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:
Dec. 23, 2014

Filed:

Jun. 05, 2012
Applicants:

Patrick Jegu, Toulouse, FR;

Manfred Birnfeld, Blagnac, FR;

Inventors:

Patrick Jegu, Toulouse, FR;

Manfred Birnfeld, Blagnac, FR;

Assignee:

Airbus Operations (SAS), Toulouse Cedex, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G06F 19/00 (2011.01); F01D 21/00 (2006.01); F02C 7/262 (2006.01); F02C 9/00 (2006.01);
U.S. Cl.
CPC ...
F01D 21/003 (2013.01); F02C 7/262 (2013.01); F02C 9/00 (2013.01); F05D 2220/323 (2013.01); F05D 2260/80 (2013.01); F05D 2270/092 (2013.01); F05D 2270/303 (2013.01); Y02T 50/671 (2013.01);
Abstract

A method and device aids in monitoring at least one turbine engine in an aircraft. The method includes determining a value illustrating a thermomechanical state of the turbine engine, and comparing the determined value with at least one threshold. The method also includes displaying in the cockpit of the aircraft, at least one indication related to the operation of the turbine engine, according to this comparison. As a result, conditions that could result in mechanical degradation or failure of the turbine engine are identified for a crew of the aircraft.


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