Aircraft wheel support mechanism

Details Aircraft wheel support mechanism Aircraft wheel support mechanism

B - Operations, Transporting

64

C

B64C 25/58 (2006.01) B64C 25/00 (2006.01) B64C 25/10 (2006.01) B64C 25/60 (2006.01)

Patent

CA 2458607

An aircraft wheel support mechanism capable of reducing the impact to the tire at the time of landing and capable of reducing the impact to the tire at the time of the wheel colliding with an obstacle lying on the runway. The mechanism comprises a suspension mechanism for rotatably supporting a wheel by the lower end of a support member connected to the fuselage, the suspension mechanism having a crank shaft assembly, and is characterized in that the crank shaft assembly comprises a horizontal support shaft rotatably supported by the lower end of the support member, an axle for rotatably supporting the wheel, and an arm positioned at right angles with the horizontal support shaft and axle for connecting one end of the horizontal support shaft to one end of the axle.

L'invention concerne un mécanisme de soutien d'une roue d'aéronef capable de diminuer le choc sur le pneu au moment de l'atterrissage, et capable de diminuer le choc sur le pneu au moment d'une collision de la roue avec un obstacle situé sur la piste. Ce mécanisme comprend un mécanisme de suspension (3) pour soutenir de façon rotative une roue (13) à l'extrémité inférieure d'un élément de soutien (2) relié au fuselage. Le mécanisme de suspension (3) possède un ensemble arbre coudé (5), et est caractérisé en ce que cet ensemble arbre coudé comprend un arbre de soutien horizontal (51) soutenu de façon rotative par l'extrémité inférieure de l'élément de soutien, un axe (52) pour soutenir de façon rotative la roue, et un bras (53) placé à angle droit avec l'arbre de soutien horizontal et l'axe pour relier une extrémité de l'arbre de soutien horizontal à une extrémité de l'axe.

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