Device for reducing the aerodynamic noise of an aircraft...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/36 (2006.01) G01K 11/16 (2006.01)

Patent

CA 2758446

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.

L'invention concerne un dispositif de limitation du bruit aérodynamique d'un atterrisseur d'aéronef déployé en phase d'atterrissage et/ou de décollage. Le dispositif comporte deux flasques (4a, 4b) destinés à boucher respectivement chaque extrémité (2a, 2b) d'un axe creux (1) de l'atterrisseur, tel qu'un axe d'articulation de deux bielles de cet atterrisseur, ainsi qu'au moins un lien (6) destiné à être engagé dans l'axe creux (1) pour relier les deux flasques (4a, 4b) l'un à l'autre afin de les maintenir plaqués aux extrémités (2a, 2b) de cet axe (1). L'invention s'applique au domaine aéronautique.

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