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:
Aug. 31, 2021

Filed:

Aug. 19, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Lawrence Chih-hui Cheung, Niskayuna, NY (US);

Nikolai N. Pastouchenko, Glenville, NY (US);

Kishore Ramakrishnan, Rexford, NY (US);

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

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/58 (2006.01); B64D 27/24 (2006.01); B64D 33/08 (2006.01); B64C 21/06 (2006.01); F04D 25/06 (2006.01); H02K 7/18 (2006.01); H02K 9/19 (2006.01); H02K 7/14 (2006.01); F04D 25/02 (2006.01); B64D 33/10 (2006.01); B64D 27/20 (2006.01); B64D 29/04 (2006.01); B64D 33/02 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
F04D 29/5806 (2013.01); B64C 21/06 (2013.01); B64D 27/20 (2013.01); B64D 27/24 (2013.01); B64D 29/04 (2013.01); B64D 33/02 (2013.01); B64D 33/08 (2013.01); B64D 33/10 (2013.01); F04D 25/02 (2013.01); F04D 25/06 (2013.01); H02K 7/14 (2013.01); H02K 7/1823 (2013.01); H02K 9/19 (2013.01); B64C 2230/04 (2013.01); B64D 2027/026 (2013.01); F05B 2220/706 (2013.01);
Abstract

A propulsion system for an aircraft includes an electric propulsion engine configured to be mounted at an aft end of the aircraft. The electric propulsion engine includes an electric motor and a fan rotatable about a central axis, the fan driven by the electric motor. The electric propulsion system additionally includes a cooling system operable with an airflow over the aft end the aircraft when the electric propulsion system is mounted to the aircraft. The cooling system is configured to cool the electric motor during operation of the electric propulsion engine.


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