DEVICE FOR REDUCING THE AERODYNAMIC NOISE OF AN AIRCRAFT LANDING GEAR

摘要

The invention relates to a device for reducing the aerodynamic noise of aircraft landing gear deployed during the landing and/or take-off phase. The device comprises two flanges (4a, 4b) for respectively blocking each end (2a, 2b) of a hollow shaft (1) of the landing gear, such as a hinge line of two connecting rods of said landing gear, as well as at least one link (6) to be inserted into the hollow shaft (1) in order to connect the two flanges (4a, 4b) together so as to retain said flanges clamped to the ends (2a, 2b) of said shaft (1). The invention can be used in the aeronautical field.