunction with needs currently defined
in architecture In some cases, smart materials have
been proposed as replacements for conventional
materi-als, and in other cases, smart materials have been
pro-posed for improving the functionality of standard
build-ing systems All of these developments can be
posi-tioned into the third category titled “Smart materials” in
Table 1 The impact of incorporating these materials into
standard architectural practice will be significant,
partic-ularly in regard to energy use and building performance,
but far more interesting potentials derive from
reconsider-ing smart materials as fundamental conceptual elements
in design rather than only as mprovements to existing
elements
As architectural design has always traditionally
in-volved integrated systems and materials—the building
envelope construction depends on the building’s
struc-tural system, the building’s HVAC system depends on the
envelope construction—then the greatest potential may
come from using smart materials to dis-integrate
cer-tain components, behaviors, or environments within the
building A smart component would be one that
func-tions intelligently without infrastructural support and also
will not disrupt the performance of surrounding systems
An example of a smart component might be a luminaire
that can sense relative luminances within a visual field
and self-adjust its focus, dimming capacity, and position
Activated smart materials
Liquid crystal film
Thermo-electric devices
Other
Direct action smart materials
Phase change materials
Photochromic films
Other
Sensor control
Computationalcontrol
Interface
Enablingtechnologies
Smart building enclosure (Wall)Discrete and transient control of multiple behaviors
Figure 2 Control of multiple behaviors via smart building assemblies.
Several different smart materials would be involved inthe development of this component, including sensorsand actuators, electroluminescents or LEDS, and perhapseven shape-memory alloys A smart assembly would op-erate at the next level of functionality beyond the smartcomponent There are many “high-tech” assemblies cur-rently used in architecture These assemblies integrateseveral types of components and technologies to achievemultiple functions For example, many of the most ad-vanced envelope systems incorporate mechanical shad-ing systems, thermal and ventilation control systems, andmultiple layers of glass into a highly integrated assem-bly intended to preserve view without incurring energypenalties A smart assembly would be designed to man-ifest the same behaviors, but do so in the most strate-gic manner (see Fig 2) Shading could be accomplished
at the micron or molecular level by using smart als, and thermal control could take place discretely andtransiently by selective placement of phase change ma-terials and thermoelectrics The smart assembly wouldmaximize functionality and minimize the number ofcomponents
materi-Many development activities have been focused on posals for “smart rooms” (see Fig 3) Most of these pro-posals accept the building as a traditional structure andseek to insert certain technologies into a room to add in-creased functionality Ubiquitous computing, teleconfer-encing, smart boards, voice and gesture recognition sys-tems, and wireless communication systems are among themany smart technologies being developed for incorporation
Trang 12pro-Surrounding environment
Human actionsand decisions
User specifiedcontrol
Smart assemblies and devicescomprising the space
Smart enclosures
- Multiple functions
Smart environmental systems
Smart user support devices
- Appliances
- Workstations
- Other
Computationalcontrol
Interface
Sensor control
- Stimuli sensorsCriteria associated
with use of environment(e.g., work performancemeasures)
Environmentaland other stimuli
Smart devices
Sensors &
controls Controlled environment
Figure 3 Smart rooms: In the current paradigm of a smart room, new smart devices are added
to increase functionalities The controlling interface is visibly and operationally present.
User-centeredenvironment
Embeddedinterfaces
Smart rooms:
Future paradigms
Human perceptions,actions and decisions
Smart assembliesand devices
Ubiquitous embedded interfaces(Transparent to user andcomputationally-driven)
Figure 4 Smart rooms—future paradigms: The interface will disappear to the user.
Trang 13into buildings A more interesting and provocative question
might be, “What would a room or building of the future be
like if we could exploit smart materials and technologies to
redesign the environment?” Smarter structures and
con-struction materials might allow significant reductions in
the size of the static building components—buildings could
become thinner, lighter, and more flexible The energy
in-tensive ambient systems in buildings could be reduced or
even eliminated if we allowed full interactivity between
the occupant and the environmental behavior (see Fig 4)
Ambient lighting systems could be replaced by discrete
sources that respond to the viewer HVAC systems could
be minimized if only the zone around an occupant were
conditioned Fundamentally, actions could be discrete and
direct—the minimum necessary at the point and time for
maximum effect
BIBLIOGRAPHY
1 D.M Addington, Boundary Layer Control of Heat Transfer in
Buildings, Harvard University Dissertation, Cambridge, MA,
1997.
2 D.M Addington, Discrete Control of Interior Environments in
Buildings, Proc ASME Fluids Eng Div., 1998.
3 E Allen, Fundamentals of Building Construction: Materials and Methods J Wiley, NY, 1999.
4 R.E Christenson and B.F Spencer, Coupled Building Control
Using Smart Damping Strategies, SPIE 7th Int Symp Smart Struct Mater., 2000.
5 J Hecht, City of Light Oxford University Press, NY, 1999.
6 N.K Khartchenko, Advanced Energy Systems Taylor &
Francis, Washington, DC, 1998.
7 R.B Peterson, Micro Thermal Engines: Is there Any Room at
the Bottom, Proc ASME Heat Transfer Div., 1999.
8 K Satori, Y Ikeda, Y Kurosawa, A Hongo, and N Takeda, Development of Small-Diameter Optical Fiber Sensors for
Damage Detection in Composite Laminates, SPIE 7th Int Symp Smart Struct Mater 2000.
9 R Shekarriz and C.J McCall, State-of-the-Art in Micro- and
Meso-Scale Heat Exchangers Proc ASME Adv Energy Syst Div., 1999.
10 M.D Symans, G.J Madden, and N Wongprasertt, Analytical and Numerical Study of a Smart Sliding Base Isolation System
for Seismic Protection of Buildings, SPIE 7th Int Symp Smart Struct Mater., 2000.
Trang 14Batteries are the major power sources for portable
elec-tronic devices and toys They are also used in
automo-biles for starting, lighting, and ignition (SLI batteries) At
present, the worldwide battery market exceeds $30 billion
per year Rapid technological advances and
miniaturiza-tion in electronics have created an ever-increasing demand
for compact, lightweight batteries For example, popular
portable electronic devices such as cellular phones,
lap-top computers, and camcorders require batteries of high
energy density Additionally, a need for more efficient use
of available energy resources as well as air-quality
con-trol have created enormous interest in electric vehicles
For example, the major automobile manufacturers around
the globe are engaged in developing advanced batteries
for electric vehicles in response to increased
environmen-tal regulations and legislative mandates The advanced
and high energy density batteries have become possible
due to the discovery and development of smart materials
and processes This article, after providing a brief
introduc-tion to the basic electrochemical concepts and the
princi-ples involved in batteries, presents the materials and
elec-trochemical aspects of high energy density (lithium-ion)
batteries
ELECTROCHEMICAL CONCEPTS
A battery is an electrochemical cell that converts the
chem-ical energy of a reaction directly into electrchem-ical energy This
section covers briefly the fundamental principles of
electro-chemical cells For more detailed information, readers are
referred to several excellent texts available in the
litera-ture (1– 4)
Electrochemical Cells
Figure 1 shows a schematic of an electrochemical cell that
consists of three components: an anode or negative
elec-trode, a cathode or positive elecelec-trode, and an electrolyte or
ionic conductor During the electrochemical reaction, the
anode M is oxidized and it gives up electrons to the
exter-nal circuit:
and the cathode X accepts the electrons from the external
circuit and is reduced:
The electrolyte, on the other hand, acts as a medium forcharge transfer between the anode and cathode as ionsinside the cell The overall cell reaction is given by addingthe two half-cell reactions (1) and (2):
M+ X → Mn ++ Xn −. (3)
The amount of electricity that passes through an trochemical cell is related by the Faraday law to the masses
elec-of reactants involved and products formed If a current elec-of
I amperes flows in the circuit for a time of t seconds, then the amount of charge Q transferred across any interface
in the cell is equal to It coulombs Now, in accordance with the Faraday law, the number of moles Nmof the reactants
M or X [see Eqs (1) and (2)] consumed by the passage of It
coulombs is given by
where n, NA, and e are, respectively, the number of electrons
given up or accepted by each M or X, Avogadro’s number,
and the charge on an electron The product NAe is called the Faraday constant F, which is equal to 96,487 C mol−1,and Eq (4) can be reduced to
weight in grams divided by the number of electrons n
in-volved in the reaction
Thermodynamics of Electrochemical Cells
The driving force for an electrochemical cell to deliver trical energy to an external circuit is the decrease in thestandard free energyG oof the cell reaction [Eq (3)] Thefree energyG o is related to the standard cell potential E o
elec-by
where n and F are, respectively, the number of electrons
involved in the reaction and the Faraday constant The cell
potential E ois the difference between the electrode
poten-tials of the cathode and anode The values of E ofor variouselectrochemical couples are given in terms of standard re-duction/oxidation potentials in textbooks and handbooks
68
Trang 15Load
CathodeX
Separator
Figure 1 Schematic of an electrochemical cell.
(5,6) A positive value of E omeans that the cell reaction
oc-curs spontaneously The standard potential E ois the
equi-librium potential when all of the cell components are in
their standard states For example, the solution species
have unit molar activities, the gases have pressures of 1
atmosphere, and the solid phases are in their most stable
form in their standard states For conditions other than the
standard state, the cell potential E is given by the Nernst
where R is the gas constant, T is the absolute temperature,
and aM n +, aX n −, aM, and aXare the activities of the products
and reactants involved in cell reaction (3) At room
tem-perature T= 298 K, the Nernst equation can be simplified
The cell potential also depends on the temperature and
pressure The dependences are related to the
where S is the entropy change and V is the volume
change Thus, the measurement of the cell potential can
be used to determine thermodynamic quantities such as
G, S, enthalpy change H, and equilibrium constants.
Polarization Losses in Electrochemical Cells
The amount of electrical energy that an electrochemicalcell can deliver is related to the free energy change of the
cell reaction [Eq (7)] However, when a current I is passed
through the cell, part of the energy is lost as waste heatdue to polarization losses in the cell The polarization losscan be classified into three types: activation polarization,concentration polarization, and ohmic polarization Acti-vation polarization is related to the kinetics of electrodereactions Concentration polarization is related to the con-centration differences of the reactants and products at theelectrode surfaces and in the bulk as a result of mass trans-
fer Ohmic polarization, usually referred to as internal IR
drop, is related to the internal impedance of the cell, which
is a sum of the ionic resistance of the electrolyte and theelectronic resistance of the electrodes
The different polarization losses are indicated ically in Fig 2 as a function of operating current (2) The
schemat-operating (measured) cell voltage Eopis given by
where Eoc is the open-circuit voltage andη is the
overvol-tage from polarization The overvolovervol-tageη is a measure of the deviation of the cell voltage Eopfrom the equilibrium
open-circuit voltage Eoc The overvoltageη from the three
different polarizations is given by
Figure 2 Variation of cell voltage with operating current
illus-trating polarization losses: (a) ohmic polarization, (b) activation polarization, and (c) concentration polarization.
Trang 16intrinsic properties of the electrodes and electrolytes as
well as the engineering design of the cell will influence
the polarization losses and hence the performance and
ef-ficiency of electrochemical cells
BATTERIES
Performance Parameters
As mentioned in the previous section, a battery is an
elec-trochemical device that converts stored chemical energy
directly into electrical energy The performance
character-istics of a battery are assessed in terms of several
param-eters discussed later (1–3) The cell voltage Eopis the
dif-ference between the electrode potentials of the cathode Ec
and anode Ea:
Although the theoretical capacity Q of a cell or half-cell
is given by Eq (6), it is often convenient to calculate the
specific capacity Qspfor purposes of comparison The
spe-cific capacity Qspis obtained by dividing the capacity Q of
the cell or half-cell by the mass m or volume V of the cell
or half-cell and is usually expressed in terms of Ah/kg or
The available energyε of a cell is given by the product of
the cell capacity Q and the average operating voltage Eop
and again is usually given in terms of either gravimetric
energy density (specific energyεsp) in Wh/kg or volumetric
energy density in Wh/L:
The power P delivered by the cell is given by the product of
the current I flowing and the associated cell voltage Eopand
is generally given in terms of gravimetric power density
(specific power Psp) in W/ kg or volumetric power density
in W/ L:
where Ispis the current density (current per unit weight or
volume)
The discharge characteristic of a battery is another
im-portant parameter, which is given in terms of a plot of cell
voltage versus capacity The discharge profile and the
fi-nal capacity obtainable depend on the current density Isp
used Figure 3 compares the discharge profiles for various
current densities A useful way of defining the influence
of current density on discharge curves is in terms of C
Figure 3 Discharge profiles at various C rates that illustrate the
influence of current density.
rates:
where Idand Qn are, respectively, discharge current and
nominal capacity For example, a C rate of τ implies that
the nominal capacity of the cell is delivered in 1/τ hoursunder the specified current density In an ideal battery, thedischarge voltage drops sharply to zero when the chemi-cal reaction reaches completion and the stored energy isfully consumed (Fig 3) The discharge curves deviate fromthe ideal curve as the discharge rate (or current density)increases due to the polarization losses discussed in theprevious section
Coulometric and energy efficiencies and cycle life of ondary (rechargeable) batteries are some additional impor-
sec-tant parameters Coulometric efficiency qcis defined as
where Ed and Ec are, respectively, the average discharge
and charge voltages A qC< 1 implies the occurrence of
un-wanted side reactions that produce heat during the ing process Intrinsic cell materials characteristics, cell en-gineering, and cell operating conditions such as current
charg-density and temperature can all influence qC A qE< qC
implies a deviation of the discharge and charge curves
Trang 17from the open-circuit voltage profile Again, polarization
losses arising from materials characteristics, cell
engineer-ing, and operating conditions can influence qE
The cycle life of a battery is the number of times it can be
charged and discharged repeatedly before the cell capacity
falls below a limiting value Generally, the limiting value
is set around 70 to 80% of the nominal capacity The cycle
life depends on the reversible characteristics (structural
and chemical stability) of the electrode materials, cell
en-gineering, and operating conditions such as temperature,
current density, and depth of discharge
Design Considerations
The equilibrium cell voltage Eoc and the capacity Q of a
battery are determined by the intrinsic properties of the
electrode materials The cell voltage can be maximized by
choosing anode materials that have a smaller work
func-tionφaand cathode materials that have a larger work
func-tionφc In other words, the anode should be a good reducing
agent that has a large negative reduction potential, and the
cathode should be a good oxidizing agent that has a large
positive reduction potential A schematic energy diagram
of an open circuit is shown in Fig 4 The open-circuit
volt-age Eocof the cell is given by
Table 1 Major Primary Battery Systems
Cell Voltage Capacity
Magnesium Mg MnO 2 Mg + 2MnO 2 + H 2 O → Mn 2 O 3 + Mg(OH) 2 2.8 271
a
or by the difference between the electrode potentials ofthe cathode and anode [Eq (14)] Thermodynamic stability
considerations also require that the Fermi energies EFof
the cathode and anode lie within the band gap Eg of theelectrolyte, as shown in Fig 4, so that no unwanted reduc-tion or oxidation of the electrolyte occurs This implies alimitation of
Alkali and alkaline-earth metals that have a smaller φa
or a larger negative reduction potential are attractive odes, and higher valent transition-metal compounds thathave a largerφcor larger positive reduction potentials areattractive cathodes to maximize the cell voltage The cellcapacity, on the other hand, is determined by the atomic
an-or molecular weight of the elements an-or compounds used
as electrodes and the degree of reaction (number of trons involved) per mole of the electrode material [Eq (6)].Lightweight elements such as hydrogen, lithium, or oxy-gen and low molecular weight compounds are preferred aselectrodes to maximize cell capacity
elec-In addition to high cell voltage and capacity, severalother criteria are important in designing a battery toachieve high efficiency and minimal energy loss The elec-trolyte should have good ionic conductivity, but should be
an electronic insulator to avoid internal short-circuiting.High ionic conductivity in the electrolyte is essential to
minimize the IR drop or ohmic polarization Using a given electrolyte, the IR drop due to electrolyte resistance can
be reduced, and the rate capability can be improved by ahigher electrode interfacial area and thin separators Theelectrode should have a high electronic conductivity and
diffusion rate for the ions to minimize the IR drop The
electronic conductivity of the electrodes can be improved
by adding electrically conducting additives such as bon The electrode reaction rates at the cathode and anodeshould be high enough to minimize activation polariza-tion This is commonly achieved by using a porous elec-trode design, which can reduce the local current density byproviding high surface area Adequate flow or passage ofelectrolytes is essential to facilitate mass transfer and min-imize concentration polarization Electrode porosity andpore size, optimum separator thickness and structure, andconcentration of the reactants in the electrolytes are im-portant factors in minimizing concentration polarization
car-In addition to these points, the electrolyte should have
Trang 18Table 2 Major Secondary Battery Systems
Cell Voltage Capacity
Nickel–cadmium Cd NiOOH Cd + 2NiOOH + 2H 2 O → 2Ni(OH) 2 + Cd(OH) 2 1.35 181
aBased only on active cathode and anode materials.
good chemical stability and should not undergo any
di-rect reaction with the electrodes In rechargeable
batter-ies, chemical reversibility on the electrodes is crucial to
maintaining good capacity retention Raw materials and
fabrication costs, cell safety, and environmental factors are
additional considerations
Types of Batteries
Batteries can be classified into two types: primary
(non-rechargeable) and secondary ((non-rechargeable) batteries
Electrode materials undergo irreversible chemical
reac-tions in primary batteries, but they exhibit reversible
chemical reactions in secondary batteries Some major
pri-mary and secondary battery systems are given in Tables 1
and 2 (2) The tables give the cell reactions, voltage, and
ca-pacity for each system Most of the primary and secondary
systems are based on aqueous electrolytes; the
lithium-based primary systems in Table 1 and the lithium-ion
system in Table 2 are based on nonaqueous electrolytes
The aqueous systems are limited in cell voltage (≤ 2.1 V)
due to a smaller separation Egbetween the highest
occu-pied molecular orbital (HOMO) and the lowest unoccuoccu-pied
molecular orbital (LUMO) of water (Fig 4) and the
con-sequent vulnerability of water to reduction/oxidation
reac-tions at higher cell voltages The use of nonaqueous
elec-trolytes that have a larger Eg, on the other hand, permits
higher cell voltages in lithium-based systems
SMART BATTERIES
The discovery of smart materials and the development of
new processes have revolutionized the electronics
indus-try over the years The continued reduction in the sizes
and weights of popular portable electronic devices such as
cellular phones and laptop computers has driven the
par-allel, development of smart batteries to power them In
this regard, lithium-ion batteries have become appealing
because they offer higher energy density (volumetric and
gravimetric) compared to other rechargeable systems (Fig
5) such as lead–acid, nickel–cadmium, and nickel–metal
hydride batteries (7) Lithium-ion batteries are smaller
and lighter compared to other systems Lithium-ion
bat-teries have become a commercial reality since Sony
Cor-poration introduced them in 1990 as a result of the
dis-covery of new materials over the years The history,
prin-ciples, current status, and future challenges of lithium-ion
technology are briefly discussed in the following sections
For more detailed information, the readers are referred toseveral references in the literature (1–3, 8–13)
us-and a cathode material that has a larger work functionφc,
as shown in [Eq (23)] Lithium metal—the lightest solid
in the periodic table—has a high specific capacity and ahigh standard oxidation potential (smallφa) and is an at-tractive anode for achieving high energy density Because
of this objective, batteries that consist of metallic lithium
as an anode and a lithium insertion compound LixMyXz
(M= transition metal and X = nonmetal) as a cathode came appealing during the 1970s; a lithium insertion com-pound is a host matrix into/from which the guest species
be-Li+ can be reversibly inserted/extracted This concept of
a secondary lithium battery was initially demonstratedusing a layered metal sulfide TiS2 as the cathode and anonaqueous electrolyte consisting of a lithium salt such asLiClO4dissolved in an organic solvent such as propylenecarbonate In this cell, the Li+ions produced at the anode
by oxidation of the metallic lithium during discharge grate through the electrolyte and are inserted into the vander Waals gap between the sulfide layers of TiS2, and theelectrons flow through the external circuit from the anode
mi-to the cathode mi-to give LixTiS2 During the charging process,the Li+ions are extracted from LixTiS2and the electrons
Figure 5 Comparison of the gravimetric and volumetric energy
densities of various rechargeable battery systems.
Trang 19In this cell, however, the chemical reactivity of metallic
lithium with the nonaqueous electrolyte results in forming
a passivating film on the anode Although the passivating
film prevents further corrosion, it leads to nonuniform
plat-ing of lithium durplat-ing chargplat-ing, which results in total cell
failure due to dendritic short-circuiting and also in serious
safety problems due to local overheating These
difficul-ties of the metallic lithium anode forced the use of lithium
insertion compounds as both anodes and cathodes These
cells are called lithium-ion cells or rocking-chair cells
be-cause the lithium ion shuttles or rocks between the cathode
and anode hosts during the charging/discharging process
(Fig 6) This strategy, however, requires careful selection
of cathode and anode pairs to maintain high cell voltage
(>3 V) and to minimize the added weight of the insertion
compound anode
Although the concept of secondary lithium batteries was
initially demonstrated by using a sulfide cathode, it was
recognized during the 1980s that it is difficult to achieve
high cell voltage using sulfide cathodes because an
over-lap of the higher valent Mn +:d energies and the top of the
S:3p energy and the formation of S2 −
2 ions lead to an cessibility of higher oxidation states for Mn + in a sulfide
inac-LixMySz; the stabilization of the higher oxidation state is
essential to maximize the work function φc and thereby
the cell voltage Eoc [Eq (23)] On the other hand, the
lo-cation of O:2p energy much below the S:3p energy and a
larger increase of the Mn +:d energies in an oxide compared
to those in a sulfide, due to a larger Madelung energy, make
the higher valent states accessible in oxides Accordingly,
transition-metal oxide hosts were pursued as cathodes
during the 1980s (14–16)
Figure 7 compares the electrochemical potential ranges
of some lithium insertion compounds versus metallic
Figure 7 Electrochemical potential ranges of some lithium
in-sertion compounds with reference to metallic lithium.
lithium Among them, LiCoO2, LiNiO2, and LiMn2O4
oxides that have a higher electrode potential of 4 V sus metallic lithium have become attractive cathodes forlithium-ion cells Graphite and coke that have lower elec-trode potentials < 1 V versus metallic lithium and are
ver-lightweight have become attractive anodes In a ion cell made from, for example, a LiCoO2 cathode and acarbon anode (Fig 6), the lithium ions migrate from theLiCoO2cathode to the LixC6anode through the electrolyte,and the electrons flow through the external circuit fromthe cathode to the anode during the charging process Ex-actly the reverse reaction occurs during the dischargingprocess
lithium-A lithium insertion compound should have several tures to be a successful electrode (cathode or anode) inlithium-ion cells:
fea-rThe cathode should have a high lithium chemical
potential (µLi(c)), and the anode should have a lowlithium chemical potential (µLi(a)) to maximize the cellvoltage:
Eoc= µLi(c)− µLi(a)
The voltage is determined by the energies involved inboth electron transfer and Li+ transfer The energyinvolved in electron transfer is related to the workfunctions of the cathode (φc) and anode (φa) as shown
in Eq (23), whereas that involved in Li+transfer isdetermined by the crystal structure and the coordi-nation geometry of the site into/from which Li+ ionsare inserted /extracted (17) If we consider only elec-
tron transfer, then Eoccan be given by Eq (23) Thisimplies that the Mn + ion in the insertion compound
LixMyOzshould have a high oxidation state to be used
as a cathode and a low oxidation state to be used as
an anode
Trang 20rThe insertion compound LixMyOzshould allow
inser-tion/extraction of a large amount of lithium x to imize the cell capacity This depends on the number
max-of available lithium sites and the accessibility max-of tiple valences for M in the insertion host
mul-rThe lithium insertion /extraction process should be
re-versible and have no or minimal changes in the hoststructure across the entire range x of lithium inser-tion /extraction to provide a good cycle life
rThe insertion compound LixMyOz should have good
electronic conductivityσeand Li+-ion conductivityσLi
to minimize polarization losses during the ing/charging process and thereby to support a highcurrent and power densities
discharg-rThe insertion compound LixMyOz should be
chem-ically stable and should not react with the trolyte across the entire range x of lithium insertion/
elec-extraction
rThe Fermi energies of the cathode and anode in the
entire range x of lithium insertion /extraction shouldlie within the band gap of the electrolyte, as shown inFig 4, to prevent any unwanted oxidation or reduction
of the electrolyte
rThe insertion compound LixMyOzshould be
inexpen-sive, environmentally benign, and lightweight
Layered Cobalt Oxide Cathodes
LiCoO2has a layer structure in which the Li+and Co3 +ions
occupy the alternate (111) planes of a rock salt structure, as
shown in Fig 8, to give a layer sequence of –O–Li–O–Co–
O– along the c axis This structure has an oxygen stacking
sequence of ABCABC along the c axis, and the Li+ and
Co3 +ions occupy the octahedral interstitial sites of the
cu-bic close-packed oxygen array Accordingly, it is designated
as an O3 layer structure The structure provides reversible
extraction /insertion of lithium ions from /into the lithium
planes Two-dimensional motion of the Li+ ions between
the strongly bonded CoO2layers provides fast lithium-ion
diffusion (highσLi), and the edge-shared CoO6octahedral
arrangement that has a direct Co–Co interaction provides
good electronic conductivityσe necessary for a high rate
A large work functionφc for the highly oxidized Co3+/4+
couple provides a high cell voltage of around 4 V, and the
discharge voltage does not change significantly as the
de-gree of lithium extraction /insertion x in Li1 −xCoO2changes
(Fig 9) These features have made LiCoO2 an attractive
cathode, and most of the commercial lithium-ion cells are
currently made from LiCoO2
However, only 50 % of the theoretical capacity of LiCoO2
that corresponds to a reversible extraction of 0.5 lithium
per Co (practical capacity of 140 Ah/kg) can be
practi-cally used The limitation in practical capacity has been
attributed in the literature (18) to an ordering of Li+
ions and consequent structural distortions around x= 0.5
in Li1 −xCoO2 However, it has been shown more recently
that the limited capacity could be due to the tendency of
Li−xCoO to lose oxygen (or react with the electrolyte) at
Li
Coc/2
O
a
Figure 8 Crystal structure of layered LiCoO2
a deep charge when (1− x) < 0.5 (19) Figure 10 shows the
variation of the oxidation state of cobalt and the oxygencontent as the lithium content (1− x) varies The data inFigure 10 were obtained by chemically extracting lithiumfrom LiCoO2using the oxidizing agent NO2PF6in a non-aqueous (acetonitrile) medium and determining the oxida-tion state of cobalt by a redox (iodometric) titration Con-stancy of the cobalt oxidation state and an oxygen contentsignificantly less than 2 at low lithium contents demon-strate the chemical instability of Li1 −xCoO2cathodes at adeep charge when (1− x) < 0.5 The tendency of Li1 −xCoO2
to lose oxygen at a deep charge is consistent with the cent X-ray absorption spectroscopic (20) and electron en-ergy loss spectroscopic (21) data The spectroscopic data in-dicate that the holes (removal of electrons) are introduced
Trang 21Figure 10 Variations of the oxidation state of the
transition-metal ions and oxygen content as lithium content varies in
Li 1 −x CoO 2−δand Li 1 −x Ni 0.85Co 0.15O 2−δ.
into the O:2p band rather than the Co:3d band during the
electrochemical extraction of lithium Introduction of a
sig-nificant amount of holes into the O:2p band will lead to
evolution of oxygen from the lattice However, note that
neutral oxygen in the presence of electrolytes in
lithium-ion cells may not be evolved under conditlithium-ions of overcharge
when (1− x) < 0.5 Instead, the cathode may react with the
electrolyte due to the highly oxidized nature of the deeply
charged Li1 −xCoO2cathode
Figure 11 shows the X-ray diffraction patterns of the
Li1−xCoO2 samples that were obtained by chemically
ex-tracting lithium from Li1 −xCoO2 The samples maintain
the initial O3 layer structure (CdCl2structure) for 0.35≤
(1− x) ≤ 1 For lithium contents (1 − x) < 0.35, a
sec-ond phase begins to form as indicated by the appearance
of a shoulder on the right-hand side of the (003) reflection
centered around 2θ = 20◦ The intensity of the new
reflec-tion increases as the lithium content decreases further, and
the end member CoO2−δconsists of reflections
correspond-ing only to the new phase The X-ray diffraction pattern
of the new phase could be indexed on the basis of a
two-phase mixture consisting of a major P3 two-phase and a minor
oxygen stacking sequences of ABBCCA and ABABAB,
re-spectively The Li+ions occupy prismatic (trigonal prism)
and octahedral sites, respectively, in the P3 and O1
struc-tures The formation of the P3 and O1 phases from the
initial O3 structure is due to sliding of the oxide ions,
as shown in Fig 12 The driving force for the sliding
ap-pears to be structural instability caused by the formation
of oxygen vacancies at low lithium contents (Fig 10) The
observed transformation of the O3 phase at low lithium
content is consistent with that found in electrochemically
prepared samples (22) The tendency to lose oxygen and theassociated structural transitions limit the practical capac-ity of LiCoO2cathodes
Layered Nickel Oxide Cathodes
LiNiO2has an O3 layer structure (Fig 8) like LiCoO2, andthe Ni3+/4+ couple that has a larger φc provides a highcell voltage of around 4 V However, LiNiO2 suffers from
a few drawbacks: (1) difficulty in synthesizing LiNiO2as
a perfectly ordered phase without mixing Li+ and Ni3 +
ions in the lithium plane (23,24), (2) Jahn–Teller tion (tetragonal structural distortion) associated with alow spin Ni3 +:d7ion (25), (3) irreversible phase transitionsduring the charge/discharge process, and (4) safety con-cerns in the charged state As a result, LiNiO2 is not apromising material for commercial cells However, some
distor-of these difficulties have been overcome by partially stituting cobalt for nickel For example, the compositionLiNi0.85Co0.15O2, has been shown to exhibit attractive elec-trochemical properties (26) It has a reversible capacity ofaround 180 Ah/kg (Fig 9) and excellent cyclability Thiscapacity is 30% higher than that of LiCoO2, and it corre-sponds to 65% of the theoretical capacity The substitution
sub-of cobalt for nickel has been found to suppress the cationdisorder and Jahn–Teller distortion, as indicated by X-rayabsorption fine structure studies (25) The higher capacity
of LiNi0.85Co0.15O2has made it an attractive alternate forLiCoO2
However, the reason for the higher capacity ofLiNi0.85Co0.15O2 compared to the analogous LiCoO2 cath-odes was not clear in the literature The structural sta-bility of the LiNi0.85Co0.15O2 cathodes during long-termcycling, particularly under mild heat, also remained to
be assessed Recent experiments on Li1 −xNi0.85Co0.15O2
samples obtained by chemically extracting lithiumfrom LiNi0.85Co0.15O2 show that the higher capacity ofLiNi0.85Co0.15O2compared to that of LiCoO2is due to its re-sistance to losing oxygen at low lithium contents Figure 10compares the variations of the average oxidation state
of the transition-metal ions and the oxygen contents
as lithium content varies in Li1 −xNi0.85Co0.15O2 and
Li1 −xCoO2 The data show that the former system hibits better stability without losing much oxygen at adeep charge Figure 13 shows the X-ray diffraction pat-terns of the Li1 −xNi0.85Co0.15O2samples that were obtained
ex-by chemically extracting lithium from LiNi0.85Co0.15O2 In
this case, the initial O3 structure is maintained for a wider
lithium content 0.23≤ (1 − x) ≤ 1, and the new phase isformed at a lower lithium content (1 − x) < 0.23 More
importantly, the X-ray diffraction pattern of the end ber NiO2−δ could also be indexed on the basis of an O3
mem-structure but had smaller lattice parameters compared
to the initial O3 phase The observation of an O3
struc-ture for the chemically prepared NiO2−δagrees with thatfound for the electrochemically prepared sample (27,28).The absence of a significant amount of oxygen vacanciesappears to prevent the sliding of oxide ion layers and thestructural transformation The absence of oxygen loss and
the maintenance of the initial O3 structure to a much
Trang 23lower lithium content (1− x) compared to that in Li1 −xCoO2
permit a higher capacity in the Li1 −xNi0.85Co0.15O2
system
The differences in oxygen loss behavior between the
Li1 −xCoO2and the Li1 −xNi0.85Co0.15O2systems can be
un-derstood by considering qualitative energy diagrams for
Li1 −xCoO2and Li1 −xNiO2(Fig 14) In LiCoO2that has a
Co3 +:3d6 configuration, the t2g band is completely filled,
and the eg band is empty As lithium is extracted from
LiCoO2, the Co3 + ions are oxidized to Co4 +, which is
ac-companied by removal of electrons from the t2gband
Be-cause the t2g band overlaps the top of the O:2p band,
deeper lithium extraction where (1− x) < 0.5 results in
a removal of electrons from the O:2p band as well The
removal of a significant amount of electron density from
the O:2p band will result in oxidation of the O2 −ions and
an ultimate loss of oxygen from the lattice In contrast,
the LiNiO2 system that has a Ni3 +:3d7 configuration
in-volves the removal of electrons only from the e band For
LiNi0.85Co0.15O2, the electrons will be removed from the eg
band for (1− x) > 0.15 Because the egband lies well abovethe O:2p band, this system does not lose oxygen down to
a lower lithium content The band diagrams in Fig 14 areconsistent with the recent spectroscopic evidence for theintroduction of holes into the O:2p band rather than intothe Co:3d band in LiCoO2(20,21) and into the Ni:3d band
in Li1 −xNiO2and Li1 −xNi0.85Co0.15O2(29,30)
To assess the structural stability of Li1 −xNi0.85Co0.15O2
cathodes during long-term cycling, chemically prepared
Li1 −xNi0.85Co0.15O2 samples were subjected to mild heatand examined by X-ray diffraction (31) The data show a
decrease in the c/a ratio of the unit cell parameters of,
for example, Li0.35Ni0.85Co0.15O2when heated at T > 50◦Cdue to migration of the Ni3 +ions from the nickel plane tothe lithium plane Interestingly, the cobalt oxide Li0.35CoO2
that has a similar degree of lithium extraction (charging)
shows little or no decrease in the c/a ratio when heated
under similar conditions Thus, the Li−xNi.85Co .15O
Trang 24Co3 + /4 +:t2g
Figure 14 Comparison of the qualitative energy diagrams of
Li1−xCoO2 and Li1−xNiO2
cathodes experience structural instability under mild heat,
whereas the Li1 −xCoO2cathodes do not under similar
con-ditions Although the LiNi0.85Co0.15O2cathode has higher
capacity (180 Ah/kg) than the LiCoO2cathode (140 Ah/kg)
and is more resistant to losing oxygen from the lattice
compared to LiCoO2, the structural instability experienced
due to cation migration may become an issue under
cy-cling at higher temperatures (T > 50◦C) The differences
in the structural stability between the two systems can be
explained by considering the mechanism of cation
migra-tion The migration of transition-metal ions from
octahe-dral sites in the transition-metal plane to the octaheoctahe-dral
sites in the lithium plane needs to occur via the
neighbor-ing empty tetrahedral sites, as shown in Fig 15 While
the low spin Co3 +:3d6ion that has strong octahedral site
stabilization energy (32) is unable to migrate to the
neigh-boring tetrahedral site, but the low spin Ni3 +:3d7ion that
has moderate octahedral site stabilization energy is able
to move to the tetrahedral site under mild heat
Figure 15 Schematic representation of the diffusion processes
of nickel ions in Li1−xNi0.85Co0.15O2 Dotted and solid squares
re-fer to tetrahedral site and lithium-ion vacancy, respectively T1
and T2refer to tetrahedral sites at (0, 0, 0.125) and (0, 0, 0.375),
respectively.
Li (8a site)
Mn (16d site)
O (32e site)
Figure 16 Crystal structure of LiMn2 O 4 spinel.
Spinel Manganese Oxide Cathodes
Although LiCoO2and LiNi0.85Co0.15O2 are attractive didates, both Co and Ni are expensive and relativelytoxic These considerations have created much interest
can-in manganese oxides because Mn is can-inexpensive and vironmentally benign (33–35) In this regard, LiMn2O4
en-that crystallizes in a three-dimensional cubic spinel ture (Fig 16) has become appealing (16) In the LiMn2O4
struc-spinel, the Li+and the Mn3+/4+ ions occupy, respectively,the 8a tetrahedral and 16d octahedral sites of the cu-bic close-packed oxygen array A strong edge-shared oc-tahedral [Mn2]O4 array permits reversible extraction ofthe Li+ ions from the tetrahedral sites without collaps-ing the three-dimensional spinel framework An additionallithium-ion can also be inserted into the empty 16c oc-tahedral sites of the spinel framework to give the lithi-ated spinel Li2[Mn2]O4 However, electrostatic repulsionbetween the Li+ ions in the 8a tetrahedral and 16c oc-tahedral sites, which share common faces, causes a dis-placement of the tetrahedral Li+ions into the neighboringempty 16c sites to give an ordered rock salt structure thathas a cation distribution of (Li2)16c[Mn2]16dO4 Thus, theo-retically, two lithium ions per LiMn2O4formula unit could
be reversibly inserted/extracted Although the edge-sharedMnO6octahedral arrangement that has direct Mn–Mn in-teraction provides good electrical (small polaron) conduc-tivityσe, the interconnected interstitial sites in the three-dimensional spinel framework provide good lithium-ionconductivityσLi
The lithium extraction/insertion from/into the 8a hedral and 16c octahedral sites of the Li[Mn2]O4spinel oc-curs in two distinct steps (16) The former occurs at around
tetra-4 V (Fig 9) maintaining the cubic spinel symmetry; in trast, the latter occurs at around 3 V by a two-phase mecha-nism involving the cubic spinel Li[Mn2]O4and the tetrago-nal lithiated spinel Li2[Mn2]O4 Although both involve the
con-Mn3+/4+ couple, the 1 V difference between the two cesses reflects the differences in the site energies (17) asdifferentiated by Eq (23) and (25) A deep energy well forthe 8a tetrahedral Li+ ions and a high activation energyrequired for the Li+ions to move from one 8a tetrahedralsite to another via an energetically unfavorable neighbor-ing 16c site lead to a higher voltage of 4 V (33) The cubic totetragonal transition from Li[Mn ]O to Li [Mn ]O is due
Trang 25pro-t2 (dxy, dyz, dzx)
(dxz, dyz)(dxy)
Figure 17 Illustration of the Jahn–Teller distortion in
man-ganese oxides: (a) Mn4+:3d3 that has cubic symmetry (no Jahn–
Teller distortion) and (b) Mn3+:3d4 that has tetragonal symmetry
(Jahn–Teller distortion).
to the Jahn–Teller distortion of the single electron in the
egorbitals of a high spin Mn3 +:3d4ion (Fig 17) A
coopera-tive distortion of the MnO6octahedra that have long Mn–O
bonds along the c axis and short Mn–O bonds along the a
and b axes results in macroscopic tetragonal symmetry for
Li2[Mn2]O4
Although, in principle, two lithium ions per LiMn2O4
formula unit could be reversibly extracted/inserted
from/into the Li[Mn2]O4 spinel framework, the cubic to
tetragonal transition is accompanied by a 16% increase
in the c /a ratio of the unit cell parameters and a 6.5%
in-crease in unit cell volume This change is too severe for
the electrodes to maintain structural integrity during the
discharge/charge cycle, and so LiMn2O4 exhibits drastic
capacity fade in the 3 V region As a result, LiMn2O4has
limited practical capacity of around 120 Ah/kg (Fig 9) that
corresponds to an extraction/insertion of 0.4 lithium per
Mn in the 4 V region Furthermore, even though it has
lim-ited capacity, LiMn2O4tends to exhibit capacity fade in the
4 V region as well, particularly at elevated temperatures
(50◦C) The capacity fade in the 4 V region has been
at-tributed to a dissolution of manganese into the electrolyte
originating from a disproportionation of Mn3 +into Mn4 +
and Mn2 +(36) and the formation of tetragonal Li2[Mn2]O4
on the surface of the particles under conditions of
nonequi-librium cycling (37)
The difficulties of lattice distortions in the LiMn2O4
spinel have motivated strategies to suppress Jahn–Teller
distortion One way to suppress Jahn–Teller distortion is to
increase the average oxidation state of manganese because
Mn4 +:3d3does not undergo Jahn–Teller distortion The
ox-idation state of manganese can be increased either by
alio-valent cationic substitutions or by increasing the oxygen
content in LiMn2O4 Using this strategy, Thackeray et al
(33,38,39) pioneered the Li–Mn–O phase diagram For
ex-ample, substituting Li for Mn in Li+xMn O increases the
oxidation state, and the end member Li4Mn5O12(x= 0.33)has an oxidation state of 4+ for Mn Similarly, the ox-idation state increases as oxygen content increases inLiMn2O4+δ, and the end member Li2Mn4O9(δ = 0.5) willhave an oxidation state of 4+ for Mn However, these de-fective spinels are difficult to synthesize by conventionalhigh-temperature procedures, and more recently solution-based syntheses have been pursued to obtain them (40,41)
It is also difficult to extract lithium from Li4Mn5O12 and
Li2Mn4O9because Mn4 +is difficult to oxidize further andtherefore they are not suitable for lithium-ion cells thathave carbon anodes Both Li4Mn5O12 and Li2Mn4O9 ex-hibit most of their capacity in the 3 V region that corre-sponds to insertion of additional lithium into the 16c sites.Nevertheless, the Jahn–Teller distortion has been shown
to be delayed until late in the discharge process in both tems (33,38,39); the cubic symmetry without Jahn–Tellerdistortion has been shown to be preserved to x = 2.5 in
sys-Li4 +xMn5O12and x= 1.7 in Li2 +xMn4O9
Other Oxide Cathodes
The difficulties of the LiMn2O4spinel also motivated theinvestigation of several nonspinel manganese oxides, par-ticularly by employing low-temperature synthesis (33–35).LiMnO2obtained by conventional synthesis does not crys-
tallize in the O3 structure of LiCoO2; it adopts an thorhombic rock salt structure in which the oxygen array
or-is dor-istorted from the ideal cubic close packing (42) ever, LiMnO2isostructural with layered LiCoO2can be ob-tained by ion exchange of NaMnO2(43) or by partial sub-stitution of Mn by Cr or Al (44) Unfortunately, both theorthorhombic LiMnO2and the layered LiMnO2(O3 struc-
How-ture) that have close-packed oxygen arrays tend to form to spinel-like phases during electrochemical cycling
trans-In this regard, Na0.5MnO2—designated as Na0.44MnO2 inthe literature—adopts a non-close-packed structure andhas drawn some attention because it does not transform tospinel-like phases (45,46) However, only a small amount
of lithium could be extracted from the ion-exchanged ple Na0.5−xLixMnO2 although additional lithium could beinserted into Na0.5−xLixMnO2 Therefore, it is not attrac-tive for lithium-ion cells that use carbon anodes Neverthe-less, it has been shown that it is a promising candidate forlithium polymer batteries that employ metallic lithium an-odes (45) Additionally, it has been shown that amorphousmanganese oxides LixNayMnOzIηsynthesized in nonaque-ous media exhibit high capacity (300 Ah/kg) and good cy-clabilty (47,48) However, the capacity occurs across thewide voltage range of 4.3 to 1.5 V that has a continuouslysloping discharge profile, which is not desirable for com-mercial cells Not much lithium could be extracted from theinitial material LixNayMnOzIη, and therefore, these amor-phous oxides also are not attractive for lithium-ion cellsfabricated using carbon anodes
sam-To improve the cyclability of the LiMn2O4spinel, tial substitution of Mn by several other transition metals
par-M= Cr, Co, Ni and Cu in LiMn2 −yMyO4has been pursued(49–52) These substitutions, however, result in the devel-opment of two plateaus that correspond to the removal oflithium from the 8a tetrahedral sites: one around 4 V that
Trang 26corresponds to the oxidation of Mn3 +to Mn4 +and the other
around 5 V that corresponds to the oxidation of the other
transition-metal ions The capacity in the 4-V region
de-creases, whereas that in the 5-V region increases as y in
LiMn2 −yMyO4increases Although an increase in the cell
voltage is attractive from the view point of energy density,
the LiMn2 −yMyO4oxides are prone to suffer from oxygen
loss and safety concerns in the 5-V region
LiVO2 adopts the O3 structure of LiCoO2 Although
lithium can be readily extracted from LiVO2, the
vana-dium ions migrate to the lithium planes for (1− x) < 0.67
in Li1 −xVO2 (53) Similarly, the LiV2O4spinel is plagued
by the migration of vanadium ions during the charge/
discharge process (54) Interestingly, a number of other
vanadium oxides such as VO2(B)—a metastable form of
VO2obtained by solution-based synthesis (55)—and V6O13
(56) exhibit high capacity and good cyclability However,
these oxides that have no lithium are not attractive for
lithium-ion cells made using carbon anodes LiCrO2 also
crystallizes in the O3 structure of LiCoO2, but it is
diffi-cult to extract lithium from this material
Iron oxides offer significant advantages in both cost and
toxicity compared to other oxides Although LiFeO2
ob-tained by conventional procedures adopts a different
struc-ture, layered LiFeO2that has the O3 structure of LiCoO2
can be obtained by an ion-exchange reaction of NaFeO2
Unfortunately, the layered LiFeO2 does not exhibit good
electrochemical properties because the high spin Fe3 +:3d5
ion tends to move around between the octahedral and
tetra-hedral sites This problem could, however, be overcome by
designing complex iron oxides that consist of poly ions such
as (SO4)2 −and (PO4)3 − For example, it was shown in the
1980s that Fe2(SO4)3that has a framework structure that
consists of FeO6octahedra which share all six corners with
(SO4)2 −tetrahedra has a capacity of around 130 Ah/kg and
a flat discharge voltage of 3.6 V (57) However, the poor
electronic conductivity of the Fe–O–X–O–Fe (X= S or P)
linkages leads to poor rate capability Nevertheless,
fol-lowing this initial concept of using poly ions, LiFePO4that
crystallizes in an olivine structure has recently been shown
to be a promising material; it exhibits a flat discharge
volt-age of around 3.4 V (58) However, LiFePO4appears to
suf-fer from limited rate capability due to insuf-ferior electronic
(σe) and lithium-ion (σLi) conductivity compared to other
oxide cathodes such as LiCoO2and LiMn2O4
Carbon Anodes
Carbon has become the material of choice for anodes in
lithium-ion cells (59,60) due to its light weight and low
electrochemical potential that lies close to that of metallic
lithium (Fig 7) Although the intercalation of alkali metals
into graphitic carbon was known for some time, the
recog-nition of a practical carbon anode began in 1989 (61) A
sub-sequent announcement by Sony Corporation in 1990
com-mercializing lithium-ion cells that have carbon anodes and
LiCoO2cathodes intensified the interest in carbon Carbon
materials can be broadly classified into two categories:
soft carbon (graphitic carbon) and hard carbon (glassy
car-bon) The former has a better ordering of graphene
lay-ers compared to the latter, and they differ significantly in
1.5Irreversiblecapacity
Figure 18 Typical first discharge/charge curves of graphite The
difference between the discharge and charge curves is irreversible capacity loss.
their physical and chemical properties The hard carbonsare typically obtained by thermal decomposition of, forexample, phenolic and epoxy resins and products frompetroleum pitch They have significant amounts of openmicropores, which tend to become closed when heated atincreasingly higher temperatures Some hard carbons havebeen shown to consist of single graphene sheets
Figure 18 shows a typical first discharge/charge curve
of graphite It has a theoretical capacity of 372 Ah/kg thatcorresponds to an insertion of one lithium per six carbonatoms (x= 1 in LixC6) It shows a significant amount of ir-reversible capacity during the first discharge/charge cycledue to unwanted, irreversible side reactions with the elec-trolyte These side reactions can lead to disintegration ofthe carbon anode and a decrease in cycle efficiency Moreimportantly, using electrolytes that consist of propylenecarbonate (PC), natural graphite cannot be charged be-cause it leads to an evolution of gas at around 1 V This
is a major drawback of the graphite anode However, usingelectrolytes that consist of other solvents such as ethylenecarbonate (EC) and diethyl carbonate (DEC), the side re-actions are suppressed, and it can be cycled without muchdifficulty
The hard carbons generally have higher capacity thangraphite Several models have been proposed to accountfor the increased capacity: adsorption of lithium on bothsides of the single graphene sheets, accommodation of ex-tra lithium into nanometer size cavities, and storage of ad-ditional lithium at the edges and surfaces are some of theexplanations Generally, the capacity of carbon materialshas been found to increase as the fraction of single layermaterial increases However, the hard carbons have a slop-ing discharge profile between 0 and 1 V, unlike graphite,which has a nearly flat discharge profile between 0 and0.3 V (Fig 18) As a result, for lithium-ion cells that usethe same cathode, the hard carbons will lead to a slightlylower cell voltage compared to graphite
Structural modifications to improve the performance ofcarbon anodes are being pursued by various groups In
Trang 27this regard, texture control, surface modification by mild
oxidation, and incorporation of other elements such as
B, O, Si, and P have been studied For example, carbon
fibers that have different textures and compositions such
as C1 −y−zSiyOzand BC2N have been investigated
Other Anodes
The irreversible capacity loss encountered in carbon
an-odes has motivated the search for other anode hosts In this
regard, a few materials have drawn attention Li4Ti5O12
that has a cubic spinel structure accommodates three
ad-ditional lithium ions per formula unit into the empty 16c
sites and has negligible change in volume (<0.1%) at a flat
discharge voltage of around 1.5 V (62) However, the higher
voltage (1.5 V) and lower capacity (160 Ah/kg) compared to
that of carbon make it less attractive SnO2is another
can-didate that has reversible capacity as high as 600 Ah/kg at
0 to 2 V, but it exhibits high capacity loss during the first
cy-cle (63) More recently, some intermetallic compounds such
as Cu6Sn5that have an NiAs-type structure have shown
promise (64), and further development of these systems is
in progress
However, all of the preceding candidates and carbon
an-odes do not contain lithium, and they require that the
cath-odes be in the lithiated (discharged) form In this regard,
anode hosts based on some lithiated transition-metal
ni-trides (59) and intermetallic compounds (65) are appealing
For example, Li7 −xMnN4and Li3 −xFeN2exhibit capacities
of, respectively, 210 and 150 Ah/kg and a flat discharge
voltage of around 1.2 V Li2.6−xCo0.4N and Li2.6−xCu0.4N
whose structures are similar to that of Li3N exhibit a much
higher capacity of around 470 Ah/kg at 0.2 to 1 V; the
for-mation of an amorphous phase during the initial stages
in the latter systems leads to high capacity Two lithium
per formula unit can be reversibly extracted from Li2CuSn
(65) Further development work is necessary to assess the
full potential of these lithium-containing anodes If
suc-cessful, they have the possibility of being coupled with
some of the lithium-free cathodes such as vanadium oxides
However, the resulting lithium-ion cells may have a lower
cell voltage compared to the currently available
lithium-ion cells fabricated using LiCoO2 cathodes and carbon
anodes
CONCLUDING REMARKS
After providing an introduction to the concepts of
elec-trochemical cells and batteries, lithium-ion batteries that
offer much higher energy density compared to other
rechargeable systems were discussed Lithium-ion
batter-ies have become commercial due to the development of
smart electrode (cathode and anode) host materials
State-of-the-art lithiumion cells are made by using a
transition-metal oxide cathode such as a layered lithium cobalt
ox-ide and a carbon anode However, only 50 to 65% of the
theoretical capacity of the currently available oxide hosts
can be practically used Chemical instability, structural
instability, or safety concerns in the charged state limit
the usable capacity, depending on the cathode host The
challenge is to develop smart cathode hosts in which atleast one lithium ion per transition-metal ion can be re-versibly extracted/inserted and at the same time reducethe material cost; such a cathode can nearly double theenergy density There are also possibilities for increasingthe capacity of anode hosts by focusing on amorphous ma-terials An alternate approach is to develop cells that uselithium-containing anodes and lithium-free cathodes Thisstrategy will allow using some of the already known highcapacity cathodes such as vanadium oxides that have bet-ter chemical stability and safety characteristics From theview points of safety, cycle, and shelf life, cathodes thathave a lower voltage (3 to 4 V) but have a significantly in-creased capacity may be desirable for future applications
ACKNOWLEDGMENTS
The author thanks the Welch Foundation (Grant F-1254)for financial assistance and Dr A M Kannan, SeungdonChoi, and Ramanan Chebiam for their assistance with thefigures
Tech-8 M.S Whittingham and A.J Jacobson, Intercalation Chemistry.
Academic Press, NY, 1982.
9 J.P Gabano, Lithium Batteries Academic Press, London,
14 K Mizushima, P.C Jones, P.J Wiseman, and J.B Goodenough,
Mat Res Bull 15: 783 (1980).
15 J.B Goodenough, K Mizushima, and T Takeda, Jpn J Appl.
Phys 19: 305 (1983).
16 M.M Thackeray, W.I.F David, P.G Bruce, and J.B.
Goodenough, Mat Res Bull 18: 461 (1983).
17 M.K Aydinol and G Ceder, J Electrochem Soc 144: 3832
(1997).
Trang 2818 J.N Reimers and J.R Dahn, J Electrochem Soc 139: 2091
(1992).
19 A Manthiram, R.V Chebiam, and F Prado, Chem Mater 13:
2951 (2001), p 269; R.V Chebiam, A.M Kannan, F Prado, and
A Manthiram, Electrochem Commun 3: 624 (2001).
20 L.A Montoro, M Abbate, and J.M Rosolen, Electrochem Solid
State Lett 3: 410 (2000).
21 A Hightower, J Graetz, C.C Ahn, P Rez, and B Fultz, 198th
Meet Electrochem Soc Phoenix, AZ, October 22–27, 2000,
24 A Hirano, R Kanno, Y Kawamoto, Y Tekeda, K Yamamura,
M Takano, K Ohyama, M Ohashi, and Y Yamaguchi, Solid
State Ionics 78: 123 (1995).
25 I Nakai, K Takahasi, Y Shiraishi, T Nakagome, and
F Nishikawa, J Solid State Chem 140: 145 (1998).
26 W Li and J Curie, J Electrochem Soc 144: 2773 (1997).
27 X.Q Yang, X Sun, and J McBreen, Electrochem Commun 2:
100 (2000).
28 L Croguennec, C Pouillerie, and C Delmas, J Electrochem.
Soc 147: 1314 (2000).
29 A.N Mansour, X.Q Yang, X Sun, J McBreen, L Croguennec,
and C Delmas, J Electrochem Soc 147: 2104 (2000).
30 M Balasubramanian, X Sun, X.Q Yang, and J.Mcbreen,
J Electrochem Soc 147: 2903 (2000).
31 R.V Chebiam, F Prado, and A Manthiram, J Electrochem.
Soc 148: A49 (2001).
32 J E Huheey, Inorganic Chemistry: Principles of Structure and
Reactivity Harper & Row, NY, 1972, p 294.
33 M.M Thackeray, Prog Solid State Chem 25: 1 (1997).
34 A Manthiram and J Kim, Chem Mat 10: 2895 (1998).
35 A Manthiram and J Kim, Recent Res Dev Electrochem 2: 31
(1999).
36 S.J Wen, T.J Richardson, L Ma, K.A Striebel, P.N Ross, and
E.J Cairns, J Electrochem Soc 143: L136 (1996).
37 M.M Thackeray, Y Shao-Horn, A.J Kahaian, K.D Kepler,
E Skinner, J.T Vaughey, and S.A Hackney, Electrochem Solid
State Lett 1: 7 (1998).
38 M.M Thackeray, A de Kock, M.H Rossouw, D.C Liles,
D Hoge, and R Bittihn, J Electrochem Soc 139: 363 (1992).
39 R.J Gummow, A de Kock, and M.M Thackeray, Solid State
43 A.R Armstrong and P.G Bruce, Nature 381: 499 (1996).
44 I.J Davidson, R.S McMillan, and J.J Murray, J Power Sources
47 J Kim and A Manthiram, Nature 390: 265 (1997).
48 J Kim and A Manthiram, Electrochem Solid State Lett 2: 55
(1999).
49 C Sigala, D Guyomard, A Verbaere, Y Piffard, and M.
Tournoux, Solid State Ionics 81: 167 (1995).
50 H Kawai, M Nagata, H Takamoto, and A.R West,
Elec-trochem Solid State Lett 1: 212 (1998).
51 Q Zhong, A Bonakdarpour, M Zhang, Y Gao, and J.R Dahn,
J Electrochem Soc 144: 205 (1997).
52 Y Ein-Eli, W.F Howard, Jr., S H Lu, S Mukerjee, J McBreen,
J.T Vaughey, and M.M Thackeray, J Electrochem Soc 145:
1238 (1998).
53 L.A de Picciotto, M.M Thackeray, W.I.F David, P.G Bruce,
and J.B Goodenough, Mat Res Bull 19: 1497 (1984).
54 L.A de Picciotto, M.M Thackeray, Mat Res Bull 20: 1409
(1985).
55 C Tsang and A Manthiram, J Electrochem Soc.144: 520
(1997).
56 C Lampe-Onnerud, J.O Thomas, M Hardgrave, and S.
Yde-Andersen, J Electrochem Soc 142: 3648 (1995).
57 A Manthiram and J B Goodenough, J Power Sources 26: 403
O Yamamoto, eds., Wiley-VCH, Weinheim, 1998, p 98.
60 M Winter and J.O Besenhard, in Lithium Ion Batteries: damentals and Performance, M Wakihara and O Yamamoto,
Fun-eds., Wiley-VCH, Weinheim, 1998, p 127.
61 R Kanno, Y Takeda, T Ichikawa, K Nakanishi, and
O Yamomoto, J Power Sources 26: 535 (1989).
62 D.W Murphy, R.J Cava, S.M Zahurak, and A Santoro, Solid
State Ionics 9 & 10: 413 (1983).
63 W Liu, X Huang, Z Wang, H Li, and L Chen, J Electrochem.
Soc 145: 59 (1998).
64 K.D Kepler, J.T Vaughey, and M.M Thackeray, Electrochem.
Solid State Lett 2: 307 (1999).
65 J.T Vaughey, K.D Kepler, R Benedek, and M.M Thackeray,
of a material because it is implanted in the body for longperiods Among many traditional materials, including met-als, alloys, and ceramics, that are available commercially,only a limited number are currently used as prostheses
or biomaterials in medicine and dentistry The tions in the second category require excellent mechanical
Trang 29applica-characteristics as well as biocompatibility The third
cate-gory is used mainly for transducers
Among smart materials, the Ti–Ni shape-memory
al-loy (SMA) has attracted the most attention for biomedical
applications in the first and second categories due to its
excellent biocompatibility and mechanical characteristics
Research on biomedical applications of the SMA started in
the 1970s with animal experiments initially, followed by
clinical tests The first example of a successful biomedical
application of the SMA was a bone plate, which was used to
repair broken bones Now, many medical and dental
appli-cations of SMAs are available, and many new appliappli-cations
are being developed On the other hand, piezoelectric
ma-terials have been widely used as transducers for medical
ultrasonic devices due to their sensor function that uses
piezoelectricity and the actuator function that uses inverse
piezoelectricity
In this article, the properties of SMAs for biomedical
applications are discussed next, followed by some clinical
examples Recent examples of biomedical applications of
SMAs are summarized there after, and finally the recent
examples of biomedical applications of piezoelectric
mate-rials are summarized
PROPERTIES OF SMAS FOR BIOMEDICAL APPLICATIONS
The properties of SMAs that are important and have led
to its wide acceptance in biomedical applications are
dis-cussed in this section Of these properties,
biocompatibili-lity, which simply means the ability of a material to be
accepted by the body, is the most important, especially for
implants The other important properties include
super-elasticity, the shape-memory effect, hysteresis, and fatigue
resistance The properties of SMAs for biomedical
applica-tions are discussed in detail in (1)
Biocompatibility
The biocompatibility of a material is its most important
property if it is used as prostheses or biomaterials in
medicine and dentistry Biocompatibility means that the
material is nontoxic during the implanted period Because
all materials generate a “foreign body reaction” when
im-planted in the body, the degree of biocompatibility is
re-lated to the extent of this reaction Due to the rigorous
demands on material properties for biocompatibilty, only
these three metallic materials were qualified for use as
implant materials: Fe–Cr–Ni, Co–Cr and Ti–Al–V before
SMA Investigations were carried out by many researchers
on the biocompatibility of Ti–Ni (2), and an extensive
re-view can be found in (1) The results of these studies show
that Ti–Ni has superior corrosion resistance due to the
for-mation of a passive titanium oxide layer (TiO2) similar to
that found on Ti alloys This oxide layer increases the
sta-bility of the surface layers by protecting the bulk material
from corrosion and creates a physical and chemical barrier
to Ni oxidation
In in vitro dissolution studies, Bishara et al (3) found
that Ti–Ni appliances release an average of 13.05µg/day
Ni in saliva, which is significantly lower than the estimated
average dietary intake of 200–300µg/day In addition, the
measured nickel blood levels of orthodontic patients whohave Ni–Ti appliances show no significant increase during
in the body and makes it possible to create a prestressafter deployment, when necessary SMA appliances arefirst in a compact state during deployment and then re-stored to their expanded shape by heating If the phasetransformation temperature of an SMA is below body tem-perature, shape recovery can easily be induced by the heat
of the body When the phase transformation temperature
is higher than the body temperature, SMA appliances areusually heated by warm salt water or a high frequencymagnetic field
In recent studies, the shape-memory effect has also beenused for actuator functions in medical applications such
as a urethral valve and artificial sphincter which are cussed later
dis-Superelasticity
SMAs exhibit superelasticity when they are in the itic phase (1,5) Figure 1 shows the typical superelasticstress–strain curve (solid line) compared with the stress–strain curve of stainless steel (dashed line) As shown inthe figure, an important feature of superelastic materials isthat they exhibit constant loading and unloading stressesacross a wide range of strain As shown in Fig 1, the
A
StrainSubthreshold
Excessiveforce zone
Figure 1 Typical stress–strain curve of superelastic materials
and stainless steel The superelastic materials exhibit constant unloading stress over a wide range of strain.
Trang 30effective strain range εeff(TN) of Ti–Ni that corresponds
to an optimal force zone is much larger than theεeff(SS)
of stainless steel Hence, a superelastic device can provide
constant pressure even if the pressed part recedes by a
lim-ited amount during the installed period On the other hand,
the pressure exerted by an appliance made from stainless
steel will drop drastically if the pressed part deforms, so
that performance deteriorates The orthodontic arch wire
that is presented as an example of an application in the
next section was the first product to use this property
Another example of applying this property is superelastic
eyeglass frames (6) These eyeglass frames have become
very popular in the United States, Europe, and Japan and
are available in almost every optician’s store These frames
can be twisted a full 180◦, but more importantly the frames
press against the head with a constant and comfortable
stress Not only is “fit” less important, but small bends
and twists that may develop do not cause discomfort to the
wearer
The superelasticity of SMAs also makes it easy to deploy
SMA stents Stents made from stainless steel are expanded
against the vessel wall by plastic deformation caused by
inflating a balloon placed inside the stent Ti–Ni stents,
on the other hand, are self-expanding More details can be
found later
Hysteresis of SMA
As shown in Fig 1, superelastic SMA exhibits a hysteretic
stress–strain relationship; the stress from A to B in the
loading phase and the stress from C to D in the unloading
are different Hysteresis is usually regarded as a drawback
in traditional engineering applications, but it is useful in
biomedical applications If the SMA is set at some stress–
strain state, E, for example, upon unloading during
deploy-ment, it should provide a light, constant force against the
organ wall, even under a certain amount of further strain
release (e.g., from E to D) On the other hand, it would
gen-erate a large resistive force to crushing if it is compressed
in the opposite direction because it takes the loading path
from E to F Hence, the SMA material exhibits a biased
stiffness at point E, which is very important in designing
a SMA stent Because the stress at the loading phase from
A to B and the stress in the unloading phase from C to D
depend on the material composition of the SMA, the
desi-rable stress–strain curve can be obtained by optimizing the
material composition
Anti-Kinking Properties
As shown in Fig 1, the stress of stainless steel remains
nearly constant in the plastic region This means that a
small increase in stress in the plastic region could lead to
a drastic increase in strain or failure of a medical
appli-ance made from stainless steel (1) On the other hand, the
stiffness of superelastic Ti–Ni increases drastically after
point B at the end of the loading plateau The increase in
stiffness would prevent the local strain in the high strain
areas from further increasing and partition the strain in
the areas of lower strain Hence, strain localization is
pre-vented by creating a more uniform strain than could be
realized by using a conventional material
EXAMPLES OF BIOMEDICAL APPLICATIONS
Orthopedic Marrow Needles Figures 2 and 3 show two types of mar-
row needles that are used in the repair of a broken thighbone (4,6–8) When a stainless steel Kunster marrow nee-dle is used, blood flow inside the bone can be blocked, andrecovery can be delayed It also has the drawback of lowtorsional strength On the other hand, a Kunster marrowneedle of SMA can be inserted into the bone in its initialstraight shape and transformed to a curved shape by heat-ing, as shown in Fig 2 Hence, the SMA Kunster marrow
Thighbone
Fracture closed
SMA aftershape recovery
After heating(b)
Figure 2 Kunster marrow needle (6).
Trang 31Heat
Figure 3 Marrow needles before and after heating (5,8).
needle can avoid the disadvantages of the stainless steel
needle The SMA Kunster marrow needle can also provide
a compressive force on the fracture surfaces
The marrow needle shown in Fig 3 has a
compli-cated shape for purposes of reinforcement, which makes it
difficult to insert in the broken bone Using the
shape-memory effect, insertion can be greatly improved, as shown
in the figure, without loosing the reinforcing function,
be-cause the needles can be inserted in a simpler shape and
the necessary size and shape are recovered by heating the
needle in the marrow
Currently available joint prostheses are made of bone
cement to be fixed in the bone Stress acting on the joint
prosthesis is quite intense and severe: three to six times the
body weight of the patient under nominal action, and the
stress is cycled up to 106times Conventional bone cement
causes several inconveniences: gradual loosening after
im-plantation, resultant infection, and other complications A
prosthetic joint made of Ti–Ni SMA was developed to avoid
such problems High wear resistance is also another
advan-tage of the Ti–Ni prosthetic joint
Bone Staple and Bone Plate The bone staple shown in
Fig 4 and the bone plate in Fig 5 are used to fix broken
bones (4–6) As shown in Fig 4, a bone staple made of SMA
can be inserted at low temperature in the holes opened in
the bone, and then heated by the body temperature, it
re-covers its original shape to provide a compressive force on
the surfaces of the broken bone Bone plates are attached
by screws for fixing broken bones Bone plates made of Ti–
Ni SMA are more effective in connecting broken bones than
bone plates made of conventional material because SMA
Figure 5 Bone plate used to fix broken bones (4–6).
bone plates provide compressive force on the fracture face of the broken bones as well as repair, as shown in Fig 5.Healing proceeds faster under uniform compressive force
sur-Dental Applications Orthodontic Fixtures Due to its superelasticity, Ti–Ni is
used in many applications in dentistry It is obvious thatsuperelasticity gives the orthodontists better mechanicalcharacteristics compared to conventional elastic materialssuch as stainless steel Figure 6a,b shows a clinical ex-ample of orthodontic treatment using a superelastic Ti–Niarch wire (5,9) When fixtures made of conventional elas-tic material such as stainless steel are used, the reformingforce drops, and the fixture loosens due to movement of theteeth Hence, the fixture must be replaced several timesbefore the treatment is finished An SMA fixture main-tains a constant reforming force in a wide range of teethmovement due its superelasticity, so that no replacement isrequired after the initial installation Clinical results alsoshowed faster movement of the teeth and a shorter chairtime compared with stainless steel wire
Tooth-root Prosthesis Among several methods that
re-store the masticatory function of patients missing morethan one tooth, a tooth-root prosthesis is considered themethod that creates the most natural masticatory func-tion Blade-type implants made of Ti–Ni SMA, as shown
in Fig 7, have been used in Japan (5,6) The open angle
of the blade is used to ensure tight initial fixation and toavoid accidental sinking during mastication But to makethe insertion operation easy, the tooth-root prosthesis is
Trang 32Misaligned teeth before treatment(b)
Normally aligned teeth after the first stage of treatment
Figure 6 Orthodontic treatment using a superelastic arch wire:
(a) misaligned teeth before treatment; (b) normally aligned teeth
after the first stage of treatment (5,9).
implanted in the jawbone as a flat shape and then the
opened shape is changed by heating Fig 8 shows an X-ray
photograph of the implanted tooth-root prosthesis More
than 5,000 clinical examples of SMA tooth-root prostheses
have been reported
Partial Denture The key to a partial denture is the
development of an attachment for connecting the partial
Figure 7 Tooth-root prosthesis (5,6).
Figure 8 X-ray photo of implanted tooth-root prosthesis (6).
denture to the retained teeth Clasps have been tionally used for about a century as the attachment for
conven-a pconven-articonven-al denture One of the drconven-awbconven-acks of clconven-asps mconven-ade
of conventional elastic materials is loosening during use;this can be improved by replacing the elastic materials by asuperelastic Ti–Ni alloy (5,10) Another drawback of clasps
is aesthetics because they are visible in the teeth ment To solve the problem, the size of the attachmentmust be smaller than the width of the teeth so that it can
align-be emalign-bedded completely in the teeth A precision ment using a small screw has recently become available,but it has to be designed and fabricated very precisely sothat it lacks flexibility to follow the change in the settingcondition during long-term use due to the shape change ofthe jawbone Because of its flexibility, this problem can besolved by using an attachment made of SMA
attach-The SMA attachment consists of two parts: a fixed partthat is made of a conventional dental porcelain-fusible castalloy and is attached to the full cast crown on the anchorteeth and a movable part that is made of Ti–Ni SMA and
is fixed on the side of the partial denture Examples ofmovable and fixed parts are shown in Fig 9
Surgical Instruments
Since superelastic tubing became available in the early tomid-1990s, a variety of catheter products and other en-dovascular devices using Ti–Ni has appeared on the mar-ket Early applications of Ti–Ni were retrieval baskets thathave Ti–Ni kink-resistant shafts, as well as a superelasticbasket to retrieve stones from kidneys, bladders, and bileducts An interesting example is the interaortic balloonpump (IABP) used in cardiac assist procedures (Fig 10).The use of Ni–Ti allowed a reduction in the size of the de-vice compared with the polymer tube designs and increasedthe flexibility and kink resistance compared with stainlesssteel tube designs (1)
Biopsy forceps made from stainless steel are very cate instruments that can be destroyed by even very slightmishandling Ti–Ni instruments, on the other hand, canhandle serious bending without buckling, kinking, or per-manent deformation Figure 11 shows a 1.5-mm biopsy for-ceps that consists of thin wall Ti–Ni tubing and a Ti–Niactuator wire inside Together they can be bent around a
Trang 33Movable part(b)
Fixed part
Figure 9 Shape-memory alloy attachment for partial denture;
(a) movable part; (b) fixed part (4,5).
radius of less than 3 cm without kinking, and still allow for
the opening and closing of the distal grasper jaws without
increased resistance The instrument continues to operate
smoothly even while bent around tortuous paths
Figure 10 The Arrow interaortic balloon pump uses a Nitinol™
tube to pressurize the balloon (1).
Figure 11 Ninitol™ tubing that has an internal actuating wire
allows this 0.8-mm diameter grasper to operate while tied in a knot (1).
Stent
The term stent is used for devices that are used to scaffold
or brace the inside circumference of tubular passages or mens, such as the esophagus biliary duct, and most impor-tantly, a host of blood vessels, including coronary, carotid,iliac, aorta, and femoral arteries (Fig 12) (1) Stenting inthe cardiovascular system is most often used as a follow-
lu-up to balloon angioplasty, a procedure in which a balloon
is placed in the diseased vessel and expanded to reopen
a clogged lumen Ballooning provides immediate ment in blood flow, but 30% of the patients have restenosedwithin a year and need further treatment The place-ment of a stent immediately after angioplasty, it has beenshown, significantly decreases the propensity for resteno-sis Stents are also used to support grafts, for example, intreating aneurysms (Fig 13)
improve-Most stents today are stainless steel and are expandedagainst a vessel wall by plastic deformation caused byinflating a balloon placed inside the stent Ti–Ni stents,
on the other hand, are self-expanding—they are shape-set
to the open configuration, compressed into a catheter, then
Figure 12 A stent that maintains vessel patency and blood flow
to the brain is portrayed in a cutaway view of the internal carotid artery (1).
Trang 34Figure 13 Stentgrafts used to exclude aneurysms, to provide an
artificial replacement for injured vessels, or prevent restenosis
after angioplasty (1).
pushed out of the catheter and allowed to expand against a
vessel wall Typically, the manufactured stent’s outer
dia-meter is about 10% greater than the vessel’s diadia-meter to
ensure that the stent anchors firmly in place The
flexibi-lity of Ti–Ni is about 10–20 times greater than stainless
steel, and it can bear a reversible strain as high as 10%
Ni–Ti stents are made from knitted or welded wire,
laser-cut or photoetched sheet, and laser-laser-cut tubing The
pre-ferred devices are laser-cut tubing, thus avoiding overlaps
and welds (Fig 14)
CURRENT BIOMEDICAL APPLICATIONS OF SMA
Artificial Urethral Valve
Urinary incontinence is the involuntary discharge of urine
caused by weakness of the urinary canal sphincter muscles
due to aging and expansion of the prostate gland
How-ever, the difference in ages, the sex of patients, and the
various causes of the disorder make it difficult to treat the
disease simply by drugs or surgery In this section, an
arti-ficial urethral valve system driven by an SMA actuator is
introduced (11)
Figure 14 Stents made from laser-cut tubing (1).
Figure 15 Artificial urethral valve.
Urethral Valve The artificial urethral valve should be
compact and should have no protrusions when it is planted in the lower abdominal region In addition, itshould be attachable onto various sizes of urethrae A com-pact urethral cylindrical valve is presented in Figs 15and 16 The valve is 15 mm across and 20 mm long It iscomposed of two semicircular stainless steel shells 0.2 mmthick and a 0.2-mm circular-arc NitinolTMplate The shellsand the NitinolTM plate are fixed together by stainlesssteel clamps Further, a cylindrical sponge rubber filling isplaced inside the valve to effect uniform contact betweenthe valve and the urinary canal In the normal state, thevalve presses on the canal, so that it is choked To free thecanal, the valve is opened by actuating the SMA element.The SMA plate, which is cylindrical at body temperature,flattens as heat is increased, and the valve, which is closed
im-by the force of the bias spring in the normal state, is opened
to release the choked urethra and allow urinary flow Toheat the SMA, a NichromeTM wire, insulated by a poly-imide membrane, was placed on the surface of the nitinolplate
Transcutaneous Energy Transformer System The energy
to drive an in-dwelled valve should be supplied from side the body A transcutaneous energy transformer systemwill be effective for this purpose (12,13) The system con-sists of two induction coils that transmit electrical energywirelessly from the primary to the secondary coil In thisstudy, the primary coil was 70 mm in diameter and had
out-12 turns, and the secondary coil was 60 mm across andhad eight turns The coils are spirals formed of twistedwires that consist of 20 lengths of copper wire 0.2 mm indiameter
Experimental Setup Figure 17 is the schematic of an
an-imal experiment that used the urethrae of male dogs ofaverage weight 12 kg, whose thickness is similar to that
of human male urethrae The urinary canal uncovered bythe cut was equipped with the SMA valve and then loadedwith water at a hydrostatic pressure of 75 cmH2O, which
is comparable to human abdominal muscle pressure Thetemperature of the valve and the flow rate of the waterpassing through the canal were measured First, the valve
Trang 35Sponge rubberUrethra
Flow meter
UrethraOutlet
Valve
Powersupply Dog
0 20 40 60
Time [s]
80 100 120 140
204060
Flow rateTemperature
Input voltage
2.5 V
Figure 18 Time variations of applied direct current, valve
temp-erature, and flow rate of water passing through the valve.
was heated by direct current from the transcutaneous ergy transformer system and then it was left to cool nat-urally by cutting the electric power to the heating wire
en-In the energy transformer system, the secondary coil wasplaced under the abdominal wall, and the primary coil onthe skin face-to-face with the secondary coil The capac-ity of the condenser to enhance the resonant effect of the
circuit was set at C2= 1.0 µH The frequency of the input
current, which should coincide with the resonant frequency
of the circuit, was 90 kHz Further, the peak-to-peakamplitude of the current was set at 25 V
Results and Discussion Figure 18 shows the
open-ing/closing functions of the valve when it was driven by thedirect current heating of the SMA The input current to theheating wire on the SMA, the temperature of the valve, andthe flow rate of water passing out through the urethra areplotted as functions of time The valve started to open, andthe water began to flow 20 seconds after electric currentwas supplied The current was cut off when the temper-ature of the valve reached 45◦C It is seen that the valvecompletely intercepted the water flow 30 seconds after theelectric current was cut off Thus, the valve possesses thenecessary function of an artificial urethral valve
Figure 19 illustrates the motor functions of thevalve when it was driven by the transcutaneous energy
0.02.0
Time [s]
204060
Flow rateTemperature
Energytransmitting
Figure 19 Opening/closing functions of valve driven by
transcu-taneous energy transformer system.
Trang 36Heating
Cooling
SMASilicone sheets
Figure 20 Schematic of the artificial sphincter using SMA.
transformer system The distance between the primary
and secondary coils was 3–4 mm, and the induced current
to the heating wire was 7.6 V in the peak-to-peak
ampli-tude The figure shows that the valve started to open and
released the choked canal 6 seconds after the electric
cur-rent was supplied The curcur-rent was cut off when the
tem-perature of the valve reached 45◦C, which was 35 seconds
after the current supply was started It is shown that the
water flow was intercepted 25 seconds after the current
was cut off These motor functions of the valve showed
that the induction coil system worked well as a
transcu-taneous energy transformer for heating the artificial
ure-thral valve
Artificial Sphincter
Similar to the urethral valve, the development of an
arti-ficial sphincter is also required for the medical treatment
of patients who have fecal incontinence due to a colostomy,
a congenitally anorectal malformation, or surgical
opera-tions for anorectal diseases The lack of an anal
sphinc-ter is the main reason for the problem In this section, an
artificial sphincter using a SMA actuator was one of the
solutions of these problems, as introduced in (14)
Figure 21 Schema of animal experiment.
Artificial anusPressure sensor
Mechanism of Artificial Sphincter A schematic drawing
of the proposed artificial sphincter is shown in Fig 20 Theactuator consists of two SMA plates joined by two hingesand the heating coils attached to the SMA plates The SMAplates are 70 mm long The width and the thickness are 18and 0.7 mm, respectively The material used for the SMAplates, Ti51at%Ni, is known to exhibit an all-round shape-memory effect (ARSME); it reverses shape to the “mem-orized” shape in its martensitic phase Because the high-est temperature for the complete reverse transformationmight reach 55◦C, thermally insulated materials such ascork sheets and sponge rubber sheets cover the outer andinner sides of the SMA plates, respectively When elec-tric power is applied to the coils for heating, the reversetransformation occurs in the SMA plates, accompanied byshape changes from a flat shape to an arc, the restrainedshape during annealing The shape change results in agap between the two SMA plates to open the intestines.After switching off the electric power, the shape of the SMAplates recovers by natural cooling, and the intestines areclosed again
Animal Experiments Animal experiments have been
conducted to examine the fundamental functions and thebiocompatibility of the actuator The experiments were car-ried out on a pig that had the same dimensions of intestines
as those of the human body
Preliminary tests of the fundamental functions of theactuator were conducted As illustrated in Fig 21, an arti-ficial anus was made in the pigs abdomen using a rectumafter the resection of its colons Then the artificial sphincterwas installed around the rectum located between the ab-dominal wall and the peritoneum (see Fig 22) The insidepressure of the rectum generated by the artificial sphincterwas measured first A pressure sensor was inserted fromthe artificial anus into the intestine and then moved out.The pressure exhibited a rise of 50 mmHg in the regionclipped by the actuator, corresponding to the width of theSMA plates: 18 mm (see Fig 23) The pressure tests werealso carried out when the inner part of the rectum was
Trang 37Figure 22 A photograph of the artificial sphincter installed in
the rectum of a pig.
subjected to pressure The inner pressure of the rectum
was generated by pouring gel into the intestines Figure 24
shows the pressure change measured during the test As
seen in Fig 24, the pressure was increased to 75 mmHg
without any leak of the gel, and then decreased by opening
the artificial sphincter using electric power Discharge of
the gel from the artificial anus was observed
A clinical test on a living pig has also been carried out
The artificial sphincter enables a controlled bowel
move-ment of the pig From the dissecting examination after six
days of experiments, neither infections nor burn scars were
observed in the body around the artificial sphincter
Fur-thermore, the artificial anus was in good condition; this
suggested that the pressure due to the artificial
sphinc-ter was tolerable Additionally, in these experiments,
50 mm Hg
Artificial sphincter Artificial anus
Figure 23 Pressure distribution in an intestine clipped by the
artificial sphincter.
20 sec
100 mm Hg
Figure 24 Pressure change in the rectum: (a) start pouring gel into the rectum; (b) switch on the
input power; (c) discharge of gel was observed.
electric power was supplied through a pair of current leadwires that penetrated the body The use of an inductivepower transmission for the power supplement of the actu-ator could lead to a complete implantation-type artificialsphincter based on further research
CURRENT BIOMEDICAL APPLICATIONS
OF PIEZOELECTRIC MATERIALS
Due to its piezoelectricity, a piezoelectric material has asensor function that can convert a mechanical signal to anelectric signal Electrical voltage generated by mechani-cal stress in piezoelectric materials decays very fast due
to charge dissipation The voltage signal takes the form
of a very brief potential wave at the onset of the appliedforce and a similar brief wave at termination It increases
as force is applied but drops to zero when the force mains constant There is no response during the stationaryplateau of the applied stimulus Voltage drops to a negativepeak as the pressure is removed and subsequently decays
re-to zero (15) The response is quite similar re-to the response
of the Pacinian corpuscle in the human skin (16),one of thesensory receptors in the dermis PVDF (polyvinylidene flu-oride) piezofilm is suitable for uses in the biomedical field,because it is very flexible and sensitive to the fast variation
of stress or strain In this section, several recent studies ofmedical applications of PVDF film are introduced
Active Palpation Sensor for Detecting Prostatic Cancer and Hypertrophy
Prostatic carcinoma and hypertrophy are examined in eral by rectal palpation where the doctor’s index finger isused as a probe together, in most cases, with ultrasonictomography The two lesions found in this study are diag-nosed by noticing their morphological features Prostatichypertrophy is a symmetrical enlargement of the prostateglands; the stiffness varies from soft to hard Prostaticcancer, on the other hand, is a hard asymmetrical uneventumor Palpation depends on the tactile perception of theforefinger, which is said to be ambiguous, subjective, andmuch affected by the physician’s experiences Hence, thedevelopment of a palpation sensor for detecting prostaticcancer and hypertrophy is important
gen-Palpation Sensor and Measurement System The geometry
of an active palpation sensor and tip probe are presented
Trang 38PVDF film
PVDF film
1 mmSponge rubberVulcanized
in Figs 25 and 26 The tip probe is mounted on a linear
z-translation aluminum bar It fits into a cylindrical outer
aluminum shell 15 mm in diameter and is driven by a dc
micromotor and crank mechanism The drive mechanism
is essentially the same as that of an electric toothbrush
The probe is positioned so that its face is to the prostate
gland, and, it is oscillated at about 50 Hz at a constant
peak-to-peak amplitude of 2 mm The probe is an assembly
of layered media
The base is a thin aluminum circular plate 10 mm in
diameter, on which a cylindrical rubber sponge 8 mm in
diameter and 4 mm thick, a PVDF piezopolymer film 6 mm
across and 28µm thick as the sensory receptor, and a thin
acetate film as a protect cover for the piezopolymer film
are stacked in sequence Furthermore, a convex layer of
vulcanized rubber 3 mm across was placed on the
sur-face of the acetate film to enhance the sensitivity of the
sensor (17)
In the experiment, the sensor head is pressed
sinu-soidally against the object, and the output signal from the
piezopolymer film is collected for 100 ms, sent to a
digi-tal storage oscilloscope for every sampling time of 0.2 ms,
and further forwarded to a personal computer via a GP-IB
interface as 500 eight-bit data for processing
Signal Processing The output voltage from the
piezo-polymer film is proportional to the rate of the strain
in-duced in the film, which means that the maximum
ampli-tude of the signal from the sensor is rather superposed
by noises from the measuring system Bearing this fact in
mind, the following data analysis can be done by using the
absolute output signal of the sensor integrated across the
period of data collection:
Figure 26 Geometry of a sensory receptor.
where I is the integrated output signal and N (= 500) is
the total number of data collected in a period of 100 ms
Clinical Test Rectal palpation was done by using the
sensor to verify the discrimination function of the sor First, the doctor examined the stiffness of the prostategland of a person by using his own index finger Next, thesensor protected by a medical rubber glove was insertedinto the subject’s rectum The relative position of the sen-sor to the prostate gland was monitored by the ultrasonicdiagnostic, and the sensor was placed face to face to theprostate gland and driven to generate sensor output Theexaminees in this time were eight in total One 74-year-oldperson was suffering from a carcinoma Four persons ofaverage age 77 were patients who had prostatic hypertro-phy, and two persons (average age 52) suffered from pro-statitis The last person diagnosed had no definite lesions
sen-on his prostate gland The stiffness of the prostate glandsdiagnosed this time was “elastic soft or elastic firm,” “def-initely elastic firm,” and “hard.” The results obtained arepresented in Table 1, which shows the average, the mini-mum and maximum output, and the standard deviation
of the output It is seen clearly that the output from theprostate gland of the diagnosis “hard” is greater than theoutput of the gland of “elastic firm.”
Haptic Sensor for Monitoring Skin Conditions
Assessing the pharmaceutical action of liniments on skindisease is a matter of importance to dermatologists Thishas drawn much attention to the development of objectivetechniques for measuring the morphological features ofskin (18) Evaluating the substantiation of the cosmeticefficacy of toiletries is another of the objective measuringtechniques The features that affect the health appraisal
Trang 39Figure 27 Tribosensor.
and/or the physical beauty of skin are the morphology such
as rashes, chaps, or wrinkles This noninvasive technology
has made great advances in the studies of dermatology
during the last decade, and several methods have been
de-veloped to measure the mechanical properties of the
der-mis such as measuring transepidermal water loss using
an evaporimeter (19) and image processing of a negative
replica of the dermis (20).These methods, however, fall in
the category of indirect measuring techniques for the
der-mis In this section, the development of haptic tribosensors
for monitoring skin conditions and distinguishing atophic
and normal healthy skins directly is introduced
Tribosensor A tactile sensor for measuring skin surface
conditions is presented in Figs 27 and 28 The sensor is a
layered medium, whose construction is analogous to that
of the human finger It is composed of an aluminum shell
as the phalanx, sponge rubber 3 mm thick as the digital
pulp, a PVDF piezopolymer film 28µm thick and 12 mm
across as the sensory receptor, an acetate film as a
protec-tive cover for the piezofilm, and gauze on the surface as the
fingerprint that enhances the tactile sensitivity of the
sen-sor The sensor was attached to the tip of an acrylic elastic
beam, and a strain gauge was mounted on the surface of
the beam to monitor the force applied to the skin by the
sensor
Aluminum pipeSponge rubberElectrodePVDFCellophane filmGauzePVDF
Figure 28 Schematic of PVDF piezofilm sensor.
Table 2 Segmented Frequency Range for Power Spectrum Integration
EarthArmSensor
Neck
Band-pass filter
GPIB
Computer Oscilloscope
Figure 29 Setup of measuring instruments.
Measuring Apparatus A measurement system using the
tribosensor is presented in Figure 29 The sensor wasmoved by hand over the sample skin to maintain a constantspeed and force The voltage signal from the PVDF sensoryfilm was sent to a digital storage oscilloscope as eight-bitquantitized digital signals of 4096 points and then trans-mitted to a personal computer via a GPIB board for signalprocessing The sampling frequency was held constant at
40 kHz In the process of measurement, it was necessary
to reduce the potential difference between the surface ofthe skin and the sensor to minimize the overlap of noises
on the sensor signal To this end, the subject and the sor were grounded by fitting a grounding conductor aroundthe wrist Still, some noises from the power sources, whichwere due to outside sources, were observed around 50 Hzand 100 MHz, respectively Thus, a band-pass filter thathad cutoff frequencies of 70 Hz and 20kHz was insertedafter the sensor to remove the noise effect
sen-Signal Processing and Identification of Skins Dermatitis
is a factor that affects the skin condition The neck skin ofsubject A, who was suffering from mossybacked atopic der-matitis, was compared with the healthy skins of subjectsB–E The sensor was moved by hand over a prescribed re-gion of skin to maintain a constant speed and force Hence,
a method of identifying sample skins employing signalprocessing and neural network-based training was intro-duced First, the variance was calculated as an index toextract the features of the collected data:
Trang 40Table 3 Rate of Correct Answer for Discrimination of Atopic and Normal Skins
where, x( j) is the jth quantitized digital signal, ¯ x is the
average of x( j), and N is the total number of digital
signals
Next, FFT analysis was introduced to extract the
fea-tures of the collected data Careful reading of the spectra
obtained led to an understanding that there were some
dif-ferences in the distribution profiles of spectra among the
subjects In the light of this, the power spectrum was
seg-mented into several frequency ranges, and the ratio of the
power in an individual frequency range to the power of
the whole frequency range was calculated and used as the
second index that described the characters of the sample
skin:
(R s)i = (S) i /S, (S ) i=
i
i (S ) i , (3)
where P( f ) is the power spectrum density, S is the
to-tal power distributed across the frequency range
consid-ered, and (S ) i is the power at frequency level i Here, the
level i(=1–4) stands for the range of frequencies given in
Table 2
Discrimination of Skin that has Atopic Dermatitis The
neural network was trained to recognize atopic and
nor-mal healthy skins The neural network employed was
a hierarchical network; the training method used was
instructor-assisted training, in which the correct answers
were provided as an aid to the training; the training
algo-rithm employed was back-propagation Two networks were
examined One was the network that used the four power
ratios (R s)i , i = 1–4, as the cell input, and the other used
the variance V in addition to (R s)i Five sets of data were
ob-tained for each skin The neural network had an input
sen-sory layer of four or five cells, an intermediate association
layer that had the same number of cells as the input layer,
and an output response layer that had a single cell The
correct output value was set to one for the atopic skin, and
zero was set for the healthy skin Training was repeated
by using the gradient descent method until the error
func-tion became sufficiently small, up to 103 and 104 cycles
The networks were constructed separately three times for
three sets of randomly selected initial values of synaptic
weights After completing the training of 12 individual
net-works, the recognition experiments were performed on the
atopic skin and the healthy skin using the newly obtained
five sets of data for each subject The results obtained are
shown in Table 3 Here, the percentage denotes the rate
of the correct answer averaged across the three networks
of randomly selected initial synaptic weights Atopic matitis cannot be identified without the input of the vari-ance, and the recognition was perfect when the variancewas introduced as the input
3 C Trepanier et al., J Biomed Mater Res 48: 165 (1999).
4 K Tanaka, Tobuse, and S Miyazaki, Mechanical Properties of Shape Memory Alloys Yokendo, 1993.
5 K Otsuka and C.M Wayman, Shape Memory Materials.
Cambridge University Press, 1998.
6 Y Suzuki, Topics on Shape Memory Alloys Nikkan Kogyo
Shimbun, 1988.
7 Ishikawa, Kinashi, and Miwa, Collections of SMA tions Kogyo Chosakai, Tokyo, 1987.
Applica-8 H Ohnishi, Artif Organs 12: 862 (1983).
9 R Sachdeva and S Miyazaki, Proc MRS Int Meet Adv Mater.
Chonan Bio-Med Mater Eng 9: 97–112 (1999).
12 J.C Schuder, H.E Stephenson, Jr., and J.F Townsent, IRE
Internet Conv Rec Pt9–9: 119–126 (1961).
13 H Matsuki, M Shiiki, K Murakami et al., Flexible
transcu-taneous transformer for artificial heart system, IEEE Trans.
Magn 26: 1548–1550 (1990).
14 T Takagi, Y Luo, S Hara, T Yambe, S Amae, and M.W.H.
Nakamura J Soc Adv Sci (in press).
15 G Harsanyi, Sensing in Polymer Films in Sensor Applications,
Technomic, Lancaster, Basel, 1995, p 97.
16 G.M Shepherd, in Neurobiology 3e., Oxford University Press,
New York, Oxford, 1994, p 272.
17 S Chonan, Z.W Jiang, M Tanaka, T Kato, and M Kamei, Int.
J Appl Elect Mech 9: 25–38 (1998).
18 H Tagami, Fragrance J 10: 11–15 (1993).
19 T Yamamura, Measuring methods of skin surface water
con-tent, Fragrance J 10: 35–41 (1993).
20 M Takahashi, Fragrance J 10: 16–26 (1993).