Machine Design i Ch5
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Transcript of Machine Design i Ch5
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Machine Design I (254325)Chapter 5
Screws, Fasteners, and the
Design of Nonpermanent
Joints
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Introduction
Archimedes screw
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Introduction
Boeings 747
2.5
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Thread Standards and Definitions
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Thread Standards and Definitions
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Thread Standards and Definitions
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The Mechanics of Power Screws
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The Mechanics of Power Screws
==
=+=
=+=
==
0cossin
0cossin
loadtheloweringfor
0cossin
0cossinloadtheraisingfor
NfNFF
fNNPF
NfNFF
fNNPF
V
LH
V
RH
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The Mechanics of Power Screws
( )
( )
[ ]
[ ]
2
and2
2/
)/(1
)/(
and)/(1
)/(
/tan
sincos
sincos
andsincos
cossin
+
=
+
=
=
+=
+=
=+
=
+=
fld
lfdFdT
fld
fdlFd
T
PdT
dfl
dlfFP
dfl
fdlFP
dl
f
fFP
f
fFP
m
mmL
m
mm
R
m
m
mL
m
mR
m
L
R
RR
m
L
TFlTTe
FlT
ff
lfd
T
2//
2/
0iftan
0locking,-self
0
0
==
=
=
>
>
>
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The Mechanics of Power Screws
CEk
lSS
A
F
d
F
A
F
d
T
dFfT
f
fld
fdlFdT
y
y
crit
r
r
ccc
c
m
mmR
1
2
buckling)JohnsonB.(J.columnshort
4
stressaxial
16
stressshearnominalmaximum
2
frictioncollaroftcoefficientheis
sec
sec
2
adsother threorAcmefor
2
2
3
=
==
=
=
+=
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The Mechanics of Power Screws
( )( )
pnd
F
pnd
F
A
V
pnd
F
pnd
Fp
cI
M
FpM
pndpndCI
n
pndF
pndF
trtr
trtr
trtr
t
tmtm
3
2/2
3
2
3
stressshearetransversthe
624
4/
4/
2462/
rootat thestressbendingthe
threadsengagedofnumbertheis
22/
stressbearingthestresses,threadnominal
2b
2
2
b
B
B
===
===
=
==
==
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The Mechanics of Power Screws
04
160
06
roottheoftopat thestressMisesvon
2z
3y
x
==
==
==
zx
r
r
yz
xy
tr
dF
d
T
pndF
power screw
compression tension
10.38 20.25 30.18 7 F0.38F, nt= 1
stress
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The Mechanics of Power Screws
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The Mechanics of Power Screws
8-1
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Threaded Fasteners
(Hexagon-head bolt)
>+
+=
in6L2
1
2
in6L4
12
boltsseriesinch-
lengththreadthe
ind
ind
L
L
T
T
27ATablesee*
200L252
200L125122
48d125L62
boltsmetric-
>+
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Threaded Fasteners
(cap-screw heads)
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Threaded Fasteners
(machine screws, nut)
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Threaded Fasteners
(machine screws, nut)
Inch-series machine screws are generally available
in sizes from No. 0 to about 3/8 in.
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Threaded Fasteners
(machine screws, nut)
Hexagonal nut dimensions are given in Table A31.
During tightening, the first thread of the nut tends to take the
entire load; but yielding occurs, with some strengthening dueto the cold work that takes place, and the load is eventuallydivided over about three nut threads. For this reason youshould never reuse nuts; in fact, it can be dangerous to do so.
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JointsFastener Stiffness
Bolt
preload compression
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JointsFastener Stiffness
At = tensile-stress area (Tables 81,82)
lt = length of threaded portion of grip Ad= major-diameter area of fastener ld= length of unthreaded portion in
grip kb = estimated effective stiffness
dttd
tdb
d
dd
t
tt
lAlAEAAk
l
EAk
l
EAk
kk
kkk
kkk
+=
==
+=+=
or111
21
21
21
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JointsFastener Stiffness
See Table 8-7
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JointsMember Stiffness
30hardened steel,cast iron or aluminum members
EA
Pdxd =
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JointsMember Stiffness
( )
( )[ ] ( )[ ]
))(tan2(
))(tan2(ln
tan
))(tan2(
))(tan2(ln
tan
2/tan2/tan
2tan
2tan
22tan
0
22
22
dDdDt
dDdDtEdPk
dDdDt
dDdDt
Ed
P
dDxdDxdx
EP
dDx
dDx
dDxrrA
EA
Pdxd
t
io
++
++==
++
++=
+++=
+
++=
+==
=
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JointsMember Stiffness
8-8Tableindefinedand
)/exp(
5.25774.0
5.05774.05ln2
5774.0
5.1,2,2/
))(155.1(
))(155.1(ln
5774.030
))(tan2(
))(tan2(ln
tan
BA
lBdAEd
k
dl
dl
Edk
dDdtlkk
dDdDt
dDdDt
Edk
dDdDt
dDdDt
EdPk
m
m
wm
=
+
+=
====
++
++==
++
++==
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JointsMember Stiffness
8-8Tableindefinedand
)/exp(
BA
lBdAEd
km =
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JointsMember Stiffness
8-2
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Bolt Strength
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Bolt Strength
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Bolt Strength
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Bolt Strength
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Tension Joints-The External Load
Fi = preload P = external tensile load Pb = portion of P taken by
bolt Pm = portion of P taken by
members
Fb= Pb+ Fi = resultant boltload Fm= Pm Fi = resultant load
on members C= fraction of external load
P carried by bolt 1 C= fraction of external
load P carried by members
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Tension Joints-The External Load
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Tension Joints-The External Load
80 %
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Relating Bolt Torque to Bolt Tension
15.0for0.2
625.0sectan1
sectan
2
2625.0
sectan1
sectan
2
25.12/)5.1(
2sectan1
sectan
2
/tan
2sec
sec
2
6)-(8and5)-(8form
===
=
+
+
=
+
+
+
=
=+=
+
+=
=
+
+=
c
i
cm
cciic
m
c
ccimi
m
cci
m
mmi
ffK
dKFT
ff
f
d
dK
Ktcoefficientorque
dfFdFf
f
f
d
dT
dddd
dfF
f
fdFT
dl
dfF
fld
fdldFT
&
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Relating Bolt Torque to Bolt Tension
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Relating Bolt Torque to Bolt Tension
8-3
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Statically Loaded Tension Joint with
Preload
n = load factor 1bolt stress proofstrength
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Statically Loaded Tension Joint with
Preload Fm = 0 (8-25)
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Statically Loaded Tension Joint with
Preload
Bowman preload = 75% proof load
Proof strength Sp = 0.85 Sy
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Statically Loaded Tension Joint with
Preload 8-4
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Gasketed Joints
boltofnumbertheis
circlebolttheofdiametertheis
63
pressureofuniformityadequatemaintainto
/)]1([
)1(
/
N
D
Nd
D
ANCnPFp
FnPCF
NA
Fp
b
b
gi
im
g
m
=
=
=
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Fatigue Loading of Tension Joints
Peterson bolt 15 percent under the head
20 percent at the end of the thread
65 percent in the thread at the nut face
Kf
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Fatigue Loading of Tension Joints
i di f T i i
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Fatigue Loading of Tension Joints
F i L di f T i J i
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Fatigue Loading of Tension Joints
iam
t
i
t
m
tt
ii
t
iba
iba
ib
A
F
A
CPA
CP
A
FFCP
A
FF
FFFFF
FFFF
+=
+=
=+
==
==
==
2
22
)(
2
2/)(2/)(
and
minmax
minmax
F i L di f T i J i
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Fatigue Loading of Tension Joints
F i L di f T i J i
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Fatigue Loading of Tension Joints
( )( )
( )
( )
am
p
p
tuti
ff
eut
tute
f
i
eut
itutef
tii
aaf
Sn
ASCF
nn
SSP
ASS
n
FC
SSCP
FASSn
AF
Sn
+=
+=
==
+
=
=
=
strengthprooftheusingyielding,ofypossibilitcheck the
1
1/GoodmanFor
2
0,1preload,noFor
2
/Goodman,For
/
saftyofFactor
0
0
F i L di f T i J i
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Fatigue Loading of Tension Joints
8-5
B lt d d Ri t d J i t L d d i
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Bolted and Riveted Joints Loaded in
Shear
B lt d d Ri t d J i t L d d i
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Bolted and Riveted Joints Loaded in
Shear
tdA
AF
AF
cIM
FtM
=
=
=
=
=
/
/
/
2/
Bolted and Riveted Joints Loaded in
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Bolted and Riveted Joints Loaded in
ShearThe usual analysis involves
Bearing in the bolt (all bolts participate) Bearing in members (all holes participate)
Shear of bolt (all bolts participate eventually)
Distinguishing between thread and shank shear Edge shearing and tearing of member (edge bolts
participate)
Tensile yielding of member across bolt holes Checking member capacity
Bolted and Riveted Joints Loaded in
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Bolted and Riveted Joints Loaded in
Shear 8-6
Bolted and Riveted Joints Loaded in
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Bolted and Riveted Joints Loaded in
Shear
Bolted and Riveted Joints Loaded in
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Bolted and Riveted Joints Loaded in
Shear Shear Joints with Eccentric Loading
Direct load or primary shear F = V1/n
n number of bolt
Moment load or secondary shear M1
Bolted and Riveted Joints Loaded in
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Bolted and Riveted Joints Loaded in
Shear
Bolted and Riveted Joints Loaded in
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Bolted and Riveted Joints Loaded in
Shear
L
L
+++=
=
==
+++=
222
1
2
1
/4
CBA
nn
C
C
B
B
A
A
CCBBAA
rrr
rMF
dF
r
F
r
F
r
F
rFrFrFM
Bolted and Riveted Joints Loaded in
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Bolted and Riveted Joints Loaded in
Shear 8-7
Reference
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Reference
Budynas, R.G. and Nisbett, J.K., Shigleys
Mechanical Engineering Design, 8th
ed.,McGraw Hill, 2008.