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. 25, 2024

Filed:

Nov. 24, 2020
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Vincent François Georges Millier, Moissy-Cramayel, FR;

Loïc Paul Yves Guillotel, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); B64D 27/16 (2006.01); B64D 27/24 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); B64D 27/16 (2013.01); B64D 27/24 (2013.01); B64D 27/026 (2024.01); B64D 2221/00 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01);
Abstract

An aircraft turbine engine includes a gas generator having a longitudinal axis (A), a fan located at an upstream end of the gas generator and configured to turn about said axis, and an electric machine of generally annular shape. The electric machine is coaxially mounted downstream of the fan and has a rotor coupled to rotate with the fan. The electric machine further includes a stator connected to an electronic power circuit by at least one rigid electrically-conductive bar.


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