The insert’s substrate – if cemented carbide – re-quires some thought, as if it is too hard, this type of insert may chip via the effects of machining vibrations, this is particularly so
Trang 1The insert’s substrate – if cemented carbide –
re-quires some thought, as if it is too hard, this type of
insert may chip via the effects of machining vibrations,
this is particularly so, if the tool geometry has an
ex-tra-positive and sharp insert cutting edge It might be
more prudent to initially choose a medium-hard
ce-mented carbide grade, as it tends to cope with a
poten-tial edge-chipping condition more readily, then, if this proves successful, a harder grade may be selected
Cutting Parameters – Decisions
Two complementary cutting parameters are the insert’s nose radius and the influence it has on the DOC For
Figure 62 Interchangeable cutting heads for machining internal features [Courtesy of Sandvik Coromant]
.
Trang 2example, when a finish boring operation is required,
then it is recommended that both a small nose radius
and DOC is used This smaller boring insert nose
ra-dius, minimises contact between the workpiece and
insert, resulting in lower tangential and radial cutting
forces For fine-boring applications, a good start point
is to choose an insert with a 0.4 mm nose radius, with
a 0.5 mm DOC It should be noted that the DOC ought to
be larger than the nose radius, this is because if it was
the other way around, cutting forces would be directed
in a radial direction – increasing potential vibrational/
bar-bending (i.e push-off ) problems
Feedrates should be identical regardless of tool’s
overhang, as any feed selection is normally based upon
the insert’s chip-breaking capabilities Avoidance of
very high feedrates when rough boring is necessary, as
it can significantly increase the tangential cutting force
component For finish boring operations, it is normally
the workpiece’s surface texture requirement that
dic-tates the maximum feedrate that can be utilised More
will be mentioned on the machined cusp height’s effect
on surface texture, this being created by the remnants
of the partial nose arc (i.e radius) of the cutting insert
and the periodic nature of the selected feedrate on the
bored workpiece’s surface, later on in the relevant
sec-tion in the book
A mistake often made by setters/machinists in
order to attempt to minimise vibrational tendencies, is
to reduce the rpm This strategy will not only decrease
productivity, but the lower rotational speed can lead
to BUE formation, which in turn, modifies the insert’s
cutting geometry and could change the cutting force
directions Instead of rpm reductions, modification
of other cutting data variables is suggested, in order
to improve these adverse vibrational/chatter effects
Sometimes even increasing the rotational speed, can
eliminate unwanted chatter
Although it is not a specific cutting performance
parameter, an often disregarded measure is that of
boring bar tool clamping In many circumstances,
cy-lindrical boring bars are simply clamped with several
setscrews, this is a poor choice of clamping method, as
at best, setscrews only contact about 10% of the boring
bar Conversely, a split-tool block, clamps along almost
‘Tool push-off’ – often termed ‘spring-cuts’ , are the result of
tool deflection, particularly when light cuts are used To
mini-mise the ‘push-off’ , very rigid workpiece-machine-tool setup
with a smaller nose radius to that of the D is recommended.
all of the boring bar’s periphery in the toolpost, allow-ing much greater tool rigidity and cuttallow-ing stability, al-leviating many of the potential problematic in-service machining conditions
3.2.3 Multiple-Boring Tools
Twin cutting insert tooling, usually consists of a cy-lindrical shank with slides mounted at the front (Fig 63a), or a U-shaped bar with cartridges (Fig 63b) The slides and cartridges can be radially adjusted, allow-ing for a range of various bored diameters to be ma-chined Normally, such tooling has a 7 mm maximum cutting depth recommended – for both edges simul-taneously in-cut With Twin-edged boring tools the
cartridges can be so arranged, that ‘Step-boring’ can
be utilised
When large diameter component features require
a boring operation, then the ‘Divided-version boring’
tooling can be exploited, but diametral accuracy is not
as good as for some of the other types of boring tool designs An advantage of the Divided-version’ boring tools, is the fact that a large diameter range can be
cov-ered, with this single tool If a ‘Universal fine-boring’
tool is utilised (Fig 63b), either internal (Fig 63b-top),
or external machining (Fig 63b – bottom), can be un-dertaken In this case, the fine-bore cartridges (1) are mounted on a radially-moveable slide (2), which is mounted on a bar (3) In the latter case of external com-ponent feature boring, there is a physical limit to the minimum diameter that can be machined – this being controlled by the bar’s actual size (i.e Here, it should be said that this particular tooling ‘setup’ can be thought
of as virtually a Trepanning operation with a boring tool) Moreover, with this external finishing operation,
the spindle must rotate in a left-hand rotation
Tri-bore tooling often having individual micro-bore
cartridge adjustment (i.e not shown), as its name im-plies, uses three cutting inserts equally-spaced at 120° apart This boring tool arrangement of cutting inserts, offers very high quality bored diametral accuracy and
‘Step-boring’ , refers to using special shims with one of the
cutting inserts axially situated a little way in front of the other, while at the same time, the cartridges are radially adjusted en-abling the front insert to cut a slightly smaller diameter to that
of the rear one It should be noted that when ‘Step-boring’ , the maximum DOC is normally 14 mm, with an associated feedrate
of 0.2 mm rev–.
Trang 3Figure 63 Twin-edged boring tooling [Courtesy of Sandvik Coromant]
.
Trang 4precision to the machined hole, but such tooling can
be somewhat more costly than when utilising a
single-insert tool
3.2.4 Boring Bar Damping
For boring bars that have an L/D ratio of <5:1, then
relatively stable cutting conditions with controllable
vibrational influences can be tolerated However, if L/D
ratios utilised are larger than this limiting value, then
potentially disastrous vibrational tendencies could
oc-cur, leading to a variety of unwanted machining and
workpiece characteristics, these include:
• Limited tool life – caused by forced and self-excited
vibrations, restricting both cutting efficiency and
tool life,
• Unacceptable machined surface texture –
vibra-tions in the form of workpiece surface chatter, can
be the cause for component rejection,
• Substandard machined roundness – vibration/
chatter effects creating high-frequency harmonic
effects on the roundness profile
Stiffness can be expressed in terms of either static, or
dynamic stiffness Static stiffness of a bar is its ability to
resist a bending force in a static condition, conversely,
dynamic stiffness is the bar’s ability to withstand
os-cillating forces (i.e vibrations) Dynamic stiffness is an
essential property for a boring bar, as it is a measure of
its capacity to dampen the vibrations occurring during
machining, being greatly dependent of its overhang As
one would expect in testing for dynamic stiffness, with
‘Harmonics’ – on a machined component are the product
of complex interactions, including method of manufacture:
component geometry, cutting data utilised, any vibrational
influences encountered and material composition and its
manufacture (e.g Powder Metallurgy parts can vary in both
porosity and density throughout the part, which may affect, or
locally destabilised the cutting edge).
NB Harmonics on the machined workpiece, can be thought
of as a uniform waveform (i.e sinewave) that is
superim-posed onto the part’s surface The part’s low frequency
harmo-nicoften has higher frequency harmonics superimposed onto
the roundness For example, a 15 undulation per revolution
(upr) harmonic, could have a 500 upr harmonic superimposed
onto it, requiring suitable a Roundness Testing Machine with
Gaussian filters to separate out the respective harmonic
con-ditions – for metrological inspection and further analysis.
a boring bar’s overhang increasing under standardised machining conditions, the amplitude will also increase However, if the boring bar was dampened in some way, perhaps by utilising a ‘shock-absorber effect’ , ma-chining could be undertaken at longer overhangs This
‘damping effect’ is indicated by the highly centralised amplitude of oscillatory movements quickly reducing with time, indicating a high level of dynamic stiffness, this being crucial for long L/D ratios Obviously, the boring bar’s cutting edge deflection at its tool tip, is directly related to the amount of bar overhang, this de-flection being the result of the applied cutting forces The magnitude of a boring bar’s deflection being de-pendent upon: bar composition, diameter, overhang and the extent and magnitude of tangential and radial cutting forces The rigidly clamped and cantilevered boring bar’s ‘free-end’ will deflect/deform by forces acting upon it and, some idea of the magnitude of this deflection can be gleaned by the simple application of
‘mechanics of materials’ , using the following formula:
Where:
∆ = Boring bar deflection (mm),
F = Cutting force (N),
L = Boring bar overhang (mm),
E = Bar material’s coefficient of elasticity (N mm–),
*I = Moment of Inertia (mm)
* For a boring bar of circular cross-section, the Mo-ment of inertia will be:
For example, assuming that if a φ25 mm steel boring bar has an L/D overhang of 4:1, with an applied cut-ting force of 100 kP, then the magnitude of bar deflec-tion, using the above formula, would be:
∆L = D = 0.083 mm
If the overhang of this boring bar was now increased
to L/D ratios of 7:1 and 10:1, respectively, this would produce tool tip deflections of:
∆L = D = 0.444 mm
∆L = 0D = 1.293 mm
Hence, these deflection values emphasise the impor-tance of reducing overhang as it increases by approxi-mately ‘cube’ of the distance Moreover, deflection can
Trang 5also be reduced by utilising a different boring bar
ma-terial, as this will improve its coefficient of elasticity
In boring-out roughing operations, any vibrations
present are only a problem if they lead to insert
dam-age For finish-boring operations, vibrational
condi-tions that may occur could be the difference between
success and failure for the finished machined part
So, the boring bar’s ability to dampen any vibrational
source becomes imperative, once a fine-boring
opera-tion is necessary Vibraopera-tions can occur in any number
of ways that could affect the boring operation, from
the constructional elements of the machine tool,
through to slideways, or their recirculating ball
bear-ings, etc Hence, the joints in a machine tool can be
regarded as a complicated dynamic system, with any
slideway motion of vibrating contact faces,
necessitat-ing lubricatnecessitat-ing oil to not only reduce any stiction and
frictional effects, but to help dampen these structural
elements Machine tool builders are acutely aware that
certain machine tool materials ‘damp’ more readily
than others Cast iron and in particular ‘Granitan’ (i.e
a product of crushed granite and epoxy resin), can
pre-dominantly act as built-in dampening media for any
vibrational sources present The main source for any
vibrations in boring, results from the long overhangs,
necessary to machine the hole depth of the
compo-nent’s feature Therefore, the magnitude of vibrations
in the overall system result from the dampening
capa-bilities of the actual boring bar
Tuned Boring Bars
A boring bar that has been ‘tuned’ , has the ability to
dampen any generated vibrations between the
work-piece and the cutting edge while machining The
‘dampening effect’ is achieved through a vibration
ab-sorbing device (i.e see Figs 61a and 62b), this has the
consequence of increasing the bar’s dynamic stiffness,
giving it the ability to withstand oscillating forces The
Coefficient of elasticity, for a steel boring bar composition,
E = 21 × 10 (N mm–), conversely, using a cemented carbide
material for an identical boring bar, E = 63 × 10 (N mm–),
giv-ing three times greater stiffness, allowgiv-ing much greater borgiv-ing
bar overhangs.
NB In reality, the boring bar’s deflection will be higher than
the values given in these examples, as the formula is based
upon the assumption that the bar is absolutely rigidly clamped,
which is impossible to achieve.
method of achieving this bar damping has already been mentioned in Section 3.2.1, with the relationships be-tween the size of the bar’s body, suspension, viscosity
of the liquid media, being carefully designed by the tooling manufacturer During the boring operation, the vibrations set the body in oscillation Hence, the body and the liquid alternate, taking each others place
in the space within the actual boring bar A pattern is established during boring, where the oscillations of the body are not in harmony with the vibrations resulting from machining This out-of-harmony, means that the
vibrations are virtually neutralised – to an acceptable
level – via the kinetic energy being transformed by the
‘system damping’ Any vibrations present during bor-ing, are relative to the amount of bar overhang, there-fore on longer boring bar lengths, they are normally fitted with some means of adjustment, so that they can
be ‘tuned’ to the frequency occurring within its range The simplest manner of achieving adjustment, is by
a rotation of a lockable set screw, which when either tightened, or slackened, affects the suspension of the body in the liquid, thus ‘tuning’ the boring bar to the actual machining conditions present
3.2.5 ‘Active-suppression’
of Vibrations
As has been stated at the beginning of Section 3.2.4, if boring bars have an L/D ratio >5:1, then vibrational ef-fects may result in tool chatter It has been observed in experimental work, that the boring bar’s tip produces
a vibration motion that follows an elliptical path in the plane normal to the longitudinal axis of the bar The ratio of the amplitude of vibration along the major and minor axes varies with cutting conditions, further-more, the inclination of these axes to the ‘radial line’
of the tool also varies Of significance, is the fact that the build-up of chatter will begin almost immediately, even before one revolution of the workpiece has oc-curred This build-up continues almost evenly until some limiting amplitude occurs, which suggests that the well-known ‘Orthogonal mode coupling’ is pres-ent, further, with the phase difference between the vi-brations causing an elliptical tool tip path, the vibra-tional energy is fed into the tool-workpiece system, promoting self-excitation
As has been suggested, the dynamic stability of the boring bar is of prime importance, with the onset of self-excited chatter, being governed by the ‘Multiple regenerative effect’ , which is a function of the so-called
Trang 6‘space phase’ This ‘space phase’ condition, is the phase
of vibration around respective turns of work,
fluctu-ating between 90° and 180° and is equal to the phase
between the inner and outer modulation Moreover,
it has been shown that by modifying the workpiece’s
rotational speed, this disturbs the ‘space phase’ and,
consequently influences the ‘time phase’ , leading to
a reduction in self-excited chatter It has been
practi-cally demonstrated that by modifying the peripheral
speed of the workpiece, this technique is only partially
successful in alleviating chatter More success can be
made by utilising damped boring bars, such as the
‘Lanchester’ type, with dynamic vibration absorbers
(DVA’s), to really suppress vibrational influences
dur-ing the bordur-ing process
Some progress has been made on the development
of DVA techniques, but the potential ‘step-change’
will occur in vibrational suppression for boring bars,
when the improvement of production versions of
‘ac-tive’ dampers for such tooling becomes a reality Just
such a potential ‘active’ boring bar is shown
schemati-cally in Fig 64 Invariably, the boring bar has a supply
of energy to it – via an external source, that controls
the cutting edge’s position by monitoring the feedback
of the relative displacement of tool’s edge with respect
to the workpiece In later research work by Matsubara
et al (1987), chatter suppression was analysed for the
boring bar using ‘feed-forward’ control of the cutting
force Further, the cutting edge was positioned in
re-sponse to this force, with these type of ‘active’ control
systems being known as: ‘Cutting edge positional
con-trol systems’
Typical of a vibrational control approach is
illus-trated by the ‘active’ boring bar already mentioned and
depicted in Fig 64, where the forces are damped in
re-sponse to the vibrational velocity of the cutting edge,
which has been termed a: ‘Vibrational velocity control
system’ In this damping technique, the boring bar
sup-pression is by a series of piezo-electric elements that
act as ‘active dampers’ Such a ‘damper’ responds to
onset of chatter vibration (i.e the high-energy
com-ponents) Moreover, the damping force achieves
opti-mal phase difference, since the phases between both
‘Lanchester boring bars’ , normally utilise an internal metal
slug which is usually surrounded by some form of: liquid/fluid
medium, DVA’s, or more primitively, sprung-loaded and as
such, the slug is free to move out-of-phase with the cutting
conditions, dictated by the boring bar’s applied cutting forces,
thereby the onset of chatter will be potentially ‘cancelled out’.
the ‘damping’ and vibrational forces are controllable This type of ‘active’ boring bar arrangement, achieves directional damping characteristics via its ‘dampers’ ,
here they control two ‘degrees of freedom’ via the ‘Re-generative feedback loop’ , which diminishes oscillatory
motion (i.e harmonics), by careful control of energy losses
In recent years with the advent of artificial intelli-gence (AI) applications to major industrial engineering problems, and more specifically, in the performance
and robustness of certain types of ‘Neural networks’ ,
the goal of obtaining some form of real-time monitor-ing and control in the machinmonitor-ing process is now closer
to reality These AI systems have been successfully utilised for applied research applications to tool wear monitoring in turning tool operations – after suitable
‘training’ of a pre-selected neural network architecture These ‘networks’ could be successfully applied to bor-ing bar vibrational monitorbor-ing and control situations More detailed information will be said on how, where and when Neural network decision-making and, why these cutting tool monitoring applications should be utilised in the production environment, later in the text
3.2.6 Hard-part Machining,
Using Boring Bars
Although ‘hard-part’ turning has been utilised for some considerable time, with the advent of polycrys-talline cubic boron nitride (PCBN) tooling, etc., it has seen little in the way of exploitation for boring opera-tions, to date One of the major reasons for this lack
of tooling application, is because most hardened parts are in the region of hardness values ranging from 42
to 66 HRC Such high component hardness, requires considerable shearing capability by the tooling to suc-cessfully machine the excess stock from the workpiece Generally, the robust nature of toolholding for turning
‘Degrees of Freedom’ , the ‘free-body kinematics’ , exhibit 6
de-grees of translatory (i.e linear) motions in space, these are: back-ward/forward, upward/downward and leftward/rightward.
NB Of some interest but in the main, to machine tool
build-ers for the purposes of volumetric calibration, are the rotary motions of: yaw, pitch and roll, giving 18 degrees of freedom, together with the 3 squareness errors, totalling 21 possible de-grees of freedom.
Trang 7Figure 64 An ‘active’ boring bar and their capacity to suppress vibrational effects on boring holes [After
Mat-subara; Yamamoto and Mizumoto; 1987]
.
Trang 8tools with their modest overhangs, does not present
in-surmountable difficulties during machining, however
for the much longer overhangs associated with boring
operations (i.e see Figs 62a and 65a), then the cutting
forces generally dictate, short L/D ratios of <5:1 and
relatively large and robust boring bars (Fig 65b)
There are considerable difficulties to be
over-come when any form of hard-part machining is
required – particularly for boring operations, when
the components have been either case- or
through-hardened, these are:
• High temperatures in the cutting zone –
necessitat-ing high temperature resistant and
thermally-sta-bility of cutting insert materials,
• Cutting force magnitudes are both higher and more
variable – robust cutting edge geometry is
neces-sary to withstand these increased shearing/cutting
force demands on the insert,
• Small chip cross sections – these exert high
pres-sure near the insert’s cutting edge, often necessitat-ing an edge preparation to the insert’s corner,
• Greater tool wear rates – often more rapid cutting
edge wear, or the tendency to catastrophic break-down of the insert,
• Workpiece stresses during cutting – these stresses
are released during machining and may present localised geometric variations to the final shape of the part,
• Poor homogeneity in the workpiece material
– hardness variations across and through the part (e.g differential case hardened depths), can lead to significant and variable cutting force loadings on the boring insert,
• Insufficient stability – if the
‘machine-tool-work-piece loop’ is not sufficiently robust, then due to the greater cutting forces when hard-part machining,
Figure 65 Boring bar operational limitations and hard part boring at relatively high speed
[Cour-tesy of Sandvik Coromant]
.
Trang 9this creates potential tool deflection which could
become a major problem
Boring Bar Deflection
When any boring operations take place, even with a
very rigid tool mounting and a small boring bar
over-hang, some vibration and tool tip deflection will
in-evitably occur, this is exacerbated by machining
hard-parts The former problem of vibration has previously
been mentioned and methods of minimising it are
possible However, tool deflections are more difficult,
if not impossible to completely eliminate, with these
longer cantilevered tools Of note regarding
overhang-ing tool deflections, are that a tool tip deflects in two
directions (i.e see Fig 66a), these are:
• Radial deflection (∆T) – affects the machined (i.e
bored) diameter,
• Tangential deflection (∆R) – causes the tip to move
downward for the centreline
In each of these tool tip deflections, both the size and
direction of the cutting forces are influenced by the
chip thickness and insert geometry selected (i.e
illus-trated in Fig 66b) The radial deflection will be equal
to the difference between the diameter which was
orig-inally set and the actual bored diameter, this can be
easily found by the simple expedient of measuring it,
then adjustment can be made for this apparent
deflec-tion The tangential deflection of the boring bar’s tip
can be established by either ‘direct’ , or ‘indirect’
met-rological techniques at the tool’s tip In Fig 66a, the
graph depicts deflections ‘∆’ (i.e both the tangential
‘∆T’ and radial deflection ‘∆R’), as a function of the cutting depth ‘aP’ Due to the fact that the tangential deflection (∆T) linearly increases with increasing DOC
(aP), it is usually recommended that machining passes are divided into a number of cuts when close toler-ances are needed (i.e in the region of IT7) – see Table
549 for an abridged version of the IT tolerances, with
*Rmax values in µm
The magnitude of radial deflection as a function
of the cutting depth, is also influenced by the ratio between the insert’s nose radius and the DOC (aP), to-gether with the boring insert’s entering angle In some
cases, a boring bar is situated slightly above the
work-piece centreline, so that when it enters the cut at full depth it will have tangentially-deflected to the actual
‘IT’ (i.e in units of µm) – represents the average value of the
basic tolerance for the ‘diameter range’ in question Hence, it will vary according to the choice of diameter range selected.
These values are related to surface texture expression of:
*Rmax (µm), which is: The maximum individual peak-to-val-ley height The Rmax values (i.e in Table 5) can be calculated
from the IT value, using the following equation, rather than
the conventional equation: Rmax = (fn/rε ) 125
this equation tends to give excessively high surface texture va-lues, thus more practical values related to IT are to be found
from:
�Rmax= �n � IT IT (µm)
Where: n = The number of IT’s.
Table 5: IT values related to the basic tolerance for various diameter ranges
-/3 Over/up to 3/10 Over/up to 10/50 Over/up to 50/180 Over/up to 180/400 Over/up to 400/800
[Source: Sandvik Coromant (1995)]
.