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. 08, 2023

Filed:

Nov. 13, 2020
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Jacques Bellera, Aix en Provence, FR;

Nicolas Queiras, Les Pennes Mirabeau, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 27/57 (2006.01); B64C 13/04 (2006.01); B64C 9/00 (2006.01); B64C 25/36 (2006.01); B64C 25/52 (2006.01); B64C 27/06 (2006.01); B64C 27/08 (2023.01); B64C 27/82 (2006.01); G05D 1/08 (2006.01);
U.S. Cl.
CPC ...
B64C 27/57 (2013.01); B64C 9/00 (2013.01); B64C 13/0421 (2018.01); B64C 25/36 (2013.01); B64C 25/52 (2013.01); B64C 27/06 (2013.01); B64C 27/08 (2013.01); B64C 27/82 (2013.01); G05D 1/0858 (2013.01);
Abstract

A method and a system for providing a rotorcraft with assistance in taking off from a slope. The rotorcraft includes at least one lift rotor provided with a plurality of blades, control devices for controlling the pitches of the blades, and landing gear provided with at least three ground contact members. The method comprises a step of measuring a piece of information relating to the forces to which each ground contact member is subjected during a landing phase for landing on the slope, a step of measuring at least one piece of information relating to the pitches of the blades during the landing phase, and a control step for controlling the pitches of the blades during the takeoff phase during which the rotorcraft takes off after the landing as a function of the measurements taken during the landing in order to enable a takeoff to be performed that is safe and simplified.


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