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. 25, 2025

Filed:

Nov. 17, 2022
Applicants:

Airbus Helicopters, Marignane, FR;

Airbus Helicopters Deutschland Gmbh, Donauworth, DE;

Inventors:

Jerome Geneix, Miramas le Vieux, FR;

Mikolaj Luszczynski, Lodz, PL;

Assignees:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/30 (2006.01); B64C 27/12 (2006.01); B64C 27/26 (2006.01); B64C 29/00 (2006.01); B64D 35/024 (2024.01); H01M 10/46 (2006.01); H02K 7/14 (2006.01);
U.S. Cl.
CPC ...
B64C 27/26 (2013.01); B64C 27/12 (2013.01); B64C 27/30 (2013.01); B64C 29/0025 (2013.01); B64D 35/024 (2024.01); H01M 10/46 (2013.01); H02K 7/14 (2013.01); B60L 2200/10 (2013.01); H01M 2220/20 (2013.01);
Abstract

A rotary wing aircraft that extends along a roll axis between a nose region and an aft region, comprising: at least one first single-blade rotor and at least one second single-blade rotor which are spaced apart from each other along the roll axis; at least one first electric machine and at least one second electric machine which are at least configured to drive in motor mode the at least one first single-blade rotor and the at least one second single-blade rotor for generating lift in hover condition of the rotary wing aircraft; at least one propulsion device that is at least configured to generate forward thrust in forward flight condition of the rotary wing aircraft; and a fixed-wing arrangement that is at least configured to provide lift in the forward flight condition.


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