SOLID SHAFTS 1 Stationary shafts with static loads The diameter of shaft subjected to simple torsion The diameter of shaft subjected to simple bending The diameter of shaft subjected to
Trang 1TABLE 12-15
Stress concentration factor,K
Stress concentration factor, K
Weld metal
Base metal
Stiffening ribs and partitions welded with end fillet welds having
Butt and T-welded corner plates, but with smooth transitions in the 1.5 1.9
shape of the plates and with machined welds
TABLE 12-16
Allowable stresses for welds under static loads
Allowable stresses Tension, Compression, Shear,
Automatic and hand welding with shielded arc and butt welding t a t 0.65 t
Trang 213
RIVETED JOINTS
A area of cross-section, m2(in2)
the cross-sectional area of rivet shank, m2(in2)
b breadth of cover plates (also with suffixes), m (in)
c distance from the centroid of the rivet group to the critical rivet,
m (in)
d diameter of rivet, m (in)
Di internal diameter of pressure vessel, m (mm)
eor l eccentricity of loading, m (in)
F force on plate or rivets (also with suffixes), kN (lbf)
h thickness of plate or shell, m (in)
hc, h1, h2 thickness of cover plate (butt strap), m (in)
i number of rivets in a pitch fine (also with suffixes 1 and 2,
respectively, for single shear and double shear rivets)
I moment of inertia, area, m4, cm4(in4)
J moment of inertia, polar, m4, cm4(in4)
K ¼ F
F0 coefficient (Table 13-11)
Mb bending moment, N m (lbf in)
p pitch on the gauge line or longitudinal pitch, m (in)
pc pitch along the caulking edge, m (in)
pd diagonal pitch, m (in)
pt transverse pitch, m (in)
Pf intensity of fluid pressure, MPa (psi)
Z section modulus of the angle section, m3, cm3(in3)
hoop stress in pressure vessel or normal stress in plate, MPa
(psi)
a allowable normal stress, MPa (psi)
c crushing stress in rivets, MPa (psi)
shear stress in rivet, MPa (psi)
a allowable shear stress, MPa (psi)
efficiency of the riveted joint
angle between a line drawn from the centroid of the rivet group
to the critical rivet and the horizontal (Fig 13-5)
Source: MACHINE DESIGN DATABOOK
Trang 3PRESSURE VESSELS
Thickness of main plates
The thickness of plate of the pressure vessel with
The rivet diameter
FIGURE 13-1 Pitch relation
2
p2
2s
d ¼ 6 ffiffiffih
p
to 6:3pffiffiffih
CM ð13-5cÞwhere h and d on mm
TABLE 13-1
Suggested types of joint
Diameter of shell, mm (in) Thickness of shell, mm (in) Type of joint
Trang 4TABLE 13-2
Minimum thickness of boiler plates
Diameter of shell, Minimum thickness after flanging, Diameter of tube sheet, Minimum thickness,
Allowable stresses in structural riveting (b)
Rivets acting in single shear Rivets acting in double shear Rivet-driving
Trang 5TABLE 13-5
Allowable stress for aluminum rivets,a
Allowable stressa, a
Values of working stressaat elevated temperatures
Minimum of the specified range of tensile strength of the material, MPa (kpsi) Maximum
Pitch of butt joints
Type of joint Diameter of rivets, d, mm Pitch, p
use for h 12:5 mm (0.5 in)
Trang 6Butt joint
The transverse pitch
For rivets, rivet holes, and strap thick
pt ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi0:5pd þ 0:25d2
q
ð13-6bÞRefer to Tables 13-9, 13-10, and Fig 13-2
Rivet hole diameters
Diameter of rivet, mm Rivet hole diameters, mm (min)
Trang 7Minimum transverse pitch as per ASME Boiler Code
For transverse pitches
Haven and Swett formula for permissible pitches
along the caulking edge of the outside cover plate
Diagonal pitch, pd, is calculated from the relation
MARGIN
Margin for longitudinal seams of all pressure vessels
and girth seams of power boiler having unsupported
heads
Margin for girth seams of power boilers having
supported heads and all unfired pressure vessels
pt¼ 1:75d þ 0:1ð p dÞ if p
d> 4 USCS ð13-8bÞwhere pt, d, and p in in
Refer to Table 13-8
pc d ¼ 14
ffiffiffiffiffiffi
h3 c
Pf
4
s
CM ð13-9aÞwhere pc, d, hcin cm, and Pf in kgf/cm2
pc d ¼ 21:38
ffiffiffiffiffiffi
h3 c
Pf 4
s
USCS ð13-9bÞwhere pc, d, hcin in, and Pf in psi
pc d ¼ 77:8
ffiffiffiffiffiffi
h3 c
Pf
4
s
SI ð13-9cÞwhere pc, d, hcin m, and Pf in N/m2
hc¼ 0:6h þ 0:0025 if h 0:038 m SI ð13-12aÞwhere hcand h in m
hc¼ 0:6h þ 0:1 if h 1:5 in USCS ð13-12bÞwhere hcand h in in
hc¼ 0:67h if h > 0:038 m SI ð13-12cÞwhere hcand h in m
hc¼ 0:67h if h > 1:5 in USCS ð13-12dÞwhere hcand h in in
13.6 CHAPTER THIRTEEN
RIVETED JOINTS
Trang 8Alcn 2I þ
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
Alcn 2I
2
þ 1 s
lp
p 2 þ 1 ðn 2 1Þp 2
2 s
lp
p 2 þ 1 ðn 2 1Þp 2
2 s
Key:
n ¼ total number of rivets in a column
F ¼ permissible load, acting with lever arm, l, kN (lbf)
Source: K Lingaiah and B R Narayana Iyengar, Machine Design Data Handbook ( fps Units), Engineering College Cooperative Society, Bangalore, India, 1962; K Lingaiah and B R Narayana Iyengar, Machine Design Data Handbook, Vol I (SI and Customary Metric Units), Suma Publishers, Bangalore, India, 1983; and K Lingaiah, Machine Design Data Handbook, Vol II (SI and Customary Metric Units), Suma Publishers, Bangalore, India, 1986.
RIVETED JOINTS 13.7
RIVETED JOINTS
Trang 9Thickness of the cover plate according to
Indian Boiler Code
Thickness of single-butt cover plate
Thickness of single-butt cover plate omitting alternate
rivet in the over rows
Thickness of double-butt cover plates of equal width
Thickness of double-butt cover plates of equal width
omitting alternate rivet in the outer rows
Thickness of the double-butt cover plates of unequal
width
For thickness of cover plates
The width of upper cover plate (narrow strap)
The width of lower cover plate (wide strap)
STRENGTH ANALYSIS OF TYPICAL
RIVETED JOINT (Fig 13-2)
The tensile strength of the solid plate
The tensile strength of the perforated strip along the
outer gauge line
The general expression for the resistance to shear of
all the rivets in one pitch length
The general expression for the resistance to crushing
of the rivets
The resistance against failure of the plate through the
second row and simultaneous shearing of the rivets in
the first row
The resistance against failure of the plate through the
second row and simultaneous crushing of the rivets in
the first row
The resistance against shearing of the rivets in the
outer row and simultaneous crushing of the rivets in
the two inner rows
h1¼ 0:625h for narrow strap ð13-17aÞ
h2¼ 0:750h for wide strap ð13-17bÞRefer to Table 13-10
Trang 10EFFICIENCY OF THE RIVETED JOINT
The efficiency of plate
The efficiency of rivet in general case
For efficiency of joints
The diameter of the rivet in general case
The pitch in general case
For pitch of joint
THE LENGTH OF THE SHANK OF RIVET
c
i2þ i1h2h
Trang 11FIGURE 13-4 Riveting of an angle to a gusset plate.
RIVETED BRACKET (Fig 13-5)
The resultant load on the farthest rivet whose distance
is c from the center of gravity of a group of rivets
MbcP
x2þPy2
2
þ 2
F
nn0
MbcP
x2þPy2
cos
#1=2ð13-33Þ
FIGURE 13-5 Riveted bracket (Bureau of Indian Standards.)
13.10 CHAPTER THIRTEEN
RIVETED JOINTS
Trang 12For rivet groups under eccentric loading value of
coefficient K
For preferred length and diameter of rivets
For collected formulas of riveted joints
5 Bureau of Indian Standards
6 Lingaiah, K., Machine Design Data Handbook, McGraw-Hill Publishing Company, New York, 1994
BIBLIOGRAPHY
Faires, V M., Design of Machine Elements, The Macmillan Company, New York, 1965
Norman, C A., E S Ault, and I F Zarobsky, Fundamentals of Machine Design, The Macmillan Company, NewYork, 1951
Vallance, A., and V L Doughtie, Design of Machine Members, McGraw-Hill Publishing Company, New York,1951
where
n ¼ number of rivets in one column
n0¼ number of rivets in one row
x, y have the meaning as shown in Fig 13-5Refer to Table 13-11
Refer to Figs 13-6 to 13-8 and Tables 13-12 to 13-13.Refer to Table 13-14
RIVETED JOINTS 13.11
RIVETED JOINTS
Trang 13FIGURE 13-6 Rivets for general purposes (less than 12 mm diameter) For preferred length and diameter combination, refer to Table 13-12.
FIGURE 13-7 Rivets for general purposes (12 to 48 mm diameter) For preferred length and diameter combination, refer to Table 13-13.
13.12 CHAPTER THIRTEEN
RIVETED JOINTS
Trang 14FIGURE 13-8 Boiler rivets (12 to 48 mm diameter) For preferred length and diameter combination, refer to Table 13-13.
RIVETED JOINTS 13.13
RIVETED JOINTS
Trang 2514
DESIGN OF SHAFTS
b width of keyway, m (in)
c machine cost, $/m ($/in) (US dollars)
D diameter of shaft (also with subscripts), m (in)
Di inside diameter of hollow shaft, m (in)
Do outside diameter of hollow shaft, m (in)
E modulus of elasticity, GPa (Mpsi)
F axial load (tensile or compressive), kN (lbf)
Fm0 the static equivalent of cyclic load, (¼ Fm Fa), kN (lbf)
G modulus of rigidity, GPa (Mpsi)
h depth of keyway, m (in)
k radius of gyration, m (in)
material cost (also with subscripts), $/kg
K ¼Di
Do
ratio of inner to outer diameter of hollow shaft
Kb numerical combined shock and fatigue factor to be applied to
computed bending moment
Kt numerical combined shock and fatigue factor to be applied to
computed twisting moment
Mb bending moment, N m (lbf in)
Mt twisting moment, N m (lbf in)
Mbm0 static equivalent of cyclic bending moment Mbm Mba,
specific weight of material, kN/m3(lbf/in)
stress (tensile or compressive) also with subscripts, MPa (psi)
shear stress (also with subscripts), MPa (psi)
ratio of maximum intensity of stress to the average value from
compressive stress only
angular deflection, deg
Source: MACHINE DESIGN DATABOOK
Trang 26Other factors in performance or in special aspect are included from time to time
in this chapter and, being applicable in their immediate context, are not given at
this stage
Note: and with the initial subscript s designates strength properties of
material used in the design which will be used and observed throughout this
handbook In some books on machine design and in this Machine Design
Data Handbook the ratios of design stresses sd=fd andsd=fd; and design
stresses yd,yd0,fd, andfd have been used instead ofsy=sf,sy=sf; and
yield strengths sy,sy and fatigue strengths,sf,sf in the design equations
for shafts [Eqs (14-1) to (14-65)] This has to be taken into consideration in
the design of shafts while using Eqs (14-1) to (14-65)
SOLID SHAFTS
(1) Stationary shafts with static loads
The diameter of shaft subjected to simple torsion
The diameter of shaft subjected to simple bending
The diameter of shaft subjected to combined
tor-sion and bending:
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
D ¼
16Mt
Trang 27The diameter of shaft subjected to axial load,
bending, and torsion:13
(a) According to maximum normal theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
(2) Rotating shafts with dynamic loads, taking
dynamic effect indirectly into consideration13
For empirical shafting formulas
The diameter of shaft subjected to simple torsion
The diameter of shaft subjected to simple bending
The diameter of shaft subjected to combined
bending and torsion
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
The diameter of shaft subjected to axial load,
bending, and torsion
(a) According to maximum normal stress theory
þ
(
MbþFD8
2
þ M2 t
2
þ M2 t
24
35
1=3ð14-7Þ
D ¼ 16yd
MbþFD8
35
1=3ð14-8Þ
Refer to Table 14-1
D ¼
16
ydfðKbMbÞ2þ ðKtMtÞ2g1=21=3
ð14-12Þ
D ¼
16
DESIGN OF SHAFTS 14.3
DESIGN OF SHAFTS
Trang 28(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
The diameter of shaft based on torsional rigidity
(3) Rotating shafts and fluctuating loads, taking
fatigue effect directly into consideration13
The diameter of shaft subjected to fluctuating
torsion
The diameter of shaft subjected to fluctuating
bending
The diameter of shaft subjected to combined
fluc-tuating torsion and bending:
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
ydfM0bmþ ðM02
bmþ M02
tmÞ1=2g
1=3ð14-20Þ
D ¼
16
Trang 29The diameter of shaft subjected to combined
fluctuating axial load, bending, and torsion
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
HOLLOW SHAFTS
(1) Stationary shafts with static loads
The outside diameter of shaft subjected to simple
torsion
The outside diameter of shaft subjected to simple
bending
The diameter of shaft subjected to combined
tor-sion and bending
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
D ¼
(16
and Fm0 ¼ Fmþsd
Do¼
16Mt
Trang 30The outside diameter of shaft subjected to axial
load, bending, and torsion
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
(2) Rotating shafts with dynamic loads, taking
dynamic effect indirectly into consideration13
The outside diameter of shaft subjected to simple
torsion
The outside diameter of shaft subjected to simple
bending
The outside diameter of shaft subjected to
com-bined bending and torsion
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
Do¼
(16
1=2!)1=3
ð14-31Þ
Do¼
(16
#1=2)1=3
ð14-32Þ
Do¼
(16
Trang 31(c) According to maximum shear energy theory
The outside diameter of shaft subjected to axial
load, bending and torsion
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
The outside diameter of shaft based on torsional
rigidity
(3) Rotating shaft with fluctuating loads, taking
fatigue effect directly into consideration
The outside diameter of shaft subjected to
Please note: If the axial load does not produce column
action, the constant need not be used to multiply the
term [FDo (1 þ K 2 )/8] throughout this chapter.
DESIGN OF SHAFTS 14.7
DESIGN OF SHAFTS
Trang 32The outside diameter of shaft subjected to
com-bined fluctuating torsion and bending
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
The outside diameter of shaft subjected to
com-bined fluctuating axial load, bending, and torsion
(a) According to maximum normal stress theory
(b) According to maximum shear stress theory
(c) According to maximum shear energy theory
Do¼
16
1=2)#1=3
ð14-48Þ
Do¼
(16
#1=2!)1=3
ð14-49Þ
Do¼
(16
where Mbm0 , M0tm, and Fm0 have the same meaning as
in Eqs (14-22a), (14-22b), and (14-25a)
14.8 CHAPTER FOURTEEN
DESIGN OF SHAFTS
Trang 33COMPARISON BETWEEN DIAMETERS OF
SOLID AND HOLLOW SHAFTS OF SAME
LENGTH
For equal strength in bending, torsion, and/or
com-bined bending and torsion, the diameter
(a) When materials of both shafts are same
(b) When materials of shafts are different
For torsional rigidity
(a) When torsional rigidities are equal
(b) When torsional rigidities are different
For equal weight
(a) When material of both shafts is same
(b) When materials of both shafts are different
For equal cost
(a) For same material and machining cost for both
shafts
(b) For no machining cost for both shafts but with
different material cost
(c) When machining costs are different and material
Note: If the axial load does not produce column action, the
constant need not be used to multiply the term
[FDo (1 þ K 2 )/8] throughout this chapter
DESIGN OF SHAFTS 14.9
DESIGN OF SHAFTS
Trang 34Instead of computing the transverse deflection, the
maximum distance between the bearings (in meters)
may be computed by the empirical formula to limit
the transverse deflection to 0.8 mm/m of length
RIGIDITY
Moor’s formula for the increase of the angle of twist
due to the keyway and applies only to the keyseated
length of shaft
EFFECT OF KEYWAYS
The lowering of the strength of shaft by keyways may
be taken into account by introducing a factor similar
to a stress-concentration factor (or Moor’s formula
for lowering the strength of shaft)
THE BUCKLING FACTOR
For short columns or when l=k 115
For long columns or when l=k 115 (Euler’s formula)
SHAFTS SUBJECTED TO VARIOUS
STRESSES
(1) Shaft subjected to steady torque and reversed
bending moment taking into consideration stress
ð14-65Þwhere
n ¼ 1 for hinged ends
¼ 2:25 for fixed ends
¼ 1:6 for both ends pinned or guided and partlyrestrained
( ¼ 1 for tensile load)
14.10 CHAPTER FOURTEEN
DESIGN OF SHAFTS
Trang 35Diameter of solid shaft:
(a) According to maximum shear stress failure
theory using Soderberg [4] criterion for
(b) According to maximum shear stress theory of
failure using modified Goodman criterion for
Diameter of hollow shaft:
(c) According to distortion-energy theory of
failure using modified Goodman criterion
for fatigue strength
(d) According to distortion-energy theory of
failure combined with Gerber parabolic
(e) According to distortion-energy theory of
failure using ASME elliptic locus for fatigue
and yielding criterion (Langer) equation
com-bined with any theories of failure can be used to
predict the fatigue strength of shaft
Kf ¼ fatigue stress-concentration factor due tobending, tension, or compression
Kfr¼ fatigue stress-concentration factor due totorsion
Kf ¼ Kf ¼ 1 for ductile material under steadystate of stress
DESIGN OF SHAFTS 14.11
DESIGN OF SHAFTS
Trang 36(2) Shaft subjected to fluctuating loads, i.e., reversed
bending and reversed torque, taking into
consid-eration stress concentration
(a) The diameter of solid shaft according to
max-imum shear stress theory of failure using
Soderberg criterion for fatigue strength
(b) The diameter of hollow shaft according to
distortion-energy theory of failure combined
with Soderberg criterion for fatigue strength
(3) Shaft subjected to constant bending and torsional
moments and reversed torsional and bending
moments at the same frequency taking into
con-sideration stress concentration
(a) The diameter of solid shaft according to
max-imum distortion energy theory of failure using
modified Goodman criterion for fatigue
strength
(b) The diameter of solid shaft according to
max-imum shear stress theory of failure combined
with modified Goodman criterion for fatigue
strength
(c) The diameter of hollow shaft according to
maximum shear stress theory of failure using
Soderberg criterion for fatigue strength
D ¼
32n
Mbe¼ static equivalent of cyclic bending moment
syð1 K4Þð4Mbe2 þ 3M2
teÞ1=21=3
ð14-72Þwhere Mbeand Mtehave the same meaning as givenunder Eq (14-71)
D ¼
16n
D ¼
32n
14.12 CHAPTER FOURTEEN
DESIGN OF SHAFTS
Trang 37(4) Cyclic axial load combined with reversed bending
and torsional moments taking into consideration
stress concentration as per ASME Code for
Design of Transmission Shafting
(a) The diameter of solid shaft according to
maximum shear stress theory of failure and
Soderberg relation for fatigue strength
(b) The diameter of hollow shaft according to
distortion-energy theory of failure combined
with modified Goodman relation for fatigue
strength
(5) The diameter of solid shaft subjected to axial,
bending, and torsional alternating loads
accord-ing to distortion-energy theory of failure
com-bined with Soderberg relation for fatigue as per
ASME Code for Design of Transmission Shafting5
D ¼ 32nsy
MbeþFaeD8
2
þ M2 te
1=2
ð14-76Þwhere Mbeand Mtehave the same meaning as givenunder Eq (14-71)
Fae¼ static equivalent axial load
a solid shaftThe value of is given by Eq (14-65)
D ¼ 32nsf
MbaþFaD2
2
þ3Mta24
1=2
þ
(32n
1=2)!1=3
ð14-78ÞNot explicit in D, use iterative methods to solve
Although ASME has withdrawn the ASME Code for Design
of Transmission Shafting, some of the ASME equations given
here have historic interest and hence are retained in this
book.
DESIGN OF SHAFTS 14.13
DESIGN OF SHAFTS
Trang 38(6) The diameter of shaft made of brittle material,
which is subjected to reversed bending and
tor-sional moments taking into consideration stress
concentration as per maximum normal stress
theory of failure combined with modified
Good-man relation for fatigue strength
(7) Shaft subjected to combined axial, bending, and
torsional reversed loads taking into consideration
stress concentration and shock
(a) The diameter of hollow shaft according to
distortion-energy theory of failure using
Soderberg relation
The symbols used in Eqs (14-80) to (14-85) and Figs
14-1 and 14-2 are different than that of the ANSI/
ASME standard B106 IM-1985 in order to remain
consistent with the symbols used in this Handbook
New ASME Code for design of transmission
shafting:
The diameter of shaft subjected to fully reversed
bending i.e., zero mean bending component and
torsional fluctuating loads, i.e alternating loads
taking into consideration stress concentration
according to distortion energy theory of failure
combined with modified Goodman relation for
fati-gue as per new ANSI/ASME code for transmission
shafting
The factor of safety, n
D ¼
16n
Do¼
16n
sutð1 K4Þ½Mbe0 þ ðMbe02þ M02teÞ1=2
1=3
ð14-80Þfor hollow shaft, where Mbe0 and Mte0 have the samemeaning as given under Eq (14-77)
14.14 CHAPTER FOURTEEN
DESIGN OF SHAFTS
Trang 39The diameter of shaft made of brittle material
sub-jected to reversed bending and torsional moments
taking into consideration stress concentration as per
maximum normal stress theory of failure combined
with modified Goodman relation for fatigue strength
For combined fatigue test data for reversed bending
combined torsion and combined with reversed torsion
on steel specimens
D ¼
16n
FIGURE 14-1 Results of fatigue Tests of steel specimens subjected to Reversed Bending and Torsion.
Source: Design of Transmission Shafting, American Society for Mechanical Engineers, New York, ANSI/ASME standard
Trang 40See Tables 14-1 to 14-6 and Fig 14-2 for further
details on shafting design;3 refer to Table 14-4 for
shock load factors Ksband Kst
For further design details on shafting Refer to Tables 14-5 to 14-7
25 (0•416) 20 (0•333) 16 (0•266) 12•5(0•208) 6•3 5
10 (0•166)
FIGURE 14-2 Nomogram for determining diameter (d), speed (n), force (F), torque (Mt ), and power (P) in Customary Metric units and System International units (K Lingaiah, Machine Design Data Handbook, Vol II, Suma Publishers, Bangalore, India, 1986.)
14.16 CHAPTER FOURTEEN
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TSDESIGN OF SHAFTS