| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a system for recovering kinetic energy from an aircraft and converting the energy into electrical power. <P>SOLUTION: A motor for a wheel W of an aircraft landing gear includes at least one stator R and at least one rotor S disposed through a space. The rotor R is coupled to the wheel W for rotation and the stator S is coupled to an axle A and/or a torque tube to thereby convert the wheel W into a motor. <P>COPYRIGHT: (C)2013,JPO&INPIT |
