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:
Jun. 09, 2020

Filed:

Dec. 05, 2017
Applicants:

Airbus Operations Gmbh, Hamburg, DE;

Airbus Operations (S.a.s.), Toulouse, FR;

Inventors:

Jan Barkowsky, Schwerin, DE;

Paul-Emile Roux, Toulouse, FR;

Laurent Duffau, Mons, FR;

Thierry Garcia, Brax, FR;

Charles Renard, Goyrans, FR;

Assignees:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 27/00 (2006.01); F02C 3/04 (2006.01); F02C 9/18 (2006.01); F02C 7/32 (2006.01); F01D 21/00 (2006.01); F04D 15/00 (2006.01); F04D 27/02 (2006.01);
U.S. Cl.
CPC ...
F04D 27/001 (2013.01); F01D 21/003 (2013.01); F02C 3/04 (2013.01); F02C 7/32 (2013.01); F02C 9/18 (2013.01); F04D 15/0088 (2013.01); F04D 27/0223 (2013.01); F05D 2220/323 (2013.01); F05D 2260/80 (2013.01); F05D 2270/101 (2013.01);
Abstract

A method for controlling takeoffs of mechanical energy and/or air on a turbine engine for the propulsion of an aircraft. It is based on a protocol for the exchange of a request/authorization between and by the energy manager and a system for controlling the turbine engine. This protocol is implemented as a result of a modification of the takeoff requirement. It is intended to check whether the surge margin is compatible with the modification of the takeoff requirement and, if the need arises, to apply temporary measures in order to prevent surge in the turbine engine, for example by providing at least a part of the energy requirements by a buffer. This permits the optimization of the operation of a turbine engine for the propulsion of an aircraft, while avoiding the risk of surge of the turbine engine.


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