B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/06 (2006.01)
Patent
CA 2685188
The present invention relates to a connecting device two curved ribs (1, 2) of an aircraft or spacecraft, with: a coupling element (5) which can be connected by means of predetermined coupling sections (6, 7) to respective connecting sections (Vl, V2) of the two ribs (1, 2); wherein at least the predetermined coupling sections (6, 7) of the coupling element (5) are rectilinear Iy designed; and in that at least the respective connecting sections (Vi, V2) of the two ribs (1, 2) each have rectilinearly running inner belt regions (15) for a respective rectilinear connection of the predetermined coupling sections {6, 7) of the coupling element (5).
La présente invention se rapporte à un dispositif de raccordement destiné à relier deux nervures courbées (1, 2) d'aéronef ou d'engin spatial, comprenant : un élément de couplage (5) qui peut être relié au moyen de sections prédéterminées de couplage (6, 7) à des sections respectives de raccordement (V1, V2) des deux nervures (1, 2), au moins l'une des sections prédéterminée de couplage (6, 7) de l'élément de couplage (5) étant conçue pour être rectilinéaire, et en ce que au moins les sections respectives de raccordement (V1, V2) des deux nervures (1, 2) possèdent chacune des zones de courroies se déplaçant de manière rectilinéaire (15) en vue d'un raccordement respectif rectilinéaire des sections prédéterminées de couplage (6, 7) de l'élément de couplage (5).
Paul Carsten
Schimmler Marc
Airbus Operations Gmbh
Oyen Wiggs Green & Mutala Llp
LandOfFree
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