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A Turbo-Brayton Cryocooler for Aircraft Superconducting SystemsHybrid turboelectric aircraft-with gas turbines driving electric generators connected to electric propulsion motors-have the potential to transform aircraft design. Decoupling power generation from propulsion enables innovative aircraft designs, such as blended-wing bodies, with distributed propulsion. These hybrid turboelectric aircraft have the potential to significantly reduce emissions, decrease fuel burn, and reduce noise, all of which are required to make air transportation growth projections sustainable. The power density requirements for these electric machines can only be achieved with superconductors, which in turn require lightweight, high-capacity cryocoolers.
Document ID
20150005302
Acquisition Source
Glenn Research Center
Document Type
Other
Authors
Dietz, Anthony
(Creare, Inc. Hanover, NH, United States)
Date Acquired
April 10, 2015
Publication Date
November 1, 2014
Publication Information
Publication: An Overview of SBIR Phase 2 Airbreathing Propulsion Technologies
Subject Category
Aircraft Design, Testing And Performance
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Public Use Permitted.
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