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:
Dec. 20, 2016

Filed:

Jun. 12, 2014
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Benoit Domingo, Aix en Provence, FR;

Guillaume Dumur, Salon de Provence, FR;

Stephane Bailly, Cabries, FR;

Assignee:

Airbus Helicopters, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/06 (2006.01); F01D 21/02 (2006.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); F01D 21/02 (2013.01); F05D 2220/329 (2013.01); F05D 2270/331 (2013.01); Y02T 50/671 (2013.01);
Abstract

A method of stopping an overspeeding engine () of a rotorcraft (). A protection device stops the overspeeding engine () on condition of a comparison between a mechanical power requirement () of the rotorcraft () and a predefined power threshold (). Stopping of the overspeeding engine () is authorized by the protection device () on condition that said mechanical power requirement () is identified as being less than or equal to the predefined power threshold (). The mechanical power requirement () of the rotorcraft () is calculated on the basis of at least one current or anticipated value for the opposing torque () of a main rotor () of the rotorcraft.


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