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:
Aug. 06, 2024

Filed:

Nov. 05, 2020
Applicant:

Safran, Paris, FR;

Inventors:

Remy Biaujaud, Moissy-Cramayel, FR;

Rene Meunier, Moissy-Cramayel, FR;

Jerome Didier Mora, Moissy-Cramayel, FR;

Florent Rougier, Moissy-Cramayel, FR;

Jerome Valire, Moissy-Cramayel, FR;

Assignee:

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2024.01); B64C 29/00 (2006.01); B64D 27/02 (2006.01); H02J 1/10 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 29/0008 (2013.01); B64D 27/026 (2024.01); H02J 1/10 (2013.01);
Abstract

The invention relates to a hybrid propulsion architecture () for an aircraft, comprising: —a first source () of a first energy type, —second sources () of a second energy type different from the first energy type, —electrical propulsion systems (), —an electric power supply network () connecting the first and second sources () to the electrical propulsion systems, such that each electrical propulsion system is powered by the first source and by one of the second sources, the architecture being characterised in that it further comprises: —means for segregating () the electrical propulsion systems, which means are arranged in the electric power supply network and configured to impose a direction of flow of the electric power from the first source to the electrical propulsion systems.


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