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Design and Development of a 200-kW Turbo-Electric Distributed Propulsion TestbedThere a few NASA funded electric and hybrid electric projects from different NASA Centers, including the NASA Armstrong Flight Research Center (AFRC) (Edwards, California). Each project identifies a specific technology gap that is currently inhibiting the growth and proliferation of relevant technologies in commercial aviation. This paper describes the design and development of a turbo-electric distributed propulsion (TeDP) hardware-in-the-loop (HIL) simulation bench, which is a test bed for discovering turbo-electric control, distributed electric control, power management control, and integration competencies while providing risk mitigation for future turbo-electric flying demonstrators.
Document ID
20170001279
Document Type
Book Chapter
External Source(s)
Authors
Papathakis, Kurt V.
(NASA Armstrong Flight Research Center Edwards, CA United States)
Date Acquired
February 3, 2017
Publication Date
January 31, 2017
Subject Category
Aircraft Propulsion And Power
Aircraft Design, Testing And Performance
Electronics And Electrical Engineering
Report/Patent Number
DFRC-E-DAA-TN38950
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
propulsion
hybrid electric
distributed

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