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. 27, 2026

Filed:

Nov. 15, 2023
Applicant:

Wright Electric Inc., Ballston Spa, NY (US);

Inventors:

Jeffrey M. Engler, Ballston Spa, NY (US);

Colin Tschida, Ballston Spa, NY (US);

Kok Long Ng, Windsor, CA;

Deven Warke, Santa Clara, CA (US);

Assignee:

Wright Electric Inc., Ballston Spa, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60L 58/34 (2019.01); B60L 58/30 (2019.01); B64D 27/31 (2024.01); B64D 27/33 (2024.01); B64D 27/355 (2024.01); B64D 31/18 (2024.01); B64D 33/10 (2006.01); H01M 8/04029 (2016.01); H01M 8/04701 (2016.01); H01M 8/083 (2016.01); H01M 12/06 (2006.01);
U.S. Cl.
CPC ...
B60L 58/34 (2019.02); B60L 58/30 (2019.02); B64D 27/31 (2024.01); B64D 27/33 (2024.01); B64D 27/355 (2024.01); B64D 31/18 (2024.01); B64D 33/10 (2013.01); H01M 8/04029 (2013.01); H01M 8/04738 (2013.01); H01M 8/083 (2013.01); H01M 12/065 (2013.01); B60L 2200/10 (2013.01); H01M 2250/20 (2013.01);
Abstract

One embodiment is an aircraft having a least one of an aircraft motor or an aircraft motor drive, and a metal-air fuel cell. The aircraft has a waste heat transfer system including a diverter system. The diverter system selectively couples the metal-air fuel cell and the at least one of the aircraft motor or the aircraft motor drive. The aircraft has a control system to operate the waste heat transfer system to selectively transfer waste heat from the at least one of the aircraft motor or the aircraft motor drive to the metal-air fuel cell. The control system determines a power output status of the metal-air fuel cell, and to operate the diverter system to transfer the waste heat from the at least one of the aircraft motor or the aircraft motor drive to the metal-air fuel cell in response to determining the power output status.


Find Patent Forward Citations

Loading…