B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/06 (2006.01)
Patent
CA 2520322
According to an exemplary embodiment of the present invention, a frame member for an aircraft is provided comprising a clip region (4) and a frame region (6). According to an aspect of this exemplary embodiment of the present invention, the clip region (4), shear web region (16) and the frame region (6) are integrated into the frame member and be formed from an extrusion mold by a milling process. Advantageously, this allows for a reduced number of individual elements for forming a frame member and provides the flexibility of variation of the forms and dimensions of a frame member for an aircraft.
L'invention concerne, dans une forme de réalisation donnée en exemple, un élément structural intégré pour aéronef qui comprend une région d'attache (4) et une région structurale (6). Dans un aspect de cette forme de réalisation, la région d'attache (4), une région d'âme de cisaillement (16) et la région structurale (6) sont intégrées dans l'élément structural et formées à partir d'un moule d'extrusion par un procédé de fraisage. L'invention permet avantageusement de réduire le nombre d'éléments individuels nécessaires pour former un élément structural, et sa flexibilité permet de varier les formes et dimensions d'un élément structural pour aéronef.
Luettig Helmut
Paul Carsten
Airbus Deutschland Gmbh
Gowling Lafleur Henderson Llp
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