Aircraft structure with air ducts integrated in structural...

Details Aircraft structure with air ducts integrated in structural... Aircraft structure with air ducts integrated in structural...

B - Operations, Transporting

64

D

B64D 13/00 (2006.01)

Patent

CA 2755421

The invention relates to an aircraft structure with load-bearing hollow structural elements (100, 101, 102) that form an aircraft fuselage (11), wherein the cavities in the structural elements are designed as air ducts (103) for an air conditioning system of the aircraft (10). The invention further relates to an aircraft with such an aircraft structure.

L'invention concerne une structure d'avion avec des éléments structuraux (100, 101, 102) porteurs, creux et formant une coque d'avion (11). Les espaces creux dans les éléments structuraux prennent la forme de compartiments de guidage d'air (103) pour une climatisation de l'avion (10). L'invention concerne en outre un avion avec une telle structure.

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