UNMANNED AERIAL VEHICLE, IMAGE PHOTOGRAPHING APPARATUS, AND CRADLE HEAD THEREOF

    公开(公告)号:EP3372888A1

    公开(公告)日:2018-09-12

    申请号:EP16861349.5

    申请日:2016-08-01

    Abstract: The present application relates to a gimbal configured to mount a photographing device. The gimbal includes a main body, a mounting shaft connected to the main body and a base disposed on the mounting shaft. The base is configured to fasten the photographing device. The gimbal further includes a fixing plate disposed on the base and a circuit board mounted between the fixing plate and the base. The circuit board is provided with a USB input interface and a USB output interface. The USB input interface is configured to form a data transmission connection to the photographing device. The USB output interface is configured to be connected to an external storage device. The present application further relates to an image photographing apparatus including the foregoing gimbal and an unmanned aerial vehicle including the foregoing image photographing apparatus. In the present application, data in the photographing device on the gimbal may be directly accessed by using a USB data line. A trouble of repeatedly dismounting and mounting the photographing device can be avoided. Friction losses of related structures of the photographing device and the gimbal are avoided, thereby prolonging service lives of the components.

    DEVICE WHEREBY AN AIRCRAFT CAN LAND ON WATER
    180.
    发明公开
    DEVICE WHEREBY AN AIRCRAFT CAN LAND ON WATER 审中-公开
    VORRICHTUNG ZURERMÖGLICHUNGDER LANDUNG EINES FLUGZEUGES AUF WASSER

    公开(公告)号:EP3135583A1

    公开(公告)日:2017-03-01

    申请号:EP11761644.1

    申请日:2011-06-20

    Abstract: The device comprises at least one folding, inflatable chamber (3), at least one runner (4) for landing on water, which is coupled to the aircraft (2) by means of the chamber (3), and at least one air intake (6) connected to the chamber. The intake (6) allows the entry of incident air into the chamber (3) in order to inflate and deploy the chamber (3), extending the runner (4) from a retracted-runner position into an extended-runner position

    Abstract translation: 该装置包括至少一个折叠的可充气室(3),至少一个用于着陆在水面上的流道(4),其通过腔室(3)联接到飞行器(2),并且至少一个进气口 (6)连接到腔室。 入口(6)允许入口空气进入腔室(3),以便使空腔(3)膨胀和展开,从而将流道(4)从缩回流道位置延伸到延伸流道位置

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