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Sizing Power Components of an Electrically Driven Tail Cone Thruster and a Range ExtenderThe aeronautics industry has been challenged on many fronts to increase efficiency, reduce emissions, and decrease dependency on carbon-based fuels. This paper provides an overview of the turboelectric and hybrid electric technologies being developed under NASA's Advanced Air Transportation Technology (AATT) Project and discusses how these technologies can impact vehicle design. The discussion includes an overview of key hybrid electric studies and technology investments, the approach to making informed investment decisions based on key performance parameters and mission studies, and the power system architectures for two candidate aircraft. Finally, the power components for a single-aisle turboelectric aircraft with an electrically driven tail cone thruster and for a hybrid-electric nine-passenger aircraft with a range extender are parametrically sized, and the sensitivity of these components to key parameters is presented.
Document ID
20160007561
Document Type
Conference Paper
Authors
Jansen, Ralph H. (NASA Glenn Research Center Cleveland, OH United States)
Bowman, Cheryl (NASA Glenn Research Center Cleveland, OH United States)
Jankovsky, Amy (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
June 15, 2016
Publication Date
June 13, 2016
Subject Category
Aircraft Propulsion and Power
Electronics and Electrical Engineering
Report/Patent Number
GRC-E-DAA-TN31785
E-19231
Meeting Information
AIAA Aviation 2016(Washington, DC)
Funding Number(s)
WBS: WBS 081876.02.03.05.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
hybrid propulsion
aircraft engines
turbogenerator

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