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:
Nov. 01, 2022

Filed:

Apr. 14, 2021
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Guillaume Dumur, Salon de Provence, FR;

Francois-Xavier Gaulmin, Salon de Provence, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); F01D 21/02 (2006.01); B64C 19/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/006 (2013.01); B64C 19/00 (2013.01);
Abstract

A method for stopping an engine of a rotorcraft in overspeed, the rotorcraft comprising at least one engine, the engine comprising a gas generator and a power assembly, the power assembly comprising at least one power turbine rotated by gases originating from the gas generator, the power assembly comprising at least one power shaft rotationally secured to the power turbine, the power assembly rotating about a longitudinal axis at a speed referred to as the 'speed of rotation'. The method comprises steps consisting in measuring a current value of the speed of rotation, determining a time derivative of the current value of the speed of rotation, referred to as the 'current derivative and automatically stopping the engine when the current derivative changes sign.


Find Patent Forward Citations

Loading…