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:
Jul. 20, 2021

Filed:

Sep. 25, 2019
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Emmanuel Mermoz, Peynier, FR;

Frederic Balayn, Vitrolles, FR;

Xavier Maraninchi, Les Pennes Mirabeau, FR;

Assignee:

Airbus Helicopters, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64D 27/24 (2006.01); B64C 27/08 (2006.01); B64C 27/26 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64D 27/24 (2013.01); B64C 27/08 (2013.01); B64C 27/26 (2013.01); B64C 29/0025 (2013.01); B64C 2201/042 (2013.01); B64C 2201/104 (2013.01); B64C 2201/108 (2013.01);
Abstract

An electrically or hybrid powered multirotor aircraft with complete redundancy on all of its functions of lift, of propulsion, and of control, the aircraft having optimized energy consumption and comprising: a longitudinal structure having two longitudinal beams; a fuselage fastened to the longitudinal structure; two fixed wings serving essentially to provide the aircraft with lift in cruising flight and arranged at respective ends of the longitudinal structure and in a common first plane; at least six rotors serving essentially to provide the aircraft with lift during stages of takeoff and landing, the rotors being arranged in a common second plane distinct from the first plane and parallel to the first plane in such a manner as not to be situated vertically above or below a fixed wing; and two propulsion propellers. An electrical or hybrid power plant serves to drive the rotors and the propulsion propellers in rotation.


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