A drone inspection device for the power industry

Abstract

This invention relates to the field of unmanned aerial vehicle (UAV) inspection technology and discloses a UAV inspection device for the power industry, comprising a body, wings fixedly connected to the outer surface of the body, a lower connecting plate fixedly connected to the lower surface of the body, a lidar fixedly connected to the front side of the lower connecting plate, the lidar being used to detect the environment and customize the inspection route, and a linear motor fixedly connected to the inner surface of the body. In this invention, the lidar can perform a wide-range detection of power facilities around the body during flight, thereby planning a safe inspection route to prevent collisions with power facilities during the movement of the body and causing damage. The monitoring camera monitors the environment and power equipment in real time, thereby enabling more reasonable obstacle avoidance. The monitoring camera can adjust its angle to improve the detection effect and can also capture images of the equipment for external inspection.

Description

Technical Field

[0001] This invention relates to the field of drone inspection technology, specifically to a drone inspection device for the power industry. Background Technology

[0002] Traditional manual inspections suffer from low efficiency and high risk. Unmanned aerial vehicle (UAV) inspection systems, equipped with visible light and infrared devices, autonomously cruise and collect high-definition data, enabling intelligent and refined operation and maintenance of power lines and effectively ensuring the safe and stable operation of the power grid. However, in existing technologies, UAV inspection equipment is relatively large and its obstacle avoidance is not good enough, making it easy to collide with power equipment and cause danger.

[0003] Patent CN219105385U discloses a drone inspection device for the power industry. This patent includes hardware, a cloud platform, and a ground command system. The hardware includes a parking platform, a drone body, and inspection components. The drone body is mounted on top of the parking platform, and the inspection components are mounted on the drone body. The inspection components include a connecting plate, a dual-light intelligent camera, an AI intelligent control box, and a positioning module. The connecting plate is mounted on the drone body, and the dual-light intelligent camera is mounted on top of the connecting plate. This drone inspection device for the power industry can adjust its flight according to the surrounding environment and has increased power consumption, thus extending inspection time and improving work efficiency. While this patent solves the aforementioned problems, it still suffers from the issues of large drone size, insufficient obstacle avoidance, and the risk of collisions with power equipment. Therefore, this patent proposes a drone inspection device for the power industry to address these problems. Summary of the Invention

[0004] The technical problem to be solved by the present invention is to provide a drone inspection device for the power industry, which addresses the shortcomings of the prior art.

[0005] To solve the above-mentioned technical problems, the technical solution adopted by the present invention is: a drone inspection device for the power industry, comprising:

[0006] The fuselage has wings fixedly connected to its outer surface, a lower connecting plate fixedly connected to its lower surface, a lidar fixedly connected to the front side of the lower connecting plate, the lidar being used to detect the environment and customize inspection routes, and a linear motor fixedly connected to its inner surface.

[0007] Equipment protection device, which is installed on the front side of the machine body, is used to protect the equipment used for inspection and detection;

[0008] A vertical drop support device is provided on both sides of the aircraft body, and the vertical drop support device is used to support the aircraft body during takeoff and landing.

[0009] As a further technical solution, the body includes:

[0010] A movable base is fixedly connected to the moving end of a linear motor. A rotating base is rotatably connected to the inner surface of the movable base, and a monitoring camera is hinged to the upper surface of the rotating base.

[0011] The sensing module is located on both sides of the surveillance camera. The sensing module is a sensor system composed of devices such as gyroscopes, accelerometers, and barometric pressure sensors.

[0012] As a further technical solution, the body also includes:

[0013] A trapezoidal retaining shell is fixedly connected to a surveillance camera, and a sliding groove is provided on the side of the trapezoidal retaining shell away from the surveillance camera;

[0014] A rotating retaining shaft is engaged with the inner surface of a trapezoidal retaining housing;

[0015] Positioning pressure plate, which is slidably connected to the inner surfaces of both sides of the surveillance camera.

[0016] As a further technical solution, the movable base is slidably connected to the inner surface of the machine body, the rotating shaft abuts against both sides of the monitoring camera, the rotating shaft is slidably connected to the inner surface of the slide groove, the sensing module is fixedly connected to the end of the rotating shaft away from the monitoring camera, the positioning pressure plate abuts against the front side of the trapezoidal housing, and an elastic telescopic rod is provided between the positioning pressure plate and the inner surface of the monitoring camera.

[0017] As a further technical solution, the equipment protection device includes:

[0018] A front baffle is slidably connected to the inner surface of the front side of the body, and the front baffle is used to enclose the monitoring camera and the sensing module inside the body.

[0019] A lever, which is fixedly connected to the front side of the front baffle;

[0020] A lifting slide shaft is fixedly connected to both sides of the front baffle.

[0021] As a further technical solution, the equipment protection device also includes:

[0022] The lower protective shell is fixedly connected to the lower surface of the machine body;

[0023] A locking post, which is fixedly connected to the rear side of the front baffle;

[0024] An inner connecting rod is fixedly connected to the lower surface of the inner side of the machine body, and a retaining strip is hinged to the circumferential surface of the inner connecting rod;

[0025] A push rod is fixedly connected to both sides of the inner surface of the movable seat.

[0026] As a further technical solution, the lifting slide shaft is slidably connected to the inner surface of the front side of the machine body, and an elastic telescopic rod is provided between the lower surface of the lifting slide shaft and the inner surface of the machine body. The lower protective shell is fixedly connected to the rear side of the lower connecting plate. A through groove for the up and down movement of the locking column is provided on the front side of the machine body. A groove is provided at the rear end of the locking column. A torsion spring is provided at the hinge of the locking bar and the inner connecting rod. The front end of the push rod abuts against the side surface of the locking bar.

[0027] As a further technical solution, the vertical support device includes:

[0028] External connecting rods are fixedly connected to the inner surfaces of both sides of the machine body;

[0029] A flipping shaft is hinged to both ends of the circumference of the outer connecting rod.

[0030] The bracket is fixedly connected to the circumferential surface of the flipping shaft.

[0031] As a further technical solution, the vertical support device also includes:

[0032] A limiting rod is fixedly connected to the circumferential surface of the bracket;

[0033] A clamping plate is hinged to the inner surfaces of both sides of the machine body, and a positioning plate is fixedly connected to the end of the clamping plate away from the push rod.

[0034] The locking block is fixedly connected to the circumferential surface of the rear end of the push rod.

[0035] As a further technical solution, a torsion spring is provided at the hinge of the flipping shaft and the outer connecting rod, a groove is provided on the upper surface of the limiting rod, a torsion spring is provided at the hinge of the clamping plate and the inner surface of the machine body, the push rod is slidably connected to the inner surface of the machine body, the clamping block is slidably connected to the inner surface of the machine body, and a keyway is provided on the inner side of the clamping plate, and the keyway and the clamping block are engaged.

[0036] The present invention, by adopting the above technical solution, can bring the following beneficial effects:

[0037] 1. This power industry drone inspection equipment utilizes a lidar system to conduct a wide-range survey of power installations around the drone during flight, thereby planning a safe inspection route to prevent collisions and damage during drone movement. A monitoring camera provides real-time monitoring of the environment and power equipment, enabling more efficient obstacle avoidance. The camera's angle can be adjusted to improve detection effectiveness, and it can also capture images of the equipment for external inspection. The sensing module detects the drone's flight attitude, acceleration, air pressure, and airflow, transmitting signals to the control center for more precise drone control and improved flight stability. A rotating hinge allows the sensing module to be removed from the trapezoidal housing, enhancing ease of use. Furthermore, the trapezoidal housing allows for adjustment of the angles of multiple sensing modules while they are installed, improving sensing performance and the device's applicability.

[0038] 2. This power industry drone inspection equipment has a front baffle that slides upwards and seals the body, thereby protecting the monitoring camera and sensing module from damage and improving the safety of the device. The lever drives the front baffle to slide downwards and insert into the lower protective shell, at which point the monitoring camera can extend out of the body to assist in the inspection.

[0039] 3. In this drone inspection equipment for the power industry, after the locking bar loses the resistance of the push rod, it is rotated by the torsion spring set at the hinge of the inner connecting rod and inserts into the groove opened at the rear end of the locking post, thereby vertically locking the front baffle and improving the protective effect of the device. The lifting slide shaft drives the front baffle to slide down, so that it does not need to be opened manually. This allows the front baffle to move down and open while following the monitoring camera to move forward, improving the ease of use of the device.

[0040] 4. The power industry drone inspection equipment has a support frame that contacts the ground to prevent the drone from being damaged by direct contact with the ground during take-off and landing, thus improving the safety and service life of the device. When it is necessary to disassemble and store the device, the locking plate is lowered so that the drone body is inserted into the groove opened on the upper surface of the limiting rod. The locking plate then moves the positioning plate to one side of the limiting rod to lock it and prevent it from rotating, thus improving the convenience of storage.

[0041] 5. In this power industry drone inspection equipment, the clamping plate drives the positioning plate to lift, thereby unlocking the limit rod. At this time, the flipping shaft is affected by the torsion spring set at the hinge of the external connecting rod, which causes it to pop out to both sides of the body and automatically flip to the bottom of the body, further improving the ease of use of the device. Attached Figure Description

[0042] Figure 1 This is a schematic diagram of the overall three-dimensional structure of the present invention;

[0043] Figure 2 This is a three-dimensional half-section structural diagram of the front side of the body of the present invention;

[0044] Figure 3 This is a three-dimensional half-section diagram of the front side of the surveillance camera of the present invention;

[0045] Figure 4 For the present invention Figure 3 A magnified structural diagram of A in the middle;

[0046] Figure 5 This is a three-dimensional half-sectional view of the front side of the protective device of the present invention;

[0047] Figure 6 For the present invention Figure 5 A magnified structural diagram of B in the diagram;

[0048] Figure 7 This is a three-dimensional half-section diagram of the front side of the vertical support device of the present invention;

[0049] Figure 8 For the present invention Figure 7 A magnified structural diagram of C.

[0050] In the diagram: 1. Airframe; 2. Wing; 3. Lower connecting plate; 4. LiDAR; 5. Linear motor; 6. Equipment protection device; 7. Vertical drop support device; 8. Moving seat; 9. Rotating seat; 10. Monitoring camera; 11. Sensing module; 12. Trapezoidal housing; 13. Slide groove; 14. Rotating locking shaft; 15. Positioning pressure plate; 61. Front baffle; 62. Paddle plate; 63. Lifting slide shaft; 64. Lower protective shell; 65. Locking post; 66. Inner connecting rod; 67. Locking strip; 68. Push rod; 71. Outer connecting rod; 72. Tilting shaft; 73. Bracket; 74. Limiting rod; 75. Locking plate; 76. Positioning plate; 77. Locking block. Detailed Implementation

[0051] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0052] Please see Figures 1-8One embodiment of the present invention is: a drone inspection device for the power industry, comprising a body 1, wings 2 fixedly connected to the outer surface of the body 1, a lower connecting plate 3 fixedly connected to the lower surface of the body 1, a lidar 4 fixedly connected to the front side of the lower connecting plate 3, the lidar 4 being used to detect the environment and customize the inspection route, a linear motor 5 fixedly connected to the inner surface of the body 1, an equipment protection device 6 disposed on the front side of the body 1, the equipment protection device 6 being used to protect the inspection and detection equipment, and vertical landing support devices 7 disposed on both sides of the body 1, the vertical landing support devices 7 being used to support the body 1 during takeoff and landing, and the lidar 4 being able to... The system conducts a large-scale survey of the electrical installations around the machine body 1, and then plans a safe patrol route to prevent collisions with electrical installations during the movement of the machine body 1. The monitoring camera 10 monitors the environment and electrical equipment in real time, and then avoids obstacles more reasonably. The monitoring camera 10 can adjust its angle to improve the detection effect, and can also capture images of the equipment for external detection. The machine body 1 includes a movable base 8, which is fixedly connected to the moving end of the linear motor 5. A rotating base 9 is rotatably connected to the inner surface of the movable base 8, and the monitoring camera 10 is hinged to the upper surface of the rotating base 9. The sensing modules 11 are set on both sides of the monitoring camera 10. The sensing module 11 is a sensor system composed of devices such as a gyroscope, accelerometer, and barometric pressure sensor. The body 1 also includes a trapezoidal retaining shell 12, which is fixedly connected to the monitoring camera 10. A sliding groove 13 is provided on the side of the trapezoidal retaining shell 12 away from the monitoring camera 10. A rotating retaining shaft 14 is engaged with the inner surface of the trapezoidal retaining shell 12. A positioning pressure plate 15 is slidably connected to the inner surfaces of both sides of the monitoring camera 10. The moving base 8 is slidably connected to the inner surface of the body 1. The rotating retaining shaft 14 abuts against both sides of the monitoring camera 10. The rotating retaining shaft 14 is slidably connected to the inner surface of the sliding groove 13. The sensing module 11 and the rotating retaining shaft 14 are located away from the monitoring camera. One end of the camera 10 is fixedly connected, and the positioning pressure plate 15 and the front side of the trapezoidal housing 12 abut against each other. An elastic telescopic rod is provided between the positioning pressure plate 15 and the inner surface of the monitoring camera 10. The sensing module 11 can sense the flight attitude, acceleration, air pressure and airflow of the aircraft 1 and transmit the signals to the control center, thereby controlling the aircraft 1 more accurately and improving flight stability. The rotating shaft 14 can pull the sensing module 11 out of the trapezoidal housing 12, which improves the ease of use of the device. The trapezoidal housing 12 can adjust the angle of each sensing module 11 while installing multiple sensing modules 11, which improves the sensing effect and the applicability of the device.

[0053] Working Principle: The wing 2 is activated, propelling the fuselage 1 upwards and allowing it to inspect electrical facilities during flight. As the fuselage 1 moves, it moves the lower connecting plate 3, which in turn moves the lidar 4. The lidar 4 is then activated, enabling it to conduct a wide-area survey of the electrical installations around the fuselage 1 during flight, thus planning a safe inspection route to prevent collisions and hazards. The linear motor 5 is activated, moving the moving base 8 forward, which in turn moves the rotating base 9 forward. The rotating base 9 then extends the monitoring camera 10 out of the fuselage 1. The monitoring camera 10 provides real-time monitoring of the environment and electrical equipment, allowing for more effective obstacle avoidance. Activating the micro-motor 1 built into the rotating base 9 and the micro-motor 2 located on one side of the hinge between the monitoring camera 10 and the rotating base 9 controls the dual-axis rotation of the monitoring camera 10, adjusting its angle and improving detection accuracy. When the device is moved near the power equipment, the monitoring camera 10 can capture images of the equipment and perform external detection. The sensing module 11 is inserted into the trapezoidal housing 12 and the slide groove 13 through the rotating clamp 14. At this time, the positioning plate 15 pops out from the monitoring camera 10 through the elastic telescopic rod to fix the rotating clamp 14 in the trapezoidal housing 12, thereby quickly fixing the sensing module 11. The sensing module 11 can sense the flight attitude, acceleration, air pressure and airflow of the aircraft 1 and transmit the signals to the control center, thereby controlling the aircraft 1 more accurately and improving flight stability. When it is necessary to disassemble and replace the sensing module 11, press the positioning plate 15 to insert it into the aircraft 1. At this time, the sensing module 11 can be pulled out of the trapezoidal housing 12 by rotating the clamp 14, which improves the ease of use of the device. Moreover, the trapezoidal housing 12 can adjust the angle of each sensing module 11 while installing multiple sensing modules 11, which improves the sensing effect and the applicability of the device.

[0054] Please see Figures 1-8Based on the above embodiments, in another embodiment of the present invention, the equipment protection device 6 includes a front baffle 61, which is slidably connected to the inner surface of the front side of the body 1. The front baffle 61 is used to enclose the monitoring camera 10 and the sensing module 11 inside the body 1. A lever 62 is fixedly connected to the front side of the front baffle 61, and a lifting slide shaft 63 is fixedly connected to both sides of the front baffle 61. The front baffle 61 slides upward and encloses the body 1, thereby protecting the monitoring camera 10 and the sensing module 11 from damage and improving the safety of the device. The lever 62 drives the front baffle 61 to slide downward and insert into the lower protective shell 64. At this time, the monitoring camera 10 can extend out of the body 1 to assist in inspection. The equipment protection device 6 also includes a lower protective shell 64, which is fixedly connected to the lower surface of the body 1. A locking post 65 is fixedly connected to the rear side of the front baffle 61, and an inner connecting rod 66 is fixedly connected to the lower inner surface of the body 1. A locking strip is hinged to the circumferential surface of the inner connecting rod 66. 67. Push rod 68 is fixedly connected to both sides of the inner surface of the movable base 8. Lifting slide shaft 63 is slidably connected to the inner surface of the front side of the body 1. An elastic telescopic rod 2 is provided between the lower surface of the lifting slide shaft 63 and the inner surface of the body 1. The lower protective shell 64 is fixedly connected to the rear side of the lower connecting plate 3. A through groove for the up and down movement of the locking post 65 is opened on the front side of the body 1. A groove is opened at the rear end of the locking post 65. A torsion spring is provided at the hinge of the locking strip 67 and the inner connecting rod 66. The front end of the push rod 68 abuts against the side surface of the locking strip 67. After the locking strip 67 loses the contact of the push rod 68, it is rotated by the torsion spring at the hinge of the locking strip 67 and inserts into the groove opened at the rear end of the locking post 65, thereby vertically locking the front baffle 61 and improving the protective effect of the device. The lifting slide shaft 63 drives the front baffle 61 to slide downward, so that it does not need to be opened manually. This allows the front baffle 61 to move downward and open while moving forward with the monitoring camera 10, improving the ease of use of the device.

[0055] Working principle: After the moving base 8 retracts the monitoring camera 10 into the body 1, it lifts the lever 62 upwards. The lever 62 drives the front baffle 61 and the lifting shaft 63 to slide upwards and close the body 1, thereby protecting the monitoring camera 10 and the sensing module 11 from damage and improving the safety of the device. When inspection is required, the lever 62 is pressed down, and the lever 62 drives the front baffle 61 to slide downwards and insert into the lower protective shell 64. At this time, the monitoring camera 10 can extend out of the body 1 to assist in the inspection. When the front baffle 61 slides upwards to reset, it drives the locking pin 65 to move upwards. When the rear end of the locking pin 65 is aligned with the locking strip 67, the moving base 8 drives the push rod 68 to continue to move backwards, and the locking strip 67 loses the push rod. After contact with 68, it rotates under the influence of the torsion spring at the hinge of 68 and the inner connecting rod 66 and inserts into the groove at the rear end of the locking post 65, thereby vertically locking the front baffle 61 and improving the protective effect of the device. After the moving seat 8 drives the push rod 68 to move forward a certain distance, the push rod 68 pushes the locking strip 67 to rotate and pull away from the locking post 65, so that the locking post 65 and the front baffle 61 lose their limit. At this time, the elastic reset action of the elastic telescopic rod 2 pulls the lifting slide shaft 63 to slide downward. The lifting slide shaft 63 drives the front baffle 61 to slide downward, so that it does not need to be opened manually. This allows the front baffle 61 to move downward and open while moving forward with the monitoring camera 10, improving the ease of use of the device.

[0056] Please see Figures 1-8 Based on the above embodiments, in another embodiment of the present invention, the descent support device 7 includes an outer connecting rod 71, which is fixedly connected to the inner surfaces of both sides of the body 1. A tilting shaft 72 is hinged to the front and rear ends of the circumference of the outer connecting rod 71. A bracket 73 is fixedly connected to the circumference of the tilting shaft 72. The bracket 73 is in contact with the ground to prevent the body 1 from being damaged by direct contact with the ground during take-off and landing, thus improving the safety and service life of the device. When the device needs to be disassembled and stored, the locking plate 75 is lowered so that the body 1 is inserted into the groove opened on the upper surface of the limiting rod 74. The locking plate 75 then moves the positioning plate 76 to one side of the limiting rod 74 to lock it and prevent it from rotating, thus improving the convenience of storage. The descent support device 7 also includes a limiting rod 74, which is fixedly connected to the circumference of the bracket 73. Plate 75 is hinged to the inner surfaces of both sides of the body 1. The end of plate 75 away from push rod 68 is fixedly connected to positioning plate 76. Block 77 is fixedly connected to the circumferential surface of the rear end of push rod 68. A torsion spring is provided at the hinge of flip shaft 72 and outer connecting rod 71. A groove is provided on the upper surface of limit rod 74. A torsion spring is provided at the hinge of plate 75 and inner surface of body 1. Push rod 68 is slidably connected to inner surface of body 1. Block 77 is slidably connected to inner surface of body 1. A keyway is provided on the inner side of plate 75, and the keyway and block 77 are engaged. Plate 75 drives positioning plate 76 to lift, thereby unlocking limit rod 74. At this time, flip shaft 72 is affected by the torsion spring at its hinge with outer connecting rod 71 and pops out to both sides of body 1 and automatically flips to the bottom of body 1, further improving the ease of use of the device.

[0057] Working principle: Rotating the flip shaft 72 causes the bracket 73 to flip along the axis of the outer connecting rod 71, making the bracket 73 contact the ground. This prevents the machine body 1 from being damaged by direct contact with the ground during take-off and landing, improving the safety and service life of the device. When it is necessary to disassemble and store the device, the bracket 73 is lifted again and retracted into both sides of the machine body 1. The bracket 73 then drives the limiting rod 74 to rotate and retract into both sides of the machine body 1. At this time, the locking plate 75 is lowered, allowing the machine body 1 to be inserted into the groove opened on the upper surface of the limiting rod 74. The locking plate 75 then drives the positioning plate 76 to move to one side of the limiting rod 74 to lock it and prevent it from rotating, improving the convenience of storage. When the device is needed, the movable seat 8 drives the push rod 68 to move forward, and the push rod 68 drives the locking block 77 to move forward. After the locking block 77 moves forward a certain distance, it is pulled out from the keyway opened on the inner side of the locking plate 75. After the locking plate 75 loses the limit of the locking block 77, it is affected by the torsion spring set at the hinge of the locking plate 75 with the inner surface of the body 1, rotates and lifts up and disengages from the limiting rod 74. The locking plate 75 then drives the positioning plate 76 to lift up, thereby unlocking the limiting rod 74. At this time, the flipping shaft 72 is affected by the torsion spring set at the hinge of the flipping shaft 72 with the outer connecting rod 71, and pops out to both sides of the body 1 and automatically flips to the bottom of the body 1, further improving the ease of use of the device.

[0058] This invention provides a drone inspection device for the power industry. Many methods and approaches exist for implementing this technical solution; the above description is merely a preferred embodiment. It should be noted that those skilled in the art can make various improvements and modifications without departing from the principles of this invention, and these improvements and modifications should also be considered within the scope of protection of this invention. All components not explicitly stated in this embodiment can be implemented using existing technologies.

Claims

1. A UAV inspection equipment for power industry, characterized in that, Include: The body (1), the outer surface of the body (1) is fixedly connected with the wing (2), the lower surface of the body (1) is fixedly connected with the lower connecting plate (3), the front side of the lower connecting plate (3) is fixedly connected with the laser radar (4), the laser radar (4) is used for detecting environment customized inspection route, the inner surface of the body (1) is fixedly connected with the linear motor (5); The device protection device (6) is arranged on the front side of the body (1), and the device protection device (6) is used for protecting the device for inspection and detection; The vertical support device (7) is arranged on both sides of the body (1), and the vertical support device (7) is used for supporting the body (1) when taking off and landing; The body (1) comprises: The moving seat (8) is fixedly connected to the moving end of the linear motor (5), the inner surface of the moving seat (8) is rotatably connected with the rotating seat (9), and the upper surface of the rotating seat (9) is hingedly connected with the monitoring camera (10); The sensing module (11) is arranged on both sides of the monitoring camera (10), and the sensing module (11) is a sensor system composed of a gyroscope, an accelerometer and an air pressure sensor; The device protection device (6) comprises: The front baffle (61) is slidably connected to the inner surface of the front side of the body (1), and the front baffle (61) is used for closing the monitoring camera (10) and the sensing module (11) inside the body (1); The dial plate (62) is fixedly connected to the front side of the front baffle (61); The lifting slide shaft (63) is fixedly connected to both sides of the front baffle (61); The device protection device (6) further comprises: The lower protection shell (64) is fixedly connected to the lower surface of the body (1); The clamping column (65) is fixedly connected to the rear side of the front baffle (61); The inner connecting rod (66) is fixedly connected to the inner lower surface of the body (1), and the circumferential surface of the inner connecting rod (66) is hingedly connected with the clamping strip (67); The push rod (68) is fixedly connected to the inner surface of the moving seat (8) on both sides; The lifting slide shaft (63) and the front inner surface of the body (1) are slidably connected, the lower surface of the lifting slide shaft (63) and the inner surface of the body (1) are provided with elastic expansion rods two, the lower protection shell (64) and the rear side of the lower connecting plate (3) are fixedly connected, the front side of the body (1) is provided with a through slot for the up-down movement of the clamping column (65), the rear end of the clamping column (65) is provided with a groove, the clamping strip (67) and the inner connecting rod (66) are provided with a torsional spring at the hinge, and the front end of the push rod (68) and the side surface of the clamping strip (67) are abutted. 2.The unmanned aerial vehicle inspection device for power industry of claim 1, wherein: The body (1) further comprises: The trapezoidal clamping shell (12) is fixedly connected to the monitoring camera (10), and the side away from the monitoring camera (10) of the trapezoidal clamping shell (12) is provided with a sliding groove (13). Rotary shaft (14) is clamped in trapezoidal shell (12) inner surface; Positioning pressing plate (15) is slidingly connected to the inner surface of the two sides of the monitoring camera (10).

3. The unmanned aerial vehicle inspection device for power industry of claim 2, wherein: The mobile seat (8) and the inner surface of the body (1) are slidingly connected, the rotary shaft (14) and the two sides of the monitoring camera (10) are abutted, the rotary shaft (14) and the inner surface of the sliding groove (13) are slidingly connected, the induction module (11) and the rotary shaft (14) are fixedly connected away from one end of the monitoring camera (10), the positioning pressing plate (15) and the front side of the trapezoidal shell (12) are abutted, and the positioning pressing plate (15) and the inner surface of the monitoring camera (10) are provided with elastic expansion rod one.

4. The unmanned aerial vehicle inspection device for the electric power industry of claim 3, wherein: The vertical support device (7) comprises: The outer connecting rod (71) is fixedly connected to the inner surface of the two sides of the body (1); The turnover shaft (72) is hinged to the circumferential surface of the outer connecting rod (71) at the front and rear ends; The bracket (73) is fixedly connected to the circumferential surface of the turnover shaft (72).

5. The unmanned aerial vehicle inspection device for power industry of claim 4, wherein: The vertical support device (7) further comprises: The limiting rod (74) is fixedly connected to the circumferential surface of the bracket (73); The clamping plate (75) is hinged to the inner surface of the two sides of the body (1), and the end of the clamping plate (75) away from the push rod (68) is fixedly connected with the positioning plate (76); The clamping block (77) is fixedly connected to the circumferential surface of the rear end of the push rod (68).

6. The unmanned aerial vehicle inspection device for the electric power industry of claim 5, wherein: The hinge between the turnover shaft (72) and the outer connecting rod (71) is provided with a torsion spring, the upper surface of the limiting rod (74) is provided with a groove, the hinge between the clamping plate (75) and the inner surface of the body (1) is provided with a torsion spring, the push rod (68) and the inner surface of the body (1) are slidingly connected, the clamping block (77) and the inner surface of the body (1) are slidingly connected, the inner side of the clamping plate (75) is provided with a key groove, and the key groove and the clamping block (77) are clamped.

Images