Debugging equipment for assembling various unmanned aerial vehicle models

Abstract

The utility model belongs to the technical field of unmanned aerial vehicle debugging, and particularly relates to debugging equipment for assembling various unmanned aerial vehicle models, which comprises a base, four slots I and four slots II are formed in the top of the base, mounting boxes are inserted into the four slots I, tension meters are fixedly mounted in the mounting boxes, and the four slots II are connected with the tension meters; a pull rope is fixedly mounted at the top end of the tension meter; a hook is fixedly mounted at the top end of the pull rope; the four limiting assemblies are located in the four mounting boxes correspondingly and used for limiting the four mounting boxes correspondingly; the four sliding grooves are all formed in the top of the base and located among the four first inserting grooves, and clamping plates are slidably installed in the sliding grooves. According to the unmanned aerial vehicle pulling force testing device, the pulling force of various unmanned aerial vehicles can be tested, it is guaranteed that personnel can conveniently debug the pulling force of the various unmanned aerial vehicles, and when the unmanned aerial vehicles are debugged, the pulling force of the unmanned aerial vehicles can be conveniently adjusted. And the unmanned aerial vehicle does not shake, so that personnel can debug the unmanned aerial vehicle conveniently.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the technical field of unmanned aerial vehicle debugging, especially relates to a debugging equipment for the assembly of various unmanned aerial vehicle models. BACKGROUND

[0002] The unmanned aerial vehicle has a lightweight body and an intelligent flight control system, can be stably hovered and flexibly turned, and is used by hobbyists to take aerial photographs, so as to capture charming scenes of mountains, rivers, seas, cities and streets from unique perspectives; the film and television industry uses it to shoot blockbuster films, so as to bring an unprecedented visual experience; in the logistics and distribution link, it can pass through congestion and accurately deliver goods to the door, and with the powerful functions, the unmanned aerial vehicle is penetrating into various industries in all directions, innovating operation modes and opening a new era of convenient and efficient flight.

[0003] Generally, the tension of four blades of the unmanned aerial vehicle needs to be detected and debugged after assembly in the production process, but the unmanned aerial vehicle models are various, including cross type, X type and H type, and the common debugging equipment can only detect and debug the same model, and cannot adapt to unmanned aerial vehicles of various models. In view of this, the utility model provides a debugging equipment for the assembly of various unmanned aerial vehicle models. CONTENT OF THE UTILITY MODEL

[0004] The utility model aims at providing a debugging equipment for the assembly of various unmanned aerial vehicle models to solve the problems in the background art.

[0005] Therefore, the utility model provides a debugging equipment for the assembly of various unmanned aerial vehicle models, which comprises:

[0006] A base is provided, four first insertion grooves and four second insertion grooves are formed in the top of the base, four installation boxes are inserted and installed in the four first insertion grooves, a tension meter is fixedly installed in the installation box, a pull rope is fixedly installed at the top of the tension meter, and a hook is fixedly installed at the top of the pull rope;

[0007] Four limiting assemblies are respectively arranged in the four installation boxes and are respectively used for limiting the four installation boxes;

[0008] Four sliding grooves are arranged on the top of the base and between the four first insertion grooves, a clamping plate is slidingly installed in the sliding groove, a rubber pad is fixedly installed on one side of the clamping plate, a threaded rod is rotatably installed in the sliding groove, and one end of the threaded rod penetrates through the clamping plate;

[0009] A driving assembly is arranged in the base and is used for driving the four threaded rods to rotate.

[0010] In the technical solution, when the cross-shaped unmanned aerial vehicle needs to be debugged, the personnel can place the unmanned aerial vehicle on the base, and hang the hooks on the four pull ropes under the four blades of the unmanned aerial vehicle respectively, then the personnel can start the unmanned aerial vehicle, the unmanned aerial vehicle flies upward and pulls the four tension gauges through the four pull ropes, at this time, the four tension gauges can test the tension of the four blades of the unmanned aerial vehicle, at this time, the personnel can judge whether the tension of the four blades of the unmanned aerial vehicle is normal by observing the data displayed on the four tension gauges, when the X-shaped and H-shaped unmanned aerial vehicles need to be tested, the personnel can release the limiting of the four installation boxes through the four limiting assemblies, the personnel can pull out the installation boxes and tension gauges from the first insertion slots and insert them into the second insertion slots, and then limit the installation boxes through the limiting assemblies, through the above operation, the personnel can pull out the four installation boxes from the four first insertion slots and insert them into the four second insertion slots, at this time, the four tension gauges will be arranged in X shape, at this time, the X-shaped unmanned aerial vehicle and the H-shaped unmanned aerial vehicle can be tested, ensuring that the tension of various unmanned aerial vehicles can be tested, and ensuring that the personnel can conveniently debug the tension of various unmanned aerial vehicles.

[0011] When the unmanned aerial vehicle is debugged, the personnel can place the unmanned aerial vehicle between the four clamping plates, then the four threaded rods can be driven to rotate through the driving assembly, under the action of the threads, the rotation of the four threaded rods will drive the four clamping plates to move respectively, until the rubber pads on the four clamping plates abut against the unmanned aerial vehicle, at the same time, the rubber pads can play a buffering role, avoiding scratching the unmanned aerial vehicle by the clamping plates, so as to clamp and fix the unmanned aerial vehicle on the top of the base, ensuring that the unmanned aerial vehicle will not shake when the personnel debugs the unmanned aerial vehicle, thereby facilitating the personnel to debug the unmanned aerial vehicle.

[0012] In the above technical solution, further, the limiting assembly comprises:

[0013] Two sliding grooves, two sliding grooves are symmetrically arranged in the installation box, a sliding block is slidably arranged in the sliding groove, one end of the sliding block penetrates through one side of the sliding groove and extends into the base, the other end of the sliding block is fixedly connected with the spring fixedly arranged on the inner wall of the sliding groove, and the top end of the sliding block penetrates through the top of the sliding groove and extends to the outside.

[0014] In the technical scheme, when the X-shaped and H-shaped unmanned aerial vehicles need to be tested, the personnel can press the two sliding blocks on the mounting box, the movement of the sliding blocks can extrude the springs to shrink, until the ends of the two sliding blocks on the mounting box are moved out of the base, at this time, the two sliding blocks can release the mounting box from the limiting, the personnel can pull out the mounting box and the tension meter from the slot one and insert it into the slot two, at this time, the inner wall of the slot two can extrude one end of the two sliding blocks, so that the two sliding blocks move and extrude the two springs to shrink, when the mounting box is completely inserted into the slot two, at this time, under the action of the rebound force of the two springs, the two springs can extrude the two sliding blocks, until the ends of the two sliding blocks are inserted into the base, at this time, the two sliding blocks can limit the mounting box, through the above operation, the personnel can pull out the four mounting boxes from the four slot one and insert them into the four slot two, at this time, the four tension meters are arranged in X shape, at this time, the X-shaped unmanned aerial vehicle and the H-shaped unmanned aerial vehicle can be tested, so as to ensure that the tension of various unmanned aerial vehicles can be tested, and the personnel can conveniently debug the tension of various unmanned aerial vehicles.

[0015] In the above technical scheme, further, one end of the sliding block is in inclined structure.

[0016] In the technical scheme, it is ensured that one end of the sliding block can be inserted into the base, and the inner walls of the slot two and the slot one can extrude the sliding block to move.

[0017] In the above technical scheme, further, the driving assembly comprises:

[0018] The rotating groove is arranged in the base and between the four sliding grooves, the bottom of the rotating groove is rotatably connected with a conical gear two, four conical gears one are arranged on the side of the conical gear two and in the rotating groove, one end of each of the four conical gears one penetrates the rotating groove and is coaxially connected with the corresponding threaded rod, a circular groove is arranged in the base below the rotating groove, a motor is fixedly arranged in the circular groove, and the output end of the motor penetrates the top of the circular groove and is coaxially connected with the conical gear two.

[0019] In the technical solution, the motor is started, the output shaft of the motor drives the conical gear two to rotate, the rotation of the conical gear two drives the four conical gears one to rotate under the meshing action, the rotation of the four conical gears one drives the four threaded rods to rotate respectively, and the rotation of the four threaded rods drives the four clamping plates to move respectively under the action of the threads, so that the four clamping plates are close to the rotating grooves, until the rubber pads on the four clamping plates are abutted on the unmanned aerial vehicle, and the rubber pads can play a buffering role, so that the unmanned aerial vehicle is prevented from being scratched by the clamping plates, so that the unmanned aerial vehicle is clamped and fixed on the top of the base, and the unmanned aerial vehicle is prevented from shaking when a person adjusts the unmanned aerial vehicle, so that the person can conveniently adjust the unmanned aerial vehicle.

[0020] In the above technical solution, further, the conical gear one is rotatably connected with the rotating groove, and the output shaft of the motor is rotatably connected with the base.

[0021] In the technical solution, the conical gear one can normally rotate in the rotating groove, and the output shaft of the motor can normally rotate in the base.

[0022] In the above technical solution, further, the mounting box is insertedly matched with the slot two, and the threaded rod is threadedly connected with the clamping plate.

[0023] In the technical solution, the mounting box can be inserted into the slot two, and the rotation of the threaded rod can drive the clamping plate to move.

[0024] In the above technical solution, further, the four slots one are distributed in a cross shape, the four slots two are distributed in a matrix form, and the base is fixedly provided with a counterweight.

[0025] In the technical solution, the structure of the four slots one, the four slots two and the base is stable.

[0026] The beneficial effects of the utility model are:

[0027] 1. The adjusting device for various unmanned aerial vehicle models is assembled, the base is arranged, the mutual cooperation of the base, the slot one, the slot two, the mounting box, the tension meter, the pull rope, the hook and the limiting assembly ensures that the tension of various unmanned aerial vehicles can be tested, and personnel can conveniently adjust the tension of various unmanned aerial vehicles.

[0028] 2. The adjusting device for various unmanned aerial vehicle models is assembled, the driving assembly is arranged, the mutual cooperation of the driving assembly, the threaded rod, the clamping plate and the rubber pad ensures that the unmanned aerial vehicle does not shake when a person adjusts the unmanned aerial vehicle, so that the person can conveniently adjust the unmanned aerial vehicle. DRAWINGS

[0029] Figure 1 It is the whole structure schematic diagram of the utility model;

[0030] Figure 2 It is the internal detailed structure schematic diagram of the base in the utility model;

[0031] Figure 3 It is the utility model Figure 2 The enlarged structure schematic diagram of A place in the utility model;

[0032] Figure 4 It is the utility model Figure 2 The enlarged structure schematic diagram of B place in the utility model;

[0033] Figure 5 It is the section structure schematic diagram of the base in the utility model;

[0034] Figure 6 It is the structure schematic diagram of tension meter explosion in the utility model.

[0035] The mark in the drawing indicates that:

[0036] 1, base; 2, slot one; 3, slot two; 4, installation box; 5, tension meter; 6, pull rope; 7, hook; 8, sliding groove; 9, sliding block; 10, spring; 11, sliding slot; 12, clamping plate; 13, rubber pad; 14, threaded rod; 15, rotating groove; 16, conical gear one; 17, conical gear two; 18, circular groove; 19, motor; 20, counterweight. DETAILED DESCRIPTION

[0037] The technical solutions in the embodiments of the present application will be clearly described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments of the present application. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art belong to the scope of protection of the present application.

[0038] In the description of the present application, it should be noted that the terms used herein are only for describing the specific embodiments, and are not intended to limit the exemplary embodiments according to the present application. In order to facilitate the description, the size of each part shown in the drawings is not drawn according to the actual proportional relationship. The technology, method and equipment known to those skilled in the relevant art may not be discussed in detail, but should be considered as part of the authorized specification under appropriate circumstances. In all examples shown and discussed here, any specific value should be interpreted as only exemplary, and not as a limitation. Therefore, other examples of exemplary embodiments can have different values. It should be noted that similar reference numerals and letters represent similar items in the following drawings, so once an item is defined in one drawing, it does not need to be further discussed in subsequent drawings.

[0039] It should be noted that the terms "first", "second", and the like in the description and in the claims of the present application are used for distinguishing between similar objects and not necessarily for describing a specific sequential or chronological order. It is to be understood that the use of these terms herein is merely for distinguishing between the objects and the terms first, second, etc. have the meaning explicitly associated with them in the context of the patent claim. The preliminary classification of this patent application has been made only for an expedient purpose and does not mean or imply that the subject technology is or will be confined to the patent classification.

[0040] It should be noted that the terms "front", "rear", "upper", "lower", "left", "right", "horizontal", "vertical", "top", "bottom", and the like as used herein are made only for the purpose of description and do not imply or represent that the device or element referred to must have a particular position or must be constructed and operated in a particular orientation, unless specifically so stated. The terms "front", "rear", "upper", "lower", "left", "right", "horizontal", "vertical", "top", "bottom", and the like, are used as terms of convenience to describe the present application and its attendant description relative to the illustrative drawings, and do not imply or represent that the device or element referred to must have a particular position or must be constructed and operated in a particular orientation, unless specifically so stated. The terms "inner", "outer" refer to the inner and outer surfaces of the profile of the components themselves.

[0041] It should be noted that the terms "comprises", "comprising", or any other variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but can include other elements not expressly listed or inherent to such process, method, article, or apparatus. An element proceeded by "comprises... a" does not, without more constraints, exclude the existence of additional identical elements in the process, method, article, or apparatus that comprises the element. Additionally, it should be noted that the terms "first", "second", or the like, as used herein do not denote any order, quantity, combination, or arrangement of constituents, but instead are used to identify various constituents. Furthermore, the use of the terms "a" and "an" and "the" and "said" and "at least one" and "one or more" to describe the various constituents of the present application are intended to be taken as meaning that there is one or more of the constituents. Additionally, it should be noted that the features described in relation to certain examples can be combined in other examples.

[0042] Example 1:

[0043] Referring to Figure 1 - Figure 6 As shown in the drawings, the embodiment provides a debugging device for assembling multiple unmanned aerial vehicle models, comprising:

[0044] The base 1, the top of the base 1 is provided with four slot one 2 and four slot two 3, four slot one 2 are inserted and installed with installation box 4, installation box 4 are fixedly installed with tension meter 5, the top of tension meter 5 is fixedly installed with pull rope 6, the top of pull rope 6 is fixedly installed with hook 7;

[0045] Four limiting assemblies, four limiting assemblies are respectively located in four installation boxes 4, and are respectively used for limiting four installation boxes 4;

[0046] Four sliding grooves 11, four sliding grooves 11 are all provided on the top of the base 1 and are located between four slot one 2, sliding groove 11 is slidably installed with clamping plate 12, one side of clamping plate 12 is fixedly installed with rubber pad 13, sliding groove 11 is rotatably installed with threaded rod 14, one end of threaded rod 14 penetrates clamping plate 12;

[0047] Driving assembly, the driving assembly is located in the base 1, and is used for driving four threaded rods 14 to rotate.

[0048] When the cross-shaped unmanned aerial vehicle needs to be debugged, the personnel can place the unmanned aerial vehicle on the base 1, and hang the hooks 7 on the four pull ropes 6 under the four blades of the unmanned aerial vehicle respectively, then the personnel can start the unmanned aerial vehicle, the unmanned aerial vehicle flies upward and pulls the four tension meters 5 through the four pull ropes 6, at this time, the four tension meters 5 can test the tension of the four blades of the unmanned aerial vehicle, at this time, the personnel can judge whether the tension of the four blades of the unmanned aerial vehicle is normal by observing the data displayed on the four tension meters 5, when the X-shaped and H-shaped unmanned aerial vehicles need to be tested, the personnel can remove the limiting of the four installation boxes 4 through the four limiting assemblies, the personnel can pull out the installation boxes 4 and the tension meters 5 from the slot one 2 and insert them into the slot two 3, and then limit the installation boxes 4 through the limiting assemblies, through the above operation, the personnel can pull out the four installation boxes 4 from the four slot one 2 and insert them into the four slot two 3, at this time, the four tension meters 5 will be arranged in X shape, at this time, the X-shaped unmanned aerial vehicle and the H-shaped unmanned aerial vehicle can be tested, to ensure that the tension of various unmanned aerial vehicles can be tested, and the personnel can conveniently debug the tension of various unmanned aerial vehicles;

[0049] When the unmanned aerial vehicle is debugged, the personnel can place the unmanned aerial vehicle between the four clamping plates 12, then the four threaded rods 14 can be driven to rotate through the driving assembly, under the action of the screw, the rotation of the four threaded rods 14 drives the four clamping plates 12 to move respectively, until the rubber pads 13 on the four clamping plates 12 abut against the unmanned aerial vehicle, and the rubber pads 13 can play a buffering role, to avoid scratching the unmanned aerial vehicle by the clamping plates 12, so as to clamp and fix the unmanned aerial vehicle on the top of the base 1, to ensure that the unmanned aerial vehicle does not shake when the personnel debugs the unmanned aerial vehicle, so as to facilitate the personnel to debug the unmanned aerial vehicle.

[0050] Embodiment 2:

[0051] The embodiment provides a debugging device for assembling various unmanned aerial vehicle models, in addition to the technical scheme of the above embodiment, further having the following technical features, the limiting assembly comprises:

[0052] Two sliding grooves 8 are symmetrically arranged in the mounting box 4, a sliding block 9 is slidably arranged in the sliding groove 8, one end of the sliding block 9 penetrates one side of the sliding groove 8 and extends into the base 1, and the other end of the sliding block 9 is fixedly provided with a spring 10 fixed to the inner wall of the sliding groove 8, and the top end of the sliding block 9 penetrates the top of the sliding groove 8 and extends to the outside.

[0053] When the X-shaped and H-shaped unmanned aerial vehicles need to be tested, the personnel can press the two sliding blocks 9 on the mounting box 4, the sliding blocks 9 move to compress the springs 10 to shrink, until the two ends of the two sliding blocks 9 on the mounting box 4 are removed from the base 1, at this time, the two sliding blocks 9 can release the limiting of the mounting box 4, the personnel can pull out the mounting box 4 and the tension meter 5 from the slot one 2 and insert them into the slot two 3, at this time, the inner wall of the slot two 3 will squeeze one end of the two sliding blocks 9, so that the two sliding blocks 9 move and squeeze the two springs 10 to shrink, when the mounting box 4 is completely inserted into the slot two 3, at this time, under the action of the rebound force of the two springs 10, the two springs 10 will squeeze the two sliding blocks 9 respectively, until the two ends of the two sliding blocks 9 are inserted into the base 1, at this time, the two sliding blocks 9 can limit the mounting box 4, through the above operation, the personnel can pull out the four mounting boxes 4 from the four slot ones 2 and insert them into the four slot twos 3, at this time, the four tension meters 5 will be arranged in an X shape, at this time, the X-shaped unmanned aerial vehicle and the H-shaped unmanned aerial vehicle can be tested, so as to ensure that the tension of various unmanned aerial vehicles can be tested, and the personnel can conveniently debug the tension of various unmanned aerial vehicles.

[0054] Embodiment 3:

[0055] The embodiment provides a debugging device for assembling various unmanned aerial vehicle models, in addition to the technical scheme of the above embodiment, further having the following technical features, one end of the sliding block 9 is in plug-in cooperation with the base 1, and the one end of the sliding block 9 is in an inclined structure.

[0056] The one end of the sliding block 9 can be inserted into the base 1, and the inner walls of the slot two 3 and the slot one 2 can squeeze the sliding block 9 to move.

[0057] Embodiment 4:

[0058] The embodiment provides a debugging device for assembling various unmanned aerial vehicle models, in addition to the technical scheme of the above embodiment, further having the following technical features, the driving assembly comprises:

[0059] The rotating groove 15 is arranged in the base 1 and between the four sliding grooves 11. The bottom of the rotating groove 15 is rotatably connected with a conical gear 2, and the circumferential side of the conical gear 2 is rotatably connected with four conical gears 1. One end of each of the four conical gears 1 penetrates the rotating groove 15 and is coaxially connected with a corresponding threaded rod 14. A circular groove 18 is arranged in the base 1 below the rotating groove 15. A motor 19 is fixedly arranged in the circular groove 18. The output shaft of the motor 19 penetrates the top of the circular groove 18 and is coaxially connected with the conical gear 2.

[0060] The motor 19 is started, the output shaft of the motor 19 drives the conical gear 2 to rotate, the conical gear 2 drives the four conical gears 1 to rotate under the meshing action, and the four conical gears 1 drive the four threaded rods 14 to rotate under the meshing action. Under the action of the threads, the four threaded rods 14 drive the four clamping plates 12 to move, so that the four clamping plates 12 move towards the rotating groove 15 until the rubber pads 13 on the four clamping plates 12 abut against the unmanned aerial vehicle. At the same time, the rubber pads 13 can play a buffering role to avoid scratching the unmanned aerial vehicle by the clamping plates 12, so as to clamp and fix the unmanned aerial vehicle on the top of the base 1, so that the unmanned aerial vehicle does not shake when a person adjusts the unmanned aerial vehicle, thereby facilitating the person to adjust the unmanned aerial vehicle.

[0061] Embodiment 5:

[0062] The embodiment provides a debugging device for assembling various unmanned aerial vehicle models. In addition to the technical solutions of the above-mentioned embodiments, the conical gear 1 is rotatably connected with the rotating groove 15, and the output shaft of the motor 19 is rotatably connected with the base 1.

[0063] The conical gear 1 can normally rotate in the rotating groove 15, and the output shaft of the motor 19 can normally rotate in the base 1.

[0064] Embodiment 6:

[0065] The embodiment provides a debugging device for assembling various unmanned aerial vehicle models. In addition to the technical solutions of the above-mentioned embodiments, the mounting box 4 is plug-in matched with the second slot 3, and the threaded rod 14 is threadedly connected with the clamping plate 12.

[0066] The mounting box 4 can be inserted into the second slot 3, and the threaded rod 14 can drive the clamping plate 12 to move.

[0067] Embodiment 7:

[0068] The embodiment provides a debugging device for assembling various unmanned aerial vehicle models, in addition to comprising the technical scheme of the above embodiment, further having the following technical features, four slot one 2 are cross-shapedly distributed, four slot two 3 are matrixly distributed, and the base 1 is fixedly installed with a counterweight 20.

[0069] Among them, the structure of four slot one 2, four slot two 3 and base 1 is stable.

[0070] Working principle: when the cross-shaped unmanned aerial vehicle needs to be debugged, personnel can place the unmanned aerial vehicle on the base 1, and hang the hooks 7 on the four pull ropes 6 under the four blades of the unmanned aerial vehicle respectively, then the personnel can start the unmanned aerial vehicle, and the unmanned aerial vehicle flies upward and pulls the four pull force gauges 5 through the four pull ropes 6, at this time, the four pull force gauges 5 can test the pulling force of the four blades of the unmanned aerial vehicle, at this time, the personnel can judge whether the pulling force of the four blades of the unmanned aerial vehicle is normal by observing the data displayed on the four pull force gauges 5, when the X-shaped and H-shaped unmanned aerial vehicles need to be tested, the personnel can press the two sliding blocks 9 on the installation box 4, and the sliding blocks 9 move to compress the springs 10 to shrink, until the ends of the two sliding blocks 9 on the installation box 4 are moved out of the base 1, at this time, the two sliding blocks 9 can release the installation box 4 from the limit, the personnel can pull out the installation box 4 and the pull force gauge 5 from the slot one 2 and insert them into the slot two 3, at this time, the inner wall of the slot two 3 can extrude one end of the two sliding blocks 9, so that the two sliding blocks 9 move and extrude the two springs 10 to shrink, when the installation box 4 is completely inserted into the slot two 3, at this time, the two springs 10 can extrude the two sliding blocks 9 under the action of the rebound force of the two springs 10, until the ends of the two sliding blocks 9 are inserted into the base 1, at this time, the two sliding blocks 9 can limit the installation box 4, through the above operation, the personnel can pull out the four installation boxes 4 from the four slot one 2 and insert them into the four slot two 3, at this time, the four pull force gauges 5 will be arranged in X shape, at this time, the X-shaped unmanned aerial vehicle and the H-shaped unmanned aerial vehicle can be tested, so as to ensure that the pulling force of various unmanned aerial vehicles can be tested, and personnel can conveniently debug the pulling force of various unmanned aerial vehicles.

[0071] When the unmanned aerial vehicle is debugged, the personnel can place the unmanned aerial vehicle between the four clamping plates 12, and then the motor 19 can be started. The output shaft of the motor 19 drives the conical gear two 17 to rotate. Under the meshing action, the rotation of the conical gear two 17 drives the four conical gears one 16 to rotate. The rotation of the four conical gears one 16 drives the four threaded rods 14 to rotate respectively. Under the action of the screw threads, the rotation of the four threaded rods 14 drives the four clamping plates 12 to move respectively, so that the four clamping plates 12 are close to the rotating grooves 15. Until the rubber pads 13 on the four clamping plates 12 are abutted on the unmanned aerial vehicle, and the rubber pads 13 can play a buffering role, avoiding scratching the unmanned aerial vehicle by the clamping plates 12. Thus, the unmanned aerial vehicle is clamped and fixed on the top of the base 1, ensuring that the unmanned aerial vehicle does not shake when the personnel debug the unmanned aerial vehicle, thereby facilitating the personnel to debug the unmanned aerial vehicle.

[0072] The embodiments of the present application are described above in combination with the drawings. In the case of no conflict, the embodiments and the features in the embodiments of the present application can be combined with each other. The present application is not limited to the above-mentioned specific embodiments. The above-mentioned specific embodiments are only illustrative, not restrictive. Those skilled in the art can make many forms under the inspiration of the present application without departing from the scope of the present application and the protection scope of the claims.

Claims

1. A debugging device for assembling various UAV models, characterized in that, Include: The base (1), the top of the base (1) is provided with four slot one (2) and four slot two (3), four the slot one (2) is inserted into the installation box (4) and is installed, the installation box (4) is fixedly installed with tension meter (5), the top of the tension meter (5) is fixedly installed with pull rope (6), the top of the pull rope (6) is fixedly installed with hook (7); Four limiting components, four the limiting components are located in four installation boxes (4) respectively, and are used for limiting four installation boxes (4) respectively; Four sliding grooves (11), four the sliding groove (11) is set up in the top of the base (1) and is located between four slot one (2), the sliding groove (11) is slidably installed with clamping plate (12), one side of the clamping plate (12) is fixedly installed with rubber pad (13), the sliding groove (11) is rotatably installed with threaded rod (14), one end of the threaded rod (14) penetrates clamping plate (12); Driving assembly, the driving assembly is located in the base (1), and is used for driving four threaded rods (14) to rotate.

2. The commissioning device for multiple drone model assembly of claim 1, wherein, The limiting component includes: Two sliding grooves (8), two the sliding groove (8) is symmetrically set up in the installation box (4), the sliding groove (8) is slidably installed with sliding block (9), one end of the sliding block (9) penetrates one side of the sliding groove (8) and extends into the base (1), the other end of the sliding block (9) is fixedly installed with spring (10) fixedly installed in the sliding groove (8), the top of the sliding block (9) penetrates the top of the sliding groove (8) and extends to the outside.

3. The commissioning device for a plurality of drone models according to claim 2, wherein, One end of the sliding block (9) is inserted into the base (1), and the other end of the sliding block (9) is inclined.

4. The debugging device for assembling multiple unmanned aerial vehicle models according to claim 1, wherein, The driving assembly includes: Rotary groove (15), the rotary groove (15) is set up in the base (1) and is located between four sliding grooves (11), the bottom of the rotary groove (15) is rotatably installed with conical gear two (17), the circumferential side of the conical gear two (17) and located in the rotary groove (15) is engagedly installed with four conical gear one (16), one end of four the conical gear one (16) penetrates the rotary groove (15) and is coaxially connected with the corresponding threaded rod (14), the base (1) and located below the rotary groove (15) is provided with circular groove (18), the circular groove (18) is fixedly installed with motor (19), the output end of the motor (19) penetrates the top of the circular groove (18) and is coaxially connected with the conical gear two (17).

5. The commissioning device for a plurality of drone models according to claim 4, wherein, The conical gear one (16) is rotatably connected with the rotary groove (15), and the output shaft of the motor (19) is rotatably connected with the base (1).

6. The commissioning device for a plurality of drone models according to claim 1, wherein, The installation box (4) is inserted into the slot two (3), and the threaded rod (14) is threadedly connected with the clamping plate (12).

7. The commissioning device for a plurality of drone models according to claim 1, wherein, Four the slot one (2) is distributed in cross shape, four the slot two (3) is distributed in matrix, the base (1) is fixedly installed with counterweight (20).

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