Booster rocket launching type unmanned aerial vehicle

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Booster rocket launching type unmanned aerial vehicle

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ZHOU TAO / GAO YAJING / YANG BIN / OUYANG QINGHUA / YAN XIANHAO / TIAN LEI / CHEN QIQUAN

The invention discloses a booster rocket launching type unmanned aerial vehicle. The booster rocket launching type unmanned aerial vehicle comprises an unmanned aerial vehicle unit and a booster rocket unit; the unmanned aerial vehicle unit comprises a fuselage, a bearing shaft is arranged below the fuselage, and the fuselage is further provided with two through holes; the prompting circuit is provided with a power supply and a first indicating lamp connected in series with the power supply; the two reinforcing seats are arranged in the internal space of the machine body to form a switch structure, and when the two reinforcing seats are switched on, the prompting circuit is switched on, and the first indicating lamp is lightened; the booster rocket unit comprises: a body; a push rod; the two metal ejector rods are arranged at intervals and are electrically connected, one end of each metal ejector rod is connected with the body, the other end of each metal ejector rod is used for penetrating through the corresponding through hole to abut against the corresponding reinforcing base, and when the two metal ejector rods abut against the two reinforcing bases respectively, the two reinforcing bases are conducted. By arranging the simple prompt circuit on the booster rocket unit, the assembly position of the metal ejector rod can be fed back, the blind insertion effect can be achieved, and the launching problem caused by the fact that the metal ejector rod does not make reliable contact with the reinforcing base is effectively solved.

本申请公开了一种助推火箭发射式无人机，包括无人机单元以及助推火箭单元；无人机单元包括：机身，下方具有承力轴，还具有两个贯穿孔；提示电路，具有电源以及与电源串联的第一指示灯；以及两个加强座，设于机身内部空间形成开关结构，当两个加强座被导通时，提示电路导通，第一指示灯点亮；助推火箭单元包括：本体；推杆；两根间隔设置且电性连接的金属顶杆，金属顶杆的一端与本体连接，另一端用于穿过对应贯穿孔后与对应的加强座相抵，当两个金属顶杆分别抵住两个加强座时，两个加强座被导通。本申请通过在助推火箭单元上设置简单提示电路能够对金属顶杆的装配位置进行反馈，能够实现盲插的效果，有效解决了金属顶杆未与加强座可靠接触导致的发射问题。

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Document information

Title :

Booster rocket launching type unmanned aerial vehicle

Additional title:

助推火箭发射式无人机

Contributors:

ZHOU TAO (author) / GAO YAJING (author) / YANG BIN (author) / OUYANG QINGHUA (author) / YAN XIANHAO (author) / TIAN LEI (author) / CHEN QIQUAN (author)

Publication date :

2024-01-23

Type of media :

Patent

Type of material :

Electronic Resource

Language :

Chinese

Classification :

IPC:

B64U