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:
Dec. 19, 2023

Filed:

Nov. 12, 2021
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Loïs Pierre Denis Vive, Moissy-Cramayel, FR;

Olivier Bedrine, Moissy-Cramayel, FR;

Thomas Drouin, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 15/10 (2006.01); F02C 7/32 (2006.01); F02C 7/275 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); F02C 7/275 (2013.01); F02C 7/32 (2013.01); F05D 2220/76 (2013.01); F05D 2260/85 (2013.01);
Abstract

A turbomachine, particularly for a rotary-wing aircraft, including a gas generator provided with a rotary shaft, a first reversible electric machine, a power turbine rotationally driven by a stream of gas generated by the gas generator, at least one accessory from among an oil pump and a fuel pump, an accessory gearbox comprising a gear train configured to drive said at least one accessory, and a second electric machine. The second electric machine is reversible, said first electric machine is mechanically coupled to the gas generator, the accessory gearbox and the second electric machine are mechanically coupled to the power turbine, and the turbomachine is devoid of any kinematic coupling between the gear train of the accessory gearbox and the shaft of the gas generator.


Find Patent Forward Citations

Loading…