Support assembly for a high lift body, high lift body arrangement, as well as wing and aircraft comprising same

Abstract

A support assembly for a high lift body, in particular a leading-edge-slat, mounted to a spar of a wing of an aircraft. The support assembly has at least two hinging organs each providing at least one hinge point for hinging the high lift body at the spar movably between a stowed position and a deployed position along a motion path involving a translatory component extending within a deployment plane extending transversely with respect to a mounting plane provided by the spar for mounting the hinging organs to the spar. Also a high lift body arrangement, a wing, and an aircraft.

Dependencies are inferred from the claim text.