B - Operations – Transporting – 29 – C
Patent
B - Operations, Transporting
29
C
B29C 70/86 (2006.01) B29C 65/00 (2006.01) B64C 1/06 (2006.01)
Patent
CA 2751015
In a method for manufacturing a shell (19), at least two shell sections (20, 22) are fabricated out of a composite fiber material, at least one compensation body (32, 34, 36, 38) comprised of a plastically deformable material is secured to at least one limiting edge (24, 26, 28, 30) of at least one shell section (20, 22), the shell sections (20, 22) are overlapped to form the shell, yielding flat seams (40, 42) between respectively adjacent shell sections (20, 22), wherein the at least one compensation body (32, 34, 36, 38) is arranged on at least one of the seams (40, 42). In order to compensate for dimensional deviations in each overlap, the shape of the corresponding compensation bodies is changed, and the shells sections (20, 22) are joined together at the seams (40, 42).
Dans un procédé de fabrication d'un corps en forme de coque (19), au moins deux parties de coque (20, 22) sont faites dans un matériau composite renforcé de fibres, au moins un corps de compensation (32, 34, 36, 38) fait dans un matériau déformable plastiquement est fixé sur au moins une arête d'extrémité (24, 26, 28, 30) d'au moins une partie de coque (20, 22), les parties de coque (20, 22) sont superposées afin de former le corps en forme de coque, en formant des jonctions plates (40, 42) entre chacune des parties de coque (20, 22) adjacentes, ledit au moins un corps de compensation (32, 34, 36, 38) étant disposé sur l'une des jonctions (40, 42). Afin de compenser les écarts de forme au niveau de chaque recouvrement, les corps de compensation correspondants sont modifiés dans leur forme et les parties de coque (20, 22) sont reliées entre elles au niveau des jonctions (40, 42).
Biesek Steffen
Goehlich Robert Alexander
Sayilgan Cihangir
Airbus Operations Gmbh
Borden Ladner Gervais Llp
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