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:
Nov. 11, 2025

Filed:

Oct. 25, 2021
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Loïs Pierre Denis Vive, Moissy-Cramayel, FR;

Thomas Drouin, Moissy-Cramayel, FR;

Olivier Bedrine, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); B64D 41/00 (2006.01); F01D 15/10 (2006.01); F02C 3/10 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); B64D 41/00 (2013.01); F02C 3/10 (2013.01); F02C 7/36 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01);
Abstract

Disclosed is a turbogenerator, in particular for an electrically-driven rotary wing aircraft, comprising a gas generator equipped with a first shaft, at least one reversible electrical machine, and a free turbine provided with a second shaft and caused to rotate by a gas flow generated by the gas generator. The second shaft is coupled to the at least one electrical machine during all phases of operation of the turbomachine, and the turbomachine further comprises a single mechanical coupling means for coupling the first mechanical shaft to the second mechanical shaft when the electrical machine is operating in motor mode and mechanically uncoupling the first mechanical shaft from the second mechanical shaft when the electrical machine is operating in generator mode.


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