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    • 3. 发明公开
    • ARCHITECTURE BI-VOIES AVEC LIAISONS CCDL REDONDANTES
    • 架构双方AVEC LIAISONS CCDL REDONDANTES
    • EP3189380A1
    • 2017-07-12
    • EP15767223.9
    • 2015-09-04
    • Safran Electronics & DefenseSafran Helicopter Engines
    • LIU, CélineMARTI, NicolasLANGFORD, Stephen
    • G05B9/03
    • G05B19/048B64D31/00G05B9/03G05B2219/24182G05B2219/25144G05B2219/25163G05B2219/25174G06F11/2007H04L12/40182
    • The present invention concerns a flight control system of an aircraft comprising: -a first processing unit (1), -a second processing unit (2), -communication means configured to establish a first two-way digital link (3) and a second two-way digital link (4) between the first processing unit (1) and the second processing unit (2), said second link (4) being redundant with the first link (3), and said first link (3) and second link (4) being likely to be active concomitantly, said system further comprising backup communication means enabling data exchanges between the first processing unit (1) and the second processing unit (2) in the case of a failure in the first link (3) and second link (4), said backup communication means comprising an array of sensors or actuators (13) and/or a secure onboard network for the avionics (14).
    • 本发明涉及飞行器的飞行控制系统,包括: - 第一处理单元(1), - 第二处理单元(2), - 通信装置,其被配置为建立第一双向数字链路(3)和第二双向数字链路 (1)和第二处理单元(2)之间的双向数字链路(4),所述第二链路(4)与第一链路(3)是冗余的,并且所述第一链路(3)和第二链路 所述系统进一步包括备用通信装置,所述备用通信装置在所述第一链路(3)中发生故障的情况下使得所述第一处理单元(1)和所述第二处理单元(2)之间的数据交换成为可能, 和第二链路(4),所述备用通信装置包括用于所述航空电子设备(14)的传感器或致动器(13)阵列和/或安全机载网络。
    • 5. 发明公开
    • Redundant actuator control system
    • Redundantes Aktuatorsteuersystem
    • EP2381322A2
    • 2011-10-26
    • EP11163677.5
    • 2011-04-26
    • Nabtesco Corporation
    • Nakagawa, ShingoFukui, Atsushi
    • G05B9/03
    • G05B9/03B64C13/42G05B23/0237G05B2219/14014G05B2219/24182G05B2219/24188G05B2219/24191G05D1/0077
    • An operation control apparatus includes a command generation portion that generates a command signal for commanding operation of a control surface, and first and second monitoring portions that monitor an abnormality of operation of first and second control portions, respectively, of the actuator control apparatus. The actuator control apparatus includes first and second control portions that generate a control signal for an actuator for driving the control surface and that are different in design, and a switching unit that switches the connection to the actuator from one of the first and second control portions to the other, when an abnormality is detected by the first and second monitoring portions. Accordingly, it is possible to monitor a generic failure, and realize redundancy enabling control of the overall operation of the actuator, from start to finish, when a generic failure has occurred, thus realizing further simplification and streamlining of the configuration.
    • 操作控制装置包括:命令生成部,其生成用于指示控制面的操作的指令信号;以及第一和第二监视部,分别监视致动器控制装置的第一和第二控制部的动作异常。 致动器控制装置包括第一和第二控制部分,其产生用于驱动控制表面并且设计不同的致动器的控制信号;以及切换单元,其从第一和第二控制部分之一切换到致动器的连接 另一方面,当第一和第二监视部分检测到异常时。 因此,当发生一般的故障时,可以监视一般的故障,并实现从始至终的致动器的整体操作的冗余,从而进一步简化和简化配置。
    • 6. 发明公开
    • Continuous median failure control system and method
    • Kurtuierliches Fehlerkontrollsystem und -verfahren mit Medianbildung
    • EP1742123A2
    • 2007-01-10
    • EP06253316.1
    • 2006-06-26
    • GENERAL ELECTRIC COMPANY
    • Toth, Carl Raymond
    • G05B9/03
    • G05B9/03G01D3/08G05B2219/14126G05B2219/24182G05B2219/24193
    • A redundant control system (10) including at least three redundant signals (12a-c) is presented. The redundant control system (10) includes a failure circuit (14) associated with each of the redundant signals (12a-c). The failure circuit (14) generates a failure signal (24) in response to an occurrence of a failure of a corresponding one of the redundant signals (12a-c). A select circuit is associated with each of the redundant signals (12a-c). The select circuit is receptive to a default signal associated with the corresponding one of the redundant signals (12a-c), to the failure signal (24), and to the corresponding one of the redundant signals (12a-c). The select circuit selects the default signal when the failure signal (24) indicates a failure of the corresponding one of the redundant signals (12a-c) and selects the corresponding one of the redundant signals (12a-c) when the failure signal (24) does not indicate a failure for the corresponding one of the redundant signals (12a-c). A median determination circuit (30) is receptive to the default signals selected and the redundant signals selected to determine a median signal (38) indicative of a median of the default signals selected and the redundant signals (12a-c) selected.
    • 提出了包括至少三个冗余信号(12a-c)的冗余控制系统(10)。 冗余控制系统(10)包括与每个冗余信号(12a-c)相关联的故障电路(14)。 故障电路(14)响应于冗余信号(12a-c)中的相应一个的故障的发生而产生故障信号(24)。 选择电路与每个冗余信号(12a-c)相关联。 所述选择电路接收与所述冗余信号(12a-c)中的对应的一个,所述故障信号(24)和所述冗余信号(12a-c)中的对应的一个相关联的默认信号。 当故障信号(24)指示冗余信号(12a-c)中的相应一个故障时,选择电路选择默认信号,并且当故障信号(24-C)选择了冗余信号 )不表示对应的一个冗余信号(12a-c)的故障。 中值确定电路(30)接受所选择的默认信号和选择的冗余信号,以确定指示所选择的默认信号的中值和选择的冗余信号(12a-c)的中值信号(38)。