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. 27, 2019

Filed:

Apr. 30, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Charles E. Kusuda, Mukilteo, WA (US);

Christopher Stephen Roper, Santa Monica, CA (US);

William Vannice, Kent, WA (US);

Arun Muley, San Pedro, CA (US);

Kevin John Maloney, Cambridge, GB;

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60H 1/00 (2006.01); F01N 5/02 (2006.01); F28D 7/02 (2006.01); F28D 1/047 (2006.01); F28D 1/06 (2006.01); F28D 7/00 (2006.01); F28D 1/02 (2006.01); F28D 15/02 (2006.01); F28D 15/04 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
F28D 1/0477 (2013.01); F28D 1/0226 (2013.01); F28D 1/06 (2013.01); F28D 7/0058 (2013.01); F28D 15/0275 (2013.01); F28D 15/04 (2013.01); F28D 2001/028 (2013.01); F28D 2021/0021 (2013.01); F28F 2210/02 (2013.01); F28F 2260/02 (2013.01);
Abstract

An aircraft including an airframe, a propulsion system, and a heat exchanger is presented. The heat exchanger of the aircraft may include (i) a structural body including a plurality of hollow channels, (ii) a first fluid positioned within the plurality of hollow channels of the structural body, (iii) a plurality of openings positioned on a first side of the structural body and in fluid communication with the plurality of hollow channels, (iv) a wick structure positioned on the first side of the structural body, and further positioned adjacent to an exterior of the plurality of hollow channels and in fluid communication with the plurality of openings, (v) an inlet to the structural body operable to provide a second fluid from an aircraft system, and (vi) an outlet from the structural body operable to receive the second fluid after receiving heat from the first fluid.


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