Aircraft system carrier element

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/06 (2006.01) B60R 13/02 (2006.01)

Patent

CA 2727211

An aircraft system carrier element (10) comprises a basic body (12) made of a sound- and heat-insulating material, in which are formed an air conditioning duct (14), which is connectable to an aircraft air conditioning system and provided for supplying an aircraft compartment (22), and a line duct (16) for receiving lines (20) that are provided for supplying the aircraft compartment (22).

L'invention concerne un élément support de système pour avions (10) comprenant un corps de base (12) constitué d'un matériau insonorisant et thermo-isolant. Dans ce corps de base (12) sont ménagés un canal de climatisation (14) pouvant être relié à une installation de climatisation d'avion et destiné à alimenter un compartiment d'avion (22) et un canal à canalisations (16) recevant des canalisations (20) destinées à alimenter le compartiment d'avion (22).

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