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The mechanism of bolt loadingIt is shown that the mechanism of bolt loading for preloaded fasteners can be effectively portrayed through simple spring models and some algebraic manipulations. Understanding schematically what is involved in such joints provides insight into the distribution of loads. The developed equations confirm that for both symmetric and nonsymmetric joints the loading plane factor and the stiffness factor directly affect the load seen in preloaded fasteners. The manner in which an external loading is transferred through the joint can be explained as energy dissipated in the various springs of both the abutment and the bolt itself.
Document ID
19930003224
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lee, H. M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:108377
NASA-TM-108377
Report Number: NAS 1.15:108377
Report Number: NASA-TM-108377
Accession Number
93N12412
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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