A vehicle-mounted unmanned aerial vehicle launching device
Patent Information
- Application Number
- CN202522058778.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-09-25
- Publication Date
- 2026-08-28
- Estimated Expiration
- 2035-09-25
AI Technical Summary
[0006]本实用新型的目的在于提供一种车载无人机发射装置,以解决上述背景技术中提出的该装置在使用的过程中只能针对同一型号的无人机进行发射,并且发射的过程中无法针对多架无人机同时起飞,在针对多个型号的无人机进行起飞时需要更换不同型号的发射装置,严重降低了该发射装置使用的便捷性的问题
[0015]1.将发射架与车架底盘稳固结合,显著提升了无人机发射的便捷性和机动性,工具箱与发控箱的内置布局,使得操作人员在车内即可完成发射前的各项准备工作,大大缩短了部署时间。
Smart Images

Figure CN224690487U_ABST
Abstract
Claims
1. A vehicle-mounted unmanned aerial vehicle (UAV) launcher, comprising a vehicle body (1) and a chassis (2) disposed at the rear end of the vehicle body (1), wherein a launcher (3) is disposed at the upper end of the chassis (2). Its features are: The launcher (3) is equipped with a toolbox (4) and a launch control box (5) inside. The lower end of the launcher (3) is equipped with a standard container mushroom head interface (8). The launcher corner piece (7) on the outside of the launcher (3) is used to control the fixation between the standard container mushroom head interface (8) and the chassis (2). The launcher (3) is equipped with a launch plate (16) inside. The upper end of the launch plate (16) is equipped with a UAV launch rail (6). The motion structure inside the launcher (3) can adjust the internal space of the launcher (3) to accommodate the launch of different UAV models. The buffer structure inside the launcher (3) can reduce the impact of the vehicle driving on bumpy roads on the UAV.
2. The vehicle-mounted unmanned aerial vehicle launching device according to claim 1, characterized in that: The motion structure includes a vertical plate (9), which is fixedly installed inside the launcher (3). A connecting plate (10) is slidably installed inside the vertical plate (9), and positioning grooves (11) are provided at equal intervals inside the vertical plate (9).
3. The vehicle-mounted unmanned aerial vehicle launching device according to claim 2, characterized in that: The connecting plate (10) is slidably installed with a positioning element (24), and the positioning element (24) is engaged with the positioning groove (11). A sliding rod (12) is fixedly installed at the end of the positioning element (24) away from the vertical plate (9).
4. The vehicle-mounted unmanned aerial vehicle launching device according to claim 3, characterized in that: The sliding rod (12) is fixedly installed with a pressing member (13) at one end away from the positioning member (24), and a telescopic rod (14) is fixedly installed between the two sets of pressing members (13), and a support spring (15) is provided inside the telescopic rod (14).
5. The vehicle-mounted unmanned aerial vehicle launching device according to claim 4, characterized in that: The buffer structure includes a limiting rod (17), which is fixedly installed at the lower end of the launch plate (16). Two sets of sliding blocks (25) are slidably installed on the outer side of the limiting rod (17), and a buffer spring (23) is provided between the two sets of sliding blocks (25).
6. The vehicle-mounted unmanned aerial vehicle launching device according to claim 5, characterized in that: The lower end of the sliding block (25) is rotatably mounted with a rotating rod (18), and the two sets of rotating rods (18) are rotatably connected. The lower end of the rotating rod (18) is rotatably mounted with a moving block (19), and the moving rod (20) is fixedly mounted at the ends of the two sets of moving blocks (19) that are far apart from each other.
7. The vehicle-mounted unmanned aerial vehicle launching device according to claim 6, characterized in that: The fixed cylinder (21) slidably installed on the outside of the moving rod (20) is fixedly connected to the upper end of the connecting plate (10), and the fixed cylinder (21) is provided with an air hole (22).
Citation Information
Patent Citations
Brake for unmanned aerial vehicle launching device and unmanned aerial vehicle launching device
CN118289252A