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Energy efficient engine: Turbine intermediate case and low-pressure turbine component test hardware detailed design reportA four stage, low pressure turbine component has been designed to power the fan and low pressure compressor system in the Energy Efficient Engine. Designs for a turbine intermediate case and an exit guide vane assembly also have been established. The components incorporate numerous technology features to enhance efficiency, durability, and performance retention. These designs reflect a positive step towards improving engine fuel efficiency on a component level. The aerodynamic and thermal/mechanical designs of the intermediate case and low pressure turbine components are presented and described. An overview of the predicted performance of the various component designs is given.
Document ID
19840020720
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Leach, K.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
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)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:167973
NASA-CR-167973
PWA-5594-191
Accession Number
84N28789
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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