CN211568303U - Unmanned aerial vehicle for circuit cruise detection - Google Patents
Unmanned aerial vehicle for circuit cruise detection Download PDFInfo
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- CN211568303U CN211568303U CN201922403305.8U CN201922403305U CN211568303U CN 211568303 U CN211568303 U CN 211568303U CN 201922403305 U CN201922403305 U CN 201922403305U CN 211568303 U CN211568303 U CN 211568303U
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- unmanned aerial
- aerial vehicle
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- detection
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Abstract
The utility model relates to an unmanned aerial vehicle detects technical field, discloses an unmanned aerial vehicle that is used for circuit to cruise and detects, include: the detection frame is of a frame structure; the supporting rod is arranged at the bottom of the detection frame and used for supporting the detection frame; the mounting plate is arranged on the support rod; the camera is arranged at one end of the detection frame; the wheel is used for being in sliding connection with an external overhead ground wire; the driving motor is fixedly arranged on the detection frame and used for driving the wheels to rotate; the flight subassembly sets up on the mounting panel for drive unmanned aerial vehicle and fly and make the wheel line on overhead earth connection. The unmanned aerial vehicle is driven by the flying assembly to fly to a position to be detected, wheels are lined on an external overhead ground wire, the wheels are driven by the driving motor to slide on the overhead ground wire, a current scene of the overhead ground wire is shot and recorded by the camera, the circuit condition is transmitted to the ground control console, and the cruising detection of the circuit is realized; the detection cost is reduced, and the horizontal balance of the unmanned aerial vehicle is stable.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle detects technical field, especially relates to an unmanned aerial vehicle that is used for circuit to cruise and detects.
Background
A drone is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can automatically land in the same way as a common aircraft landing process, and can also be recovered by a remote control parachute or a blocking net, so that the aircraft can be repeatedly used. Unmanned aerial vehicles are widely used for aerial reconnaissance, surveillance, communication, anti-dive, electronic interference and the like.
In the prior art, when high-voltage transmission towers and electric wires transmitted from power generation facilities to cities are inspected, an overhead ground wire may be damaged by lightning. The existing inspection method is to carry a person to the upper air by a helicopter and perform inspection by visual inspection, photography and the like. However, with this method of detection, helicopters and workers are at a greater risk of falling and are very costly.
Therefore, how to provide an unmanned aerial vehicle for circuit cruise detection becomes an urgent technical problem to be solved.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model lies in how to provide an unmanned aerial vehicle for circuit detection of cruising.
Therefore, according to the first aspect, the embodiment of the utility model discloses an unmanned aerial vehicle for circuit detection of cruising, include: the detection frame is of a frame structure; the supporting rod is arranged at the bottom of the detection frame, is fixedly connected with the detection frame and is used for supporting the detection frame; the mounting plate is arranged on the supporting rod and fixedly connected with the supporting rod; the camera is arranged at one end of the detection frame, is fixedly connected with the detection frame, and is used for shooting and recording the current scene of the overhead grounding wire and transmitting the circuit condition to a ground control console so as to perform cruise detection on the circuit; the wheel is used for being in sliding connection with an external overhead ground wire; the driving motor is fixedly arranged on the detection frame and used for driving the wheels to rotate so as to enable the detection frame to move along the direction of the external overhead ground wire; the flight subassembly set up in on the mounting panel for drive unmanned aerial vehicle and fly and make the wheel is being qualified for the next round of competitions in overhead earth connection.
The utility model discloses further set up to, the flight subassembly sets up to four, flight subassembly symmetric distribution in the both ends that the mounting panel is relative.
The utility model discloses further set up as, the flight subassembly includes: the flight rod is arranged on the mounting plate and is detachably connected with the mounting plate; the flight motor is arranged on the flight rod, is fixedly connected with the flight rod and is used for providing driving power for the flight assembly; flight screw, fixed connection in flight motor's output shaft for drive unmanned aerial vehicle flies.
The utility model discloses further set up to, flying motor is servo motor.
The utility model discloses further set up to, still include: and the power supply assembly is arranged on the mounting plate, is electrically connected with the driving motor and the flight assembly and is used for supplying electric energy to the driving motor and the flight assembly.
The utility model discloses further set up to, the power supply unit be for set up in the battery of mounting panel, the battery with mounting panel fixed connection.
The utility model discloses further set up to, the quantity of battery is four, and the symmetric distribution in the mounting panel.
The utility model discloses further set up to, wherein two the battery is used for providing the flight subassembly provides the electric energy, two in addition the battery is used for providing driving motor provides the electric energy.
The utility model discloses further set up to, the quantity of bracing piece is six, and symmetric distribution in the both sides of testing stand.
The utility model discloses further set up to, be located the test rack both sidesThe included angle between two adjacent support rods is 50o。
The utility model discloses following beneficial effect has: the flying assembly plays a flying role, drives the unmanned aerial vehicle to fly to a position to be detected through the flying assembly, enables the wheels to be wired on an external overhead ground wire, drives the wheels to slide on the overhead ground wire through the driving motor, shoots and records the current scene of the overhead ground wire through the camera, and transmits the circuit condition to the ground control console, so that the cruising detection of the circuit is realized; the detection cost is reduced, and the horizontal balance of the unmanned aerial vehicle is stable.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the technical solutions in the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic perspective view of an unmanned aerial vehicle for circuit cruise detection according to the present embodiment;
fig. 2 is an explosion structure diagram of the unmanned aerial vehicle for circuit cruise detection disclosed in the present embodiment.
Reference numerals: 1. a detection frame; 2. a support bar; 3. mounting a plate; 4. a camera; 5. a wheel; 6. a drive motor; 7. a flight assembly; 71. a flight bar; 72. a flying motor; 73. a flight propeller; 8. and a power supply assembly.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below 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.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; the two elements may be directly connected or indirectly connected through an intermediate medium, or may be communicated with each other inside the two elements, or may be wirelessly connected or wired connected. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
Furthermore, the technical features mentioned in the different embodiments of the invention described below can be combined with each other as long as they do not conflict with each other.
The embodiment of the utility model discloses an unmanned aerial vehicle for circuit detection of cruising, as shown in figure 1, include: the device comprises a detection frame 1, a support rod 2, a mounting plate 3, a camera 4, wheels 5, a driving motor 6 and a flight assembly 7, wherein the detection frame 1 is of a frame structure; the support rod 2 is arranged at the bottom of the detection frame 1, the support rod 2 is fixedly connected with the detection frame 1, and the support rod 2 is used for supporting the detection frame 1; the mounting plate 3 is arranged on the support rod 2, and the mounting plate 3 is fixedly connected with the support rod 2; the camera 4 is arranged at one end of the detection frame 1, the camera 4 is fixedly connected with the detection frame 1, and the camera 4 is used for shooting and recording the current scene of the overhead grounding wire and transmitting the circuit condition to a ground control console so as to perform cruise detection on the circuit; the wheel 5 is used for being in sliding connection with an external overhead ground wire; the driving motor 6 is fixedly arranged on the detection frame 1, and the driving motor 6 is used for driving the wheels 5 to rotate so as to enable the detection frame 1 to move along the direction of the external overhead ground wire; flight subassembly 7 sets up on mounting panel 3, and flight subassembly 7 is used for driving unmanned aerial vehicle to fly and makes wheel 5 be on line in overhead earth connection. In the specific implementation process, the driving motor 6 is a servo motor; the number of the wheels 5 is 3, and the wheels are sequentially arranged on the detection frame 1.
It should be noted that the flying assembly 7 takes off and acts, the flying assembly 7 drives the unmanned aerial vehicle to fly to a position to be detected, so that the wheels 5 are wired on an external overhead ground wire, the driving motor 6 drives the wheels 5 to slide on the overhead ground wire, the current scene of the overhead ground wire is shot and recorded through the camera 4, and the circuit condition is transmitted to the ground control console, so that the cruising detection of the circuit is realized; the detection cost is reduced, and the horizontal balance of the unmanned aerial vehicle is stable.
It should also be noted that the flying assembly 7 can be controlled by radio.
As shown in fig. 1, the number of the flying assemblies 7 is four, and the flying assemblies 7 are symmetrically distributed at two opposite ends of the mounting plate 3.
It should be noted that, four flight assemblies 7 distribute in unmanned aerial vehicle's four corners, and through flight assembly 7's flight effect, drive unmanned aerial vehicle and fly, conveniently improve unmanned aerial vehicle's flight stability.
As shown in fig. 1 and 2, the flying assembly 7 includes: flight bar 71, flight motor 72 and flight propeller 73, wherein: the flight bar 71 is arranged on the mounting plate 3, and the flight bar 71 is detachably connected with the mounting plate 3; the flying motor 72 is arranged on the flying rod 71, the flying motor 72 is fixedly connected with the flying rod 71, and the flying motor 72 is used for providing driving power for the flying assembly 7; flight screw 73 fixed connection is in flight motor 72's output shaft, and flight screw 73 is used for driving unmanned aerial vehicle and flies.
It should be noted that the flight motor 72 plays a driving role, and drives the flight propeller 73 to rotate, and since the flight rod 71 is arranged on the mounting plate 3, the unmanned aerial vehicle is driven to fly. When wheel 5 is being lined up on outside overhead earth connection, the unmanned aerial vehicle that this application discloses only consumes driving motor 6, and flight motor 72 is out of work, divide into flight and two systems of inspection with the battery, saves the electric quantity, can prolong inspection operating time.
As shown in fig. 2, the flying motor 72 is a servo motor.
As shown in fig. 1, the method further includes: and the power supply assembly 8 is arranged on the mounting plate 3, is electrically connected with the driving motor 6 and the flying assembly 7, and is used for providing electric energy for the driving motor 6 and the flying assembly 7.
As shown in fig. 1, the power supply assembly 8 is a battery disposed on the mounting plate 3, and the battery is fixedly connected to the mounting plate 3.
It should be noted that, battery fixed connection is on mounting panel 3, and is located the bottom of testing stand 1, can improve unmanned aerial vehicle's horizontal stability.
As shown in fig. 1, the number of the batteries is four, and the batteries are symmetrically distributed on the mounting plate 3. In a specific implementation process, the capacity of the battery can be changed according to the field requirement.
As shown in fig. 1, two of the batteries are used to power the flight assembly 7 and the other two batteries are used to power the drive motor 6.
It should be noted that the four batteries respectively provide electric energy for the flight assembly 7 and the driving motor 6, so that independent power supply is realized, the operation reliability of the unmanned aerial vehicle is improved, and the stability of the unmanned aerial vehicle system is enhanced.
As shown in fig. 1, the number of the support rods 2 is six, and the support rods are symmetrically distributed on two sides of the detection frame 1.
The working principle is as follows: the flying assembly 7 takes off and acts, the flying motor 72 drives the flying propeller 73 to rotate, so that the unmanned aerial vehicle starts flying, the unmanned aerial vehicle is driven to fly to a position to be detected, the wheels 5 are wired on the external overhead ground wire, the driving motor 6 drives the wheels 5 to slide on the overhead ground wire, the current scene of the overhead ground wire is shot and recorded through the camera 4, the circuit condition is transmitted to the ground control console, and the cruise detection of the circuit is realized; the detection cost is reduced, and the horizontal balance of the unmanned aerial vehicle is stable.
It should be understood that the above examples are only for clarity of illustration and are not intended to limit the embodiments. Other variations and modifications will be apparent to persons skilled in the art in light of the above description. And are neither required nor exhaustive of all embodiments. And obvious variations or modifications can be made without departing from the scope of the invention.
Claims (9)
1. An unmanned aerial vehicle for circuit cruise detection, comprising:
the detection frame (1) is of a frame structure;
the supporting rod (2) is arranged at the bottom of the detection frame (1), is fixedly connected with the detection frame (1) and is used for supporting the detection frame (1);
the mounting plate (3) is arranged on the supporting rod (2) and is fixedly connected with the supporting rod (2);
the camera (4) is arranged at one end of the detection frame (1), is fixedly connected with the detection frame (1), and is used for shooting and recording the current scene of the overhead grounding wire and transmitting the circuit condition to a ground control console so as to perform cruise detection on the circuit;
the wheel (5) is used for being in sliding connection with an external overhead ground wire;
the driving motor (6) is fixedly arranged on the detection frame (1) and used for driving the wheels (5) to rotate so as to enable the detection frame (1) to move along the direction of an external overhead ground wire;
flight subassembly (7), set up in on mounting panel (3) for drive unmanned aerial vehicle and fly and make wheel (5) are being qualified for the next round of competitions in overhead earth connection.
2. Unmanned aerial vehicle for circuit cruise detection according to claim 1, wherein said flying assemblies (7) are provided in four, said flying assemblies (7) being symmetrically distributed at opposite ends of said mounting plate (3).
3. The drone for circuit cruise detection according to claim 1 or 2, characterized in that said flying assembly (7) comprises:
the flight rod (71) is arranged on the mounting plate (3) and is detachably connected with the mounting plate (3);
the flying motor (72) is arranged on the flying rod (71), is fixedly connected with the flying rod (71), and is used for providing driving power for the flying assembly (7);
flight screw (73), fixed connection in the output shaft of flying motor (72) for drive unmanned aerial vehicle and fly.
4. Unmanned aerial vehicle for circuit cruise detection according to claim 3, characterized in that said flying motor (72) is a servo motor.
5. The drone for circuit cruise detection according to claim 1, further comprising:
the power supply assembly (8) is arranged on the mounting plate (3), is electrically connected with the driving motor (6) and the flying assembly (7) and is used for providing electric energy for the driving motor (6) and the flying assembly (7).
6. Unmanned aerial vehicle for circuit cruise detection according to claim 5, characterized in that, power supply component (8) is a battery provided to the mounting plate (3), the battery with mounting plate (3) fixed connection.
7. Unmanned aerial vehicle for circuit cruise detection according to claim 6, characterized in that said batteries are four in number and symmetrically distributed on said mounting plate (3).
8. Unmanned aerial vehicle for circuit cruise detection according to claim 7, wherein two of said batteries are used for supplying electric energy to said flying assembly (7) and the other two are used for supplying electric energy to said driving motor (6).
9. Unmanned aerial vehicle for circuit cruise detection according to claim 1, characterized in that the number of said support bars (2) is six and symmetrically distributed on both sides of said detection frame (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922403305.8U CN211568303U (en) | 2019-12-27 | 2019-12-27 | Unmanned aerial vehicle for circuit cruise detection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922403305.8U CN211568303U (en) | 2019-12-27 | 2019-12-27 | Unmanned aerial vehicle for circuit cruise detection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211568303U true CN211568303U (en) | 2020-09-25 |
Family
ID=72551641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922403305.8U Expired - Fee Related CN211568303U (en) | 2019-12-27 | 2019-12-27 | Unmanned aerial vehicle for circuit cruise detection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211568303U (en) |
-
2019
- 2019-12-27 CN CN201922403305.8U patent/CN211568303U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200925 Termination date: 20211227 |