NTRS - NASA Technical Reports Server

Back to Results
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
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
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
Meeting Information
Meeting: AIAA Aviation 2016
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 081876.
Distribution Limits
Work of the US Gov. Public Use Permitted.
hybrid propulsion
aircraft engines
No Preview Available