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:
Apr. 25, 2023

Filed:

Mar. 11, 2021
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Paul Eglin, Roquefort la Bedoule, FR;

Remy Huot, Marseilles, FR;

Antoine Conroy, Vitrolles, FR;

Assignee:

AIRBUS HELICOPTER, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 13/18 (2006.01); B64C 5/10 (2006.01); B64C 11/30 (2006.01); B64C 13/24 (2006.01); B64C 11/00 (2006.01); B64C 27/06 (2006.01);
U.S. Cl.
CPC ...
B64C 13/18 (2013.01); B64C 5/10 (2013.01); B64C 11/00 (2013.01); B64C 11/30 (2013.01); B64C 13/24 (2013.01); B64C 27/06 (2013.01);
Abstract

A method for optimizing the operation of at least one first propeller and of at least one second propeller of a hybrid helicopter. The method comprises the following step during a control phase: deflection, with an autopilot system, of at least one aerodynamic stabilizer member into a setpoint position having, with respect to a reference position, a target deflection angle that is a function of a setpoint deflection angle, the setpoint deflection angle being calculated by the autopilot system in order to compensate for a torque exerted by the lift rotor at zero sideslip.


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