CN218703949U

CN218703949U - Military unmanned aerial vehicle with monitoring function

Info

Publication number: CN218703949U
Application number: CN202222691618.XU
Authority: CN
Inventors: 吴子霖; 徐志勇
Original assignee: Scout Tactic Co ltd
Current assignee: Scout Tactic Co ltd
Priority date: 2022-10-13
Filing date: 2022-10-13
Publication date: 2023-03-24
Anticipated expiration: 2032-10-13

Abstract

The utility model belongs to the technical field of unmanned air vehicle, especially, for military use unmanned aerial vehicle with monitoring function to the problem of current easy damage camera, the following scheme is proposed at present, and it is including holding the case, it has the mounting bracket to hold fixed mounting on the case, the bottom of holding the case is provided with the landing leg, it is provided with the battery on the case to hold, it is provided with the control mainboard in the case to hold, be provided with signal receiver on the control mainboard, be provided with two motors on the mounting bracket, rotate on the mounting bracket and install four rotors, equal fixed mounting has the band pulley on four rotors, and the transmission is installed two belts on four band pulleys, it is provided with telescopic machanism in the case to hold, telescopic machanism includes electric putter, electric putter and the inner wall fixed connection who holds the case, the utility model discloses can receive and release the camera automatically, can reduce the damage of striking to the camera, and the security is higher, and is simple to use, convenient operation.

Description

Military unmanned aerial vehicle with monitoring function

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to a for military use unmanned aerial vehicle with monitoring function.

Background

Military unmanned aerial vehicles are unmanned aerial vehicles controlled and operated by remote control equipment or self-contained programs, and with the wide application of high and new technologies to weaponry, the development of unmanned aerial vehicles makes a breakthrough progress. Military unmanned aerial vehicle has the characteristics of exquisite structure, disguise nature are strong, convenient to use, low in cost and flexible performance, and mainly used battlefield reconnaissance, electronic interference carries weapons such as bomb tied in a bundle, guidance guided missile and carries out aggressive task to and as aerial communication relay platform, nuclear test sampler etc. the license bulletin number is CN206087353U and discloses a military unmanned aerial vehicle with monitoring function, including the unmanned aerial vehicle body, the bottom four corners of unmanned aerial vehicle body all is provided with the supporting leg, the bottom and the bracing piece of supporting leg are connected, the one end that the unmanned aerial vehicle body was kept away from to the supporting leg is provided with drive arrangement, the bottom center of baffle is provided with the telescopic link, the connecting piece that is provided with of telescopic link, the bottom of connecting piece is provided with the high definition camera, but this unmanned aerial vehicle, when stretching out the camera, all will lean on the camera to push away from the baffle at every turn, if the baffle stress is great, the camera is easily damaged to long-term use, if the baffle stress is less, is difficult to protect the camera, for this we have proposed a military with monitoring function for this.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that has the easy damage camera among the prior art, and the military unmanned aerial vehicle who provides with monitor function.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides a for military use unmanned aerial vehicle with monitoring function, is including holding the case, fixed mounting has the mounting bracket on holding the case, the bottom that holds the case is provided with the landing leg, it is provided with the battery on the case to hold, it is provided with the control mainboard to hold the incasement, be provided with signal receiver on the control mainboard, be provided with two motors on the mounting bracket, rotate on the mounting bracket and install four rotors, equal fixed mounting has the band pulley on four rotors, and the transmission is gone up to four band pulleys installs two belts, it is provided with telescopic machanism in the case to hold, telescopic machanism includes electric putter, electric putter and the inner wall fixed connection who holds the case, electric putter and two motors all with battery electric connection, electric putter and two motors all with control mainboard electric connection, electric putter is last fixed mounting panel, fixed mounting has the camera on the mounting panel, it is provided with the mechanism that opens and shuts to hold the incasement, the mechanism includes two racks, and two racks all with electric putter fixed connection, hold the incasement internal rotation and install two gears, two gears and two racks mesh mutually, equal fixed mounting has the bull stick on two bull sticks, and all install the second sprocket on two same chamber door, and all the transmission chain wheel and the same chamber door.

Preferably, two first bearings are arranged in the accommodating box, and inner rings of the two first bearings are fixedly connected with the two rotating rods.

Preferably, the mounting frame is provided with two motor bases, and the two motor bases are connected with the two motors in a clamping mode.

Preferably, the accommodating box is rotatably provided with two rotating shafts, and the two rotating shafts are fixedly connected with the two box doors.

Preferably, be provided with four second bearings on the mounting bracket, the inner circle of four second bearings respectively with the axostylus axostyle fixed connection of four rotors, be provided with the receiver in the holding box, be provided with the remote controller in the receiver.

The utility model discloses in, a military unmanned aerial vehicle's beneficial effect with monitor function: the cooperation setting of electric putter and mounting panel can release the camera and hold the case and facilitate the use among the telescopic machanism, can accomodate the camera, can protect the camera, conveniently carries, and the cooperation setting of rack, gear, bull stick, first sprocket, second sprocket and chain can rotate and open the chamber door among the mechanism that opens and shuts, makes things convenient for receiving and releasing of camera, can avoid the camera to damage because of the striking, improves the security.

The utility model discloses can receive and release the camera automatically, can reduce the striking to the damage of camera, the security is higher, simple to use, convenient operation.

Drawings

Fig. 1 is a schematic view of a three-dimensional structure of a military unmanned aerial vehicle with a monitoring function provided by the present invention;

fig. 2 is a schematic cross-sectional structural diagram of a military unmanned aerial vehicle with a monitoring function according to a first embodiment of the present invention;

fig. 3 is a schematic diagram of the right-side view structure of fig. 2 of a military unmanned aerial vehicle with a monitoring function according to the present invention;

fig. 4 is the utility model provides a for military use unmanned aerial vehicle's for military use embodiment two with monitoring function schematic diagram of sectional structure.

In the figure: 1. an accommodating case; 2. a mounting frame; 3. a support leg; 4. a battery; 5. a control main board; 6. a signal receiver; 7. a motor; 8. a pulley; 9. a belt; 10. a rotor; 11. an electric push rod; 12. mounting a plate; 13. a camera; 14. a rack; 15. a gear; 16. a rotating rod; 17. a first sprocket; 18. a second sprocket; 19. a chain; 20. a box door; 21. a torque spring; 22. a rotating electric machine.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

Example one

Referring to fig. 1-3, a military unmanned aerial vehicle with monitoring function, including holding case 1, fixed mounting has mounting bracket 2 on holding case 1, the bottom that holds case 1 is provided with landing leg 3, be provided with battery 4 on holding case 1, be provided with control mainboard 5 in holding case 1, be provided with signal receiver 6 on the control mainboard 5, be provided with two motors 7 on the mounting bracket 2, rotate on the mounting bracket 2 and install four rotors 10, equal fixed mounting has band pulley 8 on four rotors 10, the transmission is installed two belts 9 on four band pulleys 8, be provided with telescopic machanism in holding case 1, telescopic machanism includes electric putter 11, electric putter 11 and the inner wall fixed connection who holds case 1, electric putter 11 and two motors 7 all with battery 4 electric connection, electric putter 11 and two motors 7 all with control mainboard 5 electric connection, fixed mounting has mounting panel 12 on electric putter 11, fixed mounting has camera 13 on mounting panel 12, be provided with the mechanism that opens and shuts in holding case 1.

Referring to fig. 2-3, the opening and closing mechanism includes two racks 14, the two racks 14 are both fixedly connected with the electric push rod 11, two gears 15 are rotatably installed in the accommodating box 1, the two gears 15 are engaged with the two racks 14, rotating rods 16 are fixedly installed on the two gears 15, first chain wheels 17 are fixedly installed on the two rotating rods 16, two box doors 20 are rotatably installed on the accommodating box 1, second chain wheels 18 are fixedly installed on the two box doors 20, the same chain 19 is installed on the first chain wheels 17 and the second chain wheels 18 in a transmission manner, and torque springs 21 are arranged on the two box doors 20.

Referring to fig. 2-3, two first bearings are disposed in the accommodating box 1, inner rings of the two first bearings are fixedly connected to the two rotating rods 16, and the two first bearings are disposed to enable the two rotating rods 16 to rotate at fixed positions.

Referring to fig. 2-3, the mounting frame 2 is provided with four second bearings, inner rings of the four second bearings are respectively and fixedly connected with shaft rods of the four rotors 10, and the four second bearings are arranged to enable the four rotors 10 to rotate at fixed positions.

Referring to fig. 2, two rotating shafts are rotatably installed on the accommodating box 1, and the two rotating shafts are fixedly connected with the two box doors 20, and can enable the two box doors 20 to rotate at fixed positions.

Referring to fig. 2, the mounting frame 2 is provided with two motor bases, and the two motor bases are connected with the two motors 7 in a clamping manner.

In this embodiment, in use, two motors 7 are controlled through a remote controller, under the cooperation of two belt pulleys 8 and a belt 9, four rotor wings 10 are driven to rotate, control unmanned aerial vehicle flight, four rotor wings 10 fly more stably, when needing to be shot, electric push rod 11 is started, and then mounting plate 12 and two racks 14 are driven to descend, mounting plate 12 descends, and then camera 13 descends, which is convenient for use, two racks 14 descend, and then two gears 15 are driven to rotate, two gears 15 rotate, and then two rotating rods 16 rotate, and then two first chain wheels 17 rotate, under the cooperation of two chains 19, two first chain wheels 17 rotate, and then two second chain wheels 18 rotate, two box doors 20 are opened, which is convenient for camera 13 to extend out for use, when not in use, electric push rod 11 is controlled to retract camera 13, box door 20 is closed, under the elastic force of two torque springs 21, box door 20 is closed more tightly, and camera 13 can be better protected.

Example two

Referring to fig. 4, the difference between the present embodiment and the first embodiment is: hold case 1, hold fixed mounting and have mounting bracket 2 on case 1, the bottom that holds case 1 is provided with landing leg 3, it is provided with battery 4 on case 1 to hold, be provided with control mainboard 5 in the case 1, be provided with signal receiver 6 on the control mainboard 5, be provided with two motors 7 on the mounting bracket 2, rotate on the mounting bracket 2 and install four rotors 10, equal fixed mounting has band pulley 8 on four rotors 10, it has two belts 9 to transmit on four band pulleys 8, be provided with telescopic machanism in holding case 1, telescopic machanism includes electric putter 11, electric putter 11 and the inner wall fixed connection who holds case 1, electric putter 11 and two motors 7 all with battery 4 electric connection, electric putter 11 and two motors 7 all with control mainboard 5 electric connection, fixed mounting has mounting panel 12 on electric putter 11, fixed mounting has rotating electrical machines 22 on mounting panel 12, fixed mounting has camera 13 on the output shaft of rotating electrical machines 22, it is provided with the mechanism that opens and shuts in the case 1 to hold, when using camera 13, rotating electrical machines 22 can be opened, the angle of camera 13 can be adjusted, improve the shooting effect.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. A military unmanned aerial vehicle with a monitoring function comprises a containing box (1) and is characterized in that, the accommodating box (1) is fixedly provided with a mounting rack (2), the bottom of the accommodating box (1) is provided with supporting legs (3), a battery (4) is arranged on the containing box (1), a control main board (5) is arranged in the containing box (1), a signal receiver (6) is arranged on the control main board (5), the mounting rack (2) is provided with two motors (7), the mounting rack (2) is rotatably provided with four rotors (10), the four rotors (10) are respectively and fixedly provided with a belt wheel (8), the four belt wheels (8) are respectively and rotatably provided with two belts (9), a telescopic mechanism is arranged in the containing box (1), the telescopic mechanism comprises an electric push rod (11), the electric push rod (11) is fixedly connected with the inner wall of the containing box (1), the electric push rod (11) and the two motors (7) are electrically connected with the battery (4), the electric push rod (11) and the two motors (7) are both electrically connected with the control main board (5), the electric push rod (11) is fixedly provided with a mounting plate (12), the camera (13) is fixedly mounted on the mounting plate (12), and an opening and closing mechanism is arranged in the containing box (1).

2. The military unmanned aerial vehicle with the monitoring function according to claim 1, wherein the opening and closing mechanism comprises two racks (14), the two racks (14) are both fixedly connected with an electric push rod (11), two gears (15) are rotatably mounted in the accommodating box (1), the two gears (15) are meshed with the two racks (14), two rotating rods (16) are fixedly mounted on the two gears (15), first chain wheels (17) are fixedly mounted on the two rotating rods (16), two box doors (20) are rotatably mounted on the accommodating box (1), second chain wheels (18) are fixedly mounted on the two box doors (20), the same chain (19) is rotatably mounted on the first chain wheels (17) and the second chain wheels (18), and torque springs (21) are arranged on the two box doors (20).

3. The military unmanned aerial vehicle with monitoring function of claim 2, wherein two first bearings are arranged in the containing box (1), and inner rings of the two first bearings are fixedly connected with the two rotating rods (16).

4. The military unmanned aerial vehicle with monitoring function of claim 1, wherein the mounting rack (2) is provided with four second bearings, and inner rings of the four second bearings are fixedly connected with shaft rods of four rotors (10) respectively.

5. The military unmanned aerial vehicle with monitoring function of claim 2, wherein the containing box (1) is rotatably provided with two rotating shafts, and the two rotating shafts are fixedly connected with the two box doors (20).

6. The military unmanned aerial vehicle with monitoring function of claim 1, wherein the mounting rack (2) is provided with two motor bases, and the two motor bases are clamped with the two motors (7).