Lift augmentation system

Details Lift augmentation system Lift augmentation system

B - Operations, Transporting

64

C

B64C 3/54 (2006.01) B64C 3/56 (2006.01) B64C 9/34 (2006.01)

Patent

CA 2561366

This invention relates generally to a lift augmentation system for an airframe. More particularly, the invention concerns the combination of extendable/retractable wing tips with an airframe for lift augmentation as well as wings that can pivot into a deployed position. Flexible surface elements may be rolled for storage and unrolled for deployment with at least one being on the suction surface of the wing and at least one being on the pressure surface of the wing.

L'invention porte d'une manière générale sur un système hypersustentateur de cellule d'avion, et plus particulièrement sur une combinaison d'ailerons hypersustentateurs déployables/rétractables et d'ailes pouvant pivoter en position déployée et sur des éléments de surface souples enroulables et déroulables, dont un au moins se trouve côté extrados, et un autre au moins côté intrados.

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