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. 30, 2025

Filed:

Apr. 10, 2020
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Vincent Poumarede, Moissy-Cramayel, FR;

Jean-Philippe Jacques Marin, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60L 3/04 (2006.01); B60L 50/10 (2019.01); B64D 27/33 (2024.01); B64D 35/023 (2025.01); F02C 6/20 (2006.01); F02C 9/26 (2006.01); F02C 9/28 (2006.01); F02K 5/00 (2006.01);
U.S. Cl.
CPC ...
B60L 3/04 (2013.01); B60L 50/10 (2019.02); B64D 35/023 (2024.01); F02C 6/20 (2013.01); F02C 9/26 (2013.01); F02C 9/28 (2013.01); F02K 5/00 (2013.01); B64D 27/33 (2024.01);
Abstract

A hybrid propulsion installation for an aircraft, including an internal combustion engine having at least one combustion chamber; at least one electricity generator; an electrical propulsion system; electromechanical protection mechanism arranged between the or each electricity generator and the electrical propulsion system; wherein the installation also includes: an electronic computer configured to: receive at least one piece of information on a position of the electromechanical protection mechanism; receive at least one piece of information on a speed of rotation of a shaft of the internal combustion engine; and control the flow of fuel supplying the combustion chamber depending on the information received.


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