BRAKE WEAR REDUCTION APPARATUS
    1.
    发明公开

    公开(公告)号:EP3566916A1

    公开(公告)日:2019-11-13

    申请号:EP19174503.3

    申请日:2017-09-20

    IPC分类号: B60T8/17 B64C25/42 B64C25/44

    摘要: Disclosed is an apparatus for reducing brake wear comprising a brake de-selection function for selectively disabling at least one brake on a vehicle; and a controller. The controller is configured to receive torque information which relates to torque reacted by a brake on the vehicle during a braking event and wheel speed information which relates to a speed of a wheel associated with the brake during the braking event; calculate an energy input into the brake during the braking event, based on the received torque information and the received wheel speed information; determine whether the calculated energy input meets at least one predefined energy input criterion; and activate the brake de-selection function if the calculated energy input meets the at least one predefined energy input criterion.

    AIRCRAFT BRAKE TEMPERATURE MEASUREMENT
    2.
    发明公开

    公开(公告)号:EP3255399A3

    公开(公告)日:2018-06-27

    申请号:EP17171165.8

    申请日:2017-05-15

    IPC分类号: G01K1/02 G01K13/08 G01K11/24

    摘要: Disclosed is a brake temperature sensing system for an aircraft. The brake temperature sensing system comprises a sensor apparatus and an interrogation apparatus. The sensor apparatus comprises a temperature sensor for attachment to a brake disc of an aircraft brake, and a relay for attachment to the brake. The temperature sensor is configured to wirelessly transmit a measurement signal containing information relating to a temperature of the brake disc, responsive to receiving a wireless interrogation signal. The relay is configured to receive an interrogation signal from the interrogation apparatus; wirelessly transmit the interrogation signal to the temperature sensor; receive the wireless measurement signal from the temperature sensor; and transmit the received measurement signal. The interrogation apparatus comprises a controller configured to generate an interrogation signal; and a transceiver configured to transmit the generated interrogation signal to the sensor apparatus; and receive the measurement signal transmitted by the sensor apparatus.

    BRAKE WEAR REDUCTION APPARATUS
    3.
    发明公开
    BRAKE WEAR REDUCTION APPARATUS 审中-公开
    制动器减速装置

    公开(公告)号:EP3296170A1

    公开(公告)日:2018-03-21

    申请号:EP17192069.7

    申请日:2017-09-20

    IPC分类号: B60T8/17 B64C25/42

    摘要: Disclosed is an apparatus for reducing brake wear comprising a brake de-selection function for selectively disabling at least one brake on a vehicle; and a controller. The controller is configured to receive torque information which relates to torque reacted by a brake on the vehicle during a braking event and wheel speed information which relates to a speed of a wheel associated with the brake during the braking event; calculate an energy input into the brake during the braking event, based on the received torque information and the received wheel speed information; determine whether the calculated energy input meets at least one predefined energy input criterion; and activate the brake de-selection function if the calculated energy input meets the at least one predefined energy input criterion.

    摘要翻译: 公开了一种用于减少制动器磨损的设备,其包括用于选择性地禁用车辆上的至少一个制动器的制动器取消选择功能; 和一个控制器。 控制器被配置为接收与在制动事件期间由车辆上的制动器反作用的转矩有关的转矩信息以及与在制动事件期间与制动器相关联的车轮的速度相关的车轮速度信息; 基于所接收的扭矩信息和所接收的轮速信息,计算在制动事件期间输入到制动器的能量; 确定所计算的能量输入是否满足至少一个预定义的能量输入标准; 并且如果所计算的能量输入满足所述至少一个预定义的能量输入标准,则激活制动器取消选择功能。

    AIRCRAFT BRAKE TEMPERATURE MEASUREMENT
    4.
    发明公开

    公开(公告)号:EP3789744A1

    公开(公告)日:2021-03-10

    申请号:EP20204296.6

    申请日:2017-05-15

    摘要: Disclosed is a brake temperature sensing system for an aircraft. The brake temperature sensing system comprises a sensor apparatus and an interrogation apparatus. The sensor apparatus comprises a temperature sensor for attachment to a brake disc of an aircraft brake, and a relay for attachment to the brake. The temperature sensor is configured to wirelessly transmit a measurement signal containing information relating to a temperature of the brake disc, responsive to receiving a wireless interrogation signal. The relay is configured to receive an interrogation signal from the interrogation apparatus; wirelessly transmit the interrogation signal to the temperature sensor; receive the wireless measurement signal from the temperature sensor; and transmit the received measurement signal. The interrogation apparatus comprises a controller configured to generate an interrogation signal; and a transceiver configured to transmit the generated interrogation signal to the sensor apparatus; and receive the measurement signal transmitted by the sensor apparatus.

    AIRCRAFT BRAKE TEMPERATURE MEASUREMENT
    5.
    发明公开
    AIRCRAFT BRAKE TEMPERATURE MEASUREMENT 审中-公开
    飞机制动器温度测量

    公开(公告)号:EP3255399A2

    公开(公告)日:2017-12-13

    申请号:EP17171165.8

    申请日:2017-05-15

    IPC分类号: G01K1/02 G01K13/08

    摘要: Disclosed is a brake temperature sensing system for an aircraft. The brake temperature sensing system comprises a sensor apparatus and an interrogation apparatus. The sensor apparatus comprises a temperature sensor for attachment to a brake disc of an aircraft brake, and a relay for attachment to the brake. The temperature sensor is configured to wirelessly transmit a measurement signal containing information relating to a temperature of the brake disc, responsive to receiving a wireless interrogation signal. The relay is configured to receive an interrogation signal from the interrogation apparatus; wirelessly transmit the interrogation signal to the temperature sensor; receive the wireless measurement signal from the temperature sensor; and transmit the received measurement signal. The interrogation apparatus comprises a controller configured to generate an interrogation signal; and a transceiver configured to transmit the generated interrogation signal to the sensor apparatus; and receive the measurement signal transmitted by the sensor apparatus.

    摘要翻译: 公开了一种用于飞机的制动器温度感测系统。 制动器温度感测系统包括传感器装置和询问装置。 传感器装置包括用于附接到飞机制动器的制动盘的温度传感器以及用于附接到制动器的继电器。 温度传感器被配置为响应于接收到无线询问信号而无线地发送包含与制动盘的温度有关的信息的测量信号。 中继器被配置为从询问装置接收询问信号; 将询问信号无线发送到温度传感器; 接收来自温度传感器的无线测量信号; 并发送接收到的测量信号。 询问装置包括配置成产生询问信号的控制器; 以及收发器,被配置为将生成的询问信号传输到传感器装置; 并接收由传感器装置发送的测量信号。

    BRAKE MONITORING
    6.
    发明公开
    BRAKE MONITORING 审中-公开

    公开(公告)号:EP3530531A1

    公开(公告)日:2019-08-28

    申请号:EP19156791.6

    申请日:2019-02-12

    IPC分类号: B60T17/22

    摘要: Disclosed is an apparatus and a method for determining a thermal oxidation state of a brake of an aircraft landing gear. Determination of the thermal oxidation state of the brake involves determining a thermal oxidation state of the brake after a braking event, using a thermal oxidation model based on an initial thermal oxidation state before the braking event and a temperature profile of the brake with respect to time.