CN112498685A - Aerial supplementary wire rope handling equipment - Google Patents
Aerial supplementary wire rope handling equipment Download PDFInfo
- Publication number
- CN112498685A CN112498685A CN202011331055.2A CN202011331055A CN112498685A CN 112498685 A CN112498685 A CN 112498685A CN 202011331055 A CN202011331055 A CN 202011331055A CN 112498685 A CN112498685 A CN 112498685A
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- CN
- China
- Prior art keywords
- rope
- clamping jaw
- half shell
- seat
- travel switch
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Traffic Control Systems (AREA)
- Electric Cable Installation (AREA)
Abstract
An aerial auxiliary stringing device. The aerial auxiliary rope threading equipment is simple in structure, convenient to operate and capable of improving working efficiency. Including unmanned aerial vehicle, still including flexible arm and rope socket, flexible arm is established on unmanned aerial vehicle, the rope socket is used for connecting the wire rope, the connection can be dismantled on flexible arm to the rope socket. The rope seat is provided with an embedded block, the telescopic arm is provided with an embedded groove, and the embedded block is used for being connected in the embedded groove. The rope seat is characterized by further comprising a linear driver, wherein the linear driver is arranged on the telescopic arm and used for pushing the rope seat. The laser radar, the travel switch A, the travel switch B and the electromagnetic relay are connected with the rope threading device control unit. The telescopic arm is located at the top or the bottom of the unmanned aerial vehicle. The invention has convenient processing and reliable operation.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to aerial auxiliary rope threading equipment.
Background
In recent years, the unmanned aerial vehicle technology is rapidly developed, and the unmanned aerial vehicle is introduced to operate in the construction process of rope unfolding. Rope exhibition is usually aerial operation, and widely appears in many application scenarios such as high altitude rescue, electric power maintenance, outdoor exhibition, road and bridge engineering, mountain body development.
In the prior art, a rope is usually buckled on an unmanned aerial vehicle, and then a constructor ascends to cooperate and manually thread the rope and then continues the next threading operation; the method requires the cooperation of ascending a height of constructors, has high labor intensity, has potential safety hazard in ascending operation and has low working efficiency.
Disclosure of Invention
Aiming at the problems, the invention provides the aerial auxiliary rope threading equipment which is simple in structure, convenient to operate and capable of improving the working efficiency.
The technical scheme of the invention is as follows: including unmanned aerial vehicle, still including flexible arm and rope socket, flexible arm is established on unmanned aerial vehicle, the rope socket is used for connecting the wire rope, the connection can be dismantled on flexible arm to the rope socket.
The rope seat is provided with an embedded block, the telescopic arm is provided with an embedded groove, and the embedded block is used for being connected in the embedded groove.
The rope seat is characterized by further comprising a linear driver, wherein the linear driver is arranged on the telescopic arm and used for pushing the rope seat.
The device also comprises a controller, a laser radar and a clamping jaw, wherein the clamping jaw is arranged on the telescopic arm;
the clamping jaw is two enclosed semi-rings, a travel switch A is arranged on the inner side of the middle of the clamping jaw, and the travel switch A is triggered when the clamping jaw is closed;
the clamping jaw is internally provided with a pair of hemispherical rope seat shells, namely a first half shell and a second half shell, the rope seat shells are internally provided with a pair of electromagnetic relays, one electromagnetic relay is positioned in the first half shell, the other electromagnetic relay is positioned in the second half shell, and the electromagnetic relays are used for attracting the rope seat to the rope seat shells on the same side; travel switches B are arranged in the first half shell and the second half shell, and when the rope seat is sucked on one side of the rope seat shell, the travel switches B on the same side are triggered;
the laser radar, the travel switch A, the travel switch B and the electromagnetic relay are connected with the rope threading device control unit.
The telescopic arm is located at the top or the bottom of the unmanned aerial vehicle.
In the work of the unmanned aerial vehicle, the rope is placed on the rope seat, the rope seat is connected to the telescopic arm, the unmanned aerial vehicle is lifted to the position of the high-altitude hanging ring, the rope seat with the rope penetrates into the hanging ring, and the rope can reliably penetrate through the hanging ring and can reliably fall under the action of the rope seat.
The invention has convenient processing and reliable operation.
Drawings
Figure 1 is a schematic structural view of a first embodiment of the present invention,
figure 2 is a schematic diagram of the structure of the preferred embodiment of figure 1,
figure 3 is a schematic structural view of a second embodiment of the present invention,
fig. 4 is a schematic view of the connection structure of the rope holder and the clamping jaw.
In the figure, 1 is a telescopic arm, 2 is a rope socket, 3 is a threading rope, 4 is an insert block, 5 is an insert groove, 6 is a linear driver, 7 is a laser radar, 8 is a clamping jaw, 81 is a travel switch A, 82 is a rope socket shell, 821 is a half shell I, 822 is a half shell II, 83 is an electromagnetic relay, and 84 is a travel switch B.
Detailed Description
The unmanned aerial vehicle comprises an unmanned aerial vehicle, and further comprises a telescopic arm 1 and a rope seat 2, wherein the telescopic arm 1 is arranged on the unmanned aerial vehicle, the rope seat 2 is used for being connected with a rope 3, and the rope seat is detachably connected to the telescopic arm.
In the work of the unmanned aerial vehicle, the rope is placed on the rope seat, the rope seat is connected to the telescopic arm, the unmanned aerial vehicle is lifted to the position of the high-altitude hanging ring, the rope seat with the rope penetrates into the hanging ring, and the rope can reliably penetrate through the hanging ring and can reliably fall under the action of the rope seat. The telescopic arm can be remotely controlled to perform telescopic action.
The rope seat is provided with an embedded block 4, the telescopic arm is provided with an embedded groove 5, and the embedded block is used for being connected in the embedded groove.
The first embodiment of the present invention is: the threading rope directly penetrates from the middle of the hanging ring under the action of the telescopic arm, and at the moment, the telescopic arm faces the hanging hole;
drive flexible arm through unmanned aerial vehicle and stretch into the rope socket in the rings, flexible arm retraction action, the rope socket breaks away from in the caulking groove under the resistance of rings for the abaculus, and the automatic whereabouts of rope socket.
The rope seat further comprises a linear driver 6, the linear driver is arranged on the telescopic arm, and the linear driver is used for pushing the rope seat.
Therefore, the rope seat can be reliably pushed through the action of the linear driver, and the rope seat is convenient and reliable. The linear actuator is a conventional device such as an electric push rod, an air cylinder, a hydraulic cylinder, etc. The telescopic arm and the linear actuator can be operated remotely.
The device also comprises a controller 7, a laser radar 8 and a clamping jaw, wherein the clamping jaw is arranged on the telescopic arm;
the clamping jaw is two enclosed half rings, a travel switch A81 is arranged on the inner side of the middle of the clamping jaw, and the travel switch A81 is triggered when the clamping jaw is closed;
the clamping jaw is internally provided with a pair of hemispherical rope socket shells 82, namely a half shell I821 and a half shell II 822, the rope socket shells are internally provided with a pair of electromagnetic relays 83, one electromagnetic relay is positioned in the half shell I, the other electromagnetic relay is positioned in the half shell II, and the electromagnetic relays 83 are used for attracting the rope socket to the rope socket shells on the same side; travel switches B84 are arranged in the half shell I and the half shell II, and when the rope seat is sucked on one side of the rope seat shell, the travel switches B on the same side are triggered;
the laser radar, the travel switch A, the travel switch B and the electromagnetic relay are connected with the rope threading device control unit.
The second embodiment of the present invention is: the rope penetrates from the middle of the hanging ring under the action of the clamping jaw;
when the laser radar detects the lifting ring (at the moment, the telescopic arm is positioned on one side of the lifting ring), the controller controls the clamping jaw to open and the telescopic arm to extend, so that the lifting ring is positioned in the clamping jaw, the clamping jaw is closed, the travel switch A is triggered, the electromagnetic relay works, and the rope seat is released from the first half shell and is sucked to the second half shell;
and after the half shell II is sucked with the rope seat, the travel switch B is triggered, the clamping jaw is opened, and the mechanical arm retracts to finish the rope threading action.
During action, the travel switch A sends a signal to the controller so as to control the electromagnetic relay to be switched on and off; and (5) sucking the rope seat from the first half shell to the second half shell to finish the rope threading action.
When the plurality of hanging rings continuously thread the rope, the hanging rings are switched to the position of the rope seat, so that the continuous action is convenient.
The telescopic arm is located at the top or the bottom of the unmanned aerial vehicle.
On one hand, the unmanned aerial vehicle is suitable for different types of unmanned aerial vehicles (such as fixed wings or rotary wings); on the other hand, the rope threading requirement of the hanging ring at different positions is met.
The disclosure of the present application also includes the following points:
(1) the drawings of the embodiments disclosed herein only relate to the structures related to the embodiments disclosed herein, and other structures can refer to general designs;
(2) in case of conflict, the embodiments and features of the embodiments disclosed in this application can be combined with each other to arrive at new embodiments;
the above embodiments are only examples disclosed in the present application, but the scope of the present disclosure is not limited thereto, and those skilled in the art should be able to change some of the technical features of the present disclosure within the scope of the present application.
Claims (5)
1. The utility model provides an aerial supplementary wire rope handling equipment, includes unmanned aerial vehicle, its characterized in that still includes flexible arm and rope socket, flexible arm is established on unmanned aerial vehicle, the rope socket is used for connecting the wire rope handling, the connection can be dismantled on flexible arm to the rope socket.
2. The aerial auxiliary threading device of claim 1, wherein the rope base is provided with an insert, the telescopic arm is provided with an insert groove, and the insert is used for being connected in the insert groove.
3. The aerial auxiliary stringing device according to claim 2, further comprising a linear actuator provided on the telescopic arm for pushing the rope socket.
4. The aerial auxiliary stringing device as claimed in claim 1, further comprising a controller, a lidar and a clamping jaw, wherein the clamping jaw is provided on the telescopic arm;
the clamping jaw is two enclosed semi-rings, a travel switch A is arranged on the inner side of the middle of the clamping jaw, and the travel switch A is triggered when the clamping jaw is closed;
the clamping jaw is internally provided with a pair of hemispherical rope seat shells, namely a first half shell and a second half shell, the rope seat shells are internally provided with a pair of electromagnetic relays, one electromagnetic relay is positioned in the first half shell, the other electromagnetic relay is positioned in the second half shell, and the electromagnetic relays are used for attracting the rope seat to the rope seat shells on the same side; travel switches B are arranged in the first half shell and the second half shell, and when the rope seat is sucked on one side of the rope seat shell, the travel switches B on the same side are triggered;
the laser radar, the travel switch A, the travel switch B and the electromagnetic relay are connected with the rope threading device control unit.
5. An aerial auxiliary roping apparatus according to any of claims 1-4, characterized in that the telescopic boom is located at the top or bottom of the drone.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011331055.2A CN112498685B (en) | 2020-11-24 | 2020-11-24 | Aerial supplementary wire rope handling equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011331055.2A CN112498685B (en) | 2020-11-24 | 2020-11-24 | Aerial supplementary wire rope handling equipment |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112498685A true CN112498685A (en) | 2021-03-16 |
| CN112498685B CN112498685B (en) | 2021-05-28 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011331055.2A Active CN112498685B (en) | 2020-11-24 | 2020-11-24 | Aerial supplementary wire rope handling equipment |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20170087340A (en) * | 2016-01-20 | 2017-07-28 | 한국전력공사 | System and method for connection power line using dron |
| CN107359548A (en) * | 2017-08-23 | 2017-11-17 | 国网四川省电力公司检修公司 | The big span unwrapping wire platform of circuit and method based on multiple no-manned plane collaboration |
| CN208299331U (en) * | 2018-04-16 | 2018-12-28 | 湖南怀化恒光电力集团有限公司 | A kind of unmanned plane threader and multi-rotor unmanned aerial vehicle |
| CN109683629A (en) * | 2019-01-09 | 2019-04-26 | 燕山大学 | Unmanned plane electric stringing system based on integrated navigation and computer vision |
| US20190218076A1 (en) * | 2018-01-16 | 2019-07-18 | Quanta Associates, L.P. | Apparatus and method for placing and tensioning an aerial rope through a traveler of a power line |
| CN110467062A (en) * | 2019-08-16 | 2019-11-19 | 国网江苏省电力有限公司扬州供电分公司 | A kind of UAV Intelligent wire dispenser |
-
2020
- 2020-11-24 CN CN202011331055.2A patent/CN112498685B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20170087340A (en) * | 2016-01-20 | 2017-07-28 | 한국전력공사 | System and method for connection power line using dron |
| CN107359548A (en) * | 2017-08-23 | 2017-11-17 | 国网四川省电力公司检修公司 | The big span unwrapping wire platform of circuit and method based on multiple no-manned plane collaboration |
| US20190218076A1 (en) * | 2018-01-16 | 2019-07-18 | Quanta Associates, L.P. | Apparatus and method for placing and tensioning an aerial rope through a traveler of a power line |
| CN208299331U (en) * | 2018-04-16 | 2018-12-28 | 湖南怀化恒光电力集团有限公司 | A kind of unmanned plane threader and multi-rotor unmanned aerial vehicle |
| CN109683629A (en) * | 2019-01-09 | 2019-04-26 | 燕山大学 | Unmanned plane electric stringing system based on integrated navigation and computer vision |
| CN110467062A (en) * | 2019-08-16 | 2019-11-19 | 国网江苏省电力有限公司扬州供电分公司 | A kind of UAV Intelligent wire dispenser |
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| Publication number | Publication date |
|---|---|
| CN112498685B (en) | 2021-05-28 |
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