Framework wing box for a wing

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/26 (2006.01) B64C 3/00 (2006.01) E04B 1/19 (2006.01) F16B 7/18 (2006.01)

Patent

CA 2614878

The present application discloses a wing box for an aircraft wing with a framework (7) and a first shell (1), wherein the framework (7) is connected to the first shell (1) such that a load acting on the first shell (1) can be transferred by the framework (7).

La présente invention concerne un caisson de voilure d~une voilure d~aéronef avec une charpente (7) et une première coque (1), dans lequel la charpente (7) est raccordée à la première coque (1) de sorte qu~une charge agissant sur la première coque (1) peut être transférée par la charpente (7).

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