Unmanned aerial vehicle temperature testing device

Abstract

The utility model discloses an unmanned aerial vehicle temperature testing device which comprises an unmanned aerial vehicle, a connecting structure is fixedly assembled at the lower end of the unmanned aerial vehicle, a lifting structure is assembled at the lower end of the connecting structure, and a temperature tester is assembled at the lower end of the inner wall of the lifting structure. The temperature tester is driven to reach a designated working position, the lifting structure and the temperature tester can be rotated through the effect of the connecting structure, it is guaranteed that the application range of the device is wide, meanwhile, components are convenient to disassemble and replace, and through the arrangement of the lifting structure, when the temperature tester reaches the air above the designated testing position, the unmanned aerial vehicle can hover at the position; a lifting structure is used, the temperature tester is put down, it is guaranteed that temperature testing work is conducted smoothly, meanwhile, the unmanned aerial vehicle is effectively protected, damage to the unmanned aerial vehicle due to high temperature is avoided, and practicability is high.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, and in particular to a temperature testing device for unmanned aerial vehicles. Background Art

[0002] Drones are aircraft that do not require a human pilot to operate them in the cabin. They can be controlled by remote controls, computer programs, or a combination of the two. Drones come in many types and sizes, from small consumer drones to large military drones. Drones are often used for special tasks. When temperature detection is required at a specific location, some tasks cannot be completed manually. Drones need to carry temperature testers for detection. Existing equipment is fixed to the bottom of the drone and is close to the drone. The drone is easily damaged when exposed to high temperatures, and its practicality is poor. Utility Model Content

[0003] The purpose of the utility model is to provide a temperature testing device for an unmanned aerial vehicle to solve the problems raised in the above-mentioned background technology.

[0004] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a UAV temperature testing device, comprising a UAV, the lower end of which is fixedly equipped with a connecting structure, the lower end of which is equipped with a lifting structure, and the lower end of the inner wall of the lifting structure is equipped with a temperature tester.

[0005] Preferably, the connecting structure includes a support block, which is fixedly assembled at the lower end of the drone, and a rotating block is rotatably assembled on the inner wall of the support block, and a connecting plate is fixedly assembled at the lower end of the rotating block, and the lower end of the connecting plate is connected to a support via screws, and the lower end of the support is connected to the lifting structure.

[0006] Preferably, the lifting structure includes a box body, which is fixedly assembled on the lower end of the connecting structure, and a motor is fixedly assembled on the inner wall of the box body. One end of the rotating shaft is fixedly assembled on the motor shaft end of the motor, and the other end of the rotating shaft is rotatably assembled on the inner wall of the box body. A wire roller is fixedly sleeved on the outer wall of the rotating shaft, and a steel rope is fixedly wrapped around the outer wall of the wire roller. The end of the steel rope passes through the box body and is fixedly connected to an electromagnet. A metal sleeve is fixedly assembled on the lower end of the box body, and the metal sleeve is sleeved on the outer wall of the steel rope, and the metal sleeve is adsorbed on the electromagnet. A mounting frame is fixedly assembled on the lower end of the electromagnet, and the temperature tester is assembled on the inner wall of the mounting frame.

[0007] Preferably, screws are installed through both sides of the mounting frame, and the inner ends of the two screws are in contact with the temperature tester.

[0008] Preferably, the bottom surface position of the temperature tester in the retracted state is higher than the bottom surface position of the legs of the drone.

[0009] Compared with the prior art, the beneficial effects of the utility model are: the drone can be controlled by a remote control, a computer program or a combination of the two, and the temperature tester can be driven to the designated working position by adjusting the position of the drone. The lifting structure and the temperature tester can be rotated through the action of the connecting structure to ensure a wide range of use of the equipment and facilitate the disassembly and replacement of components. Through the setting of the lifting structure, when the temperature tester reaches the designated test position, the drone can hover there, and the temperature tester can be put down using the lifting structure to ensure the smooth progress of the temperature test. At the same time, the drone is effectively protected to avoid damage to the drone due to high temperature, etc. The utility model has strong practicality, and the selection of the temperature tester should be determined according to the specific application requirements, measurement range, accuracy and environmental conditions. BRIEF DESCRIPTION OF THE DRAWINGS

[0010] Figure 1 It is a schematic diagram of the structure of the utility model;

[0011] Figure 2 for Figure 1 A schematic diagram of the structure enlargement in the middle;

[0012] Figure 3 It is a three-dimensional schematic diagram of the connection structure;

[0013] Figure 4 for Figure 2 Enlarged schematic diagram of the structure at point B in the middle.

[0014] In the figure: 1-UAV, 2-connecting structure, 21-support block, 22-rotating block, 23-connecting plate, 24-support, 3-lifting structure, 31-box, 32-motor, 33-rotating shaft, 34-line roller, 35-steel rope, 36-metal sleeve, 37-electromagnet, 38-installation frame, 4-temperature tester. DETAILED DESCRIPTION

[0015] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0016] See also Figure 1-4 The utility model provides a temperature testing device for a UAV, including a UAV 1. A connecting structure 2 is fixedly mounted on the lower end of the UAV 1. A lifting structure 3 is mounted on the lower end of the connecting structure 2. A temperature tester 4 is mounted on the lower end of the inner wall of the lifting structure 3.

[0017] The drone 1 can be controlled by a remote controller, a computer program, or a combination of the two. The temperature tester 4 can be driven to reach a designated working position by adjusting the position of the drone 1. The lifting structure 3 and the temperature tester 4 can be rotated by the connecting structure 2 to ensure a wide range of use of the equipment and facilitate the disassembly and replacement of components. By setting the lifting structure 3, when the temperature tester 4 reaches the designated test position, the drone 1 can hover there, and the temperature tester 4 can be put down using the lifting structure 3 to ensure smooth temperature testing. At the same time, the drone 1 can be effectively protected to avoid damage to the drone 1 due to high temperature. The drone 1 is highly practical. The selection of the temperature tester 4 should be determined based on specific application requirements, measurement range, accuracy, and environmental conditions.

[0018] The connecting structure 2 includes a support block 21, which is fixedly assembled at the lower end of the drone 1. A rotating block 22 is rotatably assembled on the inner wall of the support block 21. A connecting plate 23 is fixedly assembled at the lower end of the rotating block 22. The lower end of the connecting plate 23 is connected to a support 24 by screws. The lower end of the support 24 is connected to the lifting structure 3.

[0019] The rotating block 22 in the connecting structure 2 can be used to rotate on the inner wall of the supporting block 21 to drive the lower end lifting structure 3 to rotate. At the same time, the screws can be removed to separate the support 24 from the connecting plate 23, which is convenient for disassembly and replacement of components and easy to use.

[0020] The lifting structure 3 includes a box body 31, which is fixedly assembled on the lower end of the connecting structure 2. A motor 32 is fixedly assembled on the inner wall of the box body 31. The motor shaft end of the motor 32 is fixedly assembled with one end of a rotating shaft 33. The other end of the rotating shaft 33 is rotatably assembled on the inner wall of the box body 31. A wire roller 34 is fixedly sleeved on the outer wall of the rotating shaft 33. A steel rope 35 is fixedly wound around the outer wall of the wire roller 34. The end of the steel rope 35 passes through the box body 31 and is fixedly connected to an electromagnet 37. A metal sleeve 36 is fixedly assembled on the lower end of the box body 31. The metal sleeve 36 is sleeved on the outer wall of the steel rope 35, and the metal sleeve 36 is adsorbed on the electromagnet 37. The lower end of the electromagnet 37 is fixedly assembled with a mounting frame 38, and the temperature tester 4 is assembled on the inner wall of the mounting frame 38.

[0021] When it is necessary to use the lifting structure 3, first when it is necessary to lower the temperature tester 4, turn off the electromagnet 37 so that there is no adsorption force between it and the metal sleeve 36, turn on the motor 32, drive the rotating shaft 33 to rotate, drive the wire roller 34 to release the steel rope 35, and at the same time, according to the gravity of the temperature tester 4, it will move downward. At this time, the steel rope 35 hangs the temperature tester 4. After reaching the appropriate position, turn off the motor 32 and perform the temperature test. The box body 31 can protect the internal components, and the installation frame 38 is used to fix the temperature tester 4.

[0022] Screws are installed through both sides of the mounting frame 38 , and the inner ends of the two screws are against the temperature tester 4 .

[0023] The screws can ensure the stability of the installation of the temperature tester 4 .

[0024] The bottom surface position of the temperature tester 4 in the retracted state is higher than the bottom surface position of the legs of the drone 1 .

[0025] It can be prevented that the temperature tester touches the bottom after the drone 1 lands.

[0026] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A temperature testing device for an unmanned aerial vehicle, characterized in that: The invention comprises an unmanned aerial vehicle (1), wherein a connection structure (2) is fixedly mounted on the lower end of the unmanned aerial vehicle (1), a lifting structure (3) is mounted on the lower end of the connection structure (2), and a temperature tester (4) is mounted on the lower end of the inner wall of the lifting structure (3).

2. The temperature testing device for an unmanned aerial vehicle according to claim 1, characterized in that: The connection structure (2) comprises a support block (21), the support block (21) is fixedly mounted on the lower end of the drone (1), a rotating block (22) is rotatably mounted on the inner wall of the support block (21), a connecting plate (23) is fixedly mounted on the lower end of the rotating block (22), the lower end of the connecting plate (23) is connected to a support (24) via screws, and the lower end of the support (24) is connected to the lifting structure (3).

3. The temperature testing device for an unmanned aerial vehicle according to claim 1, characterized in that: The lifting structure (3) comprises a box body (31), the box body (31) is fixedly mounted on the lower end of the connecting structure (2), a motor (32) is fixedly mounted on the inner wall of the box body (31), one end of a rotating shaft (33) is fixedly mounted on the motor shaft end of the motor (32), the other end of the rotating shaft (33) is rotatably mounted on the inner wall of the box body (31), a wire roller (34) is fixedly sleeved on the outer wall of the rotating shaft (33), and a steel wire is fixedly wound around the outer wall of the wire roller (34). The end of the steel rope (35) passes through the box (31) and is fixedly connected to an electromagnet (37). The lower end of the box (31) is fixedly equipped with a metal sleeve (36). The metal sleeve (36) is sleeved on the outer wall of the steel rope (35), and the metal sleeve (36) and the electromagnet (37) are attracted to each other. The lower end of the electromagnet (37) is fixedly equipped with a mounting frame (38), and the temperature tester (4) is mounted on the inner wall of the mounting frame (38).

4. The temperature testing device for an unmanned aerial vehicle according to claim 3, characterized in that: Screws are installed through both sides of the installation frame (38), and the inner ends of the two screws are in contact with the temperature tester (4).

5. The temperature testing device for an unmanned aerial vehicle according to claim 1, characterized in that: The bottom surface position of the temperature tester (4) in the retracted state is higher than the bottom surface position of the legs of the drone (1).

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