Locking/unlocking device for a one-piece cover of a thrust reverser of a turbojet engine nacelle

The present invention relates to an assembly for a turbojet engine, comprising a pylon and a nacelle, said nacelle being supported by said pylon and surrounding the turbojet engine in such a way as to define a circulation duct (51) for a secondary air flow and comprising a thrust reversing device co...

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Bibliographische Detailangaben

Hauptverfasser:	JEAN MICHEL, THOUEMENT JEAN-FRANCOIS, PUJOL REMI, CONET OLIVIER
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS HEATING HELICOPTERS HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
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