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Analysis of high load dampersHigh load damping requirements for modern jet engines are discussed. The design of damping systems which could satisfy these requirements is also discusseed. In order to evaluate high load damping requirements, engines in three major classes were studied; large transport engines, small general aviation engines, and military engines. Four damper concepts applicable to these engines were evaluated; multi-ring, cartridge, curved beam, and viscous/friction. The most promising damper concept was selected for each engine and performance was assessed relative to conventional dampers and in light of projected damping requirements for advanced jet engines.
Document ID
19820015374
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bhat, S. T.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Buono, D. F.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Hibner, D. H.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
August 21, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5779-10
NASA-CR-165503
NAS 1.26:165503
Report Number: PWA-5779-10
Report Number: NASA-CR-165503
Report Number: NAS 1.26:165503
Accession Number
82N23248
Funding Number(s)
CONTRACT_GRANT: NAS3-22518
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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