The invention relates to a cross-medium unmanned aerial vehicle carrier and an unmanned aerial vehicle launching method.The cross-medium unmanned aerial vehicle carrier comprises a pressure-resistant pipe body with the two ends communicated and an ejection device, the pressure-resistant pipe body is used for containing an unmanned aerial vehicle, a head cover is installed at one end of the pressure-resistant pipe body in a sealed mode, a tail cabin is installed at the other end of the pressure-resistant pipe body in a sealed mode, and fins and an actuator are arranged outside the pressure-resistant pipe body; a control device is mounted in the tail cabin; one end of each fin is hinged to the outside of the pressure-resistant pipe body, the fins are connected with the output end of the actuator, and the actuator is used for driving the fins to swing so as to change the included angle between the axis of the fins and the axis of the pressure-resistant pipe body; when the included angle is zero, the fins, the pressure-resistant pipe body, the head cover and the tail cabin are integrally a streamline spiral body; and when the included angle is the preset angle and the carrier floats on the water surface, the included angle between the axis of the pressure-resistant pipe body and the horizontal plane is the take-off attitude angle of the unmanned aerial vehicle, so that the attitude adjustment of the carrier is realized, the unmanned aerial vehicle can take off at the attitude angle, and the adaptability of the carrier under severe sea conditions is improved.
本发明涉及一种跨介质无人机载具及无人机发射方法,包括两端贯通的耐压管体和弹射装置,耐压管体用于容纳无人机,耐压管体的一端密封安装有头罩,耐压管体的另一端密封安装有尾舱,耐压管体的外部设置有翅片和作动器,尾舱内安装有控制装置;翅片的一端与耐压管体的外部铰接,翅片与作动器的输出端连接,作动器用于驱动翅片摆动,进而改变翅片的轴线与耐压管体的轴线之间的夹角;当夹角为零时,翅片、耐压管体、头罩和尾舱整体呈流线旋成体;当夹角为预设角度且载具浮于水面时,耐压管体的轴线与水平面的夹角为无人机的起飞姿态角,从而实现载具姿态的调整,使无人机能够在姿态角下起飞,提高载具在恶劣海况下的适应性。
Cross-medium unmanned aerial vehicle carrier and unmanned aerial vehicle launching method
跨介质无人机载具及无人机发射方法
2024-10-15
Patent
Electronic Resource
Chinese
IPC: | B64U |
Unmanned aerial vehicle launching method and unmanned aerial vehicle pneumatic launching pad
European Patent Office | 2024
|UNMANNED AERIAL VEHICLE AND METHOD FOR LAUNCHING UNMANNED AERIAL VEHICLE
European Patent Office | 2021
|European Patent Office | 2024
|European Patent Office | 2025
|