A shooting simulation auxiliary device for electric power inspection drones

By designing an adjustment mechanism for drone shooting simulation auxiliary equipment, the problem that the equipment cannot be adjusted according to the operator's height is solved, and the scope of application and reliability of the equipment are improved.

CN119741864APending Publication Date: 2025-04-01ANHUI ELECTRIC POWER TRANSMISSION & TRANSFORMATION ENG CO LTD
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202411737731.4
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-11-29
Publication Date
2025-04-01

AI Technical Summary

Technical Problem

Existing drone shooting simulation auxiliary equipment cannot adaptively adjust according to the operator's height, resulting in reduced reliability and poor results.

Method used

A shooting simulation auxiliary device including a first adjustment mechanism and a second adjustment mechanism is designed. The first adjustment mechanism drives the control table to adjust the height through the joint cooperation of the rotating rod, gear and movable rod; the second adjustment mechanism drives the distance between the seat and the control table to adjust the joint cooperation of the hydraulic cylinder, hydraulic rod and electromagnetic guide rail.

Benefits of technology

The height adjustment of the console and seat is realized, which improves the scope of application and reliability of the equipment, so that the equipment can better adapt to the height needs of different operators.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN119741864A_ABST
    Figure CN119741864A_ABST
Patent Text Reader

Abstract

The present invention discloses a shooting simulation auxiliary device for electric power inspection drones, which relates to the technical field of electric power inspection, and comprises a simulation room, wherein a first adjustment mechanism and a second adjustment mechanism are arranged in the simulation room, a control panel is arranged on the top of the first adjustment mechanism, a seat is arranged on the top of the second adjustment mechanism, and three blower mechanisms are arranged on the inner side of the simulation room, wherein the first adjustment mechanism comprises a fixed seat, wherein the fixed seat is fixedly connected to the simulation room, wherein an empty slot is provided inside the fixed seat, wherein a rotating rod is rotatably connected in the empty slot, wherein a gear is fixedly sleeved on the outer surface of the rotating rod, and wherein a movable rod is arranged in the empty slot. The shooting simulation auxiliary device for electric power inspection drones, by providing the first adjustment mechanism, has the effect of adjusting the height of the control panel, thereby improving the scope of application and solving the problem in the prior art that adaptive adjustment cannot be performed according to the height of the operator.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The present invention relates to the technical field of electric power inspection, and in particular to a shooting simulation auxiliary device for an electric power inspection unmanned aerial vehicle. Background Art

[0002] UAV is the abbreviation of unmanned aircraft, which is an unmanned aircraft controlled by radio remote control equipment and self-contained programs. In the field of power line inspection, UAVs have replaced the heavy manual inspection, making the inspection of power lines simpler and more efficient.

[0003] At present, drone shooting simulation auxiliary equipment is an indispensable auxiliary device in drone driving simulation learning. The simulation of drone flight mainly uses the simulation display to simulate different shooting scenes of drones, including different terrains, landforms, weather conditions, etc., and controls the virtual drone to fly through the simulation console, so as to master basic flight skills before actual flight shooting and reduce the risk of accidents caused by improper operation. In the prior art, a simulation controller, a seat and a writing board are all installed on a support frame, and the seat is located between the simulation controller and the writing board; when in use, the seat is used for trainees to sit, the simulation controller is used for simulated drone driving training, and the writing board is used to record important data or precautions.

[0004] However, the existing device has the following shortcomings during use: In the prior art, since the analog controller and the support frame are fixed, the height cannot be adjusted and the adjustment function is not available, which results in the inability to perform adaptive adjustment according to the height of the operator, reducing the scope of application, resulting in reduced reliability and poor use effect.

[0005] Therefore, we proposed a shooting simulation auxiliary equipment for power inspection drones to solve the above problems. Summary of the invention

[0006] The purpose of the present invention is to provide a shooting simulation auxiliary equipment for power inspection drones. By setting a first adjustment mechanism and starting a first drive motor, the first rotating shaft, the rotating wheel and the belt can be used to drive the rotating rod to rotate. When the rotating rod rotates, the gears, the movable rod and the tooth marks can be used to drive the control panel to move, so as to solve the problems raised by the above-mentioned background technology.

[0007] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a shooting simulation auxiliary equipment for electric power inspection drones, comprising a simulation room, wherein a first adjustment mechanism and a second adjustment mechanism are arranged in the simulation room, a control panel is arranged on the top of the first adjustment mechanism, a seat is arranged on the top of the second adjustment mechanism, and three blower mechanisms are arranged on the inner side of the simulation room, the first adjustment mechanism comprises a fixed seat, the fixed seat is fixedly connected to the simulation room, an empty slot is opened inside the fixed seat, a rotating rod is rotatably connected in the empty slot, a gear is fixedly sleeved on the outer surface of the rotating rod, a movable rod is arranged in the empty slot, and the The top end of the movable rod movably passes through the empty slot and extends to the outside of the fixed seat. The control console is fixedly installed on the top end of the movable rod. The outer surface of the movable rod is provided with tooth marks, and the tooth marks are meshed with gears. One side of the fixed seat is fixedly connected to a support plate, and a first driving motor is fixedly installed on the top of the support plate. The output end of the first driving motor is fixedly connected to a first rotating shaft, and one end of the first rotating shaft is rotatably connected to the fixed seat. One end of the rotating rod movably passes through the empty slot and extends to the outside of the fixed seat. The outer surface of the rotating rod and the outer surface of the first rotating shaft are fixedly sleeved with rotating wheels, and the outer surfaces of the two rotating wheels are transmission-connected with belts.

[0008] Preferably, the second adjustment mechanism comprises an electromagnetic guide rail, the electromagnetic guide rail is fixedly installed in the simulation room, an electromagnetic slider is slidably provided on the electromagnetic guide rail, and the top of the electromagnetic slider is fixedly connected to a bottom plate.

[0009] Preferably, a mounting plate is provided on the top of the base plate, the seat is fixedly mounted on the top of the mounting plate, four placement grooves are provided on the top of the base plate and the bottom of the mounting plate, and four fixing rods are fixedly connected in the four placement grooves.

[0010] Preferably, four movable blocks are sleeved on the outer surfaces of the four fixed rods, and four connecting blocks are fixedly connected between the top of the base plate and the bottom of the mounting plate, wherein two first hinged rods are hinged between two of the connecting blocks and two of the movable blocks, and two second hinged rods are hinged between the other two connecting blocks and the other two movable blocks.

[0011] Preferably, one of the first hinged rods is hinged to one of the second hinged rods, and another of the first hinged rods is hinged to another of the second hinged rods.

[0012] Preferably, a fixed plate is fixedly connected to the top of the base plate, a hydraulic cylinder is fixedly installed on one side of the fixed plate, a hydraulic rod is fixedly connected to the output end of the hydraulic cylinder, and one side of the other two movable blocks is fixedly connected to a connecting plate, and one end of the hydraulic rod movably passes through the fixed plate and is fixedly connected to the connecting plate.

[0013] Preferably, the three blowing mechanisms include three blowing shells, the three blowing shells are arranged through the inner side of the simulation room body, and three mounting frames are fixedly connected to the inner surfaces of the three blowing shells.

[0014] Preferably, three second drive motors are fixedly installed on the inner surfaces of the three mounting frames, the output ends of the three second drive motors are fixedly connected to three second rotating shafts, one end of the three second rotating shafts is fixedly connected to three blowing fan blades, and protective nets are installed at both ends of the three blowing shells.

[0015] Preferably, a limiting groove is provided on the inner side of the empty groove, a limiting plate is slidably connected in the limiting groove, and the top of the limiting plate is fixedly connected to the movable rod.

[0016] Preferably, a simulation display screen is provided on the top of the control panel, and an entrance door is hingedly connected to one side of the simulation room.

[0017] Compared with the prior art, the present invention has the following beneficial effects: 1. By setting up the first adjustment mechanism and starting the first drive motor, the first rotating shaft, the rotating wheel and the belt can be used to drive the rotating rod to rotate. When the rotating rod rotates, the gear, the movable rod and the tooth marks can be used to drive the control panel to move, thereby adjusting the height of the control panel, improving the scope of application, and solving the problem in the prior art that the height of the operator cannot be adjusted adaptively.

[0018] 2. By setting up the second adjustment mechanism and starting the hydraulic cylinder, the hydraulic rod drives the connecting plate to move, and the movement of the connecting plate drives the other two moving blocks to move. Under the action of the two first hinged rods, the two second hinged rods and the four connecting blocks, two of the moving blocks are driven to move, so that the mounting plate drives the seat to move upward, thereby adjusting the height of the seat. The electromagnetic slide block is driven by the electromagnetic guide rail together with the bottom plate to move on the electromagnetic guide rail, thereby adjusting the distance between the seat and the control panel, thereby improving practicality.

[0019] 3. By setting up a blower mechanism, different second drive motors can be turned on, so that the second drive motor drives the second rotating shaft to rotate, and the second rotating shaft drives the blower blades to rotate. The blower blades pass through the protective net to blow air. Different second drive motors are used to generate different wind directions, which enables the operator to fly the drone under different wind directions, making the operator closer to reality during the operation. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 This is a stereoscopic diagram of the main structure of a shooting simulation auxiliary device for a power inspection drone of the present invention; Figure 2This is a three-dimensional diagram of the cross-sectional structure of a simulated room in a shooting simulation auxiliary device for a power inspection drone of the present invention; Figure 3 This is a structural stereogram of a control panel in a shooting simulation auxiliary device for a power inspection UAV of the present invention; Figure 4 This is a structural stereogram of a seat in a shooting simulation auxiliary device for a power inspection drone of the present invention; Figure 5 This is a structural stereogram of a connecting plate in a shooting simulation auxiliary device for a power inspection drone of the present invention; Figure 6 It is a partial cross-sectional structural stereogram of a mounting plate in a shooting simulation auxiliary device for a power inspection drone of the present invention; Figure 7 This is a cross-sectional structural stereogram of a fixing seat in a shooting simulation auxiliary device for an electric power inspection drone according to the present invention; Figure 8 The present invention is a three-dimensional diagram of the cross-sectional structure of a blower mechanism in a shooting simulation auxiliary device for an electric power inspection drone.

[0021] In the figure: 1. Simulated room; 2. First adjustment mechanism; 201. Fixed seat; 202. Empty slot; 203. Rotating rod; 204. Gear; 205. Movable rod; 206. Tooth marks; 207. Support plate; 208. First driving motor; 209. First rotating shaft; 210. Rotating wheel; 211. Belt; 212. Limiting slot; 213. Limiting plate; 3. Second adjustment mechanism; 301. Electromagnetic guide rail; 302. Electromagnetic slider; 303. Bottom plate; 304. Mounting plate; 305 , placement slot; 306, fixed rod; 307, moving block; 308, connecting block; 309, first hinge rod; 310, second hinge rod; 311, fixed plate; 312, hydraulic cylinder; 313, hydraulic rod; 314, connecting plate; 4, control panel; 5, seat; 6, hair dryer structure; 601, blowing shell; 602, mounting frame; 603, second drive motor; 604, second rotating shaft; 605, blowing fan blades; 606, protective net; 7, simulation display screen; 8, exit and entry door. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the implementation regulations described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0023] Please see attached Figure 1 -Attached Figure 8 The present invention provides a technical solution: a shooting simulation auxiliary device for a power inspection drone, comprising a simulation room 1, a first adjustment mechanism 2 and a second adjustment mechanism 3 are arranged in the simulation room 1, a control panel 4 is arranged on the top of the first adjustment mechanism 2, a seat 5 is arranged on the top of the second adjustment mechanism 3, and three blower mechanisms 6 are arranged on the inner side of the simulation room 1.

[0024] Embodiment 1, as Figure 1 , Figure 3 and Figure 7 As shown, the first adjustment mechanism 2 includes a fixed seat 201, which is fixedly connected to the simulation room body 1. An empty slot 202 is provided inside the fixed seat 201, and a rotating rod 203 is rotatably connected in the empty slot 202. A gear 204 is fixedly sleeved on the outer surface of the rotating rod 203. A movable rod 205 is provided in the empty slot 202. The top of the movable rod 205 movably passes through the empty slot 202 and extends to the outside of the fixed seat 201. The control console 4 is fixedly installed on the top of the movable rod 205. A tooth mark 206 is provided on the outer surface of the movable rod 205. The tooth mark 206 is meshed and connected with the gear 204. A support plate 207 is fixedly connected to one side of the fixed seat 201. A first driving motor 208 is fixedly installed on the top of the support plate 207, and the output end of the first driving motor 208 is fixedly connected to the first rotating shaft 209, one end of the first rotating shaft 209 is rotatably connected to the fixed seat 201, one end of the rotating rod 203 is movable through the empty slot 202 and extends to the outside of the fixed seat 201, the outer surface of the rotating rod 203 and the outer surface of the first rotating shaft 209 are fixedly sleeved with a rotating wheel 210, the outer surfaces of the two rotating wheels 210 are transmission-connected with a belt 211, a limiting slot 212 is provided on the inner side of the empty slot 202, a limiting plate 213 is slidably connected in the limiting slot 212, and the top of the limiting plate 213 is fixedly connected to the movable rod 205.

[0025] The effect achieved by the entire embodiment 1 is as follows: by utilizing the support plate 207, the bottom of the first drive motor 208 can be supported and reinforced, so that the first drive motor 208 can provide power for the rotation of the first rotating shaft 209. The first drive motor 208 is started, and the first rotating shaft 209, the rotating wheel 210, and the belt 211 cooperate to drive the rotating rod 203 to rotate. When the rotating rod 203 rotates, the gear 204, the movable rod 205, and the tooth mark 206 cooperate to drive the movable rod 205 to move, thereby achieving the effect of adjusting the height of the control panel 4, realizing the adjustment function, and meeting the adjustment function of different needs. At the same time, when the movable rod 205 moves, the limiting plate 213 limits the movable rod 205, which on the one hand improves the stability of the movable rod 205 during the movement, and on the other hand limits the moving range of the movable rod 205 to prevent the movable rod 205 from falling off, thereby ensuring the overall safety and stability during operation.

[0026] Embodiment 2, as Figure 1 , Figure 4 and Figure 5 As shown, the second adjustment mechanism 3 includes an electromagnetic guide rail 301, which is fixedly installed in the simulation room body 1. An electromagnetic slider 302 is slidably arranged on the electromagnetic guide rail 301. The top of the electromagnetic slider 302 is fixedly connected to a bottom plate 303. A mounting plate 304 is arranged on the top of the bottom plate 303. The seat 5 is fixedly installed on the top of the mounting plate 304. Four placement grooves 305 are provided on the top of the bottom plate 303 and the bottom of the mounting plate 304. Four fixing rods 306 are fixedly connected in the four placement grooves 305. Four moving blocks 307 are sleeved on the outer surfaces of the four fixing rods 306. Four connecting blocks 308 are fixedly connected to the top of the bottom plate 303 and the bottom of the mounting plate 304. Two of the connecting blocks 308 are connected to the bottom of the mounting plate 304. Two first hinged rods 309 are hinged between the two moving blocks 307, and two second hinged rods 310 are hinged between the other two connecting blocks 308 and the other two moving blocks 307, one of the first hinged rods 309 is hinged to one of the second hinged rods 310, and the other first hinged rod 309 is hinged to the other second hinged rod 310. A fixed plate 311 is fixedly connected to the top of the bottom plate 303, a hydraulic cylinder 312 is fixedly installed on one side of the fixed plate 311, and a hydraulic rod 313 is fixedly connected to the output end of the hydraulic cylinder 312, and a connecting plate 314 is fixedly connected to one side of the other two moving blocks 307, and one end of the hydraulic rod 313 movably passes through the fixed plate 311 and is fixedly connected to the connecting plate 314.

[0027] The effect achieved by the entire embodiment 2 is as follows: by setting the second adjustment mechanism 3, the electromagnetic slider 302 can be driven by the electromagnetic guide rail 301 to move on the electromagnetic guide rail 301, thereby adjusting the distance between the seat 5 and the control console 4. The hydraulic cylinder 312 can be supported and reinforced by using the fixed plate 311, so that when the hydraulic cylinder 312 is running, the connecting plate 314 can be driven to move by the hydraulic rod 313. When the connecting plate 314 moves, with the cooperation of the two first hinged rods 309, the two second hinged rods 310 and the four connecting blocks 308, two of the moving blocks 307 can be driven to move. When the two moving blocks 307 move, the mounting plate 304 can be driven to move upward, thereby adjusting the height of the seat 5. It can be flexibly adjusted according to operational requirements. The fixed rod 306 is set to limit the moving block 307, so that the moving block 307 can move stably.

[0028] Embodiment 3, as Figure 1 , Figure 2 and Figure 8As shown, the three blower mechanisms 6 include three blower shells 601, and the three blower shells 601 are arranged throughout the inner side of the simulation room body 1, and the inner surfaces of the three blower shells 601 are fixedly connected with three mounting frames 602, and the inner surfaces of the three mounting frames 602 are fixedly installed with three second drive motors 603, and the output ends of the three second drive motors 603 are fixedly connected with three second rotating shafts 604, and one end of the three second rotating shafts 604 is fixedly connected with three blower fan blades 605, and both ends of the three blower shells 601 are installed with protective nets 606, a simulation display screen 7 is arranged on the top of the control panel 4, and an exit door 8 is hinged on one side of the simulation room body 1.

[0029] The effect achieved by the entire embodiment 3 is as follows: by setting a simulated display screen 7, it is convenient for the operator to control the virtual drone in the simulated display screen 7 to fly through the control console 4; an access door 8 is set to facilitate the operator to enter and exit the simulated room 1; during the simulated flight operation, the operator sets a blower mechanism 6 and uses a mounting frame 602 to support and reinforce the second drive motor 603, so that the second drive motor 603 can provide power for the rotation of the second rotating shaft 604; different second drive motors 603 can be turned on and used to generate different wind directions, so that the operator can fly the drone under different wind directions; different wind directions can be simulated to provide the operator with a real experience in the drone control process; this diversified wind direction simulation makes the operating environment closer to the actual flight situation; a protective net 606 is set to protect the internal structure of the blowing shell 601 and provide a safe operating environment for the operator.

[0030] The use method and working principle of the device: When in use, the operator can first open the access door 8 to enter the simulation room 1, then close the access door 8, and then start the hydraulic cylinder 312, so that the hydraulic cylinder 312 drives the hydraulic rod 313 to move, the hydraulic rod 313 drives the connecting plate 314 to move, and the connecting plate 314 moves to drive the other two moving blocks 307 to move. At this time, under the action of the two first hinged rods 309, the two second hinged rods 310 and the four connecting blocks 308, two of the moving blocks 307 are driven to move, thereby driving the mounting plate 30 4 moves upward, thereby causing the mounting plate 304 to drive the seat 5 to move upward, so that the height of the seat 5 can be adjusted. After adjusting to a suitable height, the electromagnetic slide 302 is driven to slide on the electromagnetic guide rail 301 through the electromagnetic guide rail 301. When the electromagnetic guide rail 301 slides, it drives the bottom plate 303 to move synchronously, thereby driving the seat 5 to move its position, so that the distance between the seat 5 and the control console 4 can be adjusted. After the adjustment is completed, the first drive motor 208 is then started, so that the first drive motor 208 drives the first rotating shaft 209 to rotate, and the first rotating shaft 20 9 drives one of the rotating wheels 210 to rotate, one of the rotating wheels 210 drives the belt 211 to move, the belt 211 drives the other rotating wheel 210 to rotate, the other rotating wheel 210 drives the rotating rod 203 to rotate, the rotating rod 203 drives the gear 204 to rotate, because the gear 204 is meshed with the tooth mark 206, so that the gear 204 drives the movable rod 205 to move upward, and the movable rod 205 drives the limiting plate 213 to slide upward in the limiting groove 212 synchronously, so that the movable rod 205 drives the control panel 4 to move upward, and the height of the control panel 4 can be adjusted. After adjusting the control panel 4 to a suitable height, the operator can sit on the seat 5 and control the virtual drone in the simulated display screen 7 to fly through the control panel 4. During the operation, different second drive motors 603 can be turned on, so that the second drive motor 603 drives the second rotating shaft 604 to rotate, and the second rotating shaft 604 drives the blowing fan blades 605 to rotate. The blowing fan blades 605 pass through the protective net 606 to blow air. Different second drive motors 603 are used to generate different wind directions, so that the operator can fly the drone under different wind directions.

[0031] Although the present invention has been described in detail with reference to the aforementioned embodiments, it is still possible for those skilled in the art to modify the technical solutions described in the aforementioned embodiments, or to make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A shooting simulation auxiliary device for a power inspection drone, characterized in that: The simulation room (1) comprises a simulation room body (1), wherein a first adjustment mechanism (2) and a second adjustment mechanism (3) are arranged in the simulation room body (1), a control panel (4) is arranged on the top of the first adjustment mechanism (2), a seat (5) is arranged on the top of the second adjustment mechanism (3), three blower mechanisms (6) are arranged on the inner side of the simulation room body (1), the first adjustment mechanism (2) comprises a fixed seat (201), the fixed seat (201) is fixedly connected to the simulation room body (1), a hollow groove (202) is provided inside the fixed seat (201), a rotating rod (203) is rotatably connected in the hollow groove (202), a gear (204) is fixedly sleeved on the outer surface of the rotating rod (203), a movable rod (205) is arranged in the hollow groove (202), the top end of the movable rod (205) movably passes through the hollow groove (202) and extends to the outside of the fixed seat (201), The control console (4) is fixedly mounted on the top of the movable rod (205); a tooth mark (206) is provided on the outer surface of the movable rod (205); the tooth mark (206) is meshedly connected to the gear (204); a support plate (207) is fixedly connected to one side of the fixed seat (201); a first drive motor (208) is fixedly mounted on the top of the support plate (207); an output end of the first drive motor (208) is fixedly connected to a first rotating shaft (209); one end of the first rotating shaft (209) is rotatably connected to the fixed seat (201); one end of the rotating rod (203) is movably inserted into the empty slot (202) and extends to the outside of the fixed seat (201); a rotating wheel (210) is fixedly sleeved on the outer surface of the rotating rod (203) and the outer surface of the first rotating shaft (209); and the outer surfaces of the two rotating wheels (210) are transmission-connected with belts (211).

2. The shooting simulation auxiliary device for a power inspection drone according to claim 1 is characterized in that: The second adjustment mechanism (3) comprises an electromagnetic guide rail (301), the electromagnetic guide rail (301) being fixedly installed in the simulation room (1), an electromagnetic slider (302) being slidably arranged on the electromagnetic guide rail (301), and a bottom plate (303) being fixedly connected to the top of the electromagnetic slider (302).

3. The shooting simulation auxiliary device for a power inspection drone according to claim 2 is characterized in that: A mounting plate (304) is provided on the top of the base plate (303), and the seat (5) is fixedly mounted on the top of the mounting plate (304). Four placement grooves (305) are provided on the top of the base plate (303) and the bottom of the mounting plate (304), and four fixing rods (306) are fixedly connected in the four placement grooves (305).

4. The shooting simulation auxiliary device for a power inspection drone according to claim 3 is characterized in that: Four movable blocks (307) are sleeved on the outer surfaces of the four fixed rods (306); four connecting blocks (308) are fixedly connected between the top of the base plate (303) and the bottom of the mounting plate (304); two first hinged rods (309) are hingedly connected between two of the connecting blocks (308) and two of the movable blocks (307); and two second hinged rods (310) are hingedly connected between the other two connecting blocks (308) and the other two movable blocks (307).

5. The shooting simulation auxiliary device for a power inspection drone according to claim 4 is characterized in that: One of the first hinged rods (309) is hinged to one of the second hinged rods (310), and another of the first hinged rods (309) is hinged to another of the second hinged rods (310).

6. The shooting simulation auxiliary device for a power inspection drone according to claim 5 is characterized in that: A fixing plate (311) is fixedly connected to the top of the bottom plate (303), a hydraulic cylinder (312) is fixedly mounted on one side of the fixing plate (311), a hydraulic rod (313) is fixedly connected to the output end of the hydraulic cylinder (312), and a connecting plate (314) is fixedly connected to one side of the other two moving blocks (307), and one end of the hydraulic rod (313) movably passes through the fixing plate (311) and is fixedly connected to the connecting plate (314).

7. The shooting simulation auxiliary device for a power inspection drone according to claim 1 is characterized in that: The three blowing mechanisms (6) comprise three blowing shells (601), the three blowing shells (601) being arranged through the inner side of the simulation room body (1), and the inner surfaces of the three blowing shells (601) are fixedly connected with three mounting frames (602).

8. The shooting simulation auxiliary device for a power inspection drone according to claim 7 is characterized in that: Three second drive motors (603) are fixedly mounted on the inner surfaces of the three mounting frames (602); the output ends of the three second drive motors (603) are fixedly connected to three second rotating shafts (604); one end of the three second rotating shafts (604) is fixedly connected to three blowing fan blades (605); and both ends of the three blowing housings (601) are installed with protective nets (606).

9. The shooting simulation auxiliary device for a power inspection drone according to claim 1 is characterized in that: A limiting groove (212) is provided on the inner side of the empty groove (202), a limiting plate (213) is slidably connected in the limiting groove (212), and the top of the limiting plate (213) is fixedly connected to the movable rod (205).

10. The shooting simulation auxiliary device for a power inspection drone according to claim 9, characterized in that: A simulation display screen (7) is provided on the top of the control panel (4), and an entrance door (8) is hingedly connected to one side of the simulation room (1).