Composite wing and manufacturing process thereof

Aeronautics and astronautics – Aircraft structure – Airfoil construction

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Details

244117R, 416226, B64C 320

Patent

active

053321782

ABSTRACT:
A composite wing for an aircraft comprises a plurality of elongated hollow one-piece composite spars arranged in juxtaposed generally parallel relation in an array defining an airfoil with a composite skin disposed about said assembled spars.

REFERENCES:
patent: 3028292 (1962-04-01), Hinds
patent: 3229935 (1966-01-01), Bellanca
patent: 3768922 (1973-10-01), Dixon
patent: 3779487 (1973-12-01), Ashton et al.
patent: 3962506 (1976-06-01), Dunahoo
patent: 4188171 (1980-02-01), Baskin
patent: 4206895 (1980-06-01), Olez

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