CN215285271U

CN215285271U - Multi-tube emitter for unmanned aerial vehicle

Info

Publication number: CN215285271U
Application number: CN202120675997.6U
Authority: CN
Inventors: 郑潇华; 闵雪生; 李惠国; 胡亚伟; 王振武
Original assignee: Regimental Police Detachment Huzhou Public Security Bureau
Current assignee: Regimental Police Detachment Huzhou Public Security Bureau
Priority date: 2021-04-02
Filing date: 2021-04-02
Publication date: 2021-12-24
Anticipated expiration: 2031-04-02

Abstract

The utility model provides a multitube transmitter for unmanned aerial vehicle, includes the base, installs a plurality of launching tubes on the base, set up in the both ends of base and be used for with unmanned aerial vehicle articulated first connecting piece and second connecting piece and set up in camera and control panel on the base. The utility model discloses the transmitter angle can be adjusted by oneself, but independent remote control or directly take over control right to the unmanned aerial vehicle remote control unit on moreover, consequently can not require unmanned aerial vehicle adjustment gesture, is favorable to unmanned aerial vehicle flight in-process free transmission, and control logic is simple.

Description

Multi-tube emitter for unmanned aerial vehicle

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle equipment, concretely relates to multitube transmitter for unmanned aerial vehicle.

Background

Unmanned Aerial Vehicles (UAVs) are changing in the development level of China, and Unmanned Aerial vehicles also tend to have low flying cost and are easy and convenient to control. Because the characteristic of unmanned aerial vehicle can replace the manual work to carry out the task that has the particularity, consequently unmanned aerial vehicle's application also more and more extensive, has obtained the favor of individual trade consumer.

Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle is applied in the industry and is really just needed by the unmanned aerial vehicle. At present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

Under some special scenes of police departments, an electric primer launching device needs to be loaded on the unmanned aerial vehicle, and tear shells, smoke shells and the like are launched through remote control. However, adopt the outstanding problem of unmanned aerial vehicle remote control transmission ammunition to lie in, launcher need predetermine the angle on ground, and launcher angle can't adjust when unmanned aerial vehicle is in the air operation, angle regulation can only come through adjustment unmanned aerial vehicle's gesture, angle regulation inflexibility not only, and control unmanned aerial vehicle's logic is complicated moreover, can only adjust back angle regulation again with unmanned aerial vehicle, so not only inefficiency, the very big possibility in place of input changes moreover, lead to actual effect relatively poor.

Document CN2019202232266 discloses an unmanned aerial vehicle mounted aerial trapping net emitter. The unmanned aerial vehicle hanging frame plate is connected with an unmanned aerial vehicle, and the lower part of the unmanned aerial vehicle hanging frame plate is connected to the transmitter body through a suspension arm, wherein the unmanned aerial vehicle hanging frame plate is provided with a groove matched with the bottom of the unmanned aerial vehicle, the front end of the unmanned aerial vehicle hanging frame plate is provided with a connecting interface, and the connecting interface comprises a power supply interface and a control signal interface; the suspension arm is connected with the transmitter body through a hinge, and the suspension arm adjusts the pitch angle of the transmitter body through a control signal transmitted by the unmanned aerial vehicle; the launcher body comprises three catching net bores, and the three catching net bores respectively comprise net bullets. However, the device is not suitable for the electric primer launcher because the electric primer launcher has a large size and strong impact force of the launched projectile, and even if the device can be loaded, the device can cause the launch angle to shift, and the application effect is poor.

SUMMERY OF THE UTILITY MODEL

To the problem that above-mentioned exists, the utility model aims at providing a multitube transmitter for unmanned aerial vehicle, the transmitter angle can be adjusted by oneself, but independent remote control or direct take over control right to unmanned aerial vehicle remote control unit in addition, but wide application in police affairs tasks such as military striking, group's nature incident, extreme riot case incident.

In order to achieve the above purpose, the technical solution of the present invention is as follows:

the utility model provides a multitube transmitter for unmanned aerial vehicle, includes the base, installs a plurality of launching tubes on the base, set up in the both ends of base and be used for with unmanned aerial vehicle articulated first connecting piece and second connecting piece and set up in camera and control panel on the base.

In the scheme design, the pedestal mounting is in unmanned aerial vehicle's lower extreme, and the camera can realize functions such as range finding, aim, and the control panel not only can control the transmitter and launch the ammunition, and the rotatory transmission angle that is used for adjusting the transmitter of a connecting piece in steerable first connecting piece and the second connecting piece moreover at least.

As the utility model discloses a preferred, first connecting piece include with unmanned aerial vehicle's left socle be connected first fixed plate, with first erection column that first fixed plate is connected, cup joint in outside the first erection column and with base surface connects's first connecting plate and with the drive gear that first connecting plate meshing and be connected with the driving motor output, driving motor with the control panel electricity is connected.

As the utility model discloses a preferred, driving motor install in on the mounting platform that first erection column surface was seted up.

As the utility model discloses a preferred, the second connecting piece include with unmanned aerial vehicle's right branch frame attach the second fixed plate, with the second erection column that the second fixed plate is connected and cup joint in outside the second erection column and with the second connecting plate of base surface connection.

As the utility model discloses a preferred, the surface of second erection column is through setting up the external screw thread in order to be used for spiro union fixation nut.

As the utility model discloses a preferred, second erection column one end is passed first through-hole, the other end of seting up on the second connecting plate pass the second through-hole of seting up on the second fixed plate has the fixed block at end connection.

As the utility model discloses a preferred, the camera install in with the launching tube is with the surface of one side, the control panel install in different in the surface of launching tube one side.

As the utility model discloses a preferred, seted up the internal diameter on the first connecting plate and be greater than the round hole of first erection column external diameter.

As the utility model discloses a preferred, the first connecting plate is transversal to personally submit the major arc bow, just first connecting plate surface be provided with drive gear meshed's tooth.

Preferably, the axis extension line of the first mounting post coincides with the axis extension line of the second mounting post.

To sum up, the utility model discloses following beneficial effect has:

the utility model provides a multitube transmitter for unmanned aerial vehicle not only can stable installation in the unmanned aerial vehicle lower extreme, and angular stability is adjustable moreover, can realize remote operation, has guaranteed that operating personnel's life safety, place require low, emergency treatment is fast, the transmission accuracy is high, can launch at any time.

The utility model provides a multitube transmitter for unmanned aerial vehicle can launch the ammunition many times, saves ammunition filling time, has improved efficiency.

The utility model provides a multitube transmitter for unmanned aerial vehicle can control logic freely adjust the turned angle through unmanned aerial vehicle, consequently can not require unmanned aerial vehicle adjustment gesture, is favorable to unmanned aerial vehicle flight in-process free transmission, and control logic is simple.

Drawings

Fig. 1 is a schematic structural diagram of the transmitter of the present invention.

Figure 2 is the utility model discloses a transmitter and unmanned aerial vehicle's relation of connection and schematic structure.

Fig. 3 is a schematic structural diagram of the first connecting member of the present invention.

Fig. 4 is the mounting structure schematic diagram of the driving motor of the present invention.

Fig. 5 is a schematic structural diagram of a second connecting member according to the present invention.

Fig. 6 is a schematic view of the mounting structure of the first fixing plate of the present invention.

Reference numerals: the camera comprises a base 1, a transmitting tube 11, a camera 12, a control panel 13, a first connecting piece 2, a first connecting plate 21, a round hole 211, teeth 212, a first mounting column 22, a mounting platform 221, a first fixing plate 23, a driving motor 24, a driving gear 25, a second connecting piece 3, a second connecting plate 31, a first through hole 311, a second mounting column 32, an external thread 321, a second fixing plate 33, a second through hole 331, a fixing nut 34, a fixing block 35, a left support 41 and a right support 42.

Detailed Description

Examples

As shown in fig. 1, the multi-tube launcher for the unmanned aerial vehicle provided by the present embodiment includes a base 1, six launching tubes 11 installed on the base 1, a first connecting piece 2 and a second connecting piece 3 arranged at two ends of the base 1 and used for being hinged with the unmanned aerial vehicle, and a camera 12 and a control panel 13 arranged on the base 1. In this embodiment, the camera 12 is installed on the surface of the same side as the launch tube 11 and is located at the center of the base 1, and the control board 13 is installed on the surface of a different side from the launch tube 11 and is located between the first connecting member 2 and the second connecting member 3. The extension line of the axis of the first mounting column 22 is coincident with the extension line of the axis of the second mounting column 32, so that the first connecting piece 2 and the second connecting piece 3 synchronously rotate when the base 1 rotates.

In the present embodiment, the camera 12 can perform ranging, aiming, and the like, and the control board 13 can control not only the launcher to launch the ammunition, but also the first connecting member 2 to rotate for adjusting the launching angle of the launcher. The base 1 is internally provided with electric primers for replacing firing pins in one-to-one correspondence with the firing tubes 11, while the base 1 as a whole can be opened for filling ammunition.

In this embodiment, as shown in fig. 2 to 4, the first connecting member 2 includes a first fixing plate 23 connected to a left bracket 41 of the unmanned aerial vehicle, a first mounting post 22 connected to the first fixing plate 23, a first connecting plate 21 sleeved outside the first mounting post 22 and connected to the surface of the base 1, and a driving gear 25 engaged with the first connecting plate 21 and connected to an output end of a driving motor 24. In this embodiment, the left brackets 41 are two front and rear brackets, and the first fixing plate 23 is fixedly connected between the two left brackets 41. The cross section of the first connecting plate 21 is a major arc arch, and the surface of the first connecting plate 21 is provided with teeth 212 meshed with the driving gear 25. The angular range of the major arc bow can satisfy the angular range of the first connecting plate 21 driving the base 1 to rotate. The driving motor 24 is installed on an installation platform 221 formed on the surface of the first installation column 22, and the driving motor 24 is electrically connected with the control board 13. The installation platform 221 is provided with a horizontal plane to enable the driving motor 24 to be installed stably, and further, the driving motor 24 is fixed on the surface of the installation platform 221 through four fixing screws. The inner diameter of the circular hole 211 formed in the first connecting plate 21 is larger than the outer diameter of the first mounting column 22 so as to reduce the friction between the first mounting column 22 and the first connecting plate 21.

In this embodiment, the second connecting member 3 includes a second fixing plate 33 connected to the right bracket 42 of the drone, a second mounting post 32 connected to the second fixing plate 33, and a second connecting plate 31 sleeved outside the second mounting post 32 and connected to the surface of the base 1. In this embodiment, the right brackets 42 are two front and rear brackets, and the second fixing plate 33 is fixedly connected between the two right brackets 42. The surface of the second mounting post 32 is provided with external threads 321 for screwing the fixing nut 34. The fixing nut 34 is screwed to the second mounting post 32 and abuts against a surface of the second fixing plate 33 on the side closer to the second connecting plate 31. One end of the second mounting post 32 passes through a first through hole 311 formed in the second connecting plate 31, and the other end passes through a second through hole 331 formed in the second fixing plate 33, and a fixing block 35 is connected to the end. The fixing block 35 abuts on a surface of the second fixing plate 33 on a side away from the second connecting plate 31.

The working principle of the embodiment is as follows: install base 1 in unmanned aerial vehicle's lower extreme, control unmanned aerial vehicle flies to the assigned position, then the transmission angle of base 1 is confirmed to the signal that conveys back through camera 12, and driving motor 24 is owing to with control panel 13 signal connection, consequently behind the receipt control signal, thereby the rotation angle of base 1 has been adjusted in driving motor 24's rotation angle adjustment. This device does not require unmanned aerial vehicle adjustment gesture, is favorable to unmanned aerial vehicle flight in-process free launch, and control logic is simple.

The specific embodiments described herein are merely illustrative of the spirit of the invention. Various modifications, additions and substitutions for the specific embodiments described herein may be made by those skilled in the art without departing from the spirit of the invention or exceeding the scope of the invention as defined in the accompanying claims.

Claims

1. The utility model provides a multitube transmitter for unmanned aerial vehicle, its characterized in that includes base (1), installs a plurality of launching tubes (11) on base (1), set up in the both ends of base (1) and be used for with unmanned aerial vehicle articulated first connecting piece (2) and second connecting piece (3) and set up in camera (12) and control panel (13) on base (1).

2. The multi-tube launcher for unmanned aerial vehicles according to claim 1, wherein the first connecting member (2) comprises a first fixing plate (23) connected with a left bracket (41) of the unmanned aerial vehicle, a first mounting post (22) connected with the first fixing plate (23), a first connecting plate (21) sleeved outside the first mounting post (22) and connected with the surface of the base (1), and a driving gear (25) engaged with the first connecting plate (21) and connected with an output end of a driving motor (24), and the driving motor (24) is electrically connected with the control board (13).

3. The multiple tube launcher for unmanned aerial vehicle according to claim 2, wherein the driving motor (24) is mounted on a mounting platform (221) provided on a surface of the first mounting post (22).

4. A multiple tube launcher for unmanned aerial vehicle according to claim 2, wherein the second connector (3) comprises a second fixing plate (33) connected to the right bracket (42) of the unmanned aerial vehicle, a second mounting post (32) connected to the second fixing plate (33), and a second connecting plate (31) sleeved outside the second mounting post (32) and connected to the surface of the base (1).

5. A multiple tube launcher for unmanned aerial vehicles according to claim 4, wherein the surface of the second mounting post (32) is provided with external threads (321) for screwing a fixing nut (34).

6. The multiple tube launcher for unmanned aerial vehicle according to claim 5, wherein the second mounting post (32) has one end passing through a first through hole (311) formed in the second connecting plate (31) and the other end passing through a second through hole (331) formed in the second fixing plate (33) and has a fixing block (35) connected to the end.

7. A multiple tube emitter for unmanned aerial vehicle according to claim 1, wherein said camera (12) is installed on a surface on the same side as said emitting tube (11), and said control board (13) is installed on a surface on a side different from said emitting tube (11).

8. The multi-tube launcher for unmanned aerial vehicles according to claim 2, wherein the first connecting plate (21) is formed with a circular hole (211) having an inner diameter larger than an outer diameter of the first mounting post (22).

9. A multiple tube launcher for unmanned aerial vehicles according to claim 2, wherein the first connecting plate (21) is arcuate in cross section and the first connecting plate (21) is provided with teeth (212) on its surface that engage with the drive gear (25).

10. A multiple tube launcher for unmanned aerial vehicles according to claim 4, wherein the extension of the axis of the first mounting post (22) coincides with the extension of the axis of the second mounting post (32).