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Tail-mounted engine Architecture and Design for the Subsonic Single Aft Engine Electrofan AircraftThis paper describes the turbofan engine architecture for SUbsonic Single Aft eNgine (SUSAN) Electrofan is, a transformative concept hybrid electric aircraft. SUSAN has a single tail-mounted turbofan engine that produces a portion of the requires thrust and drives a 20MW electric generator which in turn provides the power to the 16 electric propulsors located on the wing responsible for producing the remainder of the required thrust. The atypical operation of the turbofan due to the large levels of power extraction from the low pressure turbine (LPT) is described here. This paper investigates the most efficient engine architecture to enable this unique operation, as well as exploring natural gas as an alternative fuel for SUSAN.
Document ID
20210024573
Document Type
Conference Paper
Authors
Arman Mirhashemi (Glenn Research Center Cleveland, Ohio, United States)
Jeffryes W. Chapman (Glenn Research Center Cleveland, Ohio, United States)
Christopher J. Miller (Glenn Research Center Cleveland, Ohio, United States)
Julia E. Stephens (Glenn Research Center Cleveland, Ohio, United States)
Ralph H. Jansen (Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
November 18, 2021
Subject Category
Aircraft Propulsion and Power
Aircraft Design, Testing and Performance
Meeting Information
AIAA SciTech Forum (San Diego, CA)
Funding Number(s)
WBS: 533127.02.30.03.23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
EAP
Hybrid Electric Aircraft
Turbofan
Power Extraction

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NameType Tail-mounted engine Architecture and Design_20220102.pdf STI