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:
Mar. 09, 2021

Filed:

Oct. 15, 2019
Applicant:

Airbus Helicopters, Marignane, FR;

Inventor:

Alban Corpron, Salon de Provence, FR;

Assignee:

AIRBUS HELICOPTERS, Marignane, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); B64D 31/00 (2006.01); F02C 9/28 (2006.01); B64C 27/04 (2006.01); B64C 27/14 (2006.01); B64D 27/10 (2006.01); F02C 3/04 (2006.01);
U.S. Cl.
CPC ...
F02C 9/00 (2013.01); B64C 27/04 (2013.01); B64C 27/14 (2013.01); B64D 27/10 (2013.01); B64D 31/00 (2013.01); F02C 3/04 (2013.01); F02C 9/28 (2013.01); F05D 2220/329 (2013.01); F05D 2220/76 (2013.01); F05D 2220/90 (2013.01); F05D 2270/02 (2013.01); F05D 2270/023 (2013.01);
Abstract

A regulator device for automatically regulating a power plant of a rotary wing aircraft having a turbine engine includes a computer system. The computer system, while implementation of an idling mode of operation of the turbine engine is requested and the aircraft is standing on ground, implements the idling mode of operation and operates the turbine engine in compliance with idling mode of operation as a function of operational and hierarchically ordered conditions either through a first mode of regulation by regulating a speed of rotation (Ng) of a gas generator of the turbine engine or through a second mode of regulation by regulating a speed of rotation (NTL) of a free turbine of the turbine engine.


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