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:
Jul. 02, 2024

Filed:

Jul. 09, 2021
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Frederic Lacaux, Woodinville, WA (US);

Eugene V. Solodovnik, Lake Stevens, WA (US);

Vyacheslav Khozikov, Bellevue, WA (US);

Assignee:

The Boeing Company, Arlington, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02P 1/00 (2006.01); B60L 15/20 (2006.01); B60L 50/60 (2019.01); B64C 11/30 (2006.01); B64D 27/24 (2006.01); B64D 31/00 (2006.01); H02P 27/06 (2006.01); H02P 29/028 (2016.01);
U.S. Cl.
CPC ...
H02P 29/028 (2013.01); B60L 15/20 (2013.01); B60L 50/60 (2019.02); B64C 11/303 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); H02P 27/06 (2013.01); B60L 2200/10 (2013.01);
Abstract

A method for protecting an electric propulsion system in response to occurrence of a fault. The method includes the step of activating short circuits in power switches of inverters in a motor controller to redirect current regenerated by a motor which is electrically coupled to the motor controller and mechanically coupled to a propeller. The method further includes feathering the propeller while the motor is regenerating current. The protection logic is designed to address different types of faults, including faults in the high-voltage direct-current bus, faults in the motor controller, and faults in the motor.


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