A method of securing composite elements together

Details A method of securing composite elements together A method of securing composite elements together

B - Operations, Transporting

64

C

B64C 3/26 (2006.01) B64F 5/00 (2006.01) F16B 25/00 (2006.01)

Patent

CA 2454406

A method is provided of forming a wing form composite components, whereby the composite components (2 and 20) are attached together using self-tapping screws (23).

L'invention concerne un procédé destiné à la formation d'une voilure à partir de composants composites, consistant à assembler les composants composites (2, 20) à l'aide de vis autotaraudeuses (23).

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