Composite structural elements
    2.
    发明授权

    公开(公告)号:US11518495B2

    公开(公告)日:2022-12-06

    申请号:US16981499

    申请日:2019-05-02

    摘要: A composite structural member including at least one first flange element made from a first composite material, and at least one first web element made from a second composite material. The at least one first web element is connected to at least one first flange element in a non-coplanar manner along a corresponding mutual first edge via a first corner element made from a third composite material, the mutual first edge extending along a first direction. The third composite material includes a corresponding first plurality of third composite material first fibers and a corresponding second plurality of third composite material second fibers embedded in a corresponding third composite material matrix in a non-parallel orientation with respect to the third composite material first fibers, wherein the third composite material first fibers are nominally orthogonal to the mutual first edge or to the first direction.

    DEVICES, SYSTEMS AND METHODS FOR REFUELING AIR VEHICLES
    5.
    发明申请
    DEVICES, SYSTEMS AND METHODS FOR REFUELING AIR VEHICLES 审中-公开
    装备,系统和方法来修复空中的车辆

    公开(公告)号:US20140353430A1

    公开(公告)日:2014-12-04

    申请号:US14370026

    申请日:2013-01-03

    IPC分类号: B64D39/00

    摘要: A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member with a boom axis. The boom member enables fuel to be transferred from the fuel hose to a receiver aircraft along the boom axis during in-flight refueling. The device maintains a desired non-zero angular disposition between the boom axis and a forward direction at least when the refueling device is towed by the tanker aircraft in the forward direction via the fuel hose.

    摘要翻译: 公开了用于飞行中加油的各种加油装置,系统和方法。 在一个示例中,至少在飞行中加油期间,这种装置由油轮飞机经由燃料软管拖曳,并且具有具有悬臂轴线的悬臂构件。 悬臂构件使得在飞行中加油期间燃料可以沿着起重臂轴线从燃料软管传送到接收器飞机。 至少当加油装置由油轮飞机经由燃料软管向前方拖曳时,该装置在悬臂轴线和向前方向之间保持期望的非零角度布置。

    DEVICES, SYSTEMS AND METHODS FOR REFUELING AIR VEHICLES
    9.
    发明申请
    DEVICES, SYSTEMS AND METHODS FOR REFUELING AIR VEHICLES 审中-公开
    装备,系统和方法来修复空中的车辆

    公开(公告)号:US20150136911A1

    公开(公告)日:2015-05-21

    申请号:US14370017

    申请日:2013-01-03

    IPC分类号: B64D39/04

    摘要: A variety of refueling devices, systems and methods are disclosed for use in in-flight refueling. In one example one such device is towed by a tanker aircraft via a fuel hose at least during in-flight refueling, and has a boom member with a boom axis. The boom member enables fuel to be transferred from the fuel hose to a receiver aircraft along the boom axis during in-flight refueling. The device maintains a desired non-zero angular disposition between the boom axis and a forward direction at least when the refueling device is towed by the tanker aircraft in the forward direction via the fuel hose.

    摘要翻译: 公开了用于飞行中加油的各种加油装置,系统和方法。 在一个示例中,至少在飞行中加油期间,这种装置由油轮飞机经由燃料软管拖曳,并且具有具有悬臂轴线的悬臂构件。 悬臂构件使得在飞行中加油期间燃料可以沿着起重臂轴线从燃料软管传送到接收器飞机。 至少当加油装置由油轮飞机经由燃料软管向前方拖曳时,该装置在悬臂轴线和向前方向之间保持期望的非零角度布置。