B - Operations – Transporting – 29 – C
Patent
B - Operations, Transporting
29
C
B29C 65/00 (2006.01) B29C 65/72 (2006.01) B64F 5/00 (2006.01) F16L 47/00 (2006.01)
Patent
CA 2726499
The invention relates to a method for assembling two structural elements, at least one of the two being tube-shaped and including a skin made of a fiber-reinforced composite material. The ability of said element to adapt to the shape and perimeter of the junction interface is improved by providing longitudinal grooves distributed on the circumference of the junction interface. The grooves are of a sufficient length to provide the junction interface with the flexibility to accommodate, through the relative radial movement of each portion located between two grooves, the differences in shape and perimeter among the junction interfaces of the two structural elements.
L'invention concerne un procédé d'assemblage de deux éléments structuraux, au moins l' un des deux étant de forme tubulaire et comprenant une peau en matériau composite à renfort fibreux. La capacité d'adaptation en forme et en périmètre de l'interface de jonction de cet élément est améliorée en pratiquant des fentes longitudinales (5) réparties sur le pourtour de l'interface de jonction. Les fentes (5) sont de longueur suffisante pour conférer à l'interface de jonction la flexibilité adaptée pour accommoder, par le déplacement radial relatif de chaque portion située entre deux fentes, les différences de forme et de périmètre entre les interfaces de jonction des deux éléments
Gallant Guillaume
Lacombe Jean-Claude
Alrbus Operations (s.a.s)
Robic
LandOfFree
Method for the orbital assembly of aircraft sections made of... does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Method for the orbital assembly of aircraft sections made of..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method for the orbital assembly of aircraft sections made of... will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1703288