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Energy efficient engine: High pressure turbine uncooled rig technology reportResults obtained from testing five performance builds (three vane cascades and two rotating rigs of the Energy Efficient Engine uncooled rig have established the uncooled aerodynamic efficiency of the high-pressure turbine at 91.1 percent. This efficiency level was attained by increasing the rim speed and annulus area (AN(2)), and by increasing the turbine reaction level. The increase in AN(2) resulted in a performance improvement of 1.15 percent. At the design point pressure ratio, the increased reaction level rig demonstrated an efficiency of 91.1 percent. The results of this program have verified the aerodynamic design assumptions established for the Energy Efficient Engine high-pressure turbine component.
Document ID
19820024507
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gardner, W. B.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1979
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-165149
NAS 1.26:165149
PWA-5594-92
Report Number: NASA-CR-165149
Report Number: NAS 1.26:165149
Report Number: PWA-5594-92
Accession Number
82N32383
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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