Landing gear assembly for aircraft

Landing gear assembly for aircraft

  • CN 101,575,003 A
  • Filed: 12/15/2004
  • Published: 11/11/2009
  • Est. Priority Date: 12/15/2003
  • Status: Active Grant
First Claim
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1. undercarriage assembly that is used for aircraft comprises:

  • Nose-gear and main landing gear, described nose-gear and described main landing gear one of them comprises at least;

    Non rotatable base portion, described base portion is configured to be connected to the fuselage framework of aircraft;

    Wheel, described wheel are connected in described base portion and the rotation axis that can rotate is rotated with respect to described base portion;

    Be connected at least one stator of described base portion;

    Being connected in described wheel and being configured to can be with respect at least one rotor of described stator rotation;

    Wherein, described stator and described rotor are constructed to be permeable to produce magnetic flux respectively;

    AndThe magnetic flux that described stator and rotor are configured to them interacts and causes at least a situation in the following situation;

    the torque energy that electric energy is transformed into described wheel;

    And can be transformed into the electric energy that its magnitude is applicable to the rotating speed that reduces described wheel to the torque of described wheel.

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