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:
Jun. 13, 2023

Filed:

Dec. 04, 2020
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Paul Eglin, Roquefort la Bedoule, FR;

Remy Huot, Marseilles, FR;

Antoine Conroy, Vitrolles, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); B64C 27/06 (2006.01); B64C 27/56 (2006.01); B64D 27/02 (2006.01); B64D 31/14 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64C 27/06 (2013.01); B64C 27/56 (2013.01); B64D 27/02 (2013.01); B64D 31/14 (2013.01); B64D 2027/026 (2013.01);
Abstract

The present invention relates to a control method in case of engine failure of a hybrid helicopter having a power plant connected to at least one lift rotor and to at least one propeller, said lift rotor having a plurality of first blades and said at least one propeller having a plurality of second blades. The method comprises the following steps: (i) measuring a forward speed of the hybrid helicopter, (ii) on condition that said forward speed is greater than a first speed threshold and that each engine has failed, automatically implementing a first emergency piloting mode comprising a step for automatic reduction by an automatic piloting system of a pitch of said second blades toward an objective pitch making said at least one propeller produce a motive power which is transmitted to the lift rotor.


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