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:
Jan. 19, 2021

Filed:

Dec. 18, 2017
Applicant:

Raytheon Company, Waltham, MA (US);

Inventor:

Adam Wood, Oro Valley, AZ (US);

Assignee:

Raytheon Company, Waltham, MA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01P 3/00 (2006.01); B64D 33/08 (2006.01); B64D 27/16 (2006.01); F02K 7/10 (2006.01); F02K 1/82 (2006.01); F02K 7/14 (2006.01);
U.S. Cl.
CPC ...
B64D 33/08 (2013.01); B64D 27/16 (2013.01); F02K 1/825 (2013.01); F02K 7/10 (2013.01); F02K 7/14 (2013.01); F05D 2220/10 (2013.01); F05D 2260/221 (2013.01); F05D 2300/603 (2013.01);
Abstract

Passive reduction of internal jet engine component temperature in supersonic and hypersonic vehicles results from use of nanocomposite optical ceramic materials between the heat-generating portions of each jet engine and the ambient environment, allowing heat dissipation from the jet engine components directly to the ambient environment. A propulsion-airframe integrated scramjet aircraft includes a jet engine and an airframe supporting the jet engine, with at least a portion of the airframe between a heat-generating portion of the jet engine and an ambient environment comprising a nanocomposite optical ceramic material in the form of a panel or a grid of windows each supported within a frame. The nanocomposite optical ceramic material portion of the airframe disposed between the heat-generating portion of the jet engine and the ambient environment is infrared-transparent, and may transmit at least 75% of heat energy from the heat-generating portion of the jet engine to the ambient environment.


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