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Mechanics of Re-Torquing in Bolted Flange ConnectionsIt has been widely accepted that the phenomenon of time-dependent loosening of flange connections is a strong consequence of the viscous nature of the compression seal material. Characterizing the coupled interaction between gasket creep and elastic bolt stiffness has been useful in predicting conditions that facilitate leakage. Prior advances on this sub-class of bolted joints has lead to the development of (1) constitutive models for elastomerics, (2) initial tightening strategies, (3) etc. The effect of re-torque, which is a major consideration for typical bolted flange seals used on the Space Shuttle fleet, has not been fully characterized, however. The current study presents a systematic approach to characterizing bolted joint behavior as the consequence of sequentially applied torques. Based on exprimenta1 and numerical results, the optimal re-torquing parameters have been identified that allow for the negligible load loss after pre-load application
Document ID
20130012997
Acquisition Source
Kennedy Space Center
Document Type
Other
Authors
Gordon, Ali P.
(University of Central Florida Orlando, FL, United States)
Drilling Brian
(University of Central Florida Orlando, FL, United States)
Weichman, Kyle
(University of Central Florida Orlando, FL, United States)
Kammerer, Catherine
(United Space Alliance Cape Canaveral, FL, United States)
Baldwin, Frank
(United Space Alliance Cape Canaveral, FL, United States)
Date Acquired
August 27, 2013
Publication Date
May 12, 2010
Subject Category
Structural Mechanics
Report/Patent Number
KSC-2009-259
Report Number: KSC-2009-259
Meeting Information
Meeting: 40th Aerospace Mechanisms Symposia
Location: Cocoa Beach, FL
Country: United States
Start Date: May 12, 2010
End Date: May 14, 2010
Funding Number(s)
CONTRACT_GRANT: NNJ06VA01C
Distribution Limits
Public
Copyright
Public Use Permitted.
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