Frame element, aircraft air-conditioning system and method...

Details Frame element, aircraft air-conditioning system and method... Frame element, aircraft air-conditioning system and method...

B - Operations, Transporting

64

C

B64C 1/00 (2006.01) B64C 1/06 (2006.01) B64C 1/12 (2006.01) B64D 13/00 (2006.01)

Patent

CA 2659834

A frame element (10; 10') for use in an aircraft air-conditioning system is attachable to an aircraft structure (36) and includes at least one strut (12, 14, 16, 18; 12', 14', 16') which is formed at least in sections as a hollow cylinder, wherein an air inlet connection (12a, 14a; 12a', 14a') of the at least one section-wise hollow cylindrically formed strut (12, 14, 16, 18; 12', 14', 16') of the frame element (10; 100 is connectable to an air outlet duct of an aircraft air-conditioning unit, and an air outlet connection (12b, 14b; 12b', 14b') of the at least one section-wise hollow cylindrically formed strut (12, 14, 16, 18; 12', 14', 16') of the frame element (10; 100 is connectable to an air outlet opening terminating in a cabin region of an aircraft.

La présente invention concerne un élément d'armature (10; 10') à utiliser dans un système de climatisation d'aéronef, pouvant être fixé à une structure d'aéronef (36) et comprenant au moins une entretoise (12, 14, 16, 18; 12', 14', 16') qui est formée au moins par sections d'un cylindre creux, une connexion d'entrée d'air (12a, 14a; 12a', 14a') de l'entretoise (12, 14, 16, 18; 12', 14', 16') de l'élément d'armature (10; 100), formée au moins par section d'un cylindre creux, peut être connectée à une conduite de sortie d'air d'une unité de climatisation d'aéronef, et une connexion de sortie d'air (12b, 14b; 12b', 14b') de l'entretoise (12, 14, 16, 18; 12', 14', 16') de l'élément d'armature (10; 100), formée au moins par section d'un cylindre creux, peut être connectée à une ouverture de sortie d'air qui débouche dans une zone cabine de l'aéronef.

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