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.

Date of Patent:
Mar. 07, 2023

Filed:

Nov. 23, 2021
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Michael F. Stoia, Rancho Santa Margarita, CA (US);

Garrett W. Ek, O'Fallon, MO (US);

Arun Muley, San Pedro, CA (US);

Jacob T. Needels, Stanford, CA (US);

Kevin G. Bowcutt, Aliso Viejo, CA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02G 5/00 (2006.01); F02C 6/18 (2006.01); B64C 19/00 (2006.01); B64C 13/40 (2006.01);
U.S. Cl.
CPC ...
F02G 5/00 (2013.01); B64C 13/40 (2013.01); B64C 19/00 (2013.01); F02C 6/18 (2013.01); F05D 2220/64 (2013.01); F05D 2220/76 (2013.01);
Abstract

Methods and apparatus for cooling a surface on a flight vehicle and generating power include advancing the vehicle at a speed of at least Mach 3 to aerodynamically heat the surface. A first working fluid circulates through a first fluid loop that heats the first working fluid through a first heat intake thermally coupled to the surface and expands the first working fluid in a first thermal engine to generate a first work output. A second fluid loop has a second working fluid that receives heat from the first working fluid and a second thermal engine to generate a second work output. The first and second work outputs are operably coupled to first and second generators, respectively, to power primary or auxiliary systems on the flight vehicle.


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