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JT9D jet engine diagnostics programPerformance deterioration in the JT9D-7 is a flight sensitive phenomenon caused by one short term and two long term wear modes. The short term deterioration occurs primarily during airplane acceptance testing and therefore does not affect airline operation. The long term wear takes place continuously over the engine life so that the performance loss can be minimized by a sound maintenance program. Short term deterioration is primarily due to flight load induced blade and gas path seal wear which result in increased gas path running clearances. The wear occurs in all engine modules but has the most deleterious effect on the low pressure compressor and high pressure turbine performance. The wear occurs during conditions that combine minimum axisymmetric running clearances and maximum engine distortion or asymmetric closure.
Document ID
19810022657
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Olsson, W. J.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Stromberg, W. J.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Publication Information
Publication: NASA. Lewis Res. Center Aircraft Engine Diagnostics
Subject Category
Aircraft Propulsion And Power
Accession Number
81N31199
Funding Number(s)
CONTRACT_GRANT: NAS3-20632
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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