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. 18, 2022

Filed:

Sep. 28, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Gert Johannes van der Merwe, Lebanon, OH (US);

Daniel Alan Niergarth, Cincinnati, OH (US);

Peter David Toot, Mason, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 15/10 (2006.01); F04D 19/02 (2006.01); F01D 5/06 (2006.01); F01D 15/12 (2006.01); F01D 25/16 (2006.01); F01D 25/28 (2006.01); F02C 3/113 (2006.01); F02C 7/36 (2006.01); F16H 1/28 (2006.01); F16D 41/069 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); F01D 5/06 (2013.01); F01D 15/12 (2013.01); F01D 25/16 (2013.01); F01D 25/28 (2013.01); F02C 3/113 (2013.01); F02C 7/36 (2013.01); F04D 19/02 (2013.01); F05D 2220/32 (2013.01); F05D 2260/4023 (2013.01); F05D 2260/40311 (2013.01); F16D 41/069 (2013.01); F16H 1/28 (2013.01); Y02T 50/60 (2013.01);
Abstract

A gas turbine engine includes a compressor section and a turbine section. A first spool is rotatable with a first turbine of the turbine section and a first compressor of the compressor section. Additionally, a second spool is rotatable with a second turbine of the turbine section and a second compressor of the compressor section. An electric machine is positioned at least partially inward of the core air flowpath of the gas turbine engine along a radial direction of the gas turbine engine. Additionally, the exemplary gas turbine engine includes a gear assembly mechanically coupled to both the first spool and the second spool, such that the first and second spools may each drive the electric machine.


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