Latecoere

Didier Molinari

Christian Romec

Patrick Lamat

Device for opening an aircraft door in emergencies, said door being provided with an opening mechanism, including a device () for actuating the opening mechanism, having: a tubular maneuvering member (), and a second locking end () which has a stop surface (); resilient compression device (); a member for holding the second locking end (), the holding member including a rotary lock () and a lever () which is suitable for cooperating with the stop surface (), the rotary lock () being rotatable about the displacement axis of the maneuvering member (); device () for activating the actuation device () which are suitable for driving the rotary lock ().

Device for opening an aircraft door in emergencies, said device having a lever-type retention member

An emergency opening device for an aircraft door provided with an opening mechanism including an actuating device () for the opening mechanism, which includes a tubular operating member (); elastic compression device (); an activation device () for the actuation device (); the operating member () includes a first end element () and a second end element () which are freely translatable movable relative to each other along the movement axis (X).

Emergency opening device for an aircraft door, comprising a telescopic operating member

The invention relates to a guard for the upper part of a door () of an aircraft, consisting of: a composite comprising a composite and/or stainless steel strip () which forms the core of the guard () and which renders same flexible and resistant, a silicon which is optionally reinforced with fibres and a polyester.

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Toulouse, France

Didier Molinari