Assisted In-Flight Refuelling System
    1.
    发明申请
    Assisted In-Flight Refuelling System 有权
    辅助飞行加油系统

    公开(公告)号:US20110001011A1

    公开(公告)日:2011-01-06

    申请号:US12792440

    申请日:2010-06-02

    IPC分类号: B64D39/00

    摘要: An assisted in-flight refuelling system having a tanker aircraft equipped with a drogue; a fuel take-on aircraft equipped with a probe; and a drogue-probe coupling assist system designed to determine a first distance between the drogue and the take-on aircraft/probe, a second distance between the tanker aircraft and the drogue, and a third distance between the tanker aircraft and the take-on aircraft. The drogue-probe coupling assist system is also designed to determine information relative to the necessary movement of the drogue and/or the necessary movement of the take-on aircraft to couple the drogue to the probe, as a function of the first, second, and third distance.

    摘要翻译: 一个辅助的机上加油系统,具有配备有冷水的油轮飞机; 装有探头的燃油喷射飞机; 以及锥形探针联接辅助系统,其被设计用于确定锥套和接管飞行器/探针之间的第一距离,油罐飞机与锥套之间的第二距离,以及油轮飞机与接收器之间的第三距离 飞机。 锥形探针耦合辅助系统还被设计成根据第一,第二,第二,第二,第二,第二,第二,第二,第二和第二, 和第三距离。

    Assisted in-flight refuelling system
    2.
    发明授权
    Assisted in-flight refuelling system 有权
    辅助飞行加油系统

    公开(公告)号:US09334062B2

    公开(公告)日:2016-05-10

    申请号:US12792440

    申请日:2010-06-02

    摘要: An assisted in-flight refueling system having a tanker aircraft equipped with a drogue; a fuel take-on aircraft equipped with a probe; and a drogue-probe coupling assist system designed to determine a first distance between the drogue and the take-on aircraft/probe, a second distance between the tanker aircraft and the drogue, and a third distance between the tanker aircraft and the take-on aircraft. The drogue-probe coupling assist system is also designed to determine information relative to the necessary movement of the drogue and/or the necessary movement of the take-on aircraft to couple the drogue to the probe, as a function of the first, second, and third distance.

    摘要翻译: 一个辅助的机上加油系统,具有配备有冷水的油轮飞机; 装有探头的燃油喷射飞机; 以及锥形探针联接辅助系统,其被设计用于确定锥套和接管飞行器/探针之间的第一距离,油罐飞机与锥套之间的第二距离,以及油轮飞机与接收器之间的第三距离 飞机。 锥形探针耦合辅助系统还被设计成根据第一,第二,第二,第二,第二,第二,第二,第二,第二和第二, 和第三距离。