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    • 9. 发明申请
    • AIRBORNE PLATFORM FOR AIRCRAFT WITH ATTITUDE CORRECTION AND TOW HITCH ASSEMBLY
    • 飞机校准飞行员平台和拖车组件
    • US20170021927A1
    • 2017-01-26
    • US15287333
    • 2016-10-06
    • ACTION COMMUNICATION
    • Alexis GIORDANA
    • B64D3/00G01V3/17G01V3/16
    • B64D3/00G01V3/16G01V3/17G09F21/12
    • In a general aspect, a device for attaching a towed device to an aircraft in flight can include an attachment cable secured to the towed device. The attachment cable can have one end forming a closed loop and including a loop head. The device can also include a first attachment element secured to the loop head of the attachment cable, The first attachment element can include first electrical connectors. The device can further include a towing cable attached to the aircraft and a second attachment element attached to one end of the towing cable. The second attachment element can be configured to cooperate mechanically and electrically with the first attachment element. The second attachment element can include second electrical connectors configured to cooperate with the first electrical connectors. The device can still further include fasteners or guides configured to hold the loop head of the attachment cable off the ground.
    • 在一般方面,用于将牵引装置附接到飞行中的飞机的装置可以包括固定到被牵引装置的附接缆索。 连接电缆可以具有形成闭环的一端,并且包括环形头。 该装置还可以包括固定到连接电缆的环头部的第一附接元件。第一连接元件可以包括第一电连接器。 该装置还可以包括附接到飞行器的牵引缆索和附接到牵引缆线的一端的第二附接元件。 第二附接元件可以构造成与第一附接元件机械地和电气地配合。 第二附接元件可以包括被配置为与第一电连接器配合的第二电连接器。 该装置还可以包括紧固件或引导件,该紧固件或引导件构造成将附接电缆的环头保持在地面之外。