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Parametric study in weld mismatch of longitudinally welded SSME HPFTP inletWelded joints are an essential part of pressure vessels such as the Space Shuttle Main Engine (SSME) Turbopumps. Defects produced in the welding process can be detrimental to weld performance. Recently, review of the SSME high pressure fuel turbopump (HPFTP) titanium inlet x rays revealed several weld discrepancies such as penetrameter density issues, film processing discrepancies, weld width discrepancies, porosity, lack of fusion, and weld offsets. Currently, the sensitivity of welded structures to defects is of concern. From a fatigue standpoint, weld offset may have a serious effect since local yielding, in general, aggravates cyclic stress effects. Therefore, the weld offset issue is considered. Using the finite element method and mathematical formulations, parametric studies were conducted to determine the influence of weld offsets and a variation of weld widths in longitudinally welded cylindrical structures with equal wall thickness on both sides of the joint. From the study, the finite element results and theoretical solutions are presented.
Document ID
19910014189
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Min, J. B.
(NASA Headquarters Washington, DC United States)
Spanyer, K. L.
(NASA Headquarters Washington, DC United States)
Brunair, R. M.
(Sverdrup Technology, Inc., Saint Louis MO., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1991
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-103534
NAS 1.15:103534
Report Number: NASA-TM-103534
Report Number: NAS 1.15:103534
Accession Number
91N23502
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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