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    AIRCRAFT LANDING GEAR ASSEMBLY
    2.
    发明公开
    AIRCRAFT LANDING GEAR ASSEMBLY 审中-公开

    公开(公告)号：EP3597496A1

    公开(公告)日：2020-01-22

    申请号：EP18183607.3

    申请日：2018-07-16

    申请人： Safran Landing Systems UK Ltd ,  Safran Landing Systems

    发明人： Price, Neil ,  Coq, Marie

    IPC分类号： B60T17/22 ,  F16D55/36 ,  F16D66/02 ,  B64C25/42 ,  B64C25/34 ,  B60T8/52 ,  B60T8/17

    摘要： An aircraft landing gear assembly comprising: an axle having an axis, a wheel rotatably mounted on the axle to rotate about the axis, a brake arranged to selectively exert a braking torque on the wheel about the axis, a brake anchor structure having a substantially fixed position relative to the axle, a brake reaction linkage that mechanically couples the brake to the brake anchor structure, and a sensor comprising a sensor element arranged to detect a change in one or more physical properties of a component of the brake reaction linkage in order to determine a stress in the component due to the braking torque, wherein the sensor element does not contact the component.

    AIRCRAFT ASSEMBLY ACTUATION SYSTEM
    7.
    发明公开
    AIRCRAFT ASSEMBLY ACTUATION SYSTEM 审中-公开

    公开(公告)号：EP3486177A1

    公开(公告)日：2019-05-22

    申请号：EP17202886.2

    申请日：2017-11-21

    申请人： Safran Landing Systems UK Ltd ,  Safran Landing Systems

    发明人： EVANS, Roy ,  VASLIN, Jean Philippe ,  COLLET, Olivier

    IPC分类号： B64D45/00 ,  B64C25/22 ,  B64C25/24 ,  B64C13/42 ,  B64C25/26

    摘要： An aircraft assembly, comprising: a reference component; a first component (106) and a first actuator (102), the first actuator arranged to move the first component relative to the reference component; a second component (108) and a second actuator (102), the second actuator (102) arranged to move the second component relative to the reference component; a position sensor (110) arranged to measure a position of the first component (106), and to output a position value, the sensor being capable of outputting a plurality of non-zero position values; and a controller (100) arranged to control the movement of the second component (108) by the second actuator (104) based at least partially on the position value output by the position sensor (110).