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:
Oct. 15, 2019

Filed:

Jan. 02, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Florian Hoefler, Garching bei München, DE;

Thomas Ripplinger, Garching bei München, DE;

Jorge Benignos, Garching bei München, DE;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/58 (2006.01); F01D 9/06 (2006.01); F02C 7/141 (2006.01); F02K 3/06 (2006.01); F04D 19/00 (2006.01); F04D 29/56 (2006.01); F28D 21/00 (2006.01);
U.S. Cl.
CPC ...
F04D 29/5806 (2013.01); F01D 9/065 (2013.01); F02C 7/141 (2013.01); F02K 3/06 (2013.01); F04D 19/002 (2013.01); F04D 29/56 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2240/12 (2013.01); F05D 2260/213 (2013.01); F05D 2260/22141 (2013.01); F28D 2021/0021 (2013.01); F28D 2021/0089 (2013.01);
Abstract

The example embodiments are directed to a heat dissipation system for an electric aircraft engine. In an example, the aircraft engine includes an electric system configured to power an engine fan to provide thrust to an aircraft, the electric system including cooling channels to receive a coolant to cool one or more components of the electric system, a power source to power the electric system, and one or more guide vanes connected to the cooling channels of the electric system and configured to receive the coolant heated by and output from the cooling channels, wherein the one or more guide vanes are further to cool the heated coolant and transfer the cooled coolant back to the cooling channels of the electric system. By dissipating heat from electric system via the guide vanes, the cooling system can provide sufficient cooling without adding additional drag to the aircraft.


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