AIRCRAFT BRAKE CONTROL ARCHITECTURE HAVING IMPROVED POWER DISTRIBUTION AND REDUNDANCY
    1.
    发明申请
    AIRCRAFT BRAKE CONTROL ARCHITECTURE HAVING IMPROVED POWER DISTRIBUTION AND REDUNDANCY 审中-公开
    具有改进功率分配和冗余的飞机制动控制架构

    公开(公告)号:US20080258547A1

    公开(公告)日:2008-10-23

    申请号:US11736603

    申请日:2007-04-18

    IPC分类号: B60T8/88 B60T13/66 B64C25/42

    摘要: An electromechanical braking system for an aircraft, including a first power conversion module (PCM) and a second power conversion module (PCM), each configured to receive power from a respective independent power source on the aircraft. The system further includes at least one brake system control unit (BSCU) for converting an input brake command signal into a brake clamp force command signal. At least a first brake control module (BCM) and a second brake control module (BCM) are provided, each configured to receive the brake clamp force command signal from the at least one BSCU and to output a primary brake clamp force command signal and an alternate brake clamp force command signal based on the received brake clamp force command signal. A first electromechanical actuator controller (EMAC) and a second electromechanical actuator controller (EMAC) are provided, each configured to convert a brake clamp force command signal to at least one electromechanical actuator drive control signal. The first EMAC is operative based on the primary brake clamp force command signal from the first BCM or, in the event of a failure disabling the first BCM, based on the alternate brake clamp force command signal from the second BCM. The second EMAC is operative based on the primary brake clamp force command signal from the first BCM or, in the event of a failure disabling the first BCM, based on the alternate brake clamp force command signal from the second BCM. The first EMAC receives its operating power from the first PCM, and the second EMAC receives its operating power from the second PCM.

    摘要翻译: 一种用于飞机的机电制动系统,包括第一电力转换模块(PCM)和第二电力转换模块(PCM),每个配置用于从飞行器上相应的独立电源接收电力。 该系统还包括至少一个用于将输入制动指令信号转换成制动夹紧力指令信号的制动系统控制单元(BSCU)。 至少提供了第一制动控制模块(BCM)和第二制动控制模块(BCM),每个制动控制模块(BCM)被配置成从至少一个BSCU接收制动夹紧力指令信号并输出​​一次制动夹紧力指令信号 基于接收到的制动夹紧力指令信号的交替制动夹紧力指令信号。 提供了第一机电致动器控制器(EMAC)和第二机电致动器控制器(EMAC),每个机构致动器控制器(EMAC)被配置为将制动夹紧力指令信号转换为至少一个机电致动器驱动控制信号。 第一EMAC基于来自第一BCM的初级制动夹紧力指令信号或基于来自第二BCM的替代制动夹紧力命令信号在第一BCM失效的情况下操作。 第二EMAC基于来自第一BCM的初级制动夹紧力指令信号或者在基于来自第二BCM的替代制动夹紧力命令信号而使第一BCM失效的情况下操作。 第一EMAC从第一PCM接收其工作电力,而第二EMAC从第二PCM接收其工作电力。

    AIRCRAFT BRAKE CONTROL ARCHITECTURE HAVING IMPROVED ANTISKID REDUNDANCY
    2.
    发明申请
    AIRCRAFT BRAKE CONTROL ARCHITECTURE HAVING IMPROVED ANTISKID REDUNDANCY 审中-公开
    飞机制动控制架构具有改进的反恐怖主义

    公开(公告)号:US20080258548A1

    公开(公告)日:2008-10-23

    申请号:US11736601

    申请日:2007-04-18

    申请人: Bill May Henry Grant

    发明人: Bill May Henry Grant

    IPC分类号: B60T8/171 B64C25/42 B60T8/32

    摘要: According to the present invention, an electromechanical braking system is provided. The braking system includes at least one brake system control unit (BSCU) for converting an input brake command signal into a brake clamp force command signal. In addition, the braking system includes a first electromechanical actuator controller (EMAC) and a second electromechanical actuator controller (EMAC) configured to receive the brake clamp force command signal from the at least one BSCU and to convert the brake clamp force command signal to at least one electromechanical actuator drive control signal. Further, the braking system includes at least one electromechanical actuator configured to receive the at least one drive control signal and to apply a brake clamp force to at least one wheel to be braked in response to the at least one drive control signal. Moreover, the first EMAC and the second EMAC are configured to perform antiskid control in relation to the at least one wheel to be braked.

    摘要翻译: 根据本发明,提供一种机电制动系统。 制动系统包括用于将输入制动指令信号转换为制动夹紧力指令信号的至少一个制动系统控制单元(BSCU)。 另外,制动系统包括第一机电致动器控制器(EMAC)和第二机电致动器控制器(EMAC),其被配置为从至少一个BSCU接收制动夹紧力命令信号并且将制动夹紧力指令信号转换为 至少一个机电致动器驱动控制信号。 此外,制动系统包括至少一个机电致动器,其被配置为接收至少一个驱动控制信号,并且响应于至少一个驱动控制信号,向至少一个待制动的车轮施加制动夹紧力。 此外,第一EMAC和第二EMAC配置成相对于要制动的至少一个车轮进行防滑控制。