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    Articulated sensor support structure
    1.
    发明授权
    Articulated sensor support structure 有权
    铰链传感器支撑结构

    公开(公告)号：US08548314B2

    公开(公告)日：2013-10-01

    申请号：US13478764

    申请日：2012-05-23

    申请人： John Peter Zwaan ,  Makoto Ueno ,  Marc L. Schmalzel ,  Christopher E. Fisher

    发明人： John Peter Zwaan ,  Makoto Ueno ,  Marc L. Schmalzel ,  Christopher E. Fisher

    IPC分类号： G03B39/00 ,  G03B17/00

    CPC分类号： B64C39/024 ,  B64C2201/127 ,  B64D47/08 ,  G03B15/006 ,  G03B17/561

    摘要： Embodiments include an assembly comprising: (a) a camera support structure comprising: a masthead disposed on the distal end of a mast wherein the masthead is configured to receive an imaging element; where a proximal end of the mast rotatably engaging an azimuth-elevation joint assembly wherein the azimuth-elevation joint assembly comprises a first angular actuator of a first rotational degree-of-freedom and a second angular actuator of a second rotational degree of freedom; and (b) a camera support structure housing comprising an aperture and a hatch wherein the hatch is resiliently biased to close the aperture; and wherein the camera support structure is configured to overcome the hatch resilient bias by at least one of: the release of a pin restraining a loaded spring and a rotational actuation of the mast via at least one of the first angular actuator and the second angular actuator.

    摘要翻译： 实施例包括一种组件，包括：（a）照相机支撑结构，包括：桅杆，其设置在桅杆的远端上，其中桅顶被构造成接收成像元件; 其中所述桅杆的近端可旋转地接合方位角接头组件，其中所述方位角接头组件包括第一旋转自由度的第一角度致动器和第二旋转自由度的第二角度致动器; 和（b）相机支撑结构外壳，其包括孔和舱口，其中所述舱口被弹性偏压以关闭所述孔; 并且其中所述照相机支撑结构被配置为通过以下至少一个来克服所述舱口弹性偏压：释放限制装载的弹簧的销和通过所述第一角度致动器和所述第二角致动器中的至少一个的所述桅杆的旋转致动 。

    UAV PAYLOAD MODULE CAMERA ASSEMBLY AND RETRACTION MECHANISM
    3.
    发明申请
    UAV PAYLOAD MODULE CAMERA ASSEMBLY AND RETRACTION MECHANISM 有权
    无人机PAYLOAD模块摄像机组件和回退机构

    公开(公告)号：US20130193269A1

    公开(公告)日：2013-08-01

    申请号：US13730828

    申请日：2012-12-29

    申请人： John Peter Zwaan ,  Pavel Belik ,  Manolis Dimotakis ,  Christopher J. D'Aquila

    发明人： John Peter Zwaan ,  Pavel Belik ,  Manolis Dimotakis ,  Christopher J. D'Aquila

    IPC分类号： B64D47/08

    CPC分类号： B64D47/08 ,  B64C39/024 ,  B64C2201/127 ,  B64D9/00 ,  B64D27/24

    摘要： In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payload. An elongated flexible drawing member is coupled between the housing and the winch, the elongated drawing flexible member being capable of being drawn by the winch to retract the payload within the housing.

    摘要翻译： 在一个可能的实施例中，提供了一种UAV有效载荷模块缩回机构，其包括枢转地附接到壳体的有效载荷。 安装偏置构件以将有效载荷偏离壳体，并且绞盘附接到有效载荷。 细长的柔性绘图构件联接在壳体和绞盘之间，细长的拉伸柔性构件能够被绞盘牵引以将有效载荷缩回到壳体内。