Multifunctional intelligent power application unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial equipment, and discloses a multifunctional intelligent electric power application unmanned aerial vehicle which comprises a main machine, a plurality of paddle rods are fixedly installed on the outer side of the main machine, propellers are fixedly installed on the paddle rods, a camera is fixedly installed at the lower end of the main machine, and supports are fixedly installed at the positions, located on the two sides of the camera, of the main machine. Shaft seats are fixedly installed on one sides of the two supports respectively, fixing rings are fixedly installed on the sides, away from the supports, of the shaft seats, and a plurality of ejector rods are movably installed in the fixing rings. A group of shaft seats, fixing rings and adjusting wheels are respectively arranged on one sides of the two brackets, and ejector rods and damping blocks are movably mounted in the fixing rings, so that the rotating damping of the pay-off shaft can be synchronously adjusted through the matching of a plurality of adjusting blocks on the inner sides of the adjusting wheels, and the phenomenon that the pay-off shaft is damaged when a traction rope is released is prevented. The traction rope falls down quickly to cause accumulation of the traction rope at multiple points on the ground due to too fast rotation of a pay-off shaft caused by drooping gravity of the traction rope, so that the final traction length of the traction rope is easy to be insufficient.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned flight equipment technical field, especially in kind of multifunctional intelligent electric power application unmanned plane. BACKGROUND

[0002] The unmanned plane in the field of electric power is generally equipped with various sensors such as high-definition camera, infrared thermal imager and ultraviolet imager.In the inspection operation, the high-definition camera can clearly capture the line details, the infrared thermal imager can detect the line heating anomaly, and the ultraviolet imager can find the problem of corona discharge, and at the same time, it also has strong endurance and load capacity, and can carry the traction rope to assist the electric power construction.

[0003] As disclosed in the Chinese utility model patent with the announcement number CN219970006U: a kind of unmanned plane for electric power, the application includes main body, the body of unmanned plane, multiple rotors are arranged on it, clamp, as horizontal clamping clamp, is installed in the extension pipe both sides, the extension pipe is fixedly installed in main body front end bottom, when the traction rope for cable laying is pulled by the unmanned plane of this type, the rotation damping adjustment mechanism of the pay-off shaft of the pay-off equipment used by current construction is not perfect, when releasing the traction rope, due to the gravity effect of the traction rope droop, pay-off shaft is prone to rotate quickly, which makes the traction rope fall at too fast speed, and then form the accumulation of traction rope in multiple point positions on ground, once this accumulation occurs, construction personnel not only need to spend a lot of time and effort to arrange traction rope, but also can lead to the insufficient length of traction rope that can be finally pulled, and when the length of traction rope cannot meet the actual construction demand, it has to be re-wound, which seriously affects construction progress and increases construction cost. UTILITY MODEL CONTENTS

[0004] The utility model aims at providing a kind of multifunctional intelligent electric power application unmanned plane, which can effectively solve the problems in the background art.

[0005] To achieve the above-mentioned purpose, the technical scheme adopted by the utility model is as follows:

[0006] A kind of multifunctional intelligent electric power application unmanned plane, including main machine, the multiple paddle rods are fixedly installed on the outer side of the main machine, the propeller is fixedly installed on the paddle rod, the camera is fixedly installed at the lower end of the main machine, the main machine at the both sides of the camera is fixedly installed with the support, and the one side of the two support is fixedly installed with the shaft seat respectively, the one side of the shaft seat away from the support is fixedly installed with the fixed ring, the multiple top rods are movably installed in the fixed ring, the one end of the top rod relative to the center point of fixed ring is movably installed with the damping block, the one end of the fixed ring away from the shaft seat is also movably installed with the adjusting wheel, and the pay-off shaft is rotatably connected between the two shaft seats, and the multiple internal screw groove seats are fixedly installed on the one side of the support close to the shaft seat.

[0007] As a further preferred scheme of the utility model, the contact groove is arranged at the both ends of the pay-off shaft, and the contact groove is arranged at the both ends of the pay-off shaft in the fixed ring, the pay-off shaft can realize the winding of the traction rope, and the contact groove can provide conditions for the rotation damping adjustment of the pay-off shaft.

[0008] As a further preferred scheme of the utility model, the rotation groove is arranged at the outer side of the fixed ring, the rotation groove can provide conditions for the rotation installation of the adjusting wheel, and the plurality of mounting holes are arranged at the inner side of the fixed ring close to the rotation groove, the mounting hole can provide basic conditions for the installation of the ejector rod.

[0009] As a further preferred scheme of the utility model, the telescopic groove is arranged in the ejector rod, and the ejector rod is inserted and installed in one of the mounting holes.

[0010] As a further preferred scheme of the utility model, the telescopic rod is fixedly installed at one end of the damping block relative to the ejector rod, one end of the telescopic rod away from the damping block is inserted and installed in the telescopic groove in the ejector rod, the compression spring is sleeved on the outer side of the telescopic rod, one end of the compression spring abuts against the bottom of the ejector rod, and the other end of the compression spring abuts against the top of the damping block, that is, the bottom of the damping block abuts against in the contact groove through the action force of the compression spring.

[0011] As a further preferred scheme of the utility model, the rotation block is fixedly installed at the inner side of the adjusting wheel, the longitudinal section of the rotation block is L-shaped, the plurality of adjusting blocks are further fixedly installed at the inner side of the adjusting wheel close to the rotation block, the side rod is fixedly installed at the outer side of the adjusting wheel, the limiting bolt is inserted and installed in the side rod, the adjusting wheel is rotationally installed at one end of the fixed ring through the rotation block, the rotation block is rotationally installed in the rotation groove, and one end of the limiting bolt is screw-connected in one of the inner screw groove seats.

[0012] As a further preferred scheme of the utility model, the adjusting block has the arc surface relative to one side of the rotation block.

[0013] Compared with the prior art, the utility model has the beneficial effects that:

[0014] In the utility model, a group of axle seats, fixing rings and adjusting wheels are arranged on the one side of the two supports, the top rod and the damping block are movably installed in the fixing ring, the rotating damping of the pay-off shaft can be synchronously adjusted through the cooperation of the plurality of adjusting blocks in the inner side of the adjusting wheel, thereby preventing the traction rope from being accumulated on the ground in multiple points when the traction rope is released, the traction rope is caused to fall rapidly due to the excessive rotation of the pay-off shaft caused by the traction rope due to the gravity of the droop, and the final traction length of the traction rope is easily caused to be insufficient. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 It is the schematic diagram of the main body structure of the utility model;

[0016] Figure 2 It is Figure 1 It is the enlarged view of A in the middle;

[0017] Figure 3 It is the sectional view of the axle seat and the adjusting wheel of the utility model;

[0018] Figure 4 It is the schematic diagram of the axle seat structure of the utility model;

[0019] Figure 5 It is the sectional view of the top rod and the damping block of the utility model;

[0020] Figure 6 It is the schematic diagram of the adjusting wheel structure of the utility model.

[0021] In the drawing: 1, main machine;2, paddle rod;3, propeller;4, camera;5, support;6, axle seat;7, fixing ring;8, top rod;9, damping block;10, adjusting wheel;11, pay-off shaft;12, contact groove;13, mounting hole;14, rotating groove;15, telescopic groove;16, telescopic rod;17, compression spring;18, rotating block;19, adjusting block;20, side rod;21, limit bolt;22, inner screw groove seat. DETAILED DESCRIPTION

[0022] In order to make the technical means, creative features, purposes and effects realized by the utility model easy to understand, the utility model is further described below in combination with specific implementation manners.

[0023] For example, Figures 1-6As shown in the utility model provides a kind of multifunctional intelligent electric power application unmanned plane, including host computer 1, multiple paddle rods 2 are fixedly installed on the outer side of host computer 1, propeller 3 is fixedly installed on paddle rod 2, camera 4 is fixedly installed at the lower end of host computer 1, the host computer 1 located at the both sides of camera 4 is fixedly installed with bracket 5, and two bracket 5 one side is fixedly installed with shaft seat 6, shaft seat 6 is fixedly installed with fixed ring 7 on the side away from bracket 5, multiple top rods 8 are movably installed in fixed ring 7, damping block 9 is movably installed at the one end of top rod 8 relative to the center point of fixed ring 7, adjusting wheel 10 is also movably installed at the end of fixed ring 7 away from shaft seat 6, and pay-off shaft 11 is rotatably connected between the two shaft seats 6, multiple inner screw groove seats 22 are fixedly installed at the side of bracket 5 close to shaft seat 6.

[0024] As Figure 3 Shown, contact groove 12 is formed at both ends of pay-off shaft 11, and the contact groove 12 at both ends of pay-off shaft 11 is located in fixed ring 7, pay-off shaft 11 can realize the winding of traction rope, and the setting of contact groove 12 can provide conditions for the rotation damping adjustment of pay-off shaft 11.

[0025] As Figures 3-5 Shown, rotation groove 14 is formed on the outer side of fixed ring 7, rotation groove 14 can provide conditions for the rotation installation of adjusting wheel 10, multiple mounting holes 13 are formed in fixed ring 7 close to rotation groove 14, the setting of mounting hole 13 can provide basic conditions for the installation of top rod 8, expansion slot 15 is formed in top rod 8, and top rod 8 is inserted and installed in one of mounting holes 13, expansion rod 16 is fixedly installed at one end of damping block 9 relative to top rod 8, expansion rod 16 is inserted and installed in expansion slot 15 in top rod 8 away from damping block 9, compression spring 17 is sleeved on the outer side of expansion rod 16, and one end of compression spring 17 abuts against the bottom of top rod 8, the other end of compression spring 17 abuts against the top of damping block 9, that is, the bottom of damping block 9 abuts against in contact groove 12 by the action force of compression spring 17.

[0026] As Figures 3-5 、 Figure 6As shown, the adjusting wheel 10 is fixedly installed with a rotating block 18 inside, the longitudinal section of the rotating block 18 is L-shaped, a plurality of adjusting blocks 19 are fixedly installed on the inside of the adjusting wheel 10 close to the rotating block 18, a side rod 20 is fixedly installed on the outside of the adjusting wheel 10, a limiting bolt 21 is insertedly installed in the side rod 20, the adjusting wheel 10 is rotatably installed at one end of the fixed ring 7 through the rotating block 18, and the rotating block 18 is rotatably installed in the rotating groove 14, one end of the limiting bolt 21 is threadedly connected in one of the inner screw groove seats 22, the inside of the adjusting wheel 10 is provided with a plurality of adjusting blocks 19, the plurality of adjusting blocks 19 can synchronously press one end of one of the top rods 8 by rotating the adjusting wheel 10 at one end of the fixed ring 7, so that the compression spring 17 is compressed, and the pressure on the damping block 9 is increased, so that the bottom of the damping block 9 is pressed against the inside of the contact groove 12, and the damping of the rotating of the pay-off shaft 11 is adjusted, and one side of the adjusting block 19 relative to the rotating block 18 has a curved surface.

[0027] It should be noted that the utility model is a multifunctional intelligent power application unmanned aerial vehicle, when the rotating damping of the pay-off shaft 11 needs to be adjusted, the adjusting wheel 10 can be manually rotated through the side rod 20, and the plurality of adjusting blocks 19 inside the adjusting wheel 10 can gradually press one of the top rods 8 through the curved surface on one side, so that the top rod 8 is stressed, the compression spring 17 is compressed, the pressure on the damping block 9 is increased, the pressure of the bottom of the damping block 9 pressed against the inside of the contact groove 12 is increased, the pressure applied by the plurality of damping blocks 9 to the inside of the contact groove 12 is increased, and the damping of the pay-off shaft 11 when rotating is increased, so that the pay-off shaft 11 is prevented from rotating too fast due to the gravity of the traction rope when the traction rope is released, the traction rope is prevented from falling rapidly and causing the ground to be piled up at multiple points, when the rotating damping of the pay-off shaft 11 is adjusted, the limiting bolt 21 can be rotated through a tool, one end of the limiting bolt 21 is threadedly connected into the corresponding inner screw groove seat 22, the adjusting wheel 10 can be rotationally limited, the stability of the adjusting block 19 pressing the top rod 8 is ensured.

[0028] The basic principle and main features of the utility model and the advantages of the utility model are shown and described above. It should be understood by those skilled in the art that the utility model is not limited by the above-mentioned embodiments, the above-mentioned embodiments and the description in the specification are only to illustrate the principle of the utility model, various changes and improvements can be made to the utility model without departing from the spirit and scope of the utility model, and these changes and improvements all fall within the scope of the utility model claimed. The protection scope of the utility model is defined by the appended claims and their equivalents.

Claims

1. A multifunctional intelligent power application drone, characterized in that: The system includes a main unit (1), on which multiple propellers (2) are fixedly mounted on the outside. Propellers (3) are fixedly mounted on the propellers (2). A camera (4) is fixedly mounted on the lower end of the main unit (1). A bracket (5) is fixedly mounted on both sides of the main unit (1) located at the camera (4). A bearing seat (6) is fixedly mounted on one side of each of the two brackets (5). A fixing ring (7) is fixedly mounted on the side of the bearing seat (6) opposite to the bracket (5). Multiple push rods (8) are movably mounted inside the fixing ring (7). A damping block (9) is movably mounted on one end of the push rod (8) relative to the center point of the fixing ring (7). An adjusting wheel (10) is also movably mounted on the end of the fixing ring (7) opposite to the bearing seat (6). A wire feeding shaft (11) is rotatably connected between the two bearing seats (6). Multiple internal threaded seats (22) are fixedly mounted on one side of the bracket (5) near the bearing seat (6).

2. The multifunctional intelligent power application drone according to claim 1, characterized in that: The wire feeding shaft (11) has contact grooves (12) at both ends, and the contact grooves (12) at both ends of the wire feeding shaft (11) are located inside the fixing ring (7).

3. The multifunctional intelligent power application drone according to claim 2, characterized in that: The fixing ring (7) has a rotating groove (14) on its outer side, and a plurality of mounting holes (13) are provided inside the fixing ring (7) near the rotating groove (14).

4. The multifunctional intelligent power application drone according to claim 3, characterized in that: The top rod (8) has a telescopic groove (15) inside, and the top rod (8) is inserted into one of the mounting holes (13).

5. A multifunctional intelligent power application drone according to claim 4, characterized in that: The damping block (9) is fixedly mounted with a telescopic rod (16) at one end relative to the top rod (8). The end of the telescopic rod (16) away from the damping block (9) is inserted into the telescopic groove (15) inside the top rod (8). A compression spring (17) is fitted on the outside of the telescopic rod (16). One end of the compression spring (17) abuts against the bottom of the top rod (8), and the other end of the compression spring (17) abuts against the top of the damping block (9). That is, the bottom of the damping block (9) abuts against the contact groove (12) by the force of the compression spring (17).

6. The multifunctional intelligent power application drone according to claim 1, characterized in that: A rotating block (18) is fixedly installed on the inner side of the adjusting wheel (10). The longitudinal section of the rotating block (18) is L-shaped. Multiple adjusting blocks (19) are also fixedly installed on the inner side of the adjusting wheel (10) near the rotating block (18). A side rod (20) is fixedly installed on the outer side of the adjusting wheel (10). A limiting bolt (21) is inserted into the side rod (20). The adjusting wheel (10) is rotatably installed on one end of the fixing ring (7) through the rotating block (18). The rotating block (18) is rotatably installed in the rotating groove (14). One end of the limiting bolt (21) is threaded into one of the internal threaded groove seats (22).

7. A multifunctional intelligent power application drone according to claim 6, characterized in that: The adjusting block (19) has an arc surface on one side relative to the rotating block (18).

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