B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/26 (2006.01) B29C 65/00 (2006.01) F16B 5/01 (2006.01)
Patent
CA 2600878
The invention concerns an assembling device comprising a splice bar (1) and a backing plate (2) for securing at least first (3) and second (4) structural elements received between the splice bar (1) and the backing plate (2). The invention is characterized in that the backing plate (2) comprises a number of fixing points (M, N) less than the number of fixing points (P, Q) of the splice bar so that said first (3) and second (4) structural elements are fixed between the splice bar (1) and the backing plate (2) by a number of fixing points (M + N) less than the number of fixing points (P + Q) of said structural elements on the splice bar (1), the assembly being thus a non-symmetrical assembly, at least one of the structural elements being an element made of composite materials.
- L'objet de l'invention est un dispositif d'éclîssage comportant une éclisse (1) et une contre éclisse (2) de solidarisation d'au moins un premier (3) et un deuxième (4) éléments structurels reçus entre l'éclisse (1 ) et la contre éclisse (2) caractérisé en ce que la contre éclisse (2) comporte un nombre de points de fixation (M, N) inférieur au nombre de points de fixation (P, Q) de l'éclisse de sorte que lesdits premier (3) et deuxième (4) éléments structurels sont fixés entre l'éclisse (1) et la contre éclisse (2) par un nombre de points de fixation (M + N) inférieur au nombre de points de fixation (P + Q) desdits éléments structurels sur i'éciisse (1), l'éclissage étant ainsi un éclissage dissymétrique, au moins un des éléments structurels étant un élément réalisé en matériaux composites.
Airbus France
Airbus Operations Sas
Bcf Llp
LandOfFree
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