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:
Jan. 10, 2023

Filed:

Feb. 07, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventor:

Cedrik Djelassi, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/58 (2006.01); B64C 11/30 (2006.01); B64D 27/10 (2006.01); B64D 27/00 (2006.01);
U.S. Cl.
CPC ...
F02C 9/58 (2013.01); B64C 11/305 (2013.01); B64D 27/10 (2013.01); B64D 2027/005 (2013.01); F05D 2260/77 (2013.01); F05D 2270/024 (2013.01);
Abstract

The invention relates to a method for controlling the speed and the power of a turbine engine propeller, wherein at least two operating modes are implemented: —one operating mode, called 'speed mode', in which the pitch (β) of the propeller is controlled as a function of the desired propeller speed, while the fuel flow is controlled as a function of the desired torque; the other operating mode, called 'β mode', in which the fuel flow is controlled as a function of the desired propeller speed, the pitch (β) of the propeller being set to a limit angle (βmin) that limits the pitch of the propeller in the two operating modes, the pitch angle (βmin(t)) being continuously computed and updated during a flight on the basis of parameters relating to the flight conditions estimated in real time.


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