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:
Feb. 20, 2024

Filed:

Jul. 08, 2020
Applicant:

Safran, Paris, FR;

Inventors:

Clélia Level, Moissy-Cramayel, FR;

Christophe Maury, Moissy-Cramayel, FR;

René Meunier, Moissy-Cramayel, FR;

Bruno Thoraval, Moissy-Cramayel, FR;

Assignee:

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64C 29/00 (2006.01); B64D 31/00 (2006.01); B64D 35/06 (2006.01); B64D 35/08 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 29/00 (2013.01); B64D 31/00 (2013.01); B64D 35/06 (2013.01); B64D 35/08 (2013.01);
Abstract

An electric propulsion architecture for a multi-rotor vertical take-off and landing aircraft includes four electric generators; and four pairs of rotors. For each rotor, a first electric motor is configured to operate in an active mode, and a second electric motor is configured to be in a standby mode and being able to operate in an active mode in a breakdown situation. A propeller is coupled to the electric motors, wherein, for each pair of rotors, one of the electric generators powers the first electric motors, and another of the electric generators powers the second electric motors. The rotors form counter-rotors and for each counter-rotor, the electric motors are each powered by one of the four electric generators so that the four electric generators power the electric motors of the rotors of each counter-rotor.


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