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Development of the activated diffusion brazing process for fabrication of finned shell to strut turbine bladesThe activated diffusion brazing process was developed for attaching TD-NiCr and U700 finned airfoil shells to matching Rene 80 struts obstructing the finned cooling passageways. Creep forming the finned shells to struts in combination with precise preplacement of brazing alloy resulted in consistently sound joints, free of cooling passageway clogging. Extensive tensile and stress rupture testing of several joint orientation at several temperatures provided a critical assessment of joint integrity of both material combinations. Trial blades of each material combination were fabricated followed by destructive metallographic examination which verified high joint integrity.
Document ID
19720004772
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilbers, L. G.
(General Electric Co. Evendale, OH, United States)
Berry, T. F.
(General Electric Co. Evendale, OH, United States)
Kutchera, R. E.
(General Electric Co. Evendale, OH, United States)
Edmonson, R. E.
(General Electric Co. Evendale, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1971
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-72844
Report Number: NASA-CR-72844
Accession Number
72N12421
Funding Number(s)
CONTRACT_GRANT: NAS3-12433
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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