CN212220601U

CN212220601U - Unmanned aerial vehicle ground flies to control debugging device

Info

Publication number: CN212220601U
Application number: CN202021100392.6U
Authority: CN
Inventors: 倪虹霞; 张猛; 姜航; 吕晓丽; 刘红喜; 李谷雨; 王智昱; 杨宏伟; 苏紫耘
Original assignee: Changchun Institute of Applied Chemistry of CAS
Current assignee: Changchun Institute of Applied Chemistry of CAS; Changchun Institute Technology
Priority date: 2020-06-15
Filing date: 2020-06-15
Publication date: 2020-12-25
Anticipated expiration: 2030-06-15

Abstract

The utility model discloses an unmanned aerial vehicle ground flight control debugging device, which comprises a shell, wherein two motors are welded on the inner side wall of the shell, the output end of each motor is fixedly connected with a first lead screw, one end of each first lead screw, which is far away from the corresponding motor, is fixedly connected with a second lead screw, one end of each second lead screw, which is far away from the corresponding first lead screw, is rotatably connected to the inner side wall of the shell, and the outer side walls of the first lead screw and the second lead screw are symmetrically in threaded connection with two internal thread sleeve rods; when using this device, rotate opposite direction through first lead screw and second lead screw for two fixed blocks are inside or outside to be removed, can adjust the size that unmanned aerial vehicle placed simultaneously, through taking the clip out from the fixed block, fix unmanned aerial vehicle's foot rest, prevent the external factor influence that receives, make unmanned aerial vehicle produce to remove, rock etc. lead to influencing operating personnel, make operating personnel can't be fine operate unmanned aerial vehicle.

Description

Unmanned aerial vehicle ground flies to control debugging device

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle ground flight control debugging device.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. 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 + the industry application 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.

The invention is disclosed in China: CN207623786U discloses a flight control debugging protection device for multi-rotor unmanned aerial vehicle, which solves the problems that the device is difficult to detect the flight condition of the device under windy conditions, and the flight attitude cannot be adjusted, but has a certain problem;

the unmanned aerial vehicle to certain size that current unmanned aerial vehicle debugging device can only be single parks, the debugging, can't fix great or less unmanned aerial vehicle at the debugging platform, when adjusting unmanned aerial vehicle, when receiving external factor influence for unmanned aerial vehicle produces and removes, rocks etc. lead to influencing operating personnel to unmanned aerial vehicle's debugging, for this reason, provides an unmanned aerial vehicle ground flight control debugging device.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle ground flies to control debugging device to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle ground flight control debugging device comprises a shell, wherein two motors are welded on the inner side wall of the shell, the output ends of the motors are fixedly connected with a first lead screw, one end, far away from the motors, of the first lead screw is fixedly connected with a second lead screw, one end, far away from the first lead screw, of the second lead screw is rotatably connected with the inner side wall of the shell, the first lead screw and the outer side wall of the second lead screw are symmetrically in threaded connection with two internal thread loop bars, a first rod body is welded on the outer side wall of each internal thread loop bar, two first sliding grooves are symmetrically formed in the bottom wall of the inner side of the shell, one end of the first rod body is slidably connected inside the first sliding grooves, a fixed block is welded on the other end of the first rod body, a first groove is formed in the center of the upper surface of the shell, and the outer side wall of the fixed block and one end of the, two the adjacent one side of fixed block is through screw fixedly connected with sponge board, the second spout has been seted up to the inside of fixed block, the inside wall grafting of second spout has the third body of rod, the third body of rod is kept away from one side fixedly connected with clip of second spout.

As further preferable in the present technical solution: the outer side wall of the shell is fixedly connected with a switch group, and the electrical output end of the switch group is electrically connected with the electrical input end of the motor through a wire.

As further preferable in the present technical solution: the inner side wall of the shell is far away from one side of the motor and is fixedly connected with a bearing, and one end, far away from the first screw rod, of the second screw rod is fixedly connected with an inner ring of the bearing.

As further preferable in the present technical solution: the inside wall symmetry sliding connection of first spout has two second body of rods, the top fixedly connected with annular slide rail of the second body of rod, first lead screw with the lateral wall of second lead screw rotate connect in the inside wall of annular slide rail.

As further preferable in the present technical solution: the switch is characterized in that one side, away from the switch group, of the shell is fixedly connected with a handle through screws, second grooves are symmetrically formed in the four corners of the bottom of the shell, damping blocks are fixedly connected to the inner side walls of the second grooves, and universal wheels are mounted at the bottoms of the damping blocks.

As further preferable in the present technical solution: the first body of rod with the equal fixedly connected with slider of lower surface of the second body of rod, the lateral wall sliding connection of slider in the inside wall of first spout.

Compared with the prior art, the beneficial effects of the utility model are that: when using this device, rotate opposite direction through first lead screw and second lead screw for two fixed blocks are inside or outside to be removed, can adjust the size that unmanned aerial vehicle placed simultaneously, through taking the clip out from the fixed block, fix unmanned aerial vehicle's foot rest, prevent the external factor influence that receives, make unmanned aerial vehicle produce to remove, rock etc. lead to influencing operating personnel, make operating personnel can't be fine operate unmanned aerial vehicle.

Drawings

Fig. 1 is a schematic structural view of the present invention;

fig. 2 is a schematic top view structure of the present invention;

fig. 3 is a schematic view of the internal structure of the middle fixing block of the present invention;

fig. 4 is an enlarged schematic structural diagram of the area a of fig. 1 in the present invention.

In the figure: 1. a housing; 2. a motor; 3. a first rod body; 4. a first lead screw; 5. a second rod body; 6. a first chute; 7. an annular slide rail; 8. a second lead screw; 9. a slider; 10. an internal thread loop bar; 11. a bearing; 12. a handle; 13. a first groove; 14. a sponge plate; 15. a fixed block; 16. a switch group; 17. a universal wheel; 18. a second groove; 19. a damping block; 20. a second chute; 21. a third rod body; 22. and (4) a clamp.

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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Examples

Referring to fig. 1-4, the present invention provides a technical solution: an unmanned aerial vehicle ground flight control debugging device comprises a shell 1, two motors 2 are welded on the inner side wall of the shell 1, the output ends of the motors 2 are fixedly connected with a first lead screw 4, one end of the first lead screw 4, far away from the motor 2, is fixedly connected with a second lead screw 8, one end of the second lead screw 8, far away from the first lead screw 4, is rotatably connected with the inner side wall of the shell 1, two internal thread loop bars 10 are symmetrically and threadedly connected with the outer side walls of the first lead screw 4 and the second lead screw 8, a first rod body 3 is welded on the outer side walls of the two internal thread loop bars 10, two first sliding grooves 6 are symmetrically arranged on the inner side bottom wall of the shell 1, one end of the first rod body 3 is slidably connected inside the first sliding grooves 6, a fixed block 15 is welded on the other end of the first rod body 3, a first groove 13 is arranged at the center of the upper surface of the shell 1, and, screw fixedly connected with sponge board 14 is passed through to two adjacent one sides of fixed block 15, and second spout 20 has been seted up to the inside of fixed block 15, and the inside wall of second spout 20 is pegged graft and is had the third body of rod 21, and one side fixedly connected with clip 22 of second spout 20 is kept away from to the third body of rod 21.

In this embodiment, specifically: the outer side wall of the shell 1 is fixedly connected with a switch group 16, and the electrical output end of the switch group 16 is electrically connected with the electrical input end of the motor 2 through a lead; the motor 2 is controlled to start and stop by setting the switch group 16.

In this embodiment, specifically: a bearing 11 is fixedly connected to one side of the inner side wall of the shell 1, which is far away from the motor 2, and one end of the second lead screw 8, which is far away from the first lead screw 4, is fixedly connected to the inner ring of the bearing 11; through setting up bearing 11, play the support fixed action to second lead screw 8, through the friction that reduces second lead screw 8 to the life of extension second lead screw 8.

In this embodiment, specifically: the inner side wall of the first chute 6 is symmetrically connected with two second rod bodies 5 in a sliding manner, the top parts of the second rod bodies 5 are fixedly connected with annular slide rails 7, and the outer side walls of the first screw rod 4 and the second screw rod 8 are rotatably connected to the inner side wall of the annular slide rails 7; through set up annular slide rail 7 and the second body of rod 5 in the inside of casing 1, first lead screw 4 rotates in annular slide rail 7's inside with second lead screw 8, plays the supporting role through the second body of rod 5 of bottom.

In this embodiment, specifically: a handle 12 is fixedly connected to one side of the shell 1, which is far away from the switch group 16, through screws, second grooves 18 are symmetrically formed in the four corners of the bottom of the shell 1, damping blocks 19 are fixedly connected to the inner side walls of the second grooves 18, and universal wheels 17 are mounted at the bottoms of the damping blocks 19; an operator uses the handle 12 to match with the universal wheel 17, so that the shell 1 can be conveniently moved, and time and labor are saved.

In this embodiment, specifically: the lower surfaces of the first rod body 3 and the second rod body 5 are fixedly connected with a sliding block 9, and the outer side wall of the sliding block 9 is connected with the inner side wall of the first sliding chute 6 in a sliding manner; the stability of the first rod body 3 and the second rod body 5 is improved by arranging the sliding block 9.

The model of the motor 2 in this embodiment is: YE 2.

When the working principle or the structural principle is used, the motor 2 is started, the output shaft of the motor 2 drives the first screw rod 4 to rotate, the first screw rod 4 rotates rightwards, the first screw rod 4 drives the second screw rod 8 to rotate, the second screw rod 8 rotates leftwards, so that the internal thread loop bar 10 rotates inwards, meanwhile, the first rod body 3 is fixedly connected with the fixed block 15 and slides in the first chute 6, so that the internal thread loop bar 10 drives the first rod body 3 to move inwards, meanwhile, the fixing block 15 is driven to move inwards, so that the smaller unmanned aerial vehicle is clamped, the clip 22 fixes the foot rest of the unmanned aerial vehicle by drawing out the third rod body 21, by clamping the drone using the sponge plate 14, damage to the drone is prevented while clamping the drone, by fixing the drone, when operating personnel dismantles, debugs unmanned aerial vehicle, promote the efficiency of operating personnel to the unmanned aerial vehicle debugging.

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 invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle ground flight control debugging device, includes casing (1), its characterized in that: the welding of the inner side wall of the shell (1) is provided with two motors (2), the output end of each motor (2) is fixedly connected with a first lead screw (4), one end of each first lead screw (4) far away from the corresponding motor (2) is fixedly connected with a second lead screw (8), one end of each second lead screw (8) far away from the corresponding first lead screw (4) is rotatably connected to the inner side wall of the shell (1), the outer side walls of the first lead screws (4) and the second lead screws (8) are symmetrically in threaded connection with two internal thread loop bars (10), the outer side walls of the two internal thread loop bars (10) are welded with first rod bodies (3), the inner side bottom wall of the shell (1) is symmetrically provided with two first chutes (6), one end of each first rod body (3) is slidably connected to the inside of the corresponding first chute (6), and the other end of each first rod body (3) is welded with a fixing block, first recess (13) have been seted up to the upper surface center department of casing (1), the lateral wall of fixed block (15) with the equal sliding connection in the inside wall of first recess (13), two screw fixedly connected with sponge board (14) is passed through to the one side that fixed block (15) are adjacent, second spout (20) have been seted up to the inside of fixed block (15), the inside wall of second spout (20) is pegged graft and is had the third body of rod (21), keep away from the third body of rod (21) one side fixedly connected with clip (22) of second spout (20).

2. The ground flight control debugging device of the unmanned aerial vehicle of claim 1, comprising: the outer side wall of the shell (1) is fixedly connected with a switch group (16), and the electrical output end of the switch group (16) is electrically connected with the electrical input end of the motor (2) through a lead.

3. The ground flight control debugging device of the unmanned aerial vehicle of claim 1, comprising: the inner side wall of the shell (1) is far away from one side of the motor (2) and is fixedly connected with a bearing (11), and one end, far away from the first screw rod (4), of the second screw rod (8) is fixedly connected with an inner ring of the bearing (11).

4. The ground flight control debugging device of the unmanned aerial vehicle of claim 1, comprising: the inside wall symmetry sliding connection of first spout (6) has two second body of rod (5), the top fixedly connected with annular slide rail (7) of the second body of rod (5), first lead screw (4) with the lateral wall of second lead screw (8) rotate connect in the inside wall of annular slide rail (7).

5. The ground flight control debugging device for the unmanned aerial vehicle according to claim 2, wherein a handle (12) is fixedly connected to one side of the shell (1) far away from the switch group (16) through screws, second grooves (18) are symmetrically formed in four corners of the bottom of the shell (1), damping blocks (19) are fixedly connected to the inner side walls of the second grooves (18), and universal wheels (17) are mounted at the bottoms of the damping blocks (19).

6. The ground flight control debugging device of the unmanned aerial vehicle of claim 4, wherein: the first body of rod (3) with the equal fixedly connected with slider (9) of lower surface of the second body of rod (5), the lateral wall sliding connection of slider (9) in the inside wall of first spout (6).