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Direct Electricity from Heat: A Solution to Assist Aircraft Power DemandsA thermionic device produces an electrical current with the application of a thermal gradient whereby the temperature at one electrode provides enough thermal energy to eject electrons. The system is totally predicated on the thermal gradient and the work function of the electrode collector relative to the emitter electrode. Combined with a standard thermoelectric device high efficiencies may result, capable of providing electrical energy from the waste heat of gas turbine engines.
Document ID
20100012830
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Goldsby, Jon C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
March 1, 2010
Subject Category
Aeronautics (General)
Report/Patent Number
E-17191
NASA/TM-2010-216108
Report Number: E-17191
Report Number: NASA/TM-2010-216108
Funding Number(s)
WBS: WBS 561581.02.08.03.15.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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