B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 3/26 (2006.01) B64C 3/00 (2006.01) E04B 1/19 (2006.01) F16B 7/18 (2006.01)
Patent
CA 2616929
The present invention relates to a support structure for an aircraft, which support structure comprises one or several bar elements (36) and one or several junction elements (37), wherein at least one bar element (36) comprises a transition region (9) which can be made to engage at least one junction element (37). When the transition region (9) of the bar element (36) engages the junction element (37), of which there is at least one, centric force transmission takes place between the bar element (36) and the junction element (37).
La présente invention concerne une structure de support pour un avion, laquelle structure de support comprend un ou plusieurs éléments de barre (36) et un ou plusieurs éléments de jonction (37), au moins un élément de barre (36) comprenant une région de transition (9) qui peut être faite pour enclencher au moins un élément de jonction (37). Lorsque la région de transition (9) de l~élément de barre (36) enclenche l~élément de jonction (37), dont il en existe au moins un, une transmission de force centrée a lieu entre l~élément de barre (36) et l~élément de jonction (37).
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Borden Ladner Gervais Llp
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