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Weld peaking on heavy aluminum structuresWeld peaking is usually undesirable in any welded structure. In heavy structures, the forces involved in the welding process become very large and difficult to handle. With the shuttle's solid rocket booster, the weld peaking resulted in two major problems: (1) reduced mechanical properties across the weld joint, and (2) fit-up difficulties in subsequent assembly operation. Peaking from the weld shrinkage forces can be fairly well predicted in simple structures; however, in welding complicated assemblies, the amount of peaking is unpredictable because of unknown stresses from machining and forming, stresses induced by the fixturing, and stresses from welds in other parts of the assembly. When excessive peaking is encountered, it can be corrected using the shrinkage forces resulting from the welding process. Application of these forces is discussed in this report.
Document ID
19780017484
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bayless, E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Poorman, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Sexton, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1978
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-78176
Report Number: NASA-TM-78176
Accession Number
78N25427
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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