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:
Oct. 19, 2021

Filed:

Feb. 10, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Narendra Digamber Joshi, Niskayuna, NY (US);

Michael Solomon Idelchik, Niskayuna, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 15/10 (2006.01); B64D 27/18 (2006.01); B64D 27/24 (2006.01); F02C 7/32 (2006.01); F02C 6/14 (2006.01); F02K 3/06 (2006.01); F02K 5/00 (2006.01); F02C 7/36 (2006.01); F02C 6/00 (2006.01); B64D 27/02 (2006.01); B64C 11/30 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); B64D 27/02 (2013.01); B64D 27/18 (2013.01); B64D 27/24 (2013.01); F02C 6/00 (2013.01); F02C 6/14 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F02K 5/00 (2013.01); B64C 11/30 (2013.01); B64D 2027/026 (2013.01); F05D 2220/323 (2013.01); F05D 2220/36 (2013.01); F05D 2220/76 (2013.01);
Abstract

A propulsion system for an aircraft includes a turbomachine, a primary fan, and an electric machine. The turbomachine includes a first turbine and a second turbine, with at least one of the first turbine or second turbine operably connected to the electric machine and the second turbine driving the primary fan. The propulsion system additionally includes an auxiliary propulsor assembly configured to be mounted at a location away from the turbomachine and the primary fan. The electric machine is in electrical communication with the auxiliary propulsor assembly for transferring power with the auxiliary propulsor assembly during operation of the propulsion system.


Find Patent Forward Citations

Loading…