The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Jun. 28, 2022
Filed:
Dec. 13, 2019
Applicant:
United States of America As Represented BY the Administrator of Nasa, Washington, DC (US);
Inventor:
Rodger W. Dyson, Jr., Elyria, OH (US);
Assignee:
Other;
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/18 (2006.01); B64D 27/12 (2006.01); B64D 27/24 (2006.01); F02C 6/20 (2006.01); F02G 5/02 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
F02C 6/18 (2013.01); B64D 27/12 (2013.01); B64D 27/24 (2013.01); F02C 6/20 (2013.01); F02G 5/02 (2013.01); B64D 2027/026 (2013.01); F02G 2243/54 (2013.01); F02G 2254/15 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2260/208 (2013.01); F05D 2260/213 (2013.01);
Abstract
A thermal management system for an aircraft is provided that includes thermo-acoustic engines that remove and capture waste heat from the aircraft engines, heat pumps powered by the acoustic waves generated from the waste heat that remove and capture electrical component waste heat from electrical components in the aircraft, and hollow tubes disposed in the aircraft configured to propagate mechanical energy to locations throughout the aircraft and to transfer the electrical component waste heat back to the aircraft engines to reduce overall aircraft mass and improve propulsive efficiency.