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Q-FANSTM for general aviation aircraftContinued growth of general aviation over the next 10 to 15 years is dependent on continuing improvement in aircraft safety, utility, performance and cost. Moreover, these advanced aircraft will need to conform to expected government regulations controlling propulsion system emissions and noise levels. An attractive compact low noise propulsor concept, the Q-FANTM when matched to piston, rotary combustion, or gas turbine engines opens up the exciting prospect of new, cleaner airframe designs for the next generation of general aviation aircraft which will provide these improvements and meet the expected noise and pollution restriction of the 1980 time period. New Q-FAN methodology which was derived to predict Q-FAN noise, weight and cost is presented. Based on this methodology Q-FAN propulsion system performance, weight, noise, and cost trends are discussed. Then the impact of this propulsion system type on the complete aircraft is investigated for several representative aircraft size categories. Finally, example conceptual designs for Q-FAN/engine integration and aircraft installations are presented.
Document ID
19740005613
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Worobel, R.
(Hamilton Standard Windsor Locks, CT, United States)
Mayo, M. G.
(Hamilton Standard Windsor Locks, CT, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-CR-114665
Report Number: NASA-CR-114665
Accession Number
74N13726
Funding Number(s)
CONTRACT_GRANT: NAS2-6834
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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