Invention Application
US20120153086A1 Elastically Deformable Side-Edge Link for Trailing-Edge Flap Aeroacoustic Noise Reduction 有权
用于后缘翼片的气动变形侧向链路

Elastically Deformable Side-Edge Link for Trailing-Edge Flap Aeroacoustic Noise Reduction
Abstract:
A system is provided for reducing aeroacoustic noise generated by an aircraft having wings equipped with trailing-edge flaps. The system includes a plurality of elastically deformable structures. Each structure is coupled to and along one of the side edges of one of the trailing-edge flaps, and is coupled to a portion of one of the wings that is adjacent to the one of the side edges. The structures elastically deform when the trailing-edge flaps are deployed away from the wings.
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