Turbojet nacelle hood locking mechanism

Details Turbojet nacelle hood locking mechanism Turbojet nacelle hood locking mechanism

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/24 (2006.01) B64D 29/06 (2006.01) E05C 3/06 (2006.01) E05C 19/14 (2006.01) E05B 15/00 (2006.01) E05B 63/24 (2006.01)

Patent

CA 2472876

Turbojet cowl doors have bottom longitudinal edges fitted with hooking means and with locking means which comprise catches fixed on a rotary drive shaft carried by one of the doors and which co-operate with hooking members hinged about an axis on the other one of the doors. The invention relates to apparatus for locking the cowl doors of a turbojet.

Capots de nacelle de turboréacteur dont les bords longitudinaux inférieurs sont équipés de moyens d'accrochage et de verrouillage qui comprennent des loquets fixés sur un arbre d'entraînement en rotation porté par l'un des capots et qui coopèrent avec des organes d'accrochage montés articulés autour d'un axe sur l'autre des capots.

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