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. 06, 2025

Filed:

Jun. 27, 2022
Applicants:

Airbus Operations Sas, Toulouse, FR;

Airbus Sas, Blagnac, FR;

Inventors:

Pascal Pome, Toulouse, FR;

Nicolas Jolivet, Toulouse, FR;

Rémi Amargier, Toulouse, FR;

Lionel Czapla, Toulouse, FR;

Franck Alvarez, Toulouse, FR;

Kotaro Fukasaku, Toulouse, FR;

Benoît Penven, Toulouse, FR;

Delphine Jalbert, Blagnac, FR;

Laurent Lafont, Blagnac, FR;

Milan Tasic, Toulouse, FR;

Frédéric Goupil, Toulouse, FR;

Jean-Victor Lapeyre, Marignane, FR;

Emmanuel Mermoz, Marignane, FR;

Assignees:

AIRBUS OPERATIONS SAS, Toulouse, FR;

AIRBUS SAS, Blagnac, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/40 (2023.12); B64D 27/30 (2023.12);
U.S. Cl.
CPC ...
B64D 27/40 (2023.12); B64D 27/30 (2023.12); B64D 27/402 (2023.12);
Abstract

A propulsion unit, and an aircraft, with a propeller and electric motor, including at least one intermediate element interposed between the electric motor and the propeller and configured to transmit at least thrust loads generated by the propeller, a primary structure supporting the propulsion unit, at least one interface having: a first load path, configured to transmit loads perpendicular to the axis of rotation of the propeller, linking the at least one intermediate element to a support linked rigidly to or incorporated in the primary structure, a second load path, configured to transmit loads that are parallel to the axis of rotation of the propeller, linking the at least one intermediate element to a support linked rigidly to or incorporated in the primary structure.


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