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:
Aug. 30, 2022

Filed:

Nov. 15, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nicholas William Rathay, Rock City Falls, NY (US);

Gregory Alexander Natsui, Schenectady, NY (US);

Brian Magann Rush, Niskayuna, NY (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 13/00 (2006.01); B64C 30/00 (2006.01); F28F 21/00 (2006.01); B64C 1/10 (2006.01);
U.S. Cl.
CPC ...
B64D 13/00 (2013.01); B64C 1/10 (2013.01); B64C 30/00 (2013.01); F28F 21/00 (2013.01);
Abstract

A hypersonic aircraft includes one or more leading edge assemblies that are designed to manage thermal loads experienced at the leading edges during high speed or hypersonic operation. Specifically, the leading edge assemblies may include an outer wall tapered to a leading edge or stagnation point. The outer wall may define a vapor chamber and a capillary structure within the vapor chamber for circulating a working fluid in either liquid or vapor form to cool the leading edge. In addition, a thermal energy storage reservoir positioned within the vapor chamber contains a phase change material for absorbing thermal energy.


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