Four-rotor unmanned aerial vehicle debugging platform

Abstract

The utility model discloses a quad-rotor unmanned aerial vehicle debugging platform, and particularly relates to the technical field of unmanned aerial vehicles, the quad-rotor unmanned aerial vehicle debugging platform comprises a base, the top of the base is fixedly connected with two fixing blocks, the tops of the two fixing blocks are both fixedly connected with fixing rods, and the inner walls of the tops of the two fixing rods are jointly and fixedly connected with a connecting rod; the outer surface of the connecting rod is rotationally connected with a fixing base, and a supporting assembly is arranged above the base. According to the four-rotor unmanned aerial vehicle debugging platform, the supporting assembly is arranged, specifically, the motor is started to drive the supporting plate to slide upwards on the outer surface of the corresponding fixing block so as to support the fixing base, manual supporting by workers is not needed, the workers can be liberated from the tedious task, and the debugging efficiency is improved. According to the unmanned aerial vehicle, the unmanned aerial vehicle does not need to be supported by a specially-assigned person, the labor cost is reduced, and the situation that the unmanned aerial vehicle is suddenly started under the unexpected condition, and consequently workers are injured can be avoided.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field, especially four rotor unmanned plane debugging platform. BACKGROUND

[0002] The unmanned plane is called "UAV" in English, which is a kind of unmanned plane controlled by radio remote control equipment and self-provided program control device, and the four rotor unmanned plane has the characteristics of light weight, high speed and strong grip compared with other unmanned planes. Researchers may improve the vision of the unmanned plane, improve its landing technology or further improve the gripper in the future.

[0003] Before the unmanned plane flies, the debugging platform needs to be used to detect, calibrate and optimize each key part. The purpose is to ensure that the mechanical structure of the unmanned plane is normal, the power system is stable, and the flight control system is accurate, so as to ensure that the unmanned plane can fly safely and stably

[0004] The existing device needs the staff to manually hold the fixing seat for fixing the unmanned plane before detecting the unmanned plane, to ensure that it can be in a normal flight attitude state, which not only makes the staff unable to carry out other detection preparation work at the same time, but also needs a person to hold the operation, thereby increasing the labor cost, and when the staff manually holds the fixing seat, their attention is mainly concentrated on maintaining the attitude of the unmanned plane, so if the unmanned plane starts suddenly in an unexpected situation, it will cause harm to the staff, therefore, we provide a four rotor unmanned plane debugging platform to solve the above problems. UTILITY MODEL CONTENTS

[0005] The main purpose of the utility model is to provide a four rotor unmanned plane debugging platform, which can effectively solve the above problems.

[0006] To achieve the above purpose, the technical scheme adopted by the utility model is:

[0007] A four rotor unmanned plane debugging platform, comprising a base, the top of the base is fixedly connected with two fixed blocks, the top of each of the two fixed blocks is fixedly connected with a fixed rod, the inner walls of the top of the two fixed rods are fixedly connected with a connecting rod, the outer surface of the connecting rod is rotatably connected with a fixing seat, a supporting assembly is arranged above the base, and a fixing assembly is arranged in the fixing seat.

[0008] Preferably, the supporting assembly comprises a bidirectional threaded rod one, the outer surfaces of the left side and the right side of the bidirectional threaded rod one are rotatably connected with the inner walls of the same side of the fixed blocks, the left end of the fixed block located on the left side is fixedly connected with a motor, and the output end of the motor is fixedly connected with the left end of the bidirectional threaded rod one.

[0009] Preferably, the two-way threaded rod is externally threaded connected with two moving blocks, and the top inner walls of the two moving blocks are rotationally connected with rotating rods.

[0010] Preferably, the top outer surfaces of the two rotating rods are rotationally connected with connecting blocks, and the outer surfaces of the two fixed rods are slidingly connected with support plates.

[0011] Preferably, the two support plates are symmetrically arranged around the center of the two-way threaded rod, the bottom of the support plate is fixedly connected with the top of the connecting block on the same side, and the top of the support plate is in contact with the bottom of the fixed seat.

[0012] Preferably, the fixed assembly comprises a two-way threaded rod II, the front and back outer surfaces of the two-way threaded rod II are rotationally connected with the inner walls of the fixed seat, and the front of the two-way threaded rod II is fixedly connected with a rotating block.

[0013] Preferably, the outer surfaces of the two clamping plates are externally threaded connected with two clamping plates, and the left and right sides of the two clamping plates are externally threaded connected with two clamping plates.

[0014] Preferably, the top of the fixed seat is provided with two sliding grooves, the bottom of the two clamping plates is fixedly connected with two guide rods, and the outer surfaces of the two guide rods are slidingly connected with the inner walls of the sliding grooves on the same side.

[0015] Compared with the prior art, the utility model has the advantages of:

[0016] 1. The utility model discloses a supporting assembly, which is specifically opened motor drive support plate on the outer surface of the corresponding fixed block and slides upwards to support the fixed seat, so that the staff does not need to manually support, and the staff can be liberated from the tedious task, and other detection preparation work can be carried out at the same time, so that the staff does not need to be specially arranged to support operation, the labor cost is reduced, and the situation that the unmanned aerial vehicle is suddenly started in an unexpected situation and causes harm to the staff can be avoided.

[0017] 2. The utility model discloses a fixed assembly, which is specifically clockwise rotating rotating block and drives two clamping plates to move close to each other to fix the unmanned aerial vehicle on the top of the fixed seat, so that the staff does not need to fix it through several screws, the installation time of each unmanned aerial vehicle can be significantly saved, the overall debugging work efficiency is improved, and the process of tightening the screws can avoid generating certain pressure and slight deformation on the unmanned aerial vehicle body, and physical interference on the unmanned aerial vehicle is reduced. BRIEF DESCRIPTION OF DRAWINGS

[0018] Figure 1 It is a whole structure schematic view of the utility model;

[0019] Figure 2This is a schematic diagram of the overall structure of the support plate of this utility model;

[0020] Figure 3 This utility model Figure 2 A magnified structural diagram of A in the middle;

[0021] Figure 4 This is a schematic diagram of the overall structure of the fixing base of this utility model;

[0022] Figure 5 This utility model Figure 4 A magnified structural diagram of B in the diagram.

[0023] In the diagram: 1. Base; 11. Fixing block; 12. Fixing rod; 13. Connecting rod; 14. Fixing seat; 2. Support assembly; 21. Double-sided threaded rod one; 22. Motor; 23. Moving block; 231. Rotating rod; 232. Connecting block; 24. Support plate; 3. Fixing assembly; 31. Double-sided threaded rod two; 32. Rotating block; 33. Clamping plate; 34. Slide groove; 35. Guide rod. Detailed Implementation

[0024] To make the technical means, creative features, objectives and effects of this utility model easier to understand, the present utility model will be further described below in conjunction with specific embodiments.

[0025] Example 1, such as Figures 1-5 As shown, a quadcopter drone debugging platform includes a base 1. Two fixing blocks 11 are fixedly connected to the top of the base 1. Fixing rods 12 are fixedly connected to the top of each of the two fixing blocks 11. A connecting rod 13 is fixedly connected to the inner wall of the top of the two fixing rods 12. A fixing seat 14 is rotatably connected to the outer surface of the connecting rod 13. A support component 2 is provided above the base 1. A fixing component 3 is provided inside the fixing seat 14.

[0026] Specifically, in order to achieve the goal of not requiring dedicated personnel to support and operate the drones, please refer to... Figure 2 and Figure 3 In this embodiment, the support component 2 includes a bidirectional threaded rod 21. The left and right outer surfaces of the bidirectional threaded rod 21 are rotatably connected to the inner wall of the fixing block 11 on the same side. A motor 22 is fixedly connected to the left end of the fixing block 11 located on the left side. The output end of the motor 22 is fixedly connected to the left end of the bidirectional threaded rod 21.

[0027] Further reading Figure 2 In this embodiment, the outer surface of the bidirectional threaded rod 21 is threaded with two moving blocks 23, and the inner top walls of the two moving blocks 23 are rotatably connected with rotating rods 231.

[0028] In the implementation process, the motor 22 is turned on to drive the bidirectional threaded rod 21 to rotate in the inner wall of the two fixed blocks 11. The bidirectional threaded rod 21 rotates clockwise while driving the two moving blocks 23 to move closer to each other. When the moving blocks 23 move, the rotating rods 231 are rotated.

[0029] Further, referring to Figure 2 In this embodiment, the outer surfaces of the two rotating rods 231 are rotatably connected to the connecting blocks 232, and the outer surfaces of the two fixed rods 12 are slidably connected to the support plates 24.

[0030] Further, referring to Figure 2 In this embodiment, the two support plates 24 are symmetrically arranged around the center of the bidirectional threaded rod 21, the bottom of the support plate 24 is fixedly connected to the top of the connecting block 232 on the same side, and the top of the support plate 24 is in contact with the bottom of the fixed seat 14.

[0031] In the implementation process, the rotating rods 231 rotate and push the support plates 24 to slide upward on the outer surfaces of the corresponding fixed blocks 11 through the connecting blocks 232. When the support plates 24 slide upward by a certain distance, their tops will be in contact with the bottom of the fixed seat 14. The two support plates 24 can support the fixed seat 14, so that the top of the fixed unmanned aerial vehicle is in a normal flight attitude state, without the need for manual support by the staff. This not only frees the staff from this tedious task, but also allows them to perform other detection preparation work, reducing labor costs and avoiding the risk of injury to the staff in the event of an unexpected start of the unmanned aerial vehicle.

[0032] Embodiment Two, this embodiment is based on Embodiment One and sets up a fixing assembly.

[0033] Specifically, in order to achieve the purpose of quickly fixing the unmanned aerial vehicle, referring to Figure 4 and Figure 5 In this embodiment, the fixing assembly 3 includes a bidirectional threaded rod 31, the front and back outer surfaces of the bidirectional threaded rod 31 are rotatably connected to the inner walls of the fixed seat 14, and the front of the bidirectional threaded rod 31 is fixedly connected to a rotating block 32.

[0034] Further, referring to Figure 4 In this embodiment, the outer surface of the bidirectional threaded rod 31 is threadedly connected to two clamping plates 33, and the left and right sides of the two clamping plates 33 are provided with anti-slip patterns near the center of the fixed seat 14.

[0035] Further, referring to Figure 5In the embodiment, the top of the fixing seat 14 is provided with two sliding grooves 34, the bottom of each clamping plate 33 is fixedly connected with two guide rods 35, and the outer surfaces of the two guide rods 35 are slidably connected with the inner walls of the same sliding grooves 34.

[0036] In the implementation process, the rotating block 32 is rotated clockwise to drive the bidirectional threaded rod two 31 to rotate in the inner wall of the fixing seat 14, the bidirectional threaded rod two 31 is rotated to drive the two clamping plates 33 to move close to each other, the clamping plate 33 is moved to drive the guide rod 35 to slide in the inner wall of the corresponding sliding groove 34, and after the clamping plate 33 is moved by a distance, one side of the clamping plate 33 provided with anti-skid lines is in contact with the bottom surface of the unmanned aerial vehicle. The two clamping plates 33 can fix the unmanned aerial vehicle on the top of the fixing seat 14, and the unmanned aerial vehicle does not need to be fixed by the staff through several screws. Not only can the installation time of each unmanned aerial vehicle be significantly saved, and the overall debugging work efficiency be improved, but also the process of tightening the screws can avoid generating certain pressure and slight deformation on the unmanned aerial vehicle body, and reduce the physical interference on the unmanned aerial vehicle.

[0037] The working principle of the utility model is as follows: when the quad-rotor unmanned aerial vehicle needs to be detected, first, the bottom of the unmanned aerial vehicle is placed on the top of the fixing seat 14, the rotating block 32 is rotated clockwise to drive the bidirectional threaded rod two 31 to rotate in the inner wall of the fixing seat 14, the bidirectional threaded rod two 31 is rotated to drive the two clamping plates 33 to move close to each other, the clamping plate 33 is moved to drive the guide rod 35 to slide in the inner wall of the corresponding sliding groove 34, and after the clamping plate 33 is moved by a distance, one side of the clamping plate 33 provided with anti-skid lines is in contact with the bottom surface of the unmanned aerial vehicle. The two clamping plates 33 can fix the unmanned aerial vehicle on the top of the fixing seat 14, and the unmanned aerial vehicle does not need to be fixed by the staff through several screws. Not only can the installation time of each unmanned aerial vehicle be significantly saved, and the overall debugging work efficiency be improved, but also the process of tightening the screws can avoid generating certain pressure and slight deformation on the unmanned aerial vehicle body, and reduce the physical interference on the unmanned aerial vehicle.

[0038] The basic principle and main features of the present application and the advantages of the present application are shown and described above. Those skilled in the art should understand that the present application is not limited by the above embodiments, and the above embodiments and descriptions in the specification are only to illustrate the principles of the present application. Without departing from the spirit and scope of the present application, various changes and improvements can be made to the present application, and these changes and improvements all fall within the scope of the claimed present application. The scope of protection of the present application is defined by the appended claims and their equivalents.

Claims

1. A quadcopter unmanned aerial vehicle (UAV) debugging platform, comprising a base (1), wherein two fixing blocks (11) are fixedly connected to the top of the base (1), and fixing rods (12) are fixedly connected to the top of each of the two fixing blocks (11), and a connecting rod (13) is fixedly connected to the inner wall of the top of the two fixing rods (12), and a fixing seat (14) is rotatably connected to the outer surface of the connecting rod (13), characterized in that: The base (1) is provided with a support assembly (2) above, and the fixed seat (14) is internally provided with a fixing assembly (3); The support assembly (2) comprises a bidirectional threaded rod (21), the left and right outer surfaces of the bidirectional threaded rod (21) are rotatably connected with the inner walls of the fixed blocks (11) on the same side, the left end of the fixed block (11) on the left side is fixedly connected with a motor (22), and the output end of the motor (22) is fixedly connected with the left end of the bidirectional threaded rod (21).

2. The quadcopter drone commissioning platform of claim 1, wherein: The outer surface of the bidirectional threaded rod (21) is threadedly connected with two moving blocks (23), and the top inner walls of the two moving blocks (23) are rotatably connected with rotating rods (231).

3. The quadcopter drone commissioning platform of claim 2, wherein: The top outer surfaces of the two rotating rods (231) are rotatably connected with connecting blocks (232), and the outer surfaces of the two fixed rods (12) are slidably connected with support plates (24).

4. The quadcopter drone commissioning platform of claim 3, wherein: The two support plates (24) are symmetrically arranged around the center of the bidirectional threaded rod (21), the bottom of the support plate (24) is fixedly connected with the top of the connecting block (232) on the same side, and the top of the support plate (24) is in contact with the bottom of the fixed seat (14).

5. The quadcopter drone commissioning platform of claim 1, wherein: The fixing assembly (3) comprises a bidirectional threaded rod (31), the front and back outer surfaces of the bidirectional threaded rod (31) are rotatably connected with the inner walls of the fixed seat (14), and the front of the bidirectional threaded rod (31) is fixedly connected with a rotating block (32).

6. The quadcopter drone commissioning platform of claim 5, wherein: The outer surface of the bidirectional threaded rod (31) is threadedly connected with two clamping plates (33), and the left and right ends of the two clamping plates (33) close to the center of the fixed seat (14) are provided with anti-skid lines.

7. The quadcopter drone commissioning platform of claim 6, wherein: The top of the fixed seat (14) is provided with two sliding grooves (34), the bottom of the two clamping plates (33) is fixedly connected with two guide rods (35), and the outer surfaces of the two guide rods (35) are slidably connected with the inner walls of the sliding grooves (34) on the same side.

Images