System for attaching an instrument or apparatus to a load carried by an aircraft
    1.
    发明公开
    System for attaching an instrument or apparatus to a load carried by an aircraft 有权
    系统用于仪表或装置连接到由飞机承载的负载

    公开(公告)号:EP1878661A2

    公开(公告)日:2008-01-16

    申请号:EP07112269.1

    申请日:2007-07-11

    IPC分类号: B64D47/08 F42B15/08

    摘要: The system comprises an attachment device (14) including a support structure (18, 20) and at least one band member (22) for releasably connecting the support structure (18, 20) to a load (12), such as a missile, carried by an aircraft, and an aerodynamic element (32) associated to the attachment device (14). The support structure (18, 20) of the attachment device (14) includes a support bracket (18) which is open upwards and an intermediate member (20) which is adapted to be attached to the support bracket (18) to close the support bracket (20) from above. The intermediate member (20) is arranged in the assembled condition between the instrument or apparatus (10) and the load (12). The aerodynamic element (32) is releasably attached to the load (12) in front of the instrument or apparatus (10).

    摘要翻译: 该系统包括附接装置(14)包括支撑结构(18,20)和至少一个带式部件(22),用于所述支撑结构(18,20)可释放地连接到负载(12):如导弹, 通过在飞机,并以相关联的附连装置(14)的空气动力元件(32)承载。 所述附接装置(14)的支撑结构(18,20)包括支撑托架(18),所有这些是开放的向上和中间构件(20),所有这些是angepasst附连到所述支撑支架(18)以关闭所述支承 从上面支架(20)。 所述中间构件(20)在仪器或设备(10)和负载(12)之间的组装状态下被布置。 空气动力元件(32)可释放地附连到在仪器或设备(10)的前方的负载(12)。

    A method and system for the remote control of aircraft
    3.
    发明公开
    A method and system for the remote control of aircraft 有权
    费尔法恩·恩·费尔斯特伦

    公开(公告)号:EP1962442A2

    公开(公告)日:2008-08-27

    申请号:EP08150946.5

    申请日:2008-02-01

    IPC分类号: H04B7/185

    摘要: A method and a system for the remote control of aircraft are described and are based on the transmission of a flow of command signals comprising continuous command signals and discrete command signals from a ground station to a receiving arrangement on board an aircraft in accordance with a predefined encoding protocol.
    Discrete command signals are transmitted by the transmission of frames of discrete commands in which each command frame includes a command datum and its replica, which are transmitted at intercalated bits, so that the frame comprises a sequence of pairs of identical bits, and the discrete command signals are processed in the on-board arrangement by reconstruction of a pair of command data for each frame by separation of the intercalated bits of the pairs of bits and equality comparison of the states of the corresponding bits of each pair of command data so that a command datum received which is identical to the respective paired datum is considered valid.

    摘要翻译: 描述了一种用于遥控飞行器的方法和系统,并且其基于包括连续命令信号和离散命令信号的命令信号流从飞机上的地面站传输到飞机上的接收装置,根据预定义 编码协议。 离散命令信号通过离散命令的帧的发送来发送,其中每个命令帧包括以插入位发送的命令数据及其副本,使得该帧包括一对相同位的序列,并且离散命令 信号通过对每一帧的一对命令数据重新构成,通过分离比对对的插入位和每对命令数据的相应位的状态的相等比较来处理,使得 与相应的配对数据相同的接收到的命令数据被认为是有效的。

    A method and system for the remote control of aircraft
    4.
    发明公开
    A method and system for the remote control of aircraft 有权
    方法和系统,用于飞机的遥控

    公开(公告)号:EP1962442A3

    公开(公告)日:2009-03-11

    申请号:EP08150946.5

    申请日:2008-02-01

    IPC分类号: H04B7/185

    摘要: A method and a system for the remote control of aircraft are described and are based on the transmission of a flow of command signals comprising continuous command signals and discrete command signals from a ground station to a receiving arrangement on board an aircraft in accordance with a predefined encoding protocol.
    Discrete command signals are transmitted by the transmission of frames of discrete commands in which each command frame includes a command datum and its replica, which are transmitted at intercalated bits, so that the frame comprises a sequence of pairs of identical bits, and the discrete command signals are processed in the on-board arrangement by reconstruction of a pair of command data for each frame by separation of the intercalated bits of the pairs of bits and equality comparison of the states of the corresponding bits of each pair of command data so that a command datum received which is identical to the respective paired datum is considered valid.

    System for attaching an instrument or apparatus to a load carried by an aircraft
    5.
    发明公开
    System for attaching an instrument or apparatus to a load carried by an aircraft 有权
    用于将仪器或设备连接到由飞机运载的负载的系统

    公开(公告)号:EP1878661A3

    公开(公告)日:2008-03-05

    申请号:EP07112269.1

    申请日:2007-07-11

    IPC分类号: B64D47/08 F42B15/08 G03B15/00

    摘要: The system comprises an attachment device (14) including a support structure (18, 20) and at least one band member (22) for releasably connecting the support structure (18, 20) to a load (12), such as a missile, carried by an aircraft, and an aerodynamic element (32) associated to the attachment device (14). The support structure (18, 20) of the attachment device (14) includes a support bracket (18) which is open upwards and an intermediate member (20) which is adapted to be attached to the support bracket (18) to close the support bracket (20) from above. The intermediate member (20) is arranged in the assembled condition between the instrument or apparatus (10) and the load (12). The aerodynamic element (32) is releasably attached to the load (12) in front of the instrument or apparatus (10).

    摘要翻译: 该系统包括包括支撑结构(18,20)和用于将支撑结构(18,20)可释放地连接至负载(12)(例如导弹)的至少一个带构件(22)的附接装置(14) 由飞机携带,以及与附接装置(14)相关联的空气动力学元件(32)。 附接装置(14)的支撑结构(18,20)包括向上敞开的支撑托架(18)和适于附接到支撑托架(18)以关闭支撑件的中间构件(20) 从上方支架(20)。 中间构件(20)布置在仪器或设备(10)和负载(12)之间的组装状态中。 气动元件(32)可释放地附接到仪器或装置(10)前方的负载(12)。