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Advanced Propfan Engine Technology (APET) definition study, single and counter-rotation gearbox/pitch change mechanism designSingle-rotation propfan-powered regional transport aircraft were studied to identify key technology development issues and programs. The need for improved thrust specific fuel consumption to reduce fuel burned and aircraft direct operating cost is the dominant factor. Typical cycle trends for minimizing fuel consumption are reviewed, and two 10,000 shp class engine configurations for propfan propulsion systems for the 1990's are presented. Recommended engine configurations are both three-spool design with dual spool compressors and free power turbines. The benefits of these new propulsion system concepts were evaluated using an advanced airframe, and results are compared for single-rotation propfan and turbofan advanced technology propulsion systems. The single-rotation gearbox is compared to a similar design with current technology to establish the benefits of the advanced gearbox technology. The conceptual design of the advanced pitch change mechanism identified a high pressure hydraulic system that is superior to the other contenders and completely external to the gearboxes.
Document ID
19870019121
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anderson, R. D.
(General Motors Corp. Indianapolis, IN, United States)
Date Acquired
September 5, 2013
Publication Date
July 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
EDR-11283
NASA-CR-168115
NAS 1.26:168115
Accession Number
87N28554
Funding Number(s)
CONTRACT_GRANT: NAS3-23046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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