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Assessment of NASA Dual Microstructure Heat Treatment Method for Multiple Forging Batch Heat TreatmentNASA dual microstructure heat treatment technology previously demonstrated on single forging heat treat batches of a generic disk shape was successfully demonstrated on a multiple disk batch of a production shape component. A group of four Rolls-Royce Corporation 3rd Stage AE2100 forgings produced from alloy ME209 were successfully dual microstructure heat treated as a single heat treat batch. The forgings responded uniformly as evidenced by part-to-part consistent thermocouple recordings and resultant macrostructures, and from ultrasonic examination. Multiple disk DMHT processing offers a low cost alternative to other published dual microstructure processing techniques.
Document ID
20040040179
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Gayda, John
(NASA Glenn Research Center Cleveland, OH, United States)
Lemsky, Joe
(Ladish Co., Inc. Cudahy, WI, United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2004
Subject Category
Metals And Metallic Materials
Report/Patent Number
NASA/CR-2004-212950
Report Number: NASA/CR-2004-212950
Funding Number(s)
WBS: WBS 22-728-30-09
CONTRACT_GRANT: NASA Order C-80000-A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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