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The JT9D Jet Engine Diagnostics ProgramThe various engine deterioration phenomena that affect JT9D performance retention were studied, and approaches to improve performance retention of engines were identified. The program included surveys of historical data, monitoring of in service engines, ground and flight testing of instrumented engines, analysis, and analytical modeling. Performance deterioration is made up of both short and long term modes, both of which are flight cycle related phenomena. Short term deterioration occurs primarily during airplane acceptance testing prior to delivery to the airline. This effect is caused by flight load and power induced clearance closures and engine deflections with resulting rubbing of airfoils and seals. Long term deterioration is caused by erosion of airfoils and gas path seals during ground operation and take off and by cyclic induced thermal distortion of the high pressure turbine airfoils. Studies of possible remedial approaches have shown that performance retention within 1 to 2 percent of initial revenue service performance can be achieved with a proper program of hot section and cold section maintenance.
Document ID
19830009273
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Olsson, W. J.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:167966
PWA-5512-96
NASA-CR-167966
Report Number: NAS 1.26:167966
Report Number: PWA-5512-96
Report Number: NASA-CR-167966
Accession Number
83N17544
Funding Number(s)
PROJECT: RTOP 535-04-12
CONTRACT_GRANT: NAS3-20632
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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