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Energy efficient engine low-pressure compressor component test hardware detailed design reportThe aerodynamic and mechanical design description of the low pressure compressor component of the Energy Efficient Engine were used. The component was designed to meet the requirements of the Flight Propulsion System while maintaining a low cost approach in providing a low pressure compressor design for the Integrated Core/Low Spool test required in the Energy Efficient Engine Program. The resulting low pressure compressor component design meets or exceeds all design goals with the exception of surge margin. In addition, the expense of hardware fabrication for the Integrated Core/Low Spool test has been minimized through the use of existing minor part hardware.
Document ID
19830022156
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Michael, C. J. (United Technologies Corp. East Hartford, CT, United States)
Halle, J. E. (United Technologies Corp. East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5594-157
NASA-CR-165354
NAS 1.26:165354
Accession Number
83N30427
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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