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JT9D ceramic outer air seal system refinement programThe abradability and durability characteristics of the plasma sprayed system were improved by refinement and optimization of the plasma spray process and the metal substrate design. The acceptability of the final seal system for engine testing was demonstrated by an extensive rig test program which included thermal shock tolerance, thermal gradient, thermal cycle, erosion, and abradability tests. An interim seal system design was also subjected to 2500 endurance test cycles in a JT9D-7 engine.
Document ID
19820010729
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gaffin, W. O.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
January 27, 1982
Subject Category
Mechanical Engineering
Report/Patent Number
PWA-5515-165
NASA-CR-165554
Report Number: PWA-5515-165
Report Number: NASA-CR-165554
Accession Number
82N18603
Funding Number(s)
CONTRACT_GRANT: NAS3-20630
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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