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The JT8D and JT9D engine component improvement: Performance improvement programThe NASA sponsored Engine Component Improvement - Performance Improvement Program at Pratt & Whitney Aircraft advanced the state of the art of thermal barrier coatings and ceramic seal systems, demonstrated the practicality of an advanced turbine clearance control system and an advanced fan design in the JT9D engine, and demonstrated the advantages of modern cooling, sealing, and aerodynamic designs in the high pressure turbine and compressor of the JT8D engine. Several of these improvements are already in airline service in JT8D and JT9D engines, and others will enter service soon in advanced models of these engines. In addition, the technology advances are being transferred to completely new engine configurations, the PW2037 engine and the NASA sponsored Energy Efficient Engine.
Document ID
19830009272
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
May 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5515-177
NAS 1.26:167965
NASA-CR-167965
Report Number: PWA-5515-177
Report Number: NAS 1.26:167965
Report Number: NASA-CR-167965
Accession Number
83N17543
Funding Number(s)
CONTRACT_GRANT: NAS3-20630
PROJECT: RTOP 535-04-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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