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Program for refan JT8D engine design, fabrication and test, phase 2The objective of the JT8D refan program was to design, fabricate, and test certifiable modifications of the JT8D engine which would reduce noise generated by JT8D powered aircraft. This was to be accomplished without affecting reliability and maintainability, at minimum retrofit cost, and with no performance penalty. The mechanical design, engine performance and stability characteristics at sea-level and altitude, and the engine noise characteristics of the test engines are documented. Results confirmed the structural integrity of the JT8D-109. Engine operation was stable throughout the airplane flight envelope. Fuel consumption of the test engines was higher than that required to meet the goal of no airplane performance penalty, but the causes were identified and corrected during a normal pre-certification engine development program. Compared to the baseline JT8D-109 engine, the acoustically treated JT8D-109 engine showed noise reductions of 6 PNdB at takeoff and 11 PNdB at a typical approach power setting.
Document ID
19760004979
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Glass, J. A.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Zimmerman, E. S.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Scaramella, V. M.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-134876
PWA-5299
Report Number: NASA-CR-134876
Report Number: PWA-5299
Accession Number
76N12067
Funding Number(s)
CONTRACT_GRANT: NAS3-17840
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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