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AiResearch QCGAT engine, airplane, and nacelle design featuresThe quiet, clean, general aviation turbofan engine and nacelle system was designed and tested. The engine utilized the core of the AiResearch model TFE731-3 engine and incorporated several unique noise- and emissions-reduction features. Components that were successfully adapted to this core include the fan, gearbox, combustor, low-pressure turbine, and associated structure. A highly versatile workhorse nacelle incorporating interchangeable acoustic and hardwall duct liners, showed that large-engine attenuation technology could be applied to small propulsion engines. The application of the mixer compound nozzle demonstrated both performance and noise advantages on the engine. Major performance, emissions, and noise goals were demonstrated.
Document ID
19800013841
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Heldenbrand, R. W.
(AiResearch Mfg. Co. Phoenix, AZ, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Publication Information
Publication: NASA. Lewis Res. Center Gen. Aviation Propulsion
Subject Category
Aircraft Propulsion And Power
Accession Number
80N22328
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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