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. 14, 2021

Filed:

Feb. 14, 2018
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Romain Thiriet, Moissy-Cramayel, FR;

Jean Michel Bazet, Moissy-Cramayel, FR;

Jean-Luc Charles Gilbert Frealle, Moissy-Cramayel, FR;

Pierre Darfeuil, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 13/24 (2006.01); B64C 27/06 (2006.01); B64C 27/57 (2006.01); B64D 31/06 (2006.01);
U.S. Cl.
CPC ...
B64C 27/006 (2013.01); B64C 13/24 (2013.01); B64C 27/008 (2013.01); B64C 27/06 (2013.01); B64C 27/57 (2013.01); B64D 31/06 (2013.01);
Abstract

The invention relates to a method for controlling an emergency device of a helicopter, said helicopter comprising a rotor suitable for being rotated, said emergency device being suitable for supplying additional emergency propulsion power to the helicopter, in said method comprising a step () of measuring the rotation speed of the helicopter rotor, a step () of calculating the drift of the measured rotation speed, a step () of continuously verifying conditions such that the speed of rotation of the rotor is higher than a predetermined value, referred to as arming speed, and the drift of the rotation speed is lower than a predetermined value, referred to as arming drift, and a step () of activating the emergency device if the verified conditions are validated.


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