The amount of clamp load loss due to a fully reversed cyclic service load is determined for a bolted assembly in which the fastener and the joint were both tightened initially beyond their respective proportional limits. The cyclic reversed load acts in a direction parallel to the bolt axis. During the first half of each cycle, the cyclic load acts as tensile separating force that increases the fastener tension further into the nonlinear range; it simultaneously reduces the joint clamping force. Thus, after the first one half of the cycle, the clamp load is reduced from its initial value due to the plastic elongation of the fastener. During the second half cycle, the cyclic load compresses the joint further into the plastic range; simultaneously, it reduces the fastener tension. Due to the permanent set in the compressed joint, the clamp load is decreased further at the end of the second half cycle of the service load. The cumulative clamp load loss due to the permanent set in both the fastener and the joint is analytically determined using a nonlinear model. Variables investigated in this study include the joint-to-fastener stiffness ratio, the ratio of the initial fastener tension to its elastic limit, and the ratio of the external force to its maximum tensile value that would trigger joint separation.

1.
Bickford
,
J. H.
, 1995,
An Introduction to the Design and Analysis of Bolted Joints
, 3rd ed.,
Marcel–Dekker
,
New York
.
2.
Bickford
,
J. H.
, and
Nassar
,
S.
, 1998,
Handbook of Bolts and Bolted Joints
,
Marcel–Dekker
,
New York
.
3.
Nassar
,
S. A.
,
Barber
,
G. C.
, and
Zuo
,
D.
, 2005, “
Bearing Friction Torque in Bolted Joints
,”
STLE Tribol. Trans.
1040-2004,
48
, pp.
69
75
.
4.
Chapman
,
I.
,
Newham
,
J.
, and
Wallace
,
P.
, 1986, “
The Tightening of Bolts to Yield and their Performance Under Load
,”
Trans. ASME, J. Vib., Acoust., Stress, Reliab. Des.
0739-3717,
108
, p.
213
221
.
5.
Juvinall
,
R. C.
, and
Marshek
,
K. M.
, 2000,
Fundamentals of Machine Component Design
, 3rd ed.,
Wiley
,
New York
, pp.
426
431
.
6.
Nassar
,
S. A.
, and
Shoberg
,
R. S.
, 1992, “
Effect of Fastener Tightening Beyond Yield on the Behavior of Bolted Joints Under Service Loads
,”
Proceeding of the 18th Annual Conference of the AMSE
,
Michigan State University
,
East Lansing, MI
, Oct. 30–Nov. 1, pp.
1
17
.
7.
Nassar
,
S. A.
, and
Matin
,
P. H.
, 2004, “
Fastener Tightening Beyond Yield
,”
Proceedings of the ASME Pressure Vessels and Piping Conference
,
San Diego, Ca
, July 25–29, pp.
29
40
.
8.
Nassar
,
S. A.
, and
Matin
,
P. H.
, 2006, “
Clamp Load Loss Due to Fastener Elongation Beyond its Elastic Limit
,”
ASME J. Pressure Vessel Technol.
0094-9930,
128
(
3
), pp.
379
387
.
9.
Nassar
,
S. A.
, and
Matin
,
P. H.
, 2005, “
Non-Linear Strain Hardening Model For Predicting Clamp Load Loss in Bolted Joints
,”
ASME J. Mech. Des.
1050-0472,
128
(
6
), pp.
1328
1336
.
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