B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/06 (2006.01) B64D 13/00 (2006.01)
Patent
CA 2678221
The present invention relates to a fuselage (1) of an aircraft or spacecraft, with at least one shell element (2) and a structural element (7). An interspace (5; 9) to which air can be admitted by an air stream (10) is provided between the at least one shell element (2) and the structural element (7). The fuselage is distinguished by the fact that, to form the air-admitting air stream (10) as an outgoing/incoming air stream of a pressurized interior space (20) of the fuselage (1), the interspace (5; 9) is connected to a corresponding outgoing/ incoming air connection of the interior space (20). The invention also relates to a corresponding aircraft or spacecraft and to a method of actively insulating such a fuselage (1).
La présente invention concerne un fuselage (1) d'aéronef ou d'engin spatial, comportant au moins un élément coque (2) et un élément de structure (7). Un espace intercalaire (5, 9) dans lequel on peut admettre de l'air par un courant d'air est ménagé entre l'élément coque (2) et l'élément de structure (7). Ce fuselage se distingue en ce que, pour former le courant d'air d'admission d'air (10) sous forme d'un courant d'air sortant/entrant d'un espace intérieur pressurisé (20) du fuselage (1), l'espace intercalaire (5, 9) donne sur un raccordement d'air sortant/entrant de l'espace pressurisé (20). L'invention concerne également un aéronef ou un engin spatial correspondant et un procédé d'isolation active d'un tel fuselage (1).
Airbus Operations Gmbh
Oyen Wiggs Green & Mutala Llp
LandOfFree
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