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:
Jan. 24, 2023

Filed:

Dec. 05, 2019
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Elio Zoppitelli, Cabries, FR;

Michel Jamot, Aix en Provence, FR;

Jeremy Camus, Ensues la Redonne, FR;

Olivier Maegey, Aix en Provence, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/12 (2006.01); B64F 5/60 (2017.01); B60L 50/60 (2019.01); B64C 27/08 (2006.01); B64D 27/02 (2006.01); B64D 27/10 (2006.01); B64D 27/24 (2006.01); B64D 35/04 (2006.01); B64C 27/00 (2006.01); H02P 1/46 (2006.01); B64D 45/00 (2006.01); H02P 101/30 (2015.01);
U.S. Cl.
CPC ...
B64D 31/12 (2013.01); B60L 50/60 (2019.02); B64C 27/006 (2013.01); B64C 27/08 (2013.01); B64D 27/02 (2013.01); B64D 27/10 (2013.01); B64D 27/24 (2013.01); B64D 35/04 (2013.01); B64F 5/60 (2017.01); H02P 1/46 (2013.01); B60L 2200/10 (2013.01); B64D 2027/026 (2013.01); B64D 2045/0085 (2013.01); H02P 2101/30 (2015.01);
Abstract

An assistance method for assisting a pilot of a single-engined rotary-wing aircraft during a flight phase in autorotation, the aircraft including a hybrid power plant provided with a main engine, with an electric machine, with a main gearbox, and with an electrical energy storage device. The aircraft also includes a main rotor driven by the hybrid power plant. In the method, during a flight, operation of the main engine is monitored in order to detect a failure, in particular by means of a drop in power on the main rotor, then, when a failure of the main engine is detected, the electric machine is controlled to deliver auxiliary power We to the main rotor, making it possible to assist a pilot of the aircraft in performing the flight phase in autorotation following the failure.


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