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. 14, 2017

Filed:

Jan. 27, 2016
Applicant:

Airbus Helicopters, Marignane, FR;

Inventors:

Jean-Baptiste Vallart, Aix en Provence, FR;

Setareh Taheri, Aix en Provence, FR;

Samuel Leyder, Velaux, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01M 15/14 (2006.01); B64D 45/00 (2006.01); B64C 27/12 (2006.01); B64D 31/06 (2006.01); B64C 27/08 (2006.01); G01M 13/02 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B64C 27/08 (2013.01); B64C 27/12 (2013.01); B64D 31/06 (2013.01); G01M 13/02 (2013.01); B64C 27/82 (2013.01);
Abstract

A method of monitoring a power transmission system of an aircraft, the aircraft including at least one main rotor driven in rotation by a rotor mast and an auxiliary unit having an auxiliary rotor. Control means control the auxiliary rotor. A power relationship is determined providing a first reduced power parameter of the auxiliary unit as a function of a position (POS) of the control means. A setpoint limit is set for a second power parameter for the rotor mast. A current position (POSACTU) of the control means is determined and a calculated value (Vcal) is also determined at least by applying the current position (POSACTU) to the power relationship. A limit value that is not to be exceeded by a power plant is determined, with the limit value being equal to the sum at least of the setpoint limit plus the calculated value.


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