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Energy efficient engine. Volume 2. Appendix A: Component development and integration programThe large size and the requirement for precise lightening cavities in a considerable portion of the titanium fan blades necessitated the development of a new manufacturing method. The approach which was selected for development incorporated several technologies including HIP diffusion bonding of titanium sheet laminates containing removable cores and isothermal forging of the blade form. The technology bases established in HIP/DB for composite blades and in isothermal forging for fan blades were applicable for development of the manufacturing process. The process techniques and parameters for producing and inspecting the cored diffusion bonded titanium laminate blade preform were established. The method was demonstrated with the production of twelve hollow simulated blade shapes for evaluation. Evaluations of the critical experiments conducted to establish procedures to produce hollow structures by a laminate/core/diffusion bonding approach are included. In addition the transfer of this technology to produce a hollow fan blade is discussed.
Document ID
19850002683
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Moracz, D. J.
(TRW, Inc. Cleveland, OH, United States)
Cook, C. R.
(TRW, Inc. Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
October 30, 1981
Publication Information
Publisher: Pratt and Whitney Aircraft
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:173085
PWA-5594-179-VOL-2-APP-A
ER-8050-F-VOL-2-APP-A
NASA-CR-173085
SASR-7-VOL-2-APP-A
Report Number: NAS 1.26:173085
Report Number: PWA-5594-179-VOL-2-APP-A
Report Number: ER-8050-F-VOL-2-APP-A
Report Number: NASA-CR-173085
Report Number: SASR-7-VOL-2-APP-A
Accession Number
85N10991
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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