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:
Sep. 01, 2020

Filed:

Jun. 13, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Michael Thomas Gansler, Mason, OH (US);

Sridhar Adibhatla, Glendale, OH (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 19/00 (2018.01); G07C 5/08 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01); B64D 35/08 (2006.01); B64D 27/02 (2006.01); B64D 43/00 (2006.01); B64D 45/00 (2006.01);
U.S. Cl.
CPC ...
G07C 5/0808 (2013.01); B64D 27/02 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); B64D 35/08 (2013.01); G07C 5/0841 (2013.01); B64D 43/00 (2013.01); B64D 2027/026 (2013.01); B64D 2045/0085 (2013.01); F05D 2220/323 (2013.01); F05D 2260/80 (2013.01); G07C 5/08 (2013.01);
Abstract

A computer-implemented method of assessing a health of a gas turbine engine of a hybrid-electric propulsion system for an aircraft includes receiving, by one or more computing devices, data indicative of an amount of electrical power provided to, or extracted from, an electric machine. The method also includes receiving, by the one or more computing devices, data indicative of an operating parameter of the hybrid-electric propulsion system. The method also includes assessing, by the one or more computing devices, a health of the gas turbine engine based at least in part on the received data indicative of the amount of electrical power provided to, or extracted from, the electric machine and the received data indicative of the operating parameter of the hybrid electric propulsion system. The method also includes providing, by the one or more computing devices, information to a user indicative of the health of the gas turbine engine.


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