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:
Nov. 24, 2015

Filed:

Nov. 26, 2013
Applicants:

Airbus Operations (Sas), Toulouse, FR;

Airbus (Sas), Blagnac, FR;

Inventors:

Jean-Philippe Cottet, Toulouse, FR;

Hubert Patris, Metz, FR;

Manfred Birnfeld, Blagnac, FR;

Philippe Perrin, Toulouse, FR;

Stephan Ducarroir, Lagrace-Dieu, FR;

Assignees:

Airbus Operations (S.A.S.), Toulouse, FR;

Airbus (S.A.S.), Blagnac, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 21/00 (2006.01); B64D 45/00 (2006.01); B64D 43/00 (2006.01); F02C 9/00 (2006.01);
U.S. Cl.
CPC ...
B64D 45/00 (2013.01); B64D 43/00 (2013.01); F02C 9/00 (2013.01); F05D 2260/80 (2013.01); F05D 2260/85 (2013.01);
Abstract

A method and device for aiding the monitoring of a turbine engine of an aircraft, which displays on one and the same indicator of a of a display indication elements illustrating as a percentage the engine start progression or the current sub-idle state of the turbine engine, a margin to a limit temperature of the turbine engine, a margin to a maximum temperature of the turbine engine and a margin to a possible failure of the start that is generated by a too low speed increase of the turbine engine.


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