Method and device for implementing the thrust reversers of...

F - Mech Eng,Light,Heat,Weapons – 02 – C

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F02C 9/00 (2006.01) F02K 1/76 (2006.01)

Patent

CA 2721378

Method and device for implementing the thrust reversers of an aircraft. According to the invention, the following successive steps are carried out automatically: deployment (E3) of the previously armed thrust reversers of the aircraft; application (E5) of a predetermined engine speed; reduction (E6) of the engine speed; - re-furling (E7) of the thrust reversers of the aircraft.

Procédé et dispositif de mise en oeuvre des inverseurs de poussée d'un aéronef. Selon l'invention, les étapes successives suivantes sont automatiquement effectuées :.cndot. déploiement (E3) des inverseurs de poussée de l'aéronef préalablement armés; .cndot. application (E5) d'un régime prédéterminé aux moteurs; réduction (E6) du régime des moteurs; - repliement (E7) des inverseurs de poussée de l'aéronef.

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