Support device for fire-detection system

F - Mech Eng,Light,Heat,Weapons – 16 – L

Patent

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Details

F16L 3/10 (2006.01) A62C 3/08 (2006.01) B64D 33/00 (2006.01) B64D 37/32 (2006.01) F16L 3/237 (2006.01) G08B 17/04 (2006.01)

Patent

CA 2544484

The invention relates to a support device (1) which is designed to be installed between an aircraft engine and an associated thrust reverser, said device being equipped with a support means which can support at least one fire-detection element in the form of a capillary. The invention is characterised in that the support means comprises at least two retaining members (18) which can be removably assembled to one another.

La présente invention se rapporte à un dispositif de retenue (1) prévu pour être installé entre un moteur d'aéronef et un inverseur de poussée associé, ce dispositif étant pourvu d'un moyen de retenue apte à supporter au moins un élément de détection feu réalisé sous la forme d'un capillaire, caractérisé en ce que le moyen de retenue comprend au moins deux organes de maintien (18) pouvant être assemblés l'un à l'autre de façon amovible.

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