Noise reducing vortex generators on aircraft wing control...

Details Noise reducing vortex generators on aircraft wing control... Noise reducing vortex generators on aircraft wing control...

B - Operations, Transporting

64

C

B64C 23/06 (2006.01) B64C 21/10 (2006.01)

Patent

CA 2344950

Vortex generators are arranged on the edges of aircraft wing control surfaces to generate smaller vortices that weaken the main vortex that would otherwise be generated at these areas, and thereby reduce the aerodynamic generation of noise. Each vortex generator includes plural elongated elements in the form of rigid rods or flexible bristles protruding laterally outwardly from the respective edge of the control surface. The vortex generators are preferably arranged on the inboard and outboard edges of high lift flaps and slats.

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