CN218055629U

CN218055629U - Unmanned aerial vehicle cloud platform mechanism of carry grenade transmitter

Info

Publication number: CN218055629U
Application number: CN202220923584.XU
Authority: CN
Inventors: 李万根; 崔俊超; 喻江峰; 连涛
Original assignee: Hebei Zingto Aviation Technology Co ltd
Current assignee: Hebei Zingto Aviation Technology Co ltd
Priority date: 2022-04-20
Filing date: 2022-04-20
Publication date: 2022-12-16
Anticipated expiration: 2032-04-20

Abstract

The utility model provides an unmanned aerial vehicle cloud platform mechanism of carry grenade transmitter, aim module and grenade transmitter including cloud platform main part, light is aimed module and grenade transmitter and is installed respectively in cloud platform main part pitch axis both sides. The utility model discloses light aiming module and grenade transmitter are located same cloud platform system, and light aiming module and grenade transmitter realize the nimble accurate motion of course and every single move with the help of the cloud platform, are convenient for look for the target fast and implement accurate strike, strike the error little; the light aiming module and the grenade emitter synchronously move in course and respectively move in pitching mode, after the aiming module finds the target, the course axis of the grenade emitter does not need to be changed, and the grenade can be started only by adjusting the pitching firing angle, so that the target can be struck quickly; the grenade launcher adjusts the firing angle without influencing the pitching angle of the aiming module, can dynamically observe the state of the hit target in real time, can synchronously observe whether the grenade cannon hits or not, and is convenient for timely adjustment to carry out secondary hit; compared with the prior art, the method is more accurate and efficient, and user experience is better.

Description

Unmanned aerial vehicle cloud platform mechanism of carry grenade transmitter

Technical Field

The utility model belongs to the technical field of the unmanned aerial vehicle technique and specifically relates to an unmanned aerial vehicle cloud platform mechanism of carry grenade transmitter is related to.

Background

Unmanned aerial vehicle product develops rapidly in recent years, has constantly brand-new brand and product bright phase, and meanwhile, the unmanned aerial vehicle accessory that releases to the trade is also constantly emerging, and these unmanned aerial vehicle accessories play an important role in each trade field.

The grenade transmitter has the characteristics of high power, long range and small recoil, so that the grenade transmitter is very suitable for being mounted on an unmanned aerial vehicle, and the automatic grenade transmitter is mounted on a light small unmanned aerial vehicle and scientifically integrated with the light small unmanned aerial vehicle, so that the military purpose of the armed unmanned aerial vehicle is realized; in the prior art, most of grenade launchers are only directly installed on an unmanned aerial vehicle, and the course axis and the pitching axis of the grenade launcher are controlled by the attitude adjustment of the unmanned aerial vehicle; a few products add an independent shooting angle adjusting mechanism for the grenade launcher, but the heading axis is still controlled by the attitude of the unmanned aerial vehicle, for example, a rotor armed unmanned aerial vehicle carrying an automatic grenade launcher disclosed in CN201710829473.6, the automatic grenade launcher is connected with a guide rod of an aiming angle control device of an unmanned aerial vehicle platform through a connecting component, because the accuracy of the heading adjusting attitude of the unmanned aerial vehicle is low, and the pitching direction is difficult to maintain at a specific angle, the efficiency and the accuracy of the method are low; meanwhile, in the prior art, the grenade launcher of the unmanned aerial vehicle is provided with the aiming modules, some aiming modules are rigidly mounted on the grenade launcher, the image is unstable due to high-frequency vibration and low-frequency shaking of the unmanned aerial vehicle, the effect is poor, the grenade launcher can hit the target only by adjusting the pitching firing angle under the action of gravity after the target is found to be a parabola, the image of the aiming module is separated from the target due to the change of the pitching firing angle, the target is difficult to dynamically observe, and the hit rate is low; some aiming modules are installed on the cloud platform, can be nimble carry out each direction adjustment and look for the target, but in case find the target, because the grenade transmitter need adjust to with aiming module same direction, efficiency is lower, and skew motion has probably taken place for the target in the adjustment process, because the grenade transmitter relies on the difficult accurate adjustment gesture of unmanned aerial vehicle, so leads to being difficult to accurate striking moreover.

SUMMERY OF THE UTILITY MODEL

To the problem that above-mentioned background art expounded, the utility model aims to solve the technical problem that an unmanned aerial vehicle cloud platform mechanism of carry grenade transmitter is provided, solve among the prior art problem that unmanned aerial vehicle carries grenade transmitter inefficiency, precision are poor.

In order to achieve the above object, the utility model provides a following technical scheme:

the utility model provides an unmanned aerial vehicle cloud platform mechanism of carry grenade transmitter, includes cloud platform main part, light and aims module and grenade transmitter, the both sides at cloud platform main part pitch axis are installed respectively to light and aims module and grenade transmitter.

In the technical scheme, the holder main body comprises a top plate, a course motor, a connecting arm, a pitching motor A and a pitching motor B; the course motor is positioned between the bottom surface of the top plate and the top end of the connecting arm to form a tripod head course rotating shaft.

In the technical scheme, the axes of the pitching motor A and the pitching motor B are overlapped and are respectively positioned at two sides of the lower end of the connecting arm.

In the above technical scheme, the light aiming module is installed on a pitching motor B through a light aiming fixing piece, the grenade launcher further comprises a grenade launcher fixing piece, and the grenade launcher is installed on a pitching motor A through a weapon fixing piece.

In the above technical solution, the connecting arm structure is "L" shaped.

In the above technical scheme, the optical sighting module includes a fixed-focus camera, a zoom camera, and a ranging module with a ranging function.

The utility model discloses light aims module and grenade transmitter and is located same cloud platform system, and light aims module and grenade transmitter and realizes the nimble accurate motion of course and every single move with the help of the cloud platform, is convenient for look for the target fast and implement accurate striking, and the strike error is littleer; the light aiming module and the grenade emitter synchronously move in course and respectively move in pitching mode, after the aiming module finds the target, the course axis of the grenade emitter does not need to be changed, and the grenade can be started only by adjusting the pitching firing angle, so that the target can be struck quickly; the grenade launcher adjusts the firing angle without influencing the pitching angle of the aiming module, can dynamically observe the state of the hit target in real time, can synchronously observe whether the grenade cannon hits or not, and is convenient for timely adjustment to carry out secondary hit; compared with the prior art, the method is more accurate and efficient, and user experience is better.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the description below are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without inventive labor.

Fig. 1 is an explosion diagram of the structure of the embodiment of the utility model.

Fig. 2 is a schematic perspective view of an embodiment of the present invention.

Fig. 3 is a schematic diagram of the target searching mode according to the embodiment of the present invention.

Fig. 4 is a schematic view of a target hitting mode according to an embodiment of the present invention.

Fig. 5 is a schematic view of a main structure of a holder according to an embodiment of the present invention.

Wherein: the device comprises a top plate 1, an 11-course shaft motor, a 2 connecting arm, a 21 pitching motor A, a 22 pitching motor B, a 3 light aiming module, a 4 grenade emitter, a 5 weapon fixing part, a 6 screw and a 7 target.

Detailed Description

The technical solution of the present invention will be described clearly and completely with reference to the accompanying drawings of the present invention, and obviously, the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

According to the illustrations of fig. 1, 2 and 5, as an example: the utility model provides an unmanned aerial vehicle cloud platform mechanism of carry grenade transmitter, includes cloud platform main part, light and aims module and grenade transmitter, light is aimed module and grenade transmitter and is installed respectively in the both sides of cloud platform main part pitch axis, and the roof is connected with flight platforms such as unmanned aerial vehicle, and the connected mode includes but not limited to bolted connection's mode, and the linking arm upper end of "L" shape is connected to course axle motor of main cloud platform roof below, passes through screw fixed connection pitch motor A and pitch motor B at the linking arm lower extreme.

The pitching motor B is fixedly connected with a light aiming module through a screw, and the light aiming module belongs to the prior art and comprises a fixed-focus camera, a zooming camera and a distance measuring module with a distance measuring function, and can also be a pure camera; the pitching motor A is fixedly connected with a weapon fixing piece through a screw, and the weapon fixing piece is fixedly connected with the grenade launcher through a screw.

According to fig. 3 and 4, the principle of the present invention is as follows: the grenade launcher is arranged on the holder, and the course angle and the pitching angle of the grenade launcher can move, so that the grenade launcher is more flexible compared with the prior art; the grenade launcher and the aiming module are arranged on the same cloud deck system, the course moves synchronously, and the pitching can move respectively; the heading axis shares one axis, the pitching axes are independent respectively, when a target is searched, the heading and pitching of the grenade emitter and the aiming module move together, once the target is found, the heading axis is locked, the pitching axes of the grenade emitter and the aiming module start to move independently respectively, the pitching motion of the grenade emitter adjusts the firing angle, the grenade gun can hit the target through a parabola under the action of gravity, meanwhile, the pitching axis of the aiming module does not move together with the grenade emitter, but locks the target, the hit state of the target is observed in real time, the posture is adjusted and secondary hitting is performed as appropriate, and the device is more efficient, more accurate and better in experience.

Therefore, the above-mentioned embodiments are only specific embodiments of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art can easily think of the changes or substitutions within the technical scope of the present invention, and all should be covered by the scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.

Claims

1. The utility model provides a carry unmanned aerial vehicle cloud platform mechanism of grenade transmitter which characterized in that: including cloud platform main part, light aim module and grenade transmitter, the both sides at cloud platform main part pitch axis are installed respectively to light aim module and grenade transmitter.

2. The mechanism of claim 1, wherein the mechanism comprises: the holder main body comprises a top plate, a course motor, a connecting arm, a pitching motor A and a pitching motor B; the course motor is positioned between the bottom surface of the top plate and the top end of the connecting arm to form a tripod head course rotating shaft.

3. The mechanism of claim 2, wherein the mechanism comprises: the axes of the pitching motor A and the pitching motor B are overlapped and are respectively positioned at two sides of the lower end of the connecting arm.

4. The mechanism of claim 3, wherein the mechanism comprises: the connecting arm structure is L-shaped.

5. The mechanism of claim 4, wherein the mechanism comprises: the light is aimed the module and is installed on every single move motor B through the light and aims the mounting, the grenade transmitter still includes grenade transmitter mounting, and the grenade transmitter passes through the weapon mounting and installs on every single move motor A.

6. The mechanism of claim 5, wherein the mechanism comprises: the light aiming module comprises a fixed-focus camera, a zoom camera and a distance measuring module with a distance measuring function.