A composite multi-spar aircraft lifting surface comprising an integrated torsion box having a first portion of a skin continuous on the second face from a right tip to a left tip, a second portion of a skin continuous on the lateral right side of the first face from a right tip to a first central portion, a third portion of a skin continuous on the lateral left side of the first face from the left tip to a second central portion, a cover spanning between the first central portion and the second central portion. The spars, the first portion of the skin, the second portion of the skin and the third portion of the skin being an integrated multi-cell part. Also a method of manufacturing such a lifting surface.
COMPOSITE MULTI-SPAR AIRCRAFT LIFTING SURFACE
2024-01-11
Patent
Elektronische Ressource
Englisch