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Advanced oxide dispersion strengthened sheet alloys for improved combustor durabilityBurner design modifications that will take advantage of the improved creep and cyclic oxidation resistance of oxide dispersion strengthened (ODS) alloys while accommodating the reduced fatigue properties of these materials were evaluated based on preliminary analysis and life predictions, on construction and repair feasibility, and on maintenance and direct operating costs. Two designs - the film cooled, segmented louver and the transpiration cooled, segmented twin Wall - were selected for low cycle fatigue (LCF) component testing. Detailed thermal and structural analysis of these designs established the strain range and temprature at critical locations resulting in predicted lives of 10,000 cycles for MA 956 alloy. The ODs alloys, MA 956 and HDA 8077, demonstrated a 167 C (300 F) temperature advantage over Hastelloy X alloy in creep strength and oxidation resistance. The MA 956 alloy was selected for mechanical property and component test evaluations. The MA 956 alloy was superior to Hastelloy X in LCF component testing of the film cooled, segmented louver design.
Document ID
19810022662
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Henricks, R. J.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Publication Information
Publication: NASA. Lewis Res. Center Aircraft Engine Diagnostics
Subject Category
Aircraft Propulsion And Power
Accession Number
81N31204
Funding Number(s)
CONTRACT_GRANT: NAS3-20072
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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