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Progress toward determining the potential of ODS alloys for gas turbine applicationsThe Materials for Advanced Turbine Engine (MATE) Program managed by the NASA Lewis Research Center is supporting two projects to evaluate the potential of oxide dispersion strengthened (ODS) alloys for aircraft gas turbine applications. One project involves the evaluation of Incoloy (TM) MA-956 for application as a combustor liner material. An assessment of advanced engine potential will be conducted by means of a test in a P&WA 2037 turbofan engine. The other project involves the evaluation of Inconel (TM) MA 6000 for application as a high pressure turbine blade material and includes a test in a Garrett TFE 731 turbofan engine. Both projects are progressing toward these engine tests in 1984.
Document ID
19830014116
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dreshfield, R. L. (NASA Lewis Research Center Cleveland, OH, United States)
Hoppin, G., III (Garrett Turbine Engine Company Phoenix, Ariz., United States)
Sheffler, K. (Pratt and Whitney Aircraft Company East Hartford, Conn., United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Metallic Materials
Report/Patent Number
NASA-TM-83332
E-1579
NAS 1.15:83332
Report Number: NASA-TM-83332
Report Number: E-1579
Report Number: NAS 1.15:83332
Meeting Information
Meeting: Frontiers of High Temperature Mater. II
Location: London
Start Date: May 22, 1983
End Date: May 25, 1983
Sponsors: International Nickel Company
Accession Number
83N22387
Funding Number(s)
PROJECT: RTOP 505-33-1A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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