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:
Jul. 04, 2023

Filed:

Oct. 22, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Gilles Alain Marie Charier, Moissy-Cramayel, FR;

Caroline Marie Frantz, Moissy-Cramayel, FR;

Loïc Paul Yves Guillotel, Moissy-Cramayel, FR;

Vincent François Georges Millier, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 15/10 (2006.01); F02C 7/32 (2006.01); F02K 3/06 (2006.01); H02K 7/18 (2006.01); H02K 9/14 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); F02C 7/32 (2013.01); F02K 3/06 (2013.01); H02K 7/1823 (2013.01); H02K 9/14 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2260/232 (2013.01); F05D 2260/30 (2013.01);
Abstract

An aircraft turbine engine includes a gas generator and a fan arranged upstream from the gas generator and configured to generate a main gas flow, one portion of which flows in a flow path of the gas generator to form a primary flow, and another portion of which flows in a flow path around the gas generator to form a secondary flow. The gas generator includes a low-pressure compressor that includes a rotor driving the fan. The turbine engine further includes an electric machine. The electric machine includes a rotor rotated by the rotor of the low-pressure compressor, and a stator extending around the rotor of the electric machine and configured to be cooled by the primary flow.


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