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:
Oct. 04, 2022

Filed:

Mar. 30, 2018
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventors:

Pierre Darfeuil, Moissy-Cramayel, FR;

Patrick Marconi, Moissy-Cramayel, FR;

Caroline Seve, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/42 (2006.01); B64D 27/10 (2006.01); B64D 31/02 (2006.01); F02C 6/20 (2006.01);
U.S. Cl.
CPC ...
F02C 9/42 (2013.01); B64D 27/10 (2013.01); B64D 31/02 (2013.01); F02C 6/20 (2013.01); F05D 2220/329 (2013.01); F05D 2270/053 (2013.01); F05D 2270/093 (2013.01);
Abstract

A method for checking the maximum available power of a turbine engine of an aircraft equipped with two turbine engines configured to operate in parallel and together to supply a necessary power to the aircraft during a flight phase includes: placing one of the turbine engines in a maximum take-off power regime, and adjusting a power supplied by the other turbine engine, such that the turbine engines continue to supply the necessary power to the aircraft during the flight phase; determining a power supplied by the turbine engine placed in the maximum take-off power regime, and processing the supplied power determined in this way, in order to deduce a piece of information relating to the maximum available power.


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