Large-load long-endurance unmanned aerial vehicle intelligent inspection system

Abstract

The utility model discloses a large-load long-endurance unmanned aerial vehicle intelligent inspection system which comprises an unmanned aerial vehicle body, a camera module is fixedly installed at the bottom of the unmanned aerial vehicle body through a dismounting mechanism, the camera module comprises an angle adjusting assembly and a camera, and the angle adjusting assembly is installed at the lower end of the dismounting mechanism. The camera is installed on the angle adjusting assembly, the angle adjusting assembly comprises a first motor, the first motor is fixedly installed at the bottom of the fixing base, the bottom of a rotating shaft of the first motor is fixedly connected with an inverted-U-shaped frame, the lower end of the inner side of the inverted-U-shaped frame is rotationally connected with a transmission shaft, and a second motor is fixedly installed on one side of the inverted-U-shaped frame; a rotating shaft of the second motor is fixedly connected with one end of a transmission shaft, the transmission shaft is fixedly connected with a first mounting plate, and the camera is fixedly mounted on the first mounting plate; according to the utility model, the camera module can be quickly disassembled and assembled by arranging the disassembling and assembling mechanism, and the horizontal direction and the pitching angle of the camera can be adjusted by arranging the angle adjusting assembly.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field, especially a kind of big load long endurance unmanned plane intelligent inspection system. BACKGROUND

[0002] Chinese patent with the publication number CN221718831U discloses a kind of unmanned plane inspection system for unmanned plane image device, including mounting plate and support table, support table is set in mounting plate bottom end, mounting plate top end is rectangular array with four mounting holes, two installation grooves are respectively rotationally connected with fixed bolt away from the middle side of mounting plate, two installation grooves inner wall are respectively slidably connected with fixed block, two fixed blocks top end are fixedly connected with fixed plate, support table top end and fixed plate bottom end middle part are fixedly connected, shell inner wall two sides are respectively fixedly connected with second motor, shell two sides are respectively rotationally connected with camera, two cameras bottom end are respectively fixedly connected with guard plate.

[0003] The above-mentioned patent although solves some defects existing in prior art, but still has some deficiencies in actual use, for example, its fixed plate and mounting plate are fixed by multiple bolts, when the camera module at the bottom of unmanned plane needs to be replaced, the dismounting efficiency is low.

[0004] Therefore, a kind of big load long endurance unmanned plane intelligent inspection system is proposed. UTILITY MODEL CONTENT

[0005] The utility model aims at providing a kind of big load long endurance unmanned plane intelligent inspection system, to solve or at least alleviate one or more of the above problems and other aspects problems existing in prior art.

[0006] In order to achieve the above-mentioned purpose, the main technical scheme adopted by the utility model includes:

[0007] A kind of big load long endurance unmanned plane intelligent inspection system, including unmanned plane body, the bottom of the unmanned plane body is fixedly installed with camera module by dismounting mechanism, the camera module includes angle adjusting assembly and camera, the angle adjusting assembly is installed in the lower end of the dismounting mechanism, and the camera is installed on the angle adjusting assembly.

[0008] In the large load long endurance unmanned aerial vehicle intelligent inspection system according to the utility model, the dismounting mechanism comprises a mounting seat and a fixing seat, a mounting hole is formed in the middle portion of the mounting seat, sliding grooves are formed in the opposite sides of the mounting seat, the sliding grooves are communicated with the mounting hole, a screw rod is rotatably installed in the mounting hole, the screw rods are oppositely arranged at the two ends, lock rods are threadedly rotatably connected to the two ends of the screw rod, the end portions of the lock rods slide into the sliding grooves, first and second insertion holes are formed in the top and bottom four corners of the mounting seat and communicated with the sliding grooves, insertion rods are fixedly connected to the top four corners of the fixing seat, lock grooves are formed in the sides of the insertion rods, the upper ends of the insertion rods penetrate through the first insertion holes and the sliding grooves and then extend into the second insertion holes, and the end portions of the lock rods can be clamped into the lock grooves by rotating the screw rod.

[0009] In the large load long endurance unmanned aerial vehicle intelligent inspection system according to the utility model, a guide rod is fixedly connected in the mounting hole, and the lock rods are slidably sleeved on the guide rod.

[0010] In the large load long endurance unmanned aerial vehicle intelligent inspection system according to the utility model, a spring is sleeved on the guide rod, the spring is located between the two lock rods, one end of the spring abuts against one side of one of the lock rods, and the other end of the spring abuts against one side of the other lock rod.

[0011] In the large load long endurance unmanned aerial vehicle intelligent inspection system according to the utility model, mounting holes are formed in the four corners of the mounting seat, and the upper ends of the bolts penetrate through the mounting holes and are threadedly fixed in the threaded holes in the bottom of the unmanned aerial vehicle body.

[0012] In the large load long endurance unmanned aerial vehicle intelligent inspection system according to the utility model, the angle adjusting assembly comprises a first motor, the first motor is fixedly installed at the bottom of the fixing seat, a reverse U-shaped frame is fixedly connected to the bottom of the rotating shaft of the first motor, a transmission shaft is rotatably connected to the inner lower end of the reverse U-shaped frame, a second motor is fixedly installed on one side of the reverse U-shaped frame, the rotating shaft of the second motor is fixedly connected to one end of the transmission shaft, a first mounting plate is fixedly connected to the transmission shaft, and the camera is fixedly installed on the camera.

[0013] In the large load long endurance unmanned aerial vehicle intelligent inspection system according to the utility model, a second mounting plate is fixedly connected to the end of the transmission shaft away from the second motor, and a light supplementing searchlight is fixedly installed on the second mounting plate.

[0014] The locking rod is provided with a chamfer on one side facing the locking groove.

[0015] The utility model at least has the following beneficial effects:

[0016] The utility model discloses a quick dismounting mechanism is set up to the camera module is convenient for quick dismounting;

[0017] The angle adjusting assembly can adjust the horizontal direction and the pitch angle of the camera, effectively improving the inspection and shooting range of the camera.

[0018] The light supplement searchlight can supplement light to the shooting area of the camera in the case that the shooting environment is dark, to ensure the shooting effect of the camera. BRIEF DESCRIPTION OF DRAWINGS

[0019] The drawings described herein are used to provide further understanding of the present application, and form a part of the present application.

[0020] Figure 1 It is the structure schematic drawing of the utility model's big load heavy long voyage unmanned plane intelligent inspection system;

[0021] Figure 2 It is one of the local structure schematic drawing of the utility model's dismounting mechanism;

[0022] Figure 3 It is the second local structure schematic drawing of the utility model's dismounting mechanism;

[0023] Figure 4 It is the structure schematic drawing when the utility model's dismounting mechanism and camera module are installed;

[0024] Figure 5 It is the rear view structure schematic drawing of the utility model's mounting seat.

[0025] BRIEF DESCRIPTION OF DRAWINGS

[0026] 1, unmanned plane body;2, dismounting mechanism;201, mounting seat;202, assembly hole;203, sliding slot;204, screw;205, locking rod;2051, chamfer;206, first jack;207, second jack;208, mounting hole;209, guide rod;210, spring;211, fixed seat;212, plug rod;213, locking groove;3, angle adjusting assembly;301, first motor;302, inverted U-shaped frame;303, transmission shaft;304, second motor;305, first mounting plate;306, second mounting plate;4, camera;5, light supplement searchlight. DETAILED DESCRIPTION

[0027] The implementation of the present application will be described in detail below with the accompanying drawings and examples, so that the realization process of how the present application applies technical means to solve technical problems and achieve technical effects can be fully understood and implemented.

[0028] Please refer to Figures 1 to 5 The embodiment provides a large-load long-endurance unmanned aerial vehicle intelligent inspection system, which comprises an unmanned aerial vehicle body 1, a camera module is fixedly installed on the bottom of the unmanned aerial vehicle body 1 through a dismounting mechanism 2, the camera module comprises an angle adjusting assembly 3 and a camera 4, the angle adjusting assembly 3 is installed at the lower end of the dismounting mechanism 2, and the camera 4 is installed on the angle adjusting assembly 3.

[0029] Among them, the unmanned aerial vehicle body 1 is a large-load long-endurance unmanned aerial vehicle, and the large-load long-endurance unmanned aerial vehicle can be an oil-electric hybrid unmanned aerial vehicle. These unmanned aerial vehicles generate electric power by burning fuel, thereby prolonging the flight time of the unmanned aerial vehicle.

[0030] The large-load long-endurance unmanned aerial vehicle can be a fixed-wing large-load unmanned aerial vehicle. The fixed-wing unmanned aerial vehicle usually has a longer endurance and a larger load capacity. For example, some professional fixed-wing unmanned aerial vehicles, such as eBee Plus and SkyWalker X8 of SenseFly, can realize long-time flight under the condition of carrying a certain load.

[0031] In the embodiment, the dismounting mechanism 2 comprises a mounting seat 201 and a fixing seat 211, a mounting hole 202 is formed in the middle of the mounting seat 201, sliding grooves 203 are formed in the opposite sides of the mounting seat 201 and communicate with the mounting hole 202, a lead screw 204 is rotatably installed in the mounting hole 202, the lead screws 204 at two ends are oppositely threaded, lock rods 205 are threadedly rotatably connected to the two ends of the lead screw 204, the end portions of the lock rods 205 slide into the sliding grooves 203, first insertion holes 206 and second insertion holes 207 that communicate with the sliding grooves 203 are respectively formed in the top four corners and the bottom four corners of the mounting seat 201, plug rods 212 are fixedly connected to the top four corners of the fixing seat 211, lock grooves 213 are formed in the side surfaces of the plug rods 212, the upper ends of the plug rods 212 extend into the second insertion holes 207 through the first insertion holes 206 and the sliding grooves 203, and the end portions of the lock rods 205 can be clamped into the lock grooves 213 by rotating the lead screw 204.

[0032] By adopting the above technical solution, during installation, hold the fixing base 211 and insert the rod 212 into the slide groove 203 from the first insertion hole 206. Then continue to move it upward so that the upper end of the rod 212 is inserted into the second insertion hole 207. At this time, the locking groove 213 is located in the slide groove 203. Then rotate the screw 204 so that the locking rod 205 moves towards the locking groove 213. Finally, a part of the locking rod 205 is locked into the locking groove 213, thereby fixing the rod 212 on the mounting base 201. When it is necessary to disassemble the fixing base 211, rotate the screw 204 in the opposite direction so that the two locking rods 205 move away from the locking groove 213, thereby removing the locking rods 205 from the locking groove 213. At this time, pull down the fixing base 211 to disassemble the fixing base 211.

[0033] In this embodiment, in order to facilitate the smooth insertion of the locking rod 205 into the locking groove 213, a chamfer 2051 is provided on the side of the locking rod 205 facing the locking groove 213.

[0034] In this embodiment, in order to make the locking rod 205 more stable when moving, a guide rod 209 is fixedly connected inside the assembly hole 202, and the locking rod 205 is slidably sleeved on the guide rod 209.

[0035] In this embodiment, a spring 210 is sleeved on the guide rod 209. The spring 210 is located between the two locking rods 205. One end of the spring 210 abuts against one side of one of the locking rods 205, and the other end of the spring 210 abuts against one side of the other locking rod 205. With the spring 210, when the locking rod 205 is engaged in the locking groove 213, the spring 210 will compress the two locking rods 205, thereby effectively preventing the lead screw 204 from spinning and ensuring the fixing strength.

[0036] In this embodiment, mounting holes 208 are provided at all four corners of the mounting base 201. The upper end of the bolt passes through the mounting hole 208 and is threaded into the threaded hole at the bottom of the UAV body 1. The above arrangement facilitates fixing the mounting base 201 to the bottom of the UAV body 1.

[0037] In this embodiment, the angle adjustment component 3 includes a first motor 301, which is fixedly installed at the bottom of the fixed base 211. The bottom of the rotating shaft of the first motor 301 is fixedly connected to an inverted U-shaped frame 302. The lower inner end of the inverted U-shaped frame 302 is rotatably connected to a transmission shaft 303. A second motor 304 is fixedly installed on one side of the inverted U-shaped frame 302. The rotating shaft of the second motor 304 is fixedly connected to one end of the transmission shaft 303. A first mounting plate 305 is fixedly connected to the transmission shaft 303. The camera 4 is fixedly installed on the camera 4.

[0038] Through the above setting, in use, by controlling the rotation of the rotating shaft of the first motor 301, the horizontal shooting angle of the camera 4 can be adjusted, and by controlling the rotation of the rotating shaft of the second motor 304, the pitch angle of the camera 4 can be adjusted.

[0039] In the embodiment, the transmission shaft 303 is fixedly connected with the second mounting plate 306 at one end away from the second motor 304, and the light supplementing searchlight 5 is fixedly installed on the second mounting plate 306.

[0040] In order to facilitate the understanding of the above technical scheme of the utility model, the working principle or operation mode of the utility model in the actual process will be described in detail below.

[0041] Working principle: in use, the mounting seat 201 is fixed on the unmanned aerial vehicle body 1 through bolts, and then the mounting seat 211 with the camera module is fixed on the mounting seat 201, when installing, the mounting seat 211 is held, the plug rod 212 is inserted into the sliding groove 203 from the first insertion hole 206, then the plug rod 212 is inserted into the second insertion hole 207 by continuing to move upwards, at this time, the locking groove 213 is located in the sliding groove 203, then the lead screw 204 is rotated, so that the locking rod 205 moves to the direction of the locking groove 213, finally a part of the locking rod 205 is clamped into the locking groove 213, and then the plug rod 212 is fixed on the mounting seat 201, when it is necessary to disassemble the mounting seat 211, the lead screw 204 is rotated in the opposite direction, so that the two locking rods 205 move away from the locking groove 213, and then the locking rod 205 is moved out of the locking groove 213, at this time, the mounting seat 211 is pulled down to realize the disassembly of the mounting seat 211, then according to the inspection requirement, the mounting seat 211 with other inspection equipment is installed on the mounting seat 201.

[0042] The above description shows and describes several preferred embodiments of the utility model, but as mentioned above, it should be understood that the utility model is not limited to the form disclosed herein, and should not be regarded as excluding other embodiments, but can be used in various other combinations, modifications and environments, and can be modified by the above teachings or related technologies or knowledge within the scope of the utility model concept described herein. The modification and change made by the person skilled in the art without departing from the spirit and scope of the utility model should be within the protection scope of the claims attached to the utility model.

Claims

1. A heavy-load long-endurance unmanned aerial vehicle intelligent inspection system, characterized in that, The device includes a drone body (1), and a camera module is fixedly installed on the bottom of the drone body (1) through a disassembly and assembly mechanism (2). The camera module includes an angle adjustment component (3) and a camera (4). The angle adjustment component (3) is installed at the lower end of the disassembly and assembly mechanism (2), and the camera (4) is installed on the angle adjustment component (3).

2. The unmanned aerial vehicle intelligent inspection system of claim 1, wherein: The disassembly and assembly mechanism (2) includes a mounting base (201) and a fixing base (211). The mounting base (201) has an assembly hole (202) in the middle. The mounting base (201) has sliding grooves (203) on both opposite sides. The sliding grooves (203) are connected to the assembly hole (202). A lead screw (204) is rotatably installed inside the assembly hole (202). The two ends of the lead screw (204) have opposite thread directions. Both ends of the lead screw (204) are threadedly rotatably connected to a locking rod (205). The end of the locking rod (205) slides into the sliding groove (203). Inside, the four top corners and four bottom corners of the mounting base (201) are respectively provided with a first insertion hole (206) and a second insertion hole (207) that communicate with the slide groove (203). The four top corners of the fixing base (211) are fixedly connected with insertion rods (212). The side of the insertion rod (212) is provided with a locking groove (213). The upper end of the insertion rod (212) passes through the first insertion hole (206) and the slide groove (203) and extends into the second insertion hole (207). By rotating the screw (204), the end of the locking rod (205) can be inserted into the locking groove (213).

3. The unmanned aerial vehicle intelligent inspection system of claim 2, wherein: A guide rod (209) is fixedly connected inside the assembly hole (202), and the locking rod (205) is slidably sleeved on the guide rod (209).

4. The unmanned aerial vehicle intelligent inspection system of claim 3, wherein: A spring (210) is sleeved on the guide rod (209). The spring (210) is located between the two locking rods (205). One end of the spring (210) abuts against one side of one of the locking rods (205), and the other end of the spring (210) abuts against one side of the other locking rod (205).

5. The unmanned aerial vehicle intelligent inspection system of claim 4, wherein: The mounting base (201) has mounting holes (208) at all four corners. The upper end of the bolt passes through the mounting hole (208) and is then threaded into the threaded hole at the bottom of the UAV body (1).

6. The unmanned aerial vehicle intelligent inspection system of claim 5, wherein: The angle adjustment component (3) includes a first motor (301), which is fixedly installed at the bottom of the fixed base (211). The bottom of the shaft of the first motor (301) is fixedly connected to an inverted U-shaped frame (302). The lower inner end of the inverted U-shaped frame (302) is rotatably connected to a transmission shaft (303). A second motor (304) is fixedly installed on one side of the inverted U-shaped frame (302). The shaft of the second motor (304) is fixedly connected to one end of the transmission shaft (303). A first mounting plate (305) is fixedly connected to the transmission shaft (303). The camera (4) is fixedly installed on the camera (4).

7. The unmanned aerial vehicle intelligent inspection system of claim 6, wherein: The transmission shaft (303) is fixedly connected with a second mounting plate (306) at one end away from the second motor (304), and the second mounting plate (306) is fixedly installed with a light supplementing searchlight (5).

8. The unmanned aerial vehicle intelligent inspection system of claim 2, wherein: A chamfer (2051) is formed on one side of the locking rod (205) towards the locking groove (213).

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