CN216401744U - Prevent circuit of striking and patrol and examine unmanned aerial vehicle - Google Patents

Prevent circuit of striking and patrol and examine unmanned aerial vehicle Download PDF

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Publication number
CN216401744U
CN216401744U CN202122428557.3U CN202122428557U CN216401744U CN 216401744 U CN216401744 U CN 216401744U CN 202122428557 U CN202122428557 U CN 202122428557U CN 216401744 U CN216401744 U CN 216401744U
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China
Prior art keywords
unmanned aerial
aerial vehicle
frame
buckling plate
rack
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CN202122428557.3U
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Chinese (zh)
Inventor
罗延金
陈明
房俊杰
周关清
孔翔凯
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Dali Power Supply Bureau of Yunnan Power Grid Co Ltd
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Dali Power Supply Bureau of Yunnan Power Grid Co Ltd
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Abstract

The utility model provides an impact-preventing line inspection unmanned aerial vehicle which comprises a rack, a buoyancy impeller and a thrust impeller, wherein the buoyancy impeller and the thrust impeller are arranged on two sides of the rack, a support is arranged at the bottom of the rack, a camera is arranged at the front end of the rack, LED lamps for auxiliary lighting are arranged on two sides of the rack, and a detection assembly for detecting a line is arranged at the bottom of the rack. Firstly, can reduce the installation degree of difficulty of determine module, thereby the convenience that the improvement device used, secondly set up the buckling plate through the bottom at the mount pad, and set up drive gear in one side of buckling plate, can be in the same place unmanned aerial vehicle and circuit zonulae occludens, the stability that unmanned aerial vehicle detected has not only been improved, unmanned aerial vehicle and circuit bump can also be placed to the while, the security that the improvement device used from this, thereby solved unmanned aerial vehicle and examined time measuring to the circuit, easy and circuit bump and the unstable problem of circuit detection.

Description

Prevent circuit of striking and patrol and examine unmanned aerial vehicle
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a collision-preventing line inspection unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "unmanned aerial vehicle" in english and abbreviated as "UAV", is an unmanned aircraft operated by a radio remote control device and a self-contained program control device, or is autonomously operated by an onboard computer, either completely or intermittently;
the unmanned aerial vehicle is applied to various industries of life, such as dangerous high-altitude operation and cable line detection, and the unmanned aerial vehicle can only be used for detecting lines due to the fact that cables are high in position and cannot be used for borrowing force;
at present, unmanned aerial vehicle is patrolled and examined to earlier current circuit when using, because the cable is under the effect of self gravity, can take place the bending of certain degree, therefore the shape of cable is not fixed, and examine time measuring at unmanned aerial vehicle to the cable, not only need the staff to judge the position relation between unmanned aerial vehicle and the circuit according to self experience, still need continuous adjustment unmanned aerial vehicle's the way of going forward simultaneously, so examine time measuring, unmanned aerial vehicle not only causes the damage to the circuit easily, still can't keep the circuit that detects simultaneously for stability, for this, we have proposed a circuit that prevents the striking and have patrolled and examined unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Aiming at the defects of the prior art, the utility model provides the line inspection unmanned aerial vehicle capable of preventing collision, so that the problems that the unmanned aerial vehicle is easy to collide with a line and the line detection is unstable when the unmanned aerial vehicle detects the line are solved.
(II) technical scheme
In order to achieve the purpose, the utility model is realized by the following technical scheme:
the utility model provides an unmanned aerial vehicle is patrolled and examined to circuit that prevents striking, this line patrol and examine unmanned aerial vehicle contain the frame and install buoyancy impeller and the thrust impeller in the frame both sides, and there is the support bottom of frame, the camera is installed to the front end of frame, and the both sides of frame all are provided with the LED lamp that is used for auxiliary lighting to install the determine module that is used for carrying out the detection to the circuit in the bottom of frame, wherein, determine module contains:
the mounting seat is mounted at the bottom of the rack;
the cross section of the buckling plate is arc-shaped, the buckling plate is movably mounted at the bottom of the mounting seat through a bearing, a transmission gear for driving the buckling plate to rotate is mounted inside the mounting seat, and a clamping tooth mounted outside the buckling plate is meshed with the transmission gear; and
the detector is arranged on the inner side of the buckling plate and used for detecting the surface of the line.
Furthermore, the number of the buoyancy impellers is four, and two groups of buoyancy impellers are arranged on two sides of the rack respectively and used for providing upward buoyancy for the rack.
Furthermore, the number of the thrust impellers is two, and the two thrust impellers are respectively positioned on two sides of the rack and used for providing forward thrust for the rack.
Furthermore, the top of mount pad is installed the butt joint card strip that the cross section is "T" font, and butt joint card strip and the connecting plate joint of installing in the frame bottom.
Furthermore, a self-locking motor is installed inside the installation seat, and an output shaft of the self-locking motor is connected with the transmission gear.
Further, the detector includes one or more of an ammeter, a positioner, a pressure sensor, and a temperature sensor.
Further, two sets of arc-shaped electrode plates are installed at the bottom of the installation seat, the electrode plates are correspondingly attached to two sets of conductive bars installed on the outer side of the buckling plate one by one, the two sets of electrode plates are connected with battery electrodes installed inside the buckling plate through leads, and the two sets of conductive bars are connected with the positive electrode and the negative electrode of the detector through leads.
Furthermore, the inner wall of the buckling plate is provided with a sliding groove, and the detector is arranged in the sliding groove.
Furthermore, the bottom of the mounting seat is provided with two groups of arc-shaped blocking pieces, the blocking pieces are respectively connected with the ground of the mounting seat, the buckling plate is located between the blocking pieces and the mounting seat, and the detector is located in a gap between the two groups of blocking pieces.
(III) advantageous effects
The utility model provides an impact-preventing line inspection unmanned aerial vehicle, which comprises a rack, and a buoyancy impeller and a thrust impeller which are arranged on two sides of the rack, wherein the bottom of the rack is provided with a support, the front end of the rack is provided with a camera, two sides of the rack are respectively provided with an LED lamp for auxiliary illumination, and the bottom of the rack is provided with a detection assembly for detecting a line, wherein the detection assembly comprises: the mounting seat is mounted at the bottom of the rack; the cross section of the buckling plate is arc-shaped, the buckling plate is movably mounted at the bottom of the mounting seat through a bearing, a transmission gear for driving the buckling plate to rotate is mounted inside the mounting seat, and a clamping tooth mounted outside the buckling plate is meshed with the transmission gear; and the detector is arranged on the inner side of the buckling plate and is used for detecting the surface of the line. Above structure, firstly, can reduce the installation degree of difficulty of determine module, thereby improve the convenience that the device used, secondly, set up the buckling plate through the bottom at the mount pad, and set up drive gear in one side of buckling plate, can be in the same place unmanned aerial vehicle and circuit zonulae occludens, unmanned aerial vehicle detection's stability has not only been improved, unmanned aerial vehicle and circuit bump can also be placed to the while, improve the security that the device used from this, thereby solved unmanned aerial vehicle and examined time measuring to the circuit, the easy unstable problem of circuit bump and circuit detection with the circuit.
Drawings
The foregoing description is only an overview of the technical solutions of the present invention, and in order to make the technical solutions of the present invention more clearly understood and to implement them in accordance with the contents of the description, the following detailed description is given with reference to the preferred embodiments of the present invention and the accompanying drawings.
FIG. 1 is a schematic view of an overall structure of the cable tray according to one embodiment;
FIG. 2 is a second schematic view of the cable tray according to the first embodiment;
FIG. 3 is a third schematic view illustrating an overall structure of the cable tray according to the first embodiment;
FIG. 4 is a block diagram of a detection module according to one embodiment;
FIG. 5 is a cross-sectional view of a detection assembly according to one embodiment;
FIG. 6 is a schematic view of a fastener of one embodiment;
FIG. 7 is a partial cross-sectional view of a mount according to an embodiment.
Illustration of the drawings: 1. a frame; 2. a buoyant impeller; 3. a thrust impeller; 4. a camera; 5. a support; 6. a detection component; 61. a mounting seat; 62. butting the clamping strips; 63. buckling the plate; 64. a detector; 65. a transmission gear; 66. clamping teeth; 67. a conductive strip; 68. a baffle plate; 7. a connecting plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention. In addition, for the convenience of description, the terms "upper", "lower", "left" and "right" are used to refer to the same direction as the upper, lower, left, right, etc. of the drawings, and the terms "first", "second", etc. are used for descriptive distinction and have no special meaning.
Aiming at the problems in the prior art, the utility model provides a line inspection unmanned aerial vehicle for preventing collision, which comprises a frame, a buoyancy impeller and a thrust impeller, wherein the buoyancy impeller and the thrust impeller are arranged on two sides of the frame, the bottom of the frame is provided with a bracket, the front end of the frame is provided with a camera, two sides of the frame are provided with LED lamps for auxiliary illumination, and the bottom of the frame is provided with a detection component for detecting a line, wherein,
1-detection Assembly
The mounting seat is mounted at the bottom of the rack;
the cross section of the buckling plate is arc-shaped, the buckling plate is movably mounted at the bottom of the mounting seat through a bearing, a transmission gear for driving the buckling plate to rotate is mounted inside the mounting seat, and a clamping tooth mounted outside the buckling plate is meshed with the transmission gear; and
the detector is arranged on the inner side of the buckling plate and used for detecting the surface of the line.
Furthermore, the number of the buoyancy impellers is four, and two groups of buoyancy impellers are arranged on two sides of the rack respectively and used for providing upward buoyancy for the rack.
In a specific application scene, the buoyancy impellers are arranged on the two sides of the rack, so that upward buoyancy can be provided for the rack, and the rack can move in the vertical direction.
Furthermore, the number of the thrust impellers is two, and the two thrust impellers are respectively positioned on two sides of the rack and used for providing forward thrust for the rack.
In concrete application scene, through being located the both sides of frame respectively with two sets of thrust impellers, can be used for providing the thrust that advances for the frame, make things convenient for the determine module when detecting the circuit spare, can remove along the cable direction, can also keep the cable simultaneously and unmanned aerial vehicle between the position, improve the precision that detects.
Furthermore, a self-locking motor is installed inside the installation seat, and an output shaft of the self-locking motor is connected with the transmission gear.
In a specific application scene, the self-locking motor is arranged in the mounting base, an output shaft of the self-locking motor is connected with the transmission gear, the self-locking motor serves as the transmission gear, and the buckling plate meshed with the transmission gear rotates together, so that the detector arranged on the inner side of the buckling plate detects a circuit.
Further, the detector comprises one or more of an ammeter, a positioner, a pressure sensor, and a temperature sensor,
in a specific application scene, when the detector is set as an ammeter, whether the line leaks electricity or not can be detected; when the detector is set as a locator, the damaged positions of the unmanned aerial vehicle and the cable can be detected, and subsequent repair is facilitated; when the detector is arranged as a pressure sensor, the deformation of the line can be detected (because the position of the installation seat and the cable is fixed, when the pressure sensor is changed, the surface of the cable is irregular, namely the deformation is generated); when the detector is provided as a temperature sensor, it is possible to detect whether the line is damaged by heat generation.
Further, two sets of arc-shaped electrode plates are installed at the bottom of the installation seat, the electrode plates are correspondingly attached to two sets of conductive bars installed on the outer side of the buckling plate one by one, the two sets of electrode plates are connected with battery electrodes installed inside the buckling plate through leads, and the two sets of conductive bars are connected with the positive electrode and the negative electrode of the detector through leads.
In the concrete application scene, through install two sets of curved plate electrodes that are in the bottom of mount pad, and the plate electrode laminates with two sets of conducting bars one-to-one that install in the buckled plate outside, can guarantee that the battery is all the time for installing the power supply at buckled plate inner wall side detector, improves the stability of power supply.
Furthermore, the inner wall of the buckling plate is provided with a sliding groove, and the detector is arranged in the sliding groove.
In the concrete application scene, through having seted up the spout at the inner wall of buckling board, and the detector is installed in the spout, can prevent that the buckling board when rotatory, the detector from taking place the friction with the outer wall of cable.
Furthermore, the bottom of the mounting seat is provided with two groups of arc-shaped blocking pieces, the blocking pieces are respectively connected with the ground of the mounting seat, the buckling plate is located between the blocking pieces and the mounting seat, and the detector is located in a gap between the two groups of blocking pieces.
In the specific application scene, through be provided with two sets of curved separation blades that are in mount pad bottom, the mount pad bottom is provided with two sets of curved separation blades that are, can be spacing the buckling plate between separation blade and mount pad through the separation blade, avoids mount pad and buckling plate separation, improves the security that the buckling plate used.
When the unmanned aerial vehicle is used, the unmanned aerial vehicle moves above a cable, the mounting seat arranged at the bottom of the rack is sleeved outside the cable, then a self-locking motor arranged inside the mounting seat is controlled to be electrified to drive the transmission gear to rotate, and the transmission gear is correspondingly meshed with the latch outside the buckling plate, so that the buckling plate can be driven to rotate when the transmission gear rotates, the buckling plate is buckled outside the cable, the cable is fixed between the buckling plate and the mounting seat to form a channel cylinder, the stability of the space between the unmanned aerial vehicle and the cable can be ensured, then the unmanned aerial vehicle can be driven by the thrust impeller, the detector arranged on the inner side of the buckling plate can be used for detecting the outer wall of the cable, and when the detector is set as an ammeter, whether electric leakage occurs in a circuit can be detected; when the detector is set as a locator, the damaged positions of the unmanned aerial vehicle and the cable can be detected, and subsequent repair is facilitated; when the detector is arranged as a pressure sensor, the deformation of the line can be detected (because the position of the installation seat and the cable is fixed, when the pressure sensor is changed, the surface of the cable is irregular, namely the deformation is generated); when the detector is provided as a temperature sensor, it is possible to detect whether the line is damaged by heat generation.
When the surface positions of the cable need to be detected, the self-locking motor can be controlled to drive the buckling plate and the detector to rotate around the cable, so that the positions of the cable are detected, and the detection comprehensiveness is improved.
2-connecting plate
The top of mount pad is installed the butt joint card strip of transversal personally submitting "T" font, and butt joint card strip and the connecting plate joint of installing in the frame bottom.
In a specific application scene, the butt joint clamping strip with the cross section in the T shape is installed at the top of the installation seat and is clamped with the connecting plate installed at the bottom of the rack, so that the installation difficulty of the detection assembly can be reduced, the use convenience of the device is improved, and the device is convenient to install and repair.
When the detection assembly is installed, the connecting plate (the bottom of the connecting plate is provided with a clamping groove with a T-shaped cross section) is installed at the bottom of the rack, then the butt joint clamping strip at the top of the installation seat can be manually inserted into the clamping groove to form the shape shown in the figure, and finally the butt joint clamping strip and the clamping groove are connected together by using a bolt.
The first embodiment is as follows:
based on the above conception, as shown in fig. 1 to 6, the line inspection unmanned aerial vehicle for preventing collision provided by the utility model comprises a frame 1, and a buoyancy impeller 2 and a thrust impeller 3 which are installed on two sides of the frame 1, wherein a support 5 is arranged at the bottom of the frame 1, a camera 4 is installed at the front end of the frame 1, LED lamps for auxiliary illumination are arranged on two sides of the frame 1, and a detection assembly 6 for detecting a line is installed at the bottom of the frame 1, wherein the detection assembly 6 comprises:
the mounting seat 61, the mounting seat 61 is mounted at the bottom of the frame 1;
the cross section of the buckling plate 63 is arc-shaped, the buckling plate 63 is movably mounted at the bottom of the mounting seat 61 through a bearing, a transmission gear 65 for driving the buckling plate 63 to rotate is mounted inside the mounting seat 61, and a clamping tooth 66 mounted outside the buckling plate 63 is meshed with the transmission gear 65; and
and the detector 64 is installed on the inner side of the buckling plate 63 and used for detecting the surface of the line.
Further, as shown in fig. 1, the number of the buoyancy impellers 2 is four, and two groups are respectively arranged on two sides of the rack 1 to provide upward buoyancy for the rack 1.
Further, as shown in fig. 1, the number of the thrust impellers 3 is two, and the two sets of thrust impellers 3 are respectively located on two sides of the rack 1 and are used for providing forward thrust for the rack 1.
Further, as shown in fig. 2 and fig. 3, a butt joint clamping strip 62 with a cross section being "T" shaped is installed at the top of the installation seat 61, and the butt joint clamping strip 62 is clamped with the connection plate 7 installed at the bottom of the rack 1.
Further, as shown in fig. 4, a self-locking motor is installed inside the installation base 61, and an output shaft of the self-locking motor is connected with the transmission gear 65.
Further, the detector 64 includes one or more of an ammeter, a positioner, a pressure sensor, and a temperature sensor.
Further, as shown in fig. 5 and 6, two sets of arc-shaped electrode plates are mounted at the bottom of the mounting seat 61, and the electrode plates are correspondingly attached to two sets of conductive bars 67 mounted at the outer side of the fastening plate 63, the two sets of electrode plates are connected to the battery electrodes mounted inside the fastening plate 63 through wires, and the two sets of conductive bars 67 are connected to the positive and negative electrodes of the detector 64 through wires.
Further, a sliding groove is formed in the inner wall of the fastening plate 63, and the detector 64 is installed inside the sliding groove.
Further, as shown in fig. 4 and 7, two sets of arc-shaped blocking pieces 68 are disposed at the bottom of the mounting base 61, the blocking pieces 68 are respectively connected with the ground of the mounting base 61, the fastening plate 63 is located between the blocking pieces 68 and the mounting base 61, and the detector 64 is located in a gap between the two sets of blocking pieces 68.
Those skilled in the art will appreciate that the drawings are merely schematic representations of one preferred implementation scenario and that the blocks or flow diagrams in the drawings are not necessarily required to implement the present invention.
Those skilled in the art will appreciate that the modules in the devices in the implementation scenario may be distributed in the devices in the implementation scenario according to the description of the implementation scenario, or may be located in one or more devices different from the present implementation scenario with corresponding changes. The modules of the implementation scenario may be combined into one module, or may be further split into a plurality of sub-modules.
The above disclosure is only a concrete implementation scenario of the present invention, however, the present invention is not limited to this, and any changes that can be made by those skilled in the art should fall within the protection scope of the present invention.

Claims (9)

1. The utility model provides an unmanned aerial vehicle is patrolled and examined to circuit that prevents striking, its characterized in that, this unmanned aerial vehicle is patrolled and examined to line contain frame (1) and install buoyancy impeller (2) and thrust impeller (3) in frame (1) both sides, and there is support (5) bottom of frame (1), camera (4) are installed to the front end of frame (1), and the both sides of frame (1) all are provided with the LED lamp that is used for auxiliary lighting to install in the bottom of frame (1) and be used for carrying out the determine module (6) that detect to the circuit, wherein, determine module (6) contain:
the mounting seat (61), the mounting seat (61) is mounted at the bottom of the frame (1);
the cross section of the buckling plate (63) is arc-shaped, the buckling plate (63) is movably mounted at the bottom of the mounting seat (61) through a bearing, a transmission gear (65) used for driving the buckling plate (63) to rotate is mounted inside the mounting seat (61), and a clamping tooth (66) mounted outside the buckling plate (63) is meshed with the transmission gear (65); and
the detector (64), the detector (64) is installed at the inner side of the buckling plate (63) and is used for detecting the surface of the line.
2. The collision-proof line inspection unmanned aerial vehicle according to claim 1, wherein the number of the buoyancy impellers (2) is four, and two sets of buoyancy impellers are respectively arranged on two sides of the frame (1) to provide upward buoyancy for the frame (1).
3. The collision-proof line inspection unmanned aerial vehicle according to claim 1, wherein the number of the thrust impellers (3) is two, and the two thrust impellers (3) are respectively located at two sides of the frame (1) and used for providing forward thrust for the frame (1).
4. The impact-proof line inspection unmanned aerial vehicle according to claim 1, wherein a butt joint clamping strip (62) with a T-shaped cross section is installed at the top of the installation seat (61), and the butt joint clamping strip (62) is clamped with a connecting plate (7) installed at the bottom of the rack (1).
5. The line inspection unmanned aerial vehicle of claim 1, wherein the mount base (61) is internally provided with a self-locking motor, and an output shaft of the self-locking motor is connected with the transmission gear (65).
6. The crash-proof line inspection drone according to claim 1, wherein the detector (64) includes one or more of a current meter, a locator, a pressure sensor, and a temperature sensor.
7. The unmanned line inspection according to claim 1, wherein two sets of arc-shaped electrode plates are mounted at the bottom of the mounting seat (61), and the electrode plates are correspondingly attached to two sets of conductive bars (67) mounted on the outer side of the buckling plate (63), the two sets of electrode plates are connected to the battery electrodes mounted inside the buckling plate (63) through wires, and the two sets of conductive bars (67) are connected to the positive and negative electrodes of the detector (64) through wires.
8. The line inspection unmanned aerial vehicle of claim 1, wherein the inner wall of the buckling plate (63) is provided with a sliding groove, and the detector (64) is mounted inside the sliding groove.
9. The impact-preventing line inspection unmanned aerial vehicle according to claim 1, wherein two sets of arc-shaped blocking pieces (68) are arranged at the bottom of the mounting base (61), the blocking pieces (68) are respectively connected with the ground of the mounting base (61), the buckling plate (63) is located between the blocking pieces (68) and the mounting base (61), and the detector (64) is located in a gap between the two sets of blocking pieces (68).
CN202122428557.3U 2021-10-09 2021-10-09 Prevent circuit of striking and patrol and examine unmanned aerial vehicle Active CN216401744U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202122428557.3U CN216401744U (en) 2021-10-09 2021-10-09 Prevent circuit of striking and patrol and examine unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122428557.3U CN216401744U (en) 2021-10-09 2021-10-09 Prevent circuit of striking and patrol and examine unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
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CN202122428557.3U Active CN216401744U (en) 2021-10-09 2021-10-09 Prevent circuit of striking and patrol and examine unmanned aerial vehicle

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117382945A (en) * 2023-12-06 2024-01-12 山东黄金电力有限公司 Unmanned aerial vehicle is patrolled and examined to electric power

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117382945A (en) * 2023-12-06 2024-01-12 山东黄金电力有限公司 Unmanned aerial vehicle is patrolled and examined to electric power
CN117382945B (en) * 2023-12-06 2024-02-23 山东黄金电力有限公司 Unmanned aerial vehicle is patrolled and examined to electric power

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