mech1641 - w2008 lecture 05 - fatigue iv
DESCRIPTION
Fatigue LectureTRANSCRIPT
MECH1641 – Machine Design II
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Lecture 5: Fatigue IV
Homework Review
Interpreting Constant Life Diagrams
Constructing Constant Life Diagrams
Component Design for Fluctuating Loads
Review
Homework & Reading Assignment
MECH1641 – Machine Design II
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Objectives
After this lecture and associated homework, you will be able to:
Interpret a Constant Life diagram.
Calculate the fatigue life for fluctuating stresses using Constant Life diagrams.
Construct a Constant Life diagram from the S-N curve.
Apply Constant Life diagrams to the design of parts with a fluctuating load profile.
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Homework Review
1. Determine the mean stress and stress amplitude of an application that cycles between -350 and 780 MPa? Sketch the stress vs. time profile.
2. Determine the minimum stress and stress amplitude of an application with a mean stress of 925 MPa and a maximum stress of 1190 MPa. Sketch the stress vs. time profile.
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Constant Life Diagram Review
The horizontal axis is mean stress σm.
The vertical axis is stress amplitude σa.
Sy
0
-Sy
0
Sy
-Sy
Sy
0
-Sy
Sy
0
-Sy
Sy
0
-Sy
Sy
0
-Sy
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Designing for Fatigue
An S-N Curve is needed to design parts for fatigue applications involving fully reversing loads.
A Constant Life diagram is needed to design parts for fatigue applications involving fluctuating loads.
102030405060708090
100110120130140150160
1.E+00 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08 1.E+09
Life N (cycles)
Fatig
ue S
treng
th S
f (ks
i)
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Fatigue Strength Diagram for 7075-T6 Aluminum
Ref. Juvinall Figure 8.19.
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Fatigue Strength Diagram for Alloy SteelsApplicable to AISI 4340, 4130, 2330, 8630.
Ref. Juvinall Figure 8.17.
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Problem 1If a test specimen made from normalized 4130 steel with an ultimate strength of 100 ksi is subject to a maximum bending stress of 90 ksi and a minimum stress of 0, what is the expected fatigue life? Sketch the stress vs. time profile.
4: 90 90% 0 10max u minFind N Given ksi S N cyclesσ σ= = = → =
0
90 ksi
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Problem 2For an normalized 4130 test specimen with Su=100 ksi, what is the maximum stress that can be applied for 106 cycles if the loading is of the zero-to-max-to-zero type? Sketch the stress vs. time profile.
610 : 0
70% 70max min
max u
Find for N cycles Given
S ksi
σ σ
σ
= =
= =
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Problem 3For a quenched and tempered 4340 test specimen with an ultimate strength of 180 ksi, what life is expected from a fluctuating load with a mean stress of 90 ksi and a stress amplitude of 80 ksi? Sketch the stress vs. time profile.
4 4
: 90 50% 72 40%
10 3 10m u a uFind N Given ksi S ksi S
N
σ σ= = = =
< < ×
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Problem 4For a hardened 4340 test specimen with Su=230 ksi what is the highest stress amplitude that can be applied with a superimposedtensile stress of 184 ksi if infinite life is required? Sketch the stress vs. time profile.
7: 184 80% ; 10
10% 23a m u
a u
Find Given ksi S N
S ksi
σ σ
σ
= = >
= =
184 ksi
0
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Problem 5Use the empirical relationships discussed to construct the S-N Curve and the Constant Fatigue Life diagram in Excel for a precision steel part with an ultimate strength of 150 ksi, a yield strength of 120 ksi, commercially polished surface. All cross-section dimensions are under 2 in, and the loads are axial. Assume that actual fatigue test data is not available.
Ref. Juvinall Sample Problem 8.1.
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Problem 5
, 1000
:150 ; 120
For steel, 0.5For axial loading, 0.75 , and 1
For a ground surface, 0.9For a diameter<2 , axially loaded, 0.9Assume 1; 1
0.5 0.5 150 75
u y
n u
f N u T L
S
G
T R
n u
n n L G
AnalysisS ksi S ksi
S SS S C C
Cin C
C CS S ksi ksi
S S C C
=
= =
′ =
= =
==
= =′ = = × =
′=
, 1000 , 1000
75 1 0.9 0.9 1 1 61
0.75 0.75 150 1 112
S T R n
f N u T f N
C C C ksi S ksi
S S C ksi S ksi= =
= × × × × × ∴ =
= = × × ∴ =
This is all that is needed to draw the predicted S-N curve, which shows fatigue behaviour for fully fully-reversing loads only.
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102030405060708090
100110120130140150160
1.E+00 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08 1.E+09
Life N (cycles)
Fatig
ue S
treng
th S
f (ks
i)
Problem 5 ( S-N Curve)
6, 1061nf N
S S ksi=
′= =
3, 10112
f NS ksi
==
, 1 150f N uS S ksi= = =
These values can be read from this S-N curve to construct the Constant Life Diagram.
4, 1094
f NS ksi
==
5, 1077
f NS ksi
==
S-N Curve DataN Sf (ksi)
1.E+00 150 Su
1.E+03 111 Sf,N=1000
1.E+06 61 Sn
1.E+09 61 Sn
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Problem 5 (Constant Life Diagram )
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112 N=103
94 N=104
77 N=105
61 N=106
0
20
40
60
80
100
120
140
-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160Mean Stress σm (ksi)
Stre
ss A
mpl
itude
σa (
ksi)
Problem 5 (Constant Life Diagram )
σm
N=103 N=104 N=105 N=106
-120 112 94 77 610 112 94 77 61
150 0 0 0 0
σa
Constant Life Line Data
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N=103112
N=10494
N=10577
N=10661
0
20
40
60
80
100
120
140
-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160Mean Stress σm (ksi)
Stre
ss A
mpl
itude
σa (
ksi)
Problem 5 (Constant Life Diagram )
This line represents combinations of σm & σa that result in a σmax=Sy. I.e., yielding occurs above this loading, no yielding below.
Yield Envelopeσm σa
-120 0 (-Sy,0)0 120 (0,+Sy)
120 0 (+Sy,0)
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Problem 6 – Designing a Part for Fluctuating Loads
A round tensile link is subjected to fluctuating load profile between 1000 lb and 5000 lb. It is a precision member, so CG=0.9 can be used, with commercially-polished surfaces. The material is steel, Su=150 ksi, Sy=120 ksi, so that the S-N curve and Constant Life diagram from the previous question can be used. A safety factor of 2 is required.
Find the diameter required for infinite life, and the diameter required for a life of 1000 cycles. No yielding should be permitted.
Ref. Juvinall Sample Problem 8.2.
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Problem 6 (Constant Life Diagram)
Ref. Juvinall Sample Problem 8.2.
112 N=103
94 N=104
77 N=105
61 N=106
0
20
40
60
80
100
120
140
-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160Mean Stress σm (ksi)
Stre
ss A
mpl
itude
σa (
ksi)
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Problem 6 Analysis
Ref. Juvinall Sample Problem 8.2.
First, identify , :5000
The maximum stress in the part
1000The minimum stress in the part
5000 10003000
2 25000 1000
2 2
m a
fmaxmax
fminmin
f f
fmax minm m
f f
max mina
n lbnFA A
n lbnFA A
n lb n lbn lbA A
An lb n lb
A A
σ σ
σ
σ
σ σσ σ
σ σσ
×= =
×= =
× ×+ ×+
= = ∴ =
× ×−−
= =
23
2000
So the ratio 0.666, for whatever the area must be.Draw a line with this slope on the Constant Life diagram.Such a line represents all possibile combinations ofmean stress and stress amplitude for the required loa
am
fa
n lbA
σσ
σ×
∴ =
= =
2
d profile.
3000 2000 12,000 8000Also Area
4f f f f
m a m a
n lb n lb n lb n lbdA dπσ σ πσ πσ
× × × ×= = = ∴ = =
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N=103112
N=10494
N=10577
N=10661
σa/σm=0.667
0
20
40
60
80
100
120
140
-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160Mean Stress σm (ksi)
Stre
ss A
mpl
itude
σa (
ksi)
Problem 6 (Infinite Life)
Ref. Juvinall Sample Problem 8.2.
This line represents the combinations of σm & σa that describe the given load profile, from 1000 lb to 5000 lb.
σa/σm=0.667σm σa
0 0 σa=0.667σm
150 100 σa=0.667σm
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N=103112
N=10494
N=10577
N=10661
σa/σm=0.667
0
20
40
60
80
100
120
140
-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160Mean Stress σm (ksi)
Stre
ss A
mpl
itude
σa (
ksi)
Problem 6 (Infinite Life)
Ref. Juvinall Sample Problem 8.2.
Small diameters will be associated with large stresses, on this line far away from the origin. Large diameters will result in small stresses, on this line near the origin.
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N=103112
N=10494
N=10577
N=10661
σa/σm=0.667
0
20
40
60
80
100
120
140
-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160Mean Stress σm (ksi)
Stre
ss A
mpl
itude
σa (
ksi)
Problem 6 (Infinite Life)
Ref. Juvinall Sample Problem 8.2.
σm=56 ksi & σa =38 ksi will cause yielding, and produce a life of about 106 cycles. d=0.369 in
212,000 12,00021 54,000
0.369
f f
m f
n lb lb indlb
d in
πσ π×
= = × ×
∴ =
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N=103112
N=10494
N=10577
N=10661
σa/σm=0.667
0
20
40
60
80
100
120
140
-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160Mean Stress σm (ksi)
Stre
ss A
mpl
itude
σa (
ksi)
Problem 6 (No Yielding)
Ref. Juvinall Sample Problem 8.2.
σm=71 ksi & σa =48 ksi will cause yielding, and produce a life of about 104 cycles. d=0.328 in
212,000 12,00021 71,000
0.328
f f
m f
n lb lb indlb
d in
πσ π×
= = × ×
∴ =
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N=103112
N=10494
N=10577
N=10661
σa/σm=0.667
0
20
40
60
80
100
120
140
-120 -100 -80 -60 -40 -20 0 20 40 60 80 100 120 140 160Mean Stress σm (ksi)
Stre
ss A
mpl
itude
σa (
ksi)
Problem 6 (N=1000)
Ref. Juvinall Sample Problem 8.2.
σm=80 ksi & σa =53 ksi will produce a life of 103
cycles, but with considerable yielding. d=0.309 in
212,000 12,00021 80,000
0.309
f f
m f
n lb lb indlb
d in
πσ π×
= = × ×
∴ =
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Summary: S-N Curves
An S-N Curve is needed to design parts for fatigue applications involving fully reversing loads.
An estimated S-N Curve can be constructed from ultimate strength.
It is more accurate to use real fatigue test data.
102030405060708090
100110120130140150160
1.E+00 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08 1.E+09
Life N (cycles)
Fatig
ue S
tren
gth
Sf (
ksi)
S-N Curve Estimated from Ultimate Strength(better than nothing; used for prototypes)
S-N Curve Based on test data(preferred for serious design)
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Summary: Constant-Life Diagrams
A Constant Life diagram is needed to design parts for fatigue applications involving fluctuating loads.
An estimated Constant Life diagram can be constructed from the S-N curve.
It is more accurate to use real fatigue test data.
Constant Life diagram constructed from the S-N curve(better than nothing; used for prototypes)
Constant Life diagram based on test data(preferred for serious design)
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Homework and Reading AssignmentFor next class, review these notes then answer the questions below:
1. For a 4340 test specimen with Su=150 ksi, what is the predicted life for a fully reversing stress of 90 ksi?
2. What is the maximum stress that will provide the same life if the load profile is changed to a zero-to-max-to-zero type?
3. What stress amplitude will provide the same life if the load profile is fluctuating with a maximum stress of 105 ksi?
4. Also, do these problems from Juvinall, chapter 8, by creating Excel S-N curves: 8.19, 8.20, 8.23, 8.25 (Excelconstant-life diagram required for this last problem.)
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Closing Notes
Quiz 2 (4%) is on Friday January 25.
Test 1 (20%) is on Friday February 22.