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:
Jun. 01, 2021

Filed:

Mar. 31, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Jeffrey Lynn Duce, Maple Valley, WA (US);

Kent E. Karnofski, Lake Forest Park, WA (US);

Stephen D. Oehler, Maple Valley, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/36 (2006.01); F02C 7/36 (2006.01); F01D 25/24 (2006.01); B64D 27/18 (2006.01); B64D 31/06 (2006.01); H02K 7/18 (2006.01); F01D 15/10 (2006.01);
U.S. Cl.
CPC ...
F01D 25/36 (2013.01); B64D 27/18 (2013.01); B64D 31/06 (2013.01); F01D 15/10 (2013.01); F01D 25/24 (2013.01); F02C 7/36 (2013.01); H02K 7/1823 (2013.01); B64D 2221/00 (2013.01); F05D 2220/768 (2013.01); F05D 2260/4031 (2013.01); Y02T 50/60 (2013.01);
Abstract

A method of integrating an electric motor or generator as part of an aircraft engine shaft. The motor is used to rotate the rotor so as to cool the rotor in a temperature gradient. The generator is used to provide power to the aircraft. In one or more examples, a power generation device includes a gas turbine engine including a rotor shaft and a first casing around the rotor shaft; a transmission connecting the rotor shaft to a gearbox, the transmission comprising a drive shaft and a second casing around the drive shaft; and a brushless DC motor integrated with the engine and including one or more permanent magnets and one or more coils.


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