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:
Aug. 05, 2014

Filed:

Sep. 12, 2006
Applicants:

Franck Delaplace, Toulouse, FR;

Didier Ronceray, Pibrac, FR;

Jean Muller, Tournefeuille, FR;

Inventors:

Franck Delaplace, Toulouse, FR;

Didier Ronceray, Pibrac, FR;

Jean Muller, Tournefeuille, FR;

Assignee:

Airbus Operations SAS, Toulouse, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01C 23/00 (2006.01); B64D 31/08 (2006.01); B64D 31/06 (2006.01); B64D 31/10 (2006.01); G05D 1/00 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 31/08 (2013.01); B64D 31/06 (2013.01); B64D 31/10 (2013.01); B64D 27/02 (2013.01); B64D 2700/62938 (2013.01); G05D 1/0072 (2013.01);
Abstract

An energy protecting device for three and four-engined aircraft includes a detecting unit configured to detect failure of each engine. A control unit is configured to provide a protective function by controlling maximum thrust of each engine. A triggering unit is configured to monitor a plurality of parameters and trigger the control unit to provide maximum thrust at predetermined conditions of the monitored parameters. An inhibiting unit is linked to the triggering unit and is configured to inhibit the protective function, when at least one of the engine on the wings of the aircraft has failed. The control unit is also configured to control the engines that have not failed to minimize thrust imbalance.


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