AIRCRAFT BRAKE SYSTEM
    1.
    发明公开
    AIRCRAFT BRAKE SYSTEM 审中-公开
    空气制动系统

    公开(公告)号:EP2994356A1

    公开(公告)日:2016-03-16

    申请号:EP14826438.5

    申请日:2014-07-16

    IPC分类号: B60T8/42

    摘要: An aircraft emergency brake system includes a modulating emergency/parking brake valve in fluid communication with and disposed between a pressure source and a wheel brake and a lever assembly operatively connected with the brake valve. The emergency brake system is operative in first and second stages. The lever assembly includes a handle, a lock mechanism and an unlock mechanism. The handle is movable between a non-actuated position and a fully-actuated position. The brake pressure provided to the wheel brake through the brake valve depends on a position of the handle. The lock mechanism is operatively connected with the handle to obstruct the handle from moving from the first stage to the second stage. The unlock mechanism is disposed on the handle to unlock the lock mechanism allowing movement of the handle to the second stage position from the first stage position.

    VARIABLE GAIN CONTROL NOSE WHEEL STEERING SYSTEM
    7.
    发明公开
    VARIABLE GAIN CONTROL NOSE WHEEL STEERING SYSTEM 有权
    转向系统的可变增益控制前轮WITH

    公开(公告)号:EP2625578A2

    公开(公告)日:2013-08-14

    申请号:EP11831619.9

    申请日:2011-10-06

    发明人: OYAMA, Hiroki

    IPC分类号: G05D1/02

    CPC分类号: G05D1/0083 B64C25/50

    摘要: A method for determining a target steering angle for nose landing gear of an aircraft includes receiving rudder pedal input data into a steering control unit, receiving aircraft speed data into the steering control unit, calculating a normal gain, calculating a parking gain, and adding the normal gain and the parking gain to determine the target steering angle. The normal gain is a positive quantity in all aircraft speed and pedal stroke ranges. The parking gain is a positive quantity in parking and taxiing speed ranges. A nose wheel steering system is also disclosed.