Aircraft with wings whose maximum lift can be altered by...

B - Operations – Transporting – 64 – C

Patent

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B64C 13/16 (2006.01) G05D 1/08 (2006.01)

Patent

CA 2573606

The present invention relates to an aircraft with wings whose maximum lift can be altered by controllable wing components. By means of a regulating device (20), depending on flight state parameters and the actually measured load on the wings (10), wing components (11, 12) are acted upon such that the maximum possible aerodynamic lift does not exceed a desired upper limit value.

La présente invention a trait à un avion avec des ailes dont la portance maximum peut être modifiée par des éléments d'aile contrôlables. Au moyen d'un dispositif de régulation (20), suivant les paramètres d'état du vol et la charge réellement mesurée sur les ailes (10), on agit sur les éléments des ailes (11, 12) de façon à ce que la portance aérodynamique maximum possible ne dépasse pas une valeur limite supérieure désirée.

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