CN216508997U

CN216508997U - But quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting

Info

Publication number: CN216508997U
Application number: CN202220162446.4U
Authority: CN
Inventors: 朴国一
Original assignee: Shenzhen Avic Zhifei Technology Co ltd
Current assignee: Shenzhen Avic Zhifei Technology Co ltd
Priority date: 2022-01-21
Filing date: 2022-01-21
Publication date: 2022-05-13
Anticipated expiration: 2032-01-21

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses a quickly-detachable individual soldier operation and combat unmanned aerial vehicle which comprises a body, wherein a connecting table is fixedly installed on the side face of the body, a connecting arm is clamped on the side face of the connecting table, a clamping device is arranged at one end, close to the connecting table, of the connecting arm, a fixed arm is fixedly installed at one end, far away from the connecting table, of the connecting arm, a motor bin is fixedly installed at one end, far away from the clamping device, of the fixed arm, a rotary propeller is rotatably installed at the top of the motor bin, and a connecting plate is fixedly installed at the bottom of the body. This but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting connects platform, linking arm and card solid device through setting up for unmanned aerial vehicle's more convenient dismouting is carried, utilizes first spring and card piece to make linking arm and be connected between the platform more firm, has avoided unmanned aerial vehicle individual soldier to fight the time space simultaneously and has taken too big problem, makes individual soldier unmanned aerial vehicle of fighting's use more high-efficient convenient.

Description

But quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a rapidly detachable individual combat unmanned aerial vehicle.

Background

Unmanned aerial vehicle is the unmanned aircraft that utilizes radio remote control equipment and self-contained program control device to control, compares with manned aircraft, and unmanned aerial vehicle's task suitability is stronger, and unmanned aerial vehicle all has the application on military affairs and civil affairs, and in the aspect of military affairs, unmanned aerial vehicle divide into reconnaissance aircraft and target drone again.

When military individual combat, often be equipped with unmanned aerial vehicle and assist individual combat and carry out the combat, however traditional individual combat unmanned aerial vehicle is because unmanned aerial vehicle occupation space is too big, carry the use when being unfavorable for individual combat, can influence going on of individual combat task, in addition because individual combat, open-air topography is mostly uneven topography, when placing unmanned aerial vehicle and taking off, because the topography unevenness is unfavorable for unmanned aerial vehicle's vertical take-off, it is unstable when making unmanned aerial vehicle take off, influence unmanned aerial vehicle's use.

SUMMERY OF THE UTILITY MODEL

Aiming at the defects of the prior art, the utility model provides the individual combat unmanned aerial vehicle capable of being quickly disassembled and assembled, which has the advantages of being convenient to disassemble and assemble and carry, adjustable in take-off angle and higher in stability, and solves the problems in the background technology.

The utility model provides the following technical scheme: an individual combat unmanned aerial vehicle capable of being quickly disassembled and assembled comprises a machine body, wherein a connecting platform is fixedly installed on the side face of the machine body, a connecting arm is clamped on the side face of the connecting platform, a clamping device is arranged at one end, close to the connecting platform, of the connecting arm, a fixing arm is fixedly installed at one end, far away from the connecting platform, of the connecting arm, a motor bin is fixedly installed at one end, far away from the clamping device, of the fixing arm, a rotary propeller is rotatably installed at the top of the motor bin, a connecting plate is fixedly installed at the bottom of the machine body, a connecting block is fixedly installed at the bottom of the connecting plate, a stabilizing seat is arranged below the connecting block, a fixing block is fixedly installed at the top of the stabilizing seat, a rotating shaft is rotatably installed at one side of the fixing block and penetrates through the connecting block, a clamping block is fixedly installed on the surface of the rotating shaft, a fixing column is fixedly installed at the bottom of the stabilizing seat, and a sliding column is slidably connected inside the fixing column, the bottom fixed mounting of slip post has the second spring, the one end that the slip post was kept away from to the second spring is with the top fixed connection of stabilizing the seat, the positive fixed mounting of organism has the camera, one side of camera is provided with the light.

Preferably, the connecting block is fixedly connected with the rotating shaft, and the illuminating lamp is fixedly arranged on the front face of the machine body.

Preferably, the clamping device comprises a sliding groove, a first spring is fixedly mounted at the bottom of the sliding groove, and a clamping block is slidably connected inside the sliding groove.

Preferably, a sliding chute is arranged in the fixed column, and the size of the cross section of the sliding column is consistent with that of the cross section of the sliding chute in the fixed column.

Preferably, the fixture block is positioned on one side of the fixing block, which is far away from the connecting block, and a sliding groove is arranged in the sliding column.

Preferably, the surface of the rotating shaft is provided with a plurality of clamping blocks, and the size of the cross section of each clamping block is consistent with that of the cross section of the sliding groove in the sliding column.

Compared with the prior art, the utility model has the following beneficial effects:

1. this but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting connects platform, linking arm and card solid device through setting up for unmanned aerial vehicle's more convenient dismouting is carried, utilizes first spring and card piece to make linking arm and be connected between the platform more firm, has avoided unmanned aerial vehicle individual soldier to fight the time space simultaneously and has taken too big problem, makes individual soldier unmanned aerial vehicle of fighting's use more high-efficient convenient.

2. This but quick assembly disassembly's individual soldier unmanned aerial vehicle of battle through setting up connecting block, fixed block, pivot and fixture block, utilizes the pivot to make unmanned aerial vehicle's the angle of taking off can adjust for when unmanned aerial vehicle takes off to the topography of unevenness when the use in the field, through adjusting the angle of taking off, guarantee unmanned aerial vehicle's the stability of taking off perpendicularly, utilize the sliding column to carry on spacingly to the fixture block, and then guaranteed fixed after the angular adjustment.

Drawings

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a side view of the overall structure of the present invention;

FIG. 3 is an enlarged view of the structure A of FIG. 2;

FIG. 4 is a schematic view of the internal structure of the fixed column and the sliding column of the present invention;

FIG. 5 is a schematic view of a fastening device according to the present invention.

In the figure: 1. a body; 2. a connecting table; 3. a connecting arm; 4. a clamping device; 401. a sliding groove; 402. a first spring; 403. a clamping block; 5. a fixed arm; 6. a motor compartment; 7. rotating a propeller; 8. a connecting plate; 9. connecting blocks; 10. a stabilizing base; 11. a fixed block; 12. a rotating shaft; 13. a clamping block; 14. fixing a column; 15. a sliding post; 16. a second spring; 17. a camera; 18. an illuminating lamp.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-5, an individual combat unmanned aerial vehicle capable of being quickly disassembled and assembled comprises a vehicle body 1, a connecting table 2 is fixedly mounted on the side surface of the vehicle body 1, a connecting arm 3 is clamped on the side surface of the connecting table 2, a clamping device 4 is arranged at one end, close to the connecting table 2, of the connecting arm 3, a fixed arm 5 is fixedly mounted at one end, far away from the connecting table 2, of the connecting arm 3, a motor cabin 6 is fixedly mounted at one end, far away from the clamping device 4, of the fixed arm 5, a rotating propeller 7 is rotatably mounted at the top of the motor cabin 6, a connecting plate 8 is fixedly mounted at the bottom of the vehicle body 1, a connecting block 9 is fixedly mounted at the bottom of the connecting plate 8, a stabilizing seat 10 is arranged below the connecting block 9, a fixing block 11 is fixedly mounted at the top of the stabilizing seat 10, a rotating shaft 12 is rotatably mounted at one side of the fixing block 11, and the rotating shaft 12 penetrates through the connecting block 9, the fixed surface of pivot 12 installs fixture block 13, the bottom fixed mounting of stabilizing seat 10 has fixed column 14, the inside sliding connection of fixed column 14 has sliding column 15, sliding column 15's bottom fixed mounting has second spring 16, sliding column 15's one end and stabilizing seat 10's top fixed connection are kept away from to second spring 16, the positive fixed mounting of organism 1 has camera 17, one side of camera 17 is provided with light 18.

Wherein, connecting block 9 and pivot 12 fixed connection, 18 fixed mounting of light utilize light 18 to guarantee unmanned aerial vehicle at the use at night in the front of organism 1, have richened unmanned aerial vehicle task execution scene, and then make unmanned aerial vehicle's practicality higher.

The clamping device 4 comprises a sliding groove 401, a first spring 402 is fixedly mounted at the bottom of the sliding groove 401, a clamping block 403 is connected inside the sliding groove 401 in a sliding mode, the connecting arm 3 and the connecting platform 2 are connected more stably through the first spring 402 and the clamping block 403, and stability of the unmanned aerial vehicle in the process of executing a flight task is guaranteed.

The sliding groove is formed in the fixed column 14, the cross section of the sliding column 15 is the same as that of the sliding groove in the fixed column 14, and the sliding connection between the sliding column 15 and the fixed column 14 is utilized, so that the sliding column 15 effectively limits the position of the fixture block 13 through the second spring 16.

Wherein, fixture block 13 is located one side that connecting block 9 was kept away from to fixed block 11, be provided with the spout in the sliding column 15, utilize a plurality of fixture block 13 to make the angle selection to axis of rotation 12 more various, richened unmanned aerial vehicle's the applicable scene of taking off for unmanned aerial vehicle better assists open-air individual soldier combat.

The surface of the rotating shaft 12 is provided with a plurality of clamping blocks 13, the cross section of each clamping block 13 is consistent with that of the sliding groove in the sliding column 15, the rotating angle of the rotating shaft 12 is limited by the clamping blocks 13, and the angle of the machine body 1 is adjusted and limited through the connecting block 9 and the connecting plate 8.

Working principle, when the unmanned aerial vehicle is used for carrying out individual combat missions, the four connecting arms 3 and the connecting platform 2 are connected through the clamping device 4, when the unmanned aerial vehicle needs to be stored, the clamping block 403 is pressed to separate the clamping block 403 from the clamping groove on the connecting platform 2, so that the connecting arms 3 are separated from the connecting platform 2, the unmanned aerial vehicle is convenient to carry, when the unmanned aerial vehicle needs to carry out missions, the clamping block 403 is clamped into the clamping groove of the connecting platform 2 through the first spring 402, so that the unmanned aerial vehicle is convenient to assemble and disassemble, when the unmanned aerial vehicle is unfavorable for vertical takeoff due to takeoff terrain inclination, the sliding column 15 is pulled to separate the clamping block 13 from the sliding column 15, the rotating shaft 12 is rotated to adjust the angle of the connecting block 9, the vertical takeoff angle of the unmanned aerial vehicle is ensured through the angle of the connecting block 9 and the connecting plate 8, then the sliding column 15 is loosened, and the sliding column 15 is connected with the clamping block 13 through the second spring 16, thereby limiting the angle of the rotating shaft 12.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a but quick assembly disassembly's individual soldier unmanned aerial vehicle of fighting, includes organism (1), its characterized in that: the side fixed mounting of organism (1) has connection platform (2), the side joint of connecting platform (2) has linking arm (3), the one end that linking arm (3) is close to connecting platform (2) is provided with solid device of card (4), the one end fixed mounting that connecting platform (2) were kept away from in linking arm (3) has fixed arm (5), the one end fixed mounting that solid device of card (4) was kept away from in fixed arm (5) has motor storehouse (6), the top of motor storehouse (6) is rotated and is installed oar (7), the bottom fixed mounting of organism (1) has connecting plate (8), the bottom fixed mounting of connecting plate (8) has connecting block (9), the below of connecting block (9) is provided with stable seat (10), the top fixed mounting of stable seat (10) has fixed block (11), one side of fixed block (11) is rotated and is installed pivot (12), and pivot (12) through connection piece (9), the fixed surface of pivot (12) installs fixture block (13), the bottom fixed mounting of stabilizing seat (10) has fixed column (14), the inside sliding connection of fixed column (14) has sliding column (15), the bottom fixed mounting of sliding column (15) has second spring (16), the top fixed connection of the one end of sliding column (15) and stabilizing seat (10) is kept away from in second spring (16), the positive fixed mounting of organism (1) has camera (17), one side of camera (17) is provided with light (18).

2. The unmanned aerial vehicle capable of individual combat of rapid disassembly and assembly of claim 1, wherein: the connecting block (9) is fixedly connected with the rotating shaft (12), and the illuminating lamp (18) is fixedly arranged on the front surface of the machine body (1).

3. The unmanned aerial vehicle capable of individual combat of rapid disassembly and assembly of claim 1, wherein: the clamping device (4) comprises a sliding groove (401), a first spring (402) is fixedly mounted at the bottom of the sliding groove (401), and a clamping block (403) is connected inside the sliding groove (401) in a sliding mode.

4. The unmanned aerial vehicle capable of individual combat of rapid disassembly and assembly of claim 1, wherein: a sliding chute is arranged in the fixed column (14), and the size of the cross section of the sliding column (15) is consistent with that of the sliding chute in the fixed column (14).

5. The unmanned aerial vehicle capable of individual combat of rapid disassembly and assembly of claim 1, wherein: the clamping block (13) is positioned on one side, away from the connecting block (9), of the fixing block (11), and a sliding groove is formed in the sliding column (15).

6. The unmanned aerial vehicle capable of individual combat of rapid disassembly and assembly of claim 5, wherein: the surface of the rotating shaft (12) is provided with a plurality of clamping blocks (13), and the cross section of each clamping block (13) is consistent with the cross section of the sliding groove in the sliding column (15).