Aircraft electric taxi system with friction actuated, bi-directional clutch
摘要
<p>An electric taxi system (ETS) for an aircraft may comprise drive motors mounted coaxially with wheels of the aircraft. A clutch assembly may be interposed between the drive motor the wheel. The clutch assembly may transmit torque from the motor to the wheel when the wheel and a rotor of the motor rotate at the same rotational speed. The clutch assembly may selfdisengage a rotor of the motor from the wheel when the wheel rotates faster than the rotor.</p>
申请公布号
EP2455634(B1)
申请公布日期
2014.01.15
申请号
EP20110189374
申请日期
2011.11.16
申请人
HONEYWELL INTERNATIONAL, INC.
发明人
CHRISTENSEN, DONALD J.;LANGSTON, TODD;CHARLES, DAVID LANE;VELASQUEZ, RUDEY