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Energy efficient engine high-pressure turbine detailed design reportThe energy efficient engine high-pressure turbine is a single stage system based on technology advancements in the areas of aerodynamics, structures and materials to achieve high performance, low operating economics and durability commensurate with commercial service requirements. Low loss performance features combined with a low through-flow velocity approach results in a predicted efficiency of 88.8 for a flight propulsion system. Turbine airfoil durability goals are achieved through the use of advanced high-strength and high-temperature capability single crystal materials and effective cooling management. Overall, this design reflects a considerable extension in turbine technology that is applicable to future, energy efficient gas-turbine engines.
Document ID
19840020719
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Thulin, R. D.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Howe, D. C.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Singer, I. D.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-165608
PWA-5594-171
NAS 1.26:165608
Accession Number
84N28788
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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