Unmanned aerial vehicle monitoring device convenient to disassemble

Abstract

The utility model discloses an unmanned aerial vehicle monitoring device convenient to disassemble, and relates to the technical field of unmanned aerial vehicles, the unmanned aerial vehicle monitoring device comprises an unmanned aerial vehicle body, the surface of the unmanned aerial vehicle body is provided with a stabilizing mechanism, the bottom end of the unmanned aerial vehicle body is provided with a disassembling mechanism, and the bottom end of the disassembling mechanism is provided with a monitoring device. The bottom end of the base is connected with monitoring equipment, when the monitoring equipment needs to be connected with an unmanned aerial vehicle body, a cross-shaped groove formed by the base and a connecting block is aligned with a connecting base and a clamping block, at the moment, a pressing base is pressed, a movable rod drives a clamping bolt to be close to the connecting base along a communicating groove, and meanwhile an extrusion ring extrudes a spring; and when the clamping bolt moves to a downward sliding way formed by the connecting block and the connecting base, the connecting base and the clamping block are inserted into a clamping groove formed by the base and the connecting block, at the moment, the pressing base is loosened, the spring rebounds to push the extrusion ring, the movable rod is driven to reset, the clamping bolt and the connecting block are clamped to complete fixation, and the adaptability of the device is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to an unmanned plane technical field, concretely relates to an unmanned plane monitoring device convenient to disassemble. BACKGROUND

[0002] The unmanned plane is not the plane of carrying the person that uses the radio remote control equipment and the self -provided program control device to manipulate, or by the on -board computer completely or intermittently self -operated, the development of unmanned plane technology is closely related with the technology progress of multiple fields, involves power, navigation, interaction, communication, chip and platform etc.

[0003] Patent publication number CN216424770U discloses an unmanned plane monitoring device, including unmanned plane body, support frame and camera, the camera is installed lens, the support frame is installed in the lower end of unmanned plane body and symmetrically sets up two, the lower end surface of two support frames is equipped with the damping assembly, the camera is installed in the lower end of unmanned plane body.

[0004] In order to solve the problem that lens is inconvenient to clean when flying, the prior art is to use the second driving motor to drive the sponge plate to move to the front of the lens and abut against the lens, start the first driving motor, and clean the foreign matter on the lens in the process of continuous rotation of the sponge plate, but the monitoring device is inconvenient to disassemble, which leads to poor adaptability. UTILITY MODEL CONTENTS

[0005] The utility model aims at providing a kind of unmanned plane monitoring device convenient to disassemble to solve the problems raised in the above background technology.

[0006] To solve the above technical problems, the technical scheme adopted by the utility model is:

[0007] A kind of unmanned plane monitoring device convenient to disassemble, including unmanned plane body, the surface of the unmanned plane body is provided with stabilizing mechanism, the bottom of the unmanned plane body is provided with dismounting mechanism, the bottom of the dismounting mechanism is provided with monitoring equipment.

[0008] The dismounting mechanism includes connecting seat, the connecting seat is fixedly installed on the surface of unmanned plane body, the surface of the connecting seat is fixedly installed with clamping block, the clamping block is provided with two groups, the clamping block is symmetrically distributed on the surface of connecting seat, the surface of the clamping block is provided with communicating groove, the communicating groove is movably installed with movable rod in the inside, the surface of the movable rod is fixedly installed with clamping bolt.

[0009] The further improvement of the utility model technical scheme lies in that one end of the movable rod is fixedly installed with a pressing seat, the surface of the movable rod is sleeved with a spring, one end of the spring is fixedly installed with a extrusion ring, and the extrusion ring is fixedly installed on the surface of the movable rod.

[0010] The further improvement of the utility model technical scheme lies in that the bottom end of the connecting seat is movably installed with a base, the base is fixedly installed at the top end of the monitoring device, the surface of the base is fixedly installed with a connecting block, the connecting block is provided with four groups, and the connecting blocks are symmetrically distributed on the surface of the base.

[0011] The further improvement of the utility model technical scheme lies in that the interval between the two groups of connecting blocks close to the clamping blocks on one side is matched with the width of the clamping blocks, the interval between the two groups of connecting blocks close to the connecting seat on one side is matched with the width of the connecting seat, and the connecting block is matched with the clamping bolt.

[0012] The further improvement of the utility model technical scheme lies in that the stabilizing mechanism comprises screw columns, the screw columns are fixedly installed on the surface of the unmanned aerial vehicle body, the screw columns are provided with four groups, the screw columns are uniformly distributed on the surface of the unmanned aerial vehicle body, and the surface of the screw column is screw-connected with a supporting column.

[0013] The further improvement of the utility model technical scheme lies in that the inside of the supporting column is fixedly installed with a damper, the surface of the damper is fixedly installed with a buffer spring, one end of the damper is fixedly installed with a movable seat, and the movable seat is movably installed in the inside of the supporting column.

[0014] The further improvement of the utility model technical scheme lies in that the bottom end of the movable seat is fixedly installed with a universal ball head, the surface of the universal ball head is movably installed with a bearing seat, and the bottom end of the bearing seat is fixedly installed with a supporting plate.

[0015] Due to the adoption of the above technical scheme, the utility model has the following technical progress compared with the prior art:

[0016] 1. This utility model provides an easily disassembled drone monitoring device, which employs a base, connecting block, connecting seat, locking block, movable rod, compression ring, spring, bolt, pressing seat, connecting groove, and monitoring equipment. The monitoring equipment is connected to the bottom of the base. When it is necessary to connect the monitoring equipment to the drone body, the cross-shaped groove formed by the base and connecting block is aligned with the connecting seat and locking block. At this time, the pressing seat is pressed, causing the movable rod to move the bolt along the connecting groove towards the connecting seat. At the same time, the compression ring compresses the spring. When the bolt moves to the downward sliding track formed by the connecting block and connecting seat, the connecting seat and locking block insert into the locking groove formed by the base and connecting block. At this time, the pressing seat is released, causing the spring to rebound and push the compression ring, causing the movable rod to return to its original position and locking the bolt with the connecting block, thus completing the fixation. When disassembly is required, simply press the pressing seat to disengage the bolt from the connecting block, thus improving the adaptability of the device.

[0017] 2. This utility model provides an easily disassembled drone monitoring device, which employs a combination of support columns, movable seats, universal ball joints, bearing seats, support plates, threaded columns, dampers, and buffer springs. Threaded columns are installed at the bottom of the four sets of wings on the drone body, allowing for quick threaded connection between the threaded columns and support columns. This structure enables rapid disassembly of the stabilization mechanism during routine maintenance. When the drone completes its flight mission and lands, the support plate preferentially contacts the bottom. The wide-body design provides a wider contact area and more stable landing. When the support plate contacts the ground, the impact force causes the movable seat to move inwards towards the support column, where the buffer springs cushion the impact. The damper (model RB / RBC0604) prevents excessive spring rebound. Furthermore, when the drone lands and the support plate contacts uneven ground, the universal ball joint can rotate within the bearing seat to adjust the tilt angle of the support plate, achieving an adaptive effect to the ground and improving the device's adaptability. Attached Figure Description

[0018] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0019] Figure 2 This is a schematic diagram of the structure of the present invention from an axial view perspective;

[0020] Figure 3 This is a schematic diagram of the disassembly mechanism of this utility model;

[0021] Figure 4 This is a schematic diagram of the stabilizing mechanism of this utility model;

[0022] Figure 5 This is a schematic diagram of the structure of the support column of this utility model.

[0023] As shown in the figure, the utility model provides a kind of unmanned plane monitoring device of easy disassembly, including unmanned plane body 1, the surface of unmanned plane body 1 is provided with stabilizing mechanism 3, the bottom of unmanned plane body 1 is provided with dismounting mechanism 2, the bottom of dismounting mechanism 2 is provided with monitoring device 4, dismounting mechanism 2 includes connecting seat 203, connecting seat 203 is fixedly installed on the surface of unmanned plane body 1, the surface of connecting seat 203 is fixedly installed with card block 204, card block 204 is provided with two groups, card block 204 is symmetrically distributed on the surface of connecting seat 203, the surface of card block 204 is provided with communicating groove 210, communicating groove 210 is movably installed with movable rod 205, the surface of movable rod 205 is fixedly installed with card bolt 208, one end of movable rod 205 is fixedly installed with press seat 209, the surface of movable rod 205 is sleeved with spring 207, one end of spring 207 is fixedly installed with extrusion ring 206, extrusion ring 206 is fixedly installed on the surface of movable rod 205, the bottom of connecting seat 203 is movably installed with base 201, base 201 is fixedly installed on the top of monitoring device 4, the surface of base 201 is fixedly installed with connecting block 202, connecting block 202 is provided with four groups, connecting block 202 is symmetrically distributed on the surface of base 201 two by two, the distance between the side of two groups of connecting block 202 close to card block 204 and the width of card block 204 are adapted, the distance between the side of two groups of connecting block 202 close to connecting seat 203 and the width of connecting seat 203 are adapted, connecting block 202 is adapted with card bolt 208. DETAILED DESCRIPTION

[0024] The utility model makes further detailed description in combination with example:

[0025] Example 1

[0026] As Figures 1-5 shown, the utility model provides a kind of unmanned plane monitoring device of easy disassembly, including unmanned plane body 1, the surface of unmanned plane body 1 is provided with stabilizing mechanism 3, the bottom of unmanned plane body 1 is provided with dismounting mechanism 2, the bottom of dismounting mechanism 2 is provided with monitoring device 4, dismounting mechanism 2 includes connecting seat 203, connecting seat 203 is fixedly installed on the surface of unmanned plane body 1, the surface of connecting seat 203 is fixedly installed with card block 204, card block 204 is provided with two groups, card block 204 is symmetrically distributed on the surface of connecting seat 203, the surface of card block 204 is provided with communicating groove 210, communicating groove 210 is movably installed with movable rod 205, the surface of movable rod 205 is fixedly installed with card bolt 208, one end of movable rod 205 is fixedly installed with press seat 209, the surface of movable rod 205 is sleeved with spring 207, one end of spring 207 is fixedly installed with extrusion ring 206, extrusion ring 206 is fixedly installed on the surface of movable rod 205, the bottom of connecting seat 203 is movably installed with base 201, base 201 is fixedly installed on the top of monitoring device 4, the surface of base 201 is fixedly installed with connecting block 202, connecting block 202 is provided with four groups, connecting block 202 is symmetrically distributed on the surface of base 201 two by two, the distance between the side of two groups of connecting block 202 close to card block 204 and the width of card block 204 are adapted, the distance between the side of two groups of connecting block 202 close to connecting seat 203 and the width of connecting seat 203 are adapted, connecting block 202 is adapted with card bolt 208.

[0027] In the embodiment, the bottom end of the base 201 is connected with the monitoring device 4, when it is needed to connect the monitoring device 4 with the unmanned aerial vehicle body 1, the cross-shaped recess formed by the base 201 and the connecting block 202 is aligned with the connecting seat 203 and the clamping block 204, at this time, the pressing seat 209 is pressed, so that the movable rod 205 drives the clamping bolt 208 to move along the communication groove 210 to the connecting seat 203, and the extrusion ring 206 extrudes the spring 207, so that the spring 207 is compressed, when the clamping bolt 208 moves to the downward slide formed by the connecting block 202 and the connecting seat 203, the connecting seat 203 and the clamping block 204 are inserted into the clamping groove formed by the base 201 and the connecting block 202, at this time, the pressing seat 209 is released, so that the spring 207 rebounds to push the extrusion ring 206, drives the movable rod 205 to reset and makes the clamping bolt 208 and the connecting block 202 clamped, the fixing is completed, when it is needed to disassemble, only the pressing seat 209 is pressed, so that the clamping bolt 208 is separated from the connecting block 202, and the device is disassembled, the adaptability of the device is improved.

[0028] Embodiment 2

[0029] As Figures 1-5 shown, on the basis of the embodiment 1, the utility model provides a technical scheme: preferably, the stabilizing mechanism 3 includes threaded column 306, threaded column 306 fixed mounting in the surface of unmanned aerial vehicle body 1, threaded column 306 sets up four groups, threaded column 306 evenly distributes in the surface of unmanned aerial vehicle body 1, the surface of threaded column 306 is connected with support column 301, support column 301's inside fixed mounting has damper 307, damper 307's surface fixed mounting has buffer spring 308, damper 307 one end fixed mounting has movable seat 302, movable seat 302 movable mounting in the inside of support column 301, movable seat 302's bottom end fixed mounting has universal ball head 303, universal ball head 303's surface movable mounting has bearing seat 304, bearing seat 304's bottom end fixed mounting has support plate 305.

[0030] In the embodiment, the four groups of flying wings of the unmanned aerial vehicle body 1 are provided with threaded columns 306 at the bottom end, so that the threaded columns 306 can be quickly screwed with the support columns 301. In daily maintenance, the stable mechanism 3 can be quickly disassembled. When the unmanned aerial vehicle body 1 completes the flight task and lands, the support plate 305 is in contact with the bottom end first. The wide-body design makes the contact surface wider and the landing more stable. When the support plate 305 contacts the ground, the impact force makes the movable seat 302 move to the inside of the support column 301. The buffer spring 308 buffers it, and the damper 307 avoids the spring from rebounding too fast. The model of the damper 307 is RB / RBC0604. At the same time, when the unmanned aerial vehicle body 1 lands, the support plate 305 contacts the uneven ground. The universal ball head 303 can rotate in the bearing seat 304 to adjust the inclination angle of the support plate 305, so as to adapt to the ground and improve the adaptability of the device.

[0031] The working principle of the unmanned aerial vehicle monitoring device will be described below.

[0032] As Figures 1-5As shown, the bottom end of the base 201 is connected with the monitoring device 4, when it is needed to connect the monitoring device 4 with the unmanned aerial vehicle body 1, the cross-shaped groove formed by the base 201 and the connecting block 202 is aligned with the connecting seat 203 and the clamping block 204, at this time, the pressing seat 209 is pressed, so that the movable rod 205 drives the clamping bolt 208 to move along the communication groove 210 to the connecting seat 203, at the same time, the extrusion ring 206 extrudes the spring 207, so that the spring 207 is compressed, when the clamping bolt 208 moves to the downward slide formed by the connecting block 202 and the connecting seat 203, the connecting seat 203 and the clamping block 204 are inserted into the clamping groove formed by the base 201 and the connecting block 202, at this time, the pressing seat 209 is released, so that the spring 207 rebounds to push the extrusion ring 206, drives the movable rod 205 to reset and makes the clamping bolt 208 and the connecting block 202 clamped, the fixing is completed, when it is needed to disassemble, only the pressing seat 209 is pressed, so that the clamping bolt 208 is separated from the connecting block 202, and then the device is disassembled, the threaded column 306 is arranged at the bottom end of the four groups of flying wings of the unmanned aerial vehicle body 1, so that the threaded column 306 can be quickly screwed with the supporting column 301, the structure can quickly disassemble the stabilizing mechanism 3 during daily maintenance, when the unmanned aerial vehicle body 1 completes the flight task, the supporting plate 305 contacts the bottom end first during landing, the wide body design makes the contact surface wider, and the landing is more stable, when the supporting plate 305 contacts the ground, the impact force makes the movable seat 302 move to the inside of the supporting column 301, the buffer spring 308 buffers it, and the damper 307 avoids the spring rebounding too fast, the model of the damper 307 is RB / RBC0604, at the same time, when the unmanned aerial vehicle body 1 lands, the supporting plate 305 contacts the uneven ground, the universal ball head 303 can rotate in the bearing seat 304 to adjust the inclination angle of the supporting plate 305, so that the ground is self-adapted, and the adaptability of the device is improved.

[0033] The above is a detailed description of the general utility model, but some modifications or improvements can be made on the basis of the utility model, which is obvious to those skilled in the art. Therefore, the modifications or improvements without departing from the spirit of the utility model are within the protection scope of the utility model.

Claims

1. A drone monitoring device for easy detachment, comprising a drone body (1), characterized in that: The surface of the unmanned aerial vehicle body (1) is provided with a stabilizing mechanism (3), the bottom end of the unmanned aerial vehicle body (1) is provided with a dismounting mechanism (2), and the bottom end of the dismounting mechanism (2) is provided with a monitoring device (4); The dismounting mechanism (2) comprises a connecting seat (203) fixedly installed on the surface of the unmanned aerial vehicle body (1), a clamping block (204) fixedly installed on the surface of the connecting seat (203), two groups of clamping blocks (204) symmetrically distributed on the surface of the connecting seat (203), and a communication groove (210) provided on the surface of the clamping block (204).

2. The drone monitoring device of claim 1, wherein: One end of the movable rod (205) is fixedly installed with a pressing seat (209), the surface of the movable rod (205) is sleeved with a spring (207), one end of the spring (207) is fixedly installed with a pressing ring (206), and the pressing ring (206) is fixedly installed on the surface of the movable rod (205).

3. The drone monitoring device of claim 1, wherein: The bottom end of the connecting seat (203) is movably installed with a base (201), the base (201) is fixedly installed on the top end of the monitoring device (4), the surface of the base (201) is fixedly installed with a connecting block (202), the connecting block (202) is provided with four groups, and the connecting blocks (202) are symmetrically distributed on the surface of the base (201).

4. The easily detachable drone monitoring device of claim 3, wherein: The distance between the two groups of connecting blocks (202) near the side of the clamping block (204) is matched with the width of the clamping block (204), the distance between the two groups of connecting blocks (202) near the side of the connecting seat (203) is matched with the width of the connecting seat (203), and the connecting block (202) is matched with the clamping block (208).

5. The drone monitoring device of claim 1, wherein: The stabilizing mechanism (3) comprises a threaded column (306) fixedly installed on the surface of the unmanned aerial vehicle body (1), four groups of threaded columns (306) uniformly distributed on the surface of the unmanned aerial vehicle body (1), and a support column (301) threadedly connected with the surface of the threaded column (306).

6. The easily detachable drone monitoring device of claim 5, wherein: The inside of the support column (301) is fixedly installed with a damper (307), the surface of the damper (307) is fixedly installed with a buffer spring (308), one end of the damper (307) is fixedly installed with a movable seat (302), and the movable seat (302) is movably installed in the inside of the support column (301).

7. The easily detachable drone monitoring device of claim 6, wherein: The bottom end of the movable seat (302) is fixedly installed with a universal ball head (303), the surface of the universal ball head (303) is movably installed with a bearing seat (304), and the bottom end of the bearing seat (304) is fixedly installed with a support plate (305).

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