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:
Aug. 25, 2020

Filed:

Dec. 08, 2017
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Setareh Taheri, Aix en Provence, FR;

Nicolas Certain, Aix en Provence, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/12 (2006.01); F02C 9/28 (2006.01); B64D 31/06 (2006.01); B64C 27/57 (2006.01); F02C 9/00 (2006.01); F02C 3/10 (2006.01);
U.S. Cl.
CPC ...
B64C 27/12 (2013.01); B64C 27/57 (2013.01); B64D 31/06 (2013.01); F02C 3/10 (2013.01); F02C 9/00 (2013.01); F02C 9/28 (2013.01); F02D 2200/101 (2013.01); F02D 2200/1002 (2013.01); F02D 2200/501 (2013.01); F02D 2250/18 (2013.01); F05D 2220/329 (2013.01); F05D 2270/02 (2013.01); F05D 2270/052 (2013.01);
Abstract

A regulator device for regulating a speed of rotation, of a shaft of a gas generator of at least one turboshaft engine of a rotorcraft. The rotorcraft has at least one main rotor for regulating at least lift and/or propulsion for said rotorcraft in the air; a control member for controlling a collective pitch of the blades of said at least one main rotor, said control member serving to generate a control setpoint for said collective pitch; at least one turboshaft engine suitable for driving rotation of said at least one main rotor, said at least one engine producing, at least temporarily, a drive torque that is transmitted to said at least one main rotor; and measurement means for taking at each instant a measurement of said drive torque transmitted by said at least one engine to said at least one main rotor.


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