Other

Latecoere

Latelec

Amalric, Bernard

Cannac, Frederic

Taillefer, Jean-Paul

Sauvager, Christophe

Bonnafous, Nicolas

Bernard Amalric

Cyrille Bessettes

Bastien Puertolas

Christophe Perrier

Cyrille Delame

Gerard Boucourt

Vincent Banasiak

Bertrand Florentz

Antoine Torris

Olivier Come

Damien Morrison

Martial Grimm

Jean Charles Bernadac

Olivier Escalaup

Philippe Gri

Frédéric Cannac

Jean-Paul Taillefer

The invention aims to make aircraft doors easier to open by preventing ice formation or, at the very least, favoring rapid breaking of the ice on the door edges connected to the skin of the fuselage. To that end, it is provided to supply energy along the door when specific conditions are met. According to one embodiment, an anti-icing/de-icing system for an aircraft door () according to the invention includes an excitation energy source and devices (to) for dissipating such energy extending parallel to a side surface () of the aircraft door (), along a sealing gasket () support () secured to the door () across from a fuselage () side surface () framing () the door (). The sealing gasket () of the door () is compressed against bearing () from a side surface () of the fuselage () when the door () is closed.

Anti-icing / de-icing system for aircraft door and aircraft door equipped with such a system

The invention relates to optimize the use of electronic cabinets in connector technology, using simplified internal connector technology and flexibility in adapting the external connector technology to the connectors of the cabling assemblies&#x2014;electronic and/or optical connector technologies&#x2014;and on the structurally. To this end, according to an embodiment, an overall box-shaped electronic cabinet () that is fitted with at least one detachable interconnection module () is provided with a bottom wall () including a bottom card () connected to a set of electronic modules (). The rear wall () is extended by edges () provided with connectors (C, C) that are capable of being coupled to the connectors (C, C) that are arranged on a side surface () of the detachable interconnection module () (). Devices for closing and releasably locking the at least one detachable interconnection module () are provided between a handle () of an interconnection module () and the side wall () of the cabinet ().

Method for integrating a detachable interconnection module in a cabinet, cabinet thus fitted, and aircraft comprising a bay consisting of such cabinets

The invention relates to an umbrella including a security system having a triggering device located on the contact area of the mast with the ground. The triggering device includes a slider, a slider return spring, a flexible transmission assembly connected to the head of the slider; a mechanism to inactivate the trigger, including a cam pivotally mounted on the trigger and capable of resting against the mast.

Bottom-triggering wind safety umbrella

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L'Union, France

Bernard Amalric