The present disclosure provides an electric thrust reverser system for an aircraft engine nacelle, including a mechanism for actuating a thrust reverser mechanism. The actuating mechanism includes a first drive cylinder and a second drive cylinder. Each cylinder includes a mechanical connection casing, a primary lock (8) and a movable rod secured to a point connected to the associated thrust reverser mechanism. A motor-actuated drive unit is mechanically connected, via flexible shafts, to the mechanical connection casings of each drive cylinder and set in motion by the command of a control unit via an electrical connection. A tertiary lock is disposed for securing the associated thrust reverser mechanism, to a fixed structure of the nacelle.
SYSTÈME D'INVERSEUR DE POUSSÉE ÉLECTRIQUE POUR NACELLE DE MOTEUR D'AÉRONEF ET NACELLE DE MOTEUR D'AÉRONEF AINSI ÉQUIPÉE
ELECTRIC THRUST REVERSER SYSTEM FOR AN AIRCRAFT ENGINE NACELLE AND AIRCRAFT ENGINE NACELLE PROVIDED WITH SAME
ELEKTRISCHES SCHUBUMKEHRSYSTEM FÜR EINE TRIEBWERKSGONDEL UND TRIEBWERKSGONDEL DAMIT
2019-03-06
Patent
Electronic Resource
French
IPC: | F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge / B66F HOISTING, LIFTING, HAULING, OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD , Hub-, Verhol- oder Schubvorrichtungen, soweit nicht anderweitig vorgesehen, z.B. Vorrichtungen mit unmittelbarer Krafteinwirkung auf die Last / F16H Getriebe , GEARING |
SYSTÈME DE PROTECTION CONTRE LE GIVRE POUR NACELLE DE MOTEUR D'AÉRONEF
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|SYSTEME DE PROTECTION CONTRE LE GIVRE POUR NACELLE DE MOTEUR D'AERONEF
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