Aircraft wings

Aeronautics and astronautics – Aircraft structure – Airfoil construction

Patent

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Details

416226, 416230, 416244R, 244131, B64C 318

Patent

active

054960029

ABSTRACT:
A wing made of composite fibre materials, especially carbon fibre reinforced plastics, comprises shell components having a thin-walled, pre-formed wing skin and tubular rods as stringers. The stringers are provided with a connection element and a compression plate at the fuselage end of the wing. The external sides of the compression plates are all in one plane. The wing is attached by screws, which are screwed through the connection element at the fuselage side into the connection elements of the rods forming the stringers. The rods forming the stringers are adhered to the inside of the wing skin. The spaces between the rods may be filled with a light, compression-proof material.

REFERENCES:
patent: 2540482 (1951-02-01), Hervey
patent: 2593714 (1952-04-01), Robinson
patent: 3013614 (1961-12-01), Platt
patent: 3105557 (1963-10-01), Wigil
patent: 3368599 (1968-02-01), Dailey
patent: 4725021 (1988-02-01), Priddy
patent: 5332178 (1974-07-01), Williams

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