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:
May. 20, 2025

Filed:

Apr. 10, 2020
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Lois Pierre Denis Vive, Moissy-Cramayel, FR;

Thomas Klonowski, Moissy-Cramayel, FR;

Camel Serghine, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H02J 3/36 (2006.01); B64C 27/08 (2023.01); B64D 27/02 (2006.01); B64D 27/24 (2024.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 27/08 (2013.01); H02J 3/36 (2013.01); B64D 27/026 (2024.01); B64D 2221/00 (2013.01); H02J 2310/44 (2020.01);
Abstract

A hybrid propulsion system for a multi-rotor rotary-wing aircraft, including: an internal combustion engine, an electric machine coupled to the internal combustion engine, a rectifier connected to the electric machine, a converter, an electric network connecting the rectifier to the converter, electric motors connected to the converter, rotary-blade assemblies coupled to the electric motors, wherein the system includes: a detector configured to detect a reduction in a demand for electrical power within the system to below a predetermined value, a bypass circuit configured to bypass the electric machine when the detector detects a reduction in the demand for electrical power.


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