NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Cost/benefit analysis of advanced materials technologies for future aircraft turbine enginesThe cost/benefits of advance commercial gas turbine materials are described. Development costs, estimated payoffs and probabilities of success are discussed. The materials technologies investigated are: (1) single crystal turbine blades, (2) high strength hot isostatic pressed turbine disk, (3) advanced oxide dispersion strengthened burner liner, (4) bore entry cooled hot isostatic pressed turbine disk, (5) turbine blade tip - outer airseal system, and (6) advance turbine blade alloys.
Document ID
19770007083
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bisset, J. W. (United Technologies Corp. East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-135107
PWA-5453
Accession Number
77N14026
Funding Number(s)
CONTRACT_GRANT: NAS3-20072
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available