Process for reducing noise generated by an aircraft landing...

B - Operations – Transporting – 64 – C

Patent

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B64C 25/16 (2006.01) F15D 1/10 (2006.01)

Patent

CA 2628633

The invention concerns a method and apparatus for reducing the noise generated by an aircraft undercarriage when the aircraft is flying and the undercarriage is deployed, includes coating at least a portion of a structural element of the undercarriage in a material that is of lower density than the material of the structural element in order to give this portion an aerodynamic shape suitable for smoothing a stream of air flowing around the portion.

L'invention concerne un procédé de réduction de bruit généré par un atterrisseur d'aéronef lorsque l'aéronef vole et que l'atterrisseur est déployé, consistant à enrober au moins une partie d'un élément structurel d'atterrisseur d'un matériau moins dense que celui de l'élément structurel pour donner à ladite partie une forme aérodynamique propre à régulariser un flux d'air s'écoulant autour de ladite partie.

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