CN218022167U - Four-rotor unmanned aerial vehicle for inspection - Google Patents
Four-rotor unmanned aerial vehicle for inspection Download PDFInfo
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- CN218022167U CN218022167U CN202222342363.6U CN202222342363U CN218022167U CN 218022167 U CN218022167 U CN 218022167U CN 202222342363 U CN202222342363 U CN 202222342363U CN 218022167 U CN218022167 U CN 218022167U
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Abstract
The utility model relates to a household daily necessities field especially relates to a four rotor unmanned aerial vehicle who patrols and examines usefulness. The quad-rotor unmanned aerial vehicle for inspection comprises an unmanned aerial vehicle main body, wherein four unmanned aerial vehicle rotors are rotatably connected to the surface of the unmanned aerial vehicle main body; high definition digtal camera, high definition digtal camera set up in unmanned aerial vehicle main part below, rotating device fixed mounting are in unmanned aerial vehicle main part bottom, coupling mechanism, and coupling mechanism sets up in high definition digtal camera top. The utility model provides a four rotor unmanned aerial vehicle of patrolling and examining usefulness makes things convenient for quick assembly disassembly high definition digtal camera through installation rotating device and coupling mechanism, makes things convenient for quick adjustment, has improved high definition digtal camera's maintenance speed, conveniently adjusts high definition digtal camera's angle, has improved four rotor unmanned aerial vehicle's performance's advantage.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to a four rotor unmanned aerial vehicle of usefulness patrolling and examining.
Background
Unmanned aerial vehicle is the unmanned aerial vehicle who utilizes radio remote control equipment and the program control device manipulation of oneself, unmanned aerial vehicle's application is more and more extensive, at the in-process of patrolling and examining, can use four rotor unmanned aerial vehicle, current four rotor unmanned aerial vehicle, the camera of installation is through bolt fixed connection, after using a period, need overhaul the adjustment to the camera, the inconvenient dismouting that carries out fast of camera of bolt fastening, the maintenance speed of camera has been reduced, and simultaneously, current four rotor unmanned aerial vehicle, be through the remote controller regulation four rotor unmanned aerial vehicle angle, adjust the angle of camera, lead to the unable smooth flight in-process of four rotor unmanned aerial vehicle, adjust the angle of camera, four rotor unmanned aerial vehicle's performance has been reduced.
Therefore, it is necessary to provide a new quad-rotor drone for inspection to solve the above technical problems.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides a four rotor unmanned aerial vehicle of usefulness patrolling and examining.
The utility model provides a four rotor unmanned aerial vehicle of usefulness of patrolling and examining includes: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body, wherein four unmanned aerial vehicle rotor wings are rotatably connected to the surface of the unmanned aerial vehicle main body; the unmanned aerial vehicle comprises an unmanned aerial vehicle body, a rotating device, the rotating device is fixedly installed at the bottom of the unmanned aerial vehicle body and comprises a rotating installation shell, a rotating installation groove, a rotating driving motor, symmetrical connection holes and a rotating connection rod, the unmanned aerial vehicle body is fixedly provided with the rotating installation shell, the rotating installation shell is internally provided with the rotating installation groove, the inner wall of the rotating installation groove is fixedly connected with the rotating driving motor, the surface of the rotating installation shell is symmetrically provided with the symmetrical connection holes, the inner wall of each symmetrical connection hole is in threaded connection with the corresponding rotating connection rod, and the rotating connection rod is in threaded connection with the inner wall of the unmanned aerial vehicle body; coupling mechanism, coupling mechanism sets up in high definition digtal camera top, through coupling mechanism, conveniently with unmanned aerial vehicle main part and high definition digtal camera fast assembly, start and rotate driving motor, rotate driving motor output shaft and drive high definition digtal camera angle regulation, will rotate the installation shell and be close to the unmanned aerial vehicle main part, rotate the rotation connecting rod, will rotate the connecting rod and send into symmetrical connection hole inner wall, with unmanned aerial vehicle main part and rotation installation shell high-speed joint.
Preferably, unmanned aerial vehicle main part surface symmetry fixedly connected with support frame carries out the outrigger to the unmanned aerial vehicle main part, before the unmanned aerial vehicle main part takes off, prevents that unmanned aerial vehicle main part and high definition digtal camera are direct and ground contact, reduces the wearing and tearing on unmanned aerial vehicle main part and high definition digtal camera surface.
Preferably, rotate driving motor output shaft fixedly connected with angle adjusting plate, rotate driving motor output shaft and drive angle adjusting plate and rotate, angle adjusting plate drives coupling mechanism and rotates, drives high definition digtal camera angle regulation.
Preferably, the whole streamlined that is of unmanned aerial vehicle main part, not only handsome in appearance, at the flight in-process, reduce the resistance of air, promoted the airspeed of unmanned aerial vehicle main part.
Preferably, the unmanned aerial vehicle main part adopts carbon-fibre composite to make, and carbon-fibre composite is a new material that mechanical properties is excellent, can improve the physical strength of unmanned aerial vehicle main part, prolongs the life of unmanned aerial vehicle main part.
Preferably, the connecting mechanism comprises a fixed connecting shell, symmetrical chutes, symmetrical fixture blocks and reset springs, a fixed connecting shell is arranged above the high-definition camera, symmetrical chutes are symmetrically formed in the surface of the fixed connecting shell, symmetrical fixture blocks are connected to the inner walls of the symmetrical chutes in a swinging manner, reset springs are fixedly connected to the inner walls of the symmetrical chutes, the symmetrical fixture blocks and the reset springs are fixedly connected, a symmetrical assembling plate is symmetrically arranged on the surface of the high-definition camera, a rotary lead screw is connected to the inner walls of the high-definition camera and the symmetrical assembling plate in a threaded manner, the rotary lead screw is rotated, the symmetrical assembling plate is fixed on the surface of the high-definition camera, the high-definition camera is close to the connecting mechanism, the symmetrical fixture blocks are pressed, the symmetrical fixture blocks are sent into the symmetrical chutes, the reset springs are tightened, the symmetrical fixture blocks are released from the symmetrical fixture blocks, the symmetrical fixture blocks are shifted out of the symmetrical chute, the inner walls of the symmetrical fixture blocks are sent into the symmetrical assembling plate, the fixed connecting shell and the high-definition camera are fixedly connected, and the unmanned aerial vehicle main body and the high-definition camera are conveniently and quickly assembled.
Preferably, the edge positions of the symmetrical clamping blocks are provided with round corners, so that the friction force of the edge positions of the symmetrical clamping blocks is reduced, when the symmetrical clamping blocks enter the symmetrical sliding grooves and the inner walls of the symmetrical assembling plates, the abrasion of the symmetrical sliding grooves and the inner walls of the symmetrical assembling plates is reduced, and the service life of the fixed connecting shell and the service life of the symmetrical assembling plates are prolonged.
Compared with the prior art, the utility model provides a four rotor unmanned aerial vehicle of usefulness of patrolling and examining has following beneficial effect:
1. the utility model provides a four rotor unmanned aerial vehicle of usefulness patrolls and examines, through installation rotating device and coupling mechanism, make things convenient for quick assembly disassembly high definition digtal camera, convenient quick adjustment has improved high definition digtal camera's maintenance speed, conveniently adjusts high definition digtal camera's angle, has improved four rotor unmanned aerial vehicle's performance.
2. The utility model provides a four rotor unmanned aerial vehicle of usefulness patrolling and examining has seted up the fillet through symmetrical fixture block border position, reduces symmetrical fixture block border position's frictional force, when symmetrical fixture block got into symmetrical spout and symmetry equipment inboard wall, reduces the wearing and tearing of symmetrical spout and symmetry equipment inboard wall, prolongs the service life of fixed connection shell and symmetry equipment board.
Drawings
Fig. 1 is a schematic structural view of a preferred embodiment of a quad-rotor unmanned aerial vehicle for inspection according to the present invention;
FIG. 2 is a schematic bottom view of the structure of FIG. 1;
FIG. 3 is an enlarged schematic view of a portion of FIG. 1;
FIG. 4 is a schematic view of the rotating apparatus shown in FIG. 1;
fig. 5 is a schematic structural view of the connection mechanism shown in fig. 1.
Reference numbers in the figures: 1. an unmanned aerial vehicle main body; 2. a rotor wing of the unmanned aerial vehicle; 3. a support frame; 4. a high-definition camera; 5. a rotating device; 51. rotating the mounting shell; 52. rotating the mounting groove; 53. rotating the drive motor; 54. connecting holes symmetrically; 55. rotating the connecting rod; 6. a connecting mechanism; 61. a fixed connection housing; 62. symmetrical chutes; 63. symmetrical clamping blocks; 64. a return spring; 7. an angle adjusting plate; 8. a symmetrical assembly plate; 9. and rotating the screw rod.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention will be further described in detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
The following detailed description is provided for the specific embodiments of the present invention.
Please refer to fig. 1 to 4, an embodiment of the utility model provides a quad-rotor unmanned aerial vehicle who patrols and examines usefulness, the quad-rotor unmanned aerial vehicle who patrols and examines usefulness includes: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, wherein four unmanned aerial vehicle rotor wings 2 are rotatably connected to the surface of the unmanned aerial vehicle main body 1; high definition digtal camera 4, high definition digtal camera 4 sets up in unmanned aerial vehicle main part 1 below, rotating device 5 is fixed to be installed in unmanned aerial vehicle main part 1 bottom, rotating device 5 includes rotating installation shell 51, rotate mounting groove 52, rotate driving motor 53, symmetric connection hole 54 and rotating connecting rod 55, unmanned aerial vehicle main part 1 is fixed to be installed and rotates installation shell 51, rotating installation shell 51 is inside to be seted up and rotates mounting groove 52, rotate mounting groove 52 inner wall fixedly connected with and rotate driving motor 53, rotate installation shell 51 surface symmetry and seted up symmetric connection hole 54, symmetric connection hole 54 inner wall threaded connection has rotating connecting rod 55, and rotating connecting rod 55 and unmanned aerial vehicle main part 1 inner wall threaded connection; coupling mechanism 6, coupling mechanism 6 sets up in high definition digtal camera 4 top, through coupling mechanism 6, conveniently with unmanned aerial vehicle main part 1 and high definition digtal camera 4 fast assembly, start and rotate driving motor 53, it drives high definition digtal camera 4 angle regulation to rotate driving motor 53 output shaft, will rotate installation shell 51 and be close to unmanned aerial vehicle main part 1, rotate rotation connecting rod 55, will rotate connecting rod 55 and send into symmetrical connecting hole 54 inner wall, with unmanned aerial vehicle main part 1 with rotate installation shell 51 high-speed joint.
In the embodiment of the utility model, please refer to fig. 1 and fig. 3, the surface symmetry fixedly connected with support frame 3 of unmanned aerial vehicle main part 1 carries out the stable support to unmanned aerial vehicle main part 1, before unmanned aerial vehicle main part 1 takes off, prevents that unmanned aerial vehicle main part 1 and high definition digtal camera 4 from direct and ground contact, reduces the wearing and tearing on unmanned aerial vehicle main part 1 and high definition digtal camera 4 surface.
In the embodiment of the utility model, please refer to fig. 3 and fig. 4, rotate driving motor 53 output shaft fixedly connected with angle adjustment plate 7, rotate driving motor 53 output shaft and drive angle adjustment plate 7 and rotate, angle adjustment plate 7 drives coupling mechanism 6 and rotates, drives high definition digtal camera 4 angle regulation.
The utility model discloses an in the embodiment, please refer to fig. 1 and fig. 4, unmanned aerial vehicle main part 1 wholly is streamlined, and not only handsome in appearance reduces the resistance of air at the flight in-process, has promoted unmanned aerial vehicle main part 1's flying speed.
In the embodiment of the utility model, please refer to fig. 1 and fig. 2, unmanned aerial vehicle main part 1 adopts carbon-fibre composite to make, and carbon-fibre composite is a new material that mechanical properties is excellent, can improve unmanned aerial vehicle main part 1's physical strength, prolongs unmanned aerial vehicle main part 1's service life.
The embodiment of the utility model provides an in, please refer to fig. 3 and fig. 5, coupling mechanism 6 includes fixed connection shell 61, symmetry spout 62, symmetry fixture block 63 and reset spring 64, high definition digtal camera 4 top is provided with fixed connection shell 61, fixed connection shell 61 surface symmetry has seted up symmetry spout 62, symmetry spout 62 inner wall rocks and is connected with symmetry fixture block 63, symmetry spout 62 inner wall fixedly connected with reset spring 64, and symmetry fixture block 63 and reset spring 64 fixed connection, high definition digtal camera 4 surface symmetry is provided with symmetry equipment board 8, and high definition digtal camera 4 and the 8 inner wall threaded connection of symmetry equipment board have rotation lead screw 9, rotation lead screw 9, fix symmetry equipment board 8 on high definition digtal camera 4 surface, be close to coupling mechanism 6 with high definition digtal camera 4, press symmetry fixture block 63, send into symmetry spout 62 inside with symmetry fixture block 63, reset spring 64 tightens up, symmetry equipment board 8 hugs closely fixed connection shell 61, relieve symmetry fixture block 63, reset spring 64 opens, symmetry fixture block 63 shifts out symmetry chute 62, send into symmetry fixture block 63 into symmetry equipment board 8 inner wall, with fixed connection shell 61 and the convenience high definition digtal camera 4, unmanned aerial vehicle main part is assembled with unmanned aerial vehicle 4 and unmanned aerial vehicle quick assembly main part.
In the embodiment of the present invention, please refer to fig. 5, the edge of the symmetric fixture block 63 is provided with a rounded corner, so as to reduce the friction force at the edge of the symmetric fixture block 63, and when the symmetric fixture block 63 enters the inner wall of the symmetric chute 62 and the symmetric assembly plate 8, the abrasion of the inner wall of the symmetric chute 62 and the symmetric assembly plate 8 is reduced, and the service life of the fixed connection shell 61 and the symmetric assembly plate 8 is prolonged.
The utility model provides a four rotor unmanned aerial vehicle's that patrol and examine usefulness theory of operation as follows: through coupling mechanism 6, it is convenient with unmanned aerial vehicle main part 1 and high definition digtal camera 4 fast assembly, rotate rotation lead screw 9, fix symmetry equipment board 8 on high definition digtal camera 4 surface, be close to coupling mechanism 6 with high definition digtal camera 4, press symmetry fixture block 63, send symmetry fixture block 63 into inside symmetry spout 62, reset spring 64 tightens up, fixed connection shell 61 is hugged closely to symmetry equipment board 8, it releases symmetry fixture block 63, reset spring 64 resets and opens, symmetry fixture block 63 shifts out symmetry spout 62, send symmetry fixture block 63 into symmetry equipment board 8 inner wall, with fixed connection shell 61 and high definition digtal camera 4 fixed connection, conveniently with unmanned aerial vehicle main part 1 and high definition digtal camera 4 fast assembly, start rotation driving motor 53, rotation driving motor 53 output shaft drives high definition digtal camera 4 angle regulation, it is close to unmanned aerial vehicle main part 1 to rotate installation shell 51, rotate rotation connecting rod 55, will rotate connecting rod 55 and send into symmetry connecting hole 54 inner wall, unmanned aerial vehicle main part 1 and rotation installation shell 51 fast connection.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structures or equivalent processes of the present invention are used in the specification and the attached drawings, or directly or indirectly applied to other related technical fields, and the same principle is included in the protection scope of the present invention.
Claims (8)
1. A quad-rotor unmanned aerial vehicle for routing inspection, comprising:
the unmanned aerial vehicle comprises an unmanned aerial vehicle main body (1), wherein four unmanned aerial vehicle rotor wings (2) are rotatably connected to the surface of the unmanned aerial vehicle main body (1);
the high-definition camera (4), the high-definition camera (4) is arranged below the unmanned aerial vehicle main body (1), and is characterized in that;
the unmanned aerial vehicle comprises a rotating device (5), wherein the rotating device (5) is fixedly installed at the bottom of an unmanned aerial vehicle main body (1), the rotating device (5) comprises a rotating installation shell (51), a rotating installation groove (52), a rotating driving motor (53), symmetrical connection holes (54) and a rotating connection rod (55), the unmanned aerial vehicle main body (1) is fixedly installed with the rotating installation shell (51), the rotating installation groove (52) is formed in the rotating installation shell (51), the rotating driving motor (53) is fixedly connected to the inner wall of the rotating installation groove (52), the symmetrical connection holes (54) are symmetrically formed in the surface of the rotating installation shell (51), the rotating connection rod (55) is in threaded connection with the inner wall of the symmetrical connection holes (54), and the rotating connection rod (55) is in threaded connection with the inner wall of the unmanned aerial vehicle main body (1);
the connecting mechanism (6) is arranged above the high-definition camera (4).
2. The quad-rotor unmanned aerial vehicle for inspection according to claim 1, wherein the unmanned aerial vehicle body (1) is fixedly connected with a support frame (3) in a surface symmetry manner.
3. The inspection quad-rotor unmanned aerial vehicle according to claim 1, wherein an angle adjusting plate (7) is fixedly connected to an output shaft of the rotary driving motor (53).
4. The inspection quad-rotor Unmanned Aerial Vehicle (UAV) of claim 1, wherein the UAV body (1) is streamline overall.
5. The inspection quad-rotor Unmanned Aerial Vehicle (UAV) of claim 1, wherein the UAV body (1) is made of carbon fiber composite material.
6. The inspection quad-rotor unmanned aerial vehicle according to claim 1, wherein the connecting mechanism (6) comprises a fixed connecting shell (61), symmetrical sliding grooves (62), symmetrical clamping blocks (63) and a return spring (64), the fixed connecting shell (61) is arranged above the high-definition camera (4), the symmetrical sliding grooves (62) are symmetrically formed in the surface of the fixed connecting shell (61), the symmetrical clamping blocks (63) are connected to the inner walls of the symmetrical sliding grooves (62) in a swinging mode, the return spring (64) is fixedly connected to the inner walls of the symmetrical sliding grooves (62), and the symmetrical clamping blocks (63) and the return spring (64) are fixedly connected.
7. The inspection quad-rotor Unmanned Aerial Vehicle (UAV) according to claim 6, wherein the symmetrical fixture blocks (63) are provided with rounded corners at edge positions.
8. The inspection quad-rotor unmanned aerial vehicle according to claim 1, wherein symmetrical assembling plates (8) are symmetrically arranged on the surface of the high-definition camera (4), and rotating screw rods (9) are connected to the inner walls of the high-definition camera (4) and the symmetrical assembling plates (8) in a threaded manner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222342363.6U CN218022167U (en) | 2022-09-05 | 2022-09-05 | Four-rotor unmanned aerial vehicle for inspection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222342363.6U CN218022167U (en) | 2022-09-05 | 2022-09-05 | Four-rotor unmanned aerial vehicle for inspection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218022167U true CN218022167U (en) | 2022-12-13 |
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ID=84353231
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222342363.6U Active CN218022167U (en) | 2022-09-05 | 2022-09-05 | Four-rotor unmanned aerial vehicle for inspection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218022167U (en) |
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2022
- 2022-09-05 CN CN202222342363.6U patent/CN218022167U/en active Active
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