CN110155331B - Connecting device for connecting unmanned aerial vehicle and throwing and hanging device and using method thereof - Google Patents
Connecting device for connecting unmanned aerial vehicle and throwing and hanging device and using method thereof Download PDFInfo
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- CN110155331B CN110155331B CN201910003283.8A CN201910003283A CN110155331B CN 110155331 B CN110155331 B CN 110155331B CN 201910003283 A CN201910003283 A CN 201910003283A CN 110155331 B CN110155331 B CN 110155331B
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- 238000000034 method Methods 0.000 title claims description 8
- 210000000078 claw Anatomy 0.000 claims description 6
- 230000035939 shock Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 11
- 238000012423 maintenance Methods 0.000 abstract description 5
- 239000003973 paint Substances 0.000 abstract 1
- 229910000838 Al alloy Inorganic materials 0.000 description 5
- 238000007689 inspection Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 239000004922 lacquer Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 241000251468 Actinopterygii Species 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002146 bilateral effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000012857 repacking Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a connecting device for connecting unmanned aerial vehicle and throwing and hanging device, including the mainboard, set up throwing and hanging device connecting piece and set up the unmanned aerial vehicle connecting piece of mainboard upper surface at the mainboard lower surface, unmanned aerial vehicle connecting piece is including setting up first cardboard and the second cardboard at the mainboard both ends, first cardboard forms first draw-in groove after being connected with the mainboard, second cardboard forms the second draw-in groove after being connected with the mainboard, but wherein second cardboard swing joint with the mainboard. The connecting device of the present disclosure has a simple structure, can realize the quick installation and disassembly of the throwing and hanging device and the unmanned aerial vehicle, on the basis of not changing the original structure of the unmanned aerial vehicle, realizes the connection of the throwing and hanging device on the unmanned aerial vehicle without hanging points, and can not collide with the exterior paint of the unmanned aerial vehicle to cause no damage to the unmanned aerial vehicle, thereby improving the utilization rate of the unmanned aerial vehicle and reducing the maintenance cost.
Description
Technical Field
The disclosure relates to the technical field related to electric power inspection, in particular to a connecting device for connecting an unmanned aerial vehicle and a throwing and hanging device and a using method thereof.
Background
The statements in this section merely provide background information related to the present disclosure and may not necessarily constitute prior art.
The unmanned aerial vehicle is used as the main power of the daily power system inspection, and the aspects of the structure, the size, the performance and the like of the unmanned aerial vehicle are suitable for the daily power inspection requirement. The power transmission operation room is provided with power transmission maintenance and live working, the two working usually need to manually throw the traction rope, the efficiency and the accuracy of the manually throwing the traction rope are lower, and certain potential safety hazards exist.
At present, unmanned aerial vehicle development is rapid, and many industries adopt unmanned operation, have improved work efficiency and quality greatly, all sell on the unmanned aerial vehicle throwing and hanging device market now, but unmanned aerial vehicle throwing and hanging device's use has certain requirement to unmanned aerial vehicle: firstly, the mounted unmanned aerial vehicle is opened in flight control, and has no shell closed, so that the throwing and hanging device is convenient to connect and communicate with the unmanned aerial vehicle; secondly, the unmanned aerial vehicle is provided with a hanging point which is convenient for installing the throwing and hanging device. Many unmanned aerial vehicle do not possess the condition of these two aspects, like big stiff unmanned aerial vehicle of 2, to the unmanned aerial vehicle that does not set up the hanging point, if need set up to throw and hang the device and need set up the mounting hole on the fuselage, the warranty rule of product is because the damage of artificial reason or to make the change to the product can not guarantee, the product that the people were dismantled also can not guarantee the scope, it is visible, set up the mounting hole with unmanned aerial vehicle after, make unmanned aerial vehicle unable carry out the guarantee of later stage, unable assembly is thrown and is hung the device and has been restricted unmanned aerial vehicle's application range, the utilization ratio of unmanned aerial vehicle has been caused, the cost of maintenance has been increased in the repacking unmanned aerial vehicle that does not have the hanging point.
Disclosure of Invention
The utility model discloses in order to solve above-mentioned problem, a connecting device and application method of connecting unmanned aerial vehicle and throwing and hanging device has been proposed, has set up throwing and has hung device connecting piece and unmanned aerial vehicle connecting piece, and this disclosed connecting device simple structure can realize throwing and hanging device and unmanned aerial vehicle's quick installation and dismantlement, on the basis of not changing unmanned aerial vehicle original structure, has realized connecting on unmanned aerial vehicle that does not have the hanging point and has thrown and hang the device to can not collide with the outer lacquer of fuselage, do not have any damage to unmanned aerial vehicle fuselage, improved unmanned aerial vehicle's rate of utilization, reduced cost of maintenance.
In order to achieve the above purpose, the present disclosure adopts the following technical scheme:
one or more embodiments provide a connecting device for connecting unmanned aerial vehicle and throwing and hanging device, including the mainboard, set up throwing and hanging device connecting piece and set up the unmanned aerial vehicle connecting piece of mainboard upper surface at the mainboard lower surface, unmanned aerial vehicle connecting piece is including setting up first cardboard and the second cardboard at the mainboard both ends, first cardboard forms first draw-in groove after being connected with the mainboard, second cardboard forms the second draw-in groove after being connected with the mainboard, but wherein second cardboard and mainboard swing joint.
Further, the first cardboard is straight board, through first spliced pole fixed connection on the mainboard, the high and unmanned aerial vehicle's of first spliced pole joint position thickness phase-match.
Further, the second cardboard is straight board, but link post swing joint through the second on the mainboard, but the height that the second links the post and unmanned aerial vehicle's joint position thickness phase-match.
Further, the novel elastic device comprises an elastic device, wherein the elastic device is connected with the main board and the second clamping board, one end of the second connecting column is fixedly connected with the second clamping board, a pin shaft is fixedly arranged at the other end of the second connecting column, a pin shaft hole is formed in the main board, and the pin shaft hole are movably connected.
Further, the loosening and tightening device comprises a claw screw and a nut matched with the claw screw.
Further, one end of the second connecting column is fixedly connected with a second clamping plate, the other end of the second connecting column is provided with a threaded hole, and the second connecting column is movably connected with the main board through a bolt.
Further, the surface of connecting unmanned aerial vehicle one side on the mainboard and the surface of being connected with unmanned aerial vehicle on the unmanned aerial vehicle connecting piece set up the shock pad.
Based on the use method of the connecting device for connecting the unmanned aerial vehicle and the throwing and hanging device, the method comprises the following steps:
the throwing and hanging device is connected with the connecting device through a connecting part of the throwing and hanging device;
disassembling the elastic conveying device;
rotating the second clamping plate to clamp the first clamping groove at the clamping position of the unmanned aerial vehicle;
The second clamping plate is turned back to the original position, and the second clamping groove is clamped at the other clamping position of the unmanned aerial vehicle;
And installing an elastic device to fasten the second clamping plate.
Compared with the prior art, the beneficial effects of the present disclosure are:
(1) The connecting device of the present disclosure has set up and has thrown and has hung device connecting piece and unmanned aerial vehicle connecting piece, connecting device simple structure can realize throwing and hanging device and unmanned aerial vehicle's quick installation and dismantlement, on the basis of not changing unmanned aerial vehicle original structure, has realized connecting on unmanned aerial vehicle that does not have the hanging point and has thrown and hang the device to can not collide with the outer lacquer of fuselage, have not any damage to unmanned aerial vehicle fuselage, improved unmanned aerial vehicle's rate of utilization, reduced cost of maintenance.
(2) The elastic device that this disclosure set up realizes the location of second cardboard after the fastening, can not rotate when the atress, can reliably press from both sides the joint position of tight unmanned aerial vehicle, has improved connecting device's reliability.
Drawings
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this specification, illustrate embodiments of the application and together with the description serve to explain the application.
FIG. 1 is a schematic structural view of a connection device;
Wherein: 1. the first clamping plate comprises 1-1 parts of a first clamping groove, 2 parts of a first connecting column, 3 parts of a main board, 4 parts of a second connecting column, 5 parts of a second clamping plate, 5-1 parts of a second clamping groove, 6 parts of a claw screw, 7 parts of an installation screw, 8 parts of a pin shaft, 9 parts of a nut.
The specific embodiment is as follows:
The disclosure is further described below with reference to the drawings and examples.
It should be noted that the following detailed description is exemplary and is intended to provide further explanation of the application. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this application belongs.
It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of exemplary embodiments according to the present application. As used herein, the singular is also intended to include the plural unless the context clearly indicates otherwise, and furthermore, it is to be understood that the terms "comprises" and/or "comprising" when used in this specification are taken to specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof. It should be noted that, without conflict, the embodiments of the present application and features of the embodiments may be combined with each other. The embodiments will be described in detail below with reference to the accompanying drawings.
In the technical scheme disclosed in one or more embodiments, as shown in fig. 1, a connecting device for connecting a unmanned aerial vehicle and a throwing and hanging device comprises a main board 3, a throwing and hanging device connecting part arranged on the lower surface of the main board 3 and an unmanned aerial vehicle connecting part arranged on the upper surface of the main board, wherein the throwing and hanging device connecting part is used for connecting the throwing and hanging device, and the unmanned aerial vehicle connecting part is used for connecting the unmanned aerial vehicle. The connection part of the throwing and hanging device is matched with the installation mode and the installation position of the existing throwing and hanging device, the installation modes of most throwing and hanging devices in the market are in threaded connection, installation holes are formed, the connection can be realized by arranging screw rods or nuts at the corresponding positions of the connection part of the throwing and hanging device, and the connection can be realized by arranging 6 installation holes of some throwing and hanging devices and arranging 6 installation screw rods 7 on the connection part of the throwing and hanging device and configuring matched nuts.
The unmanned aerial vehicle connecting part is including setting up first cardboard 1 and the second cardboard 5 at the mainboard both ends, first cardboard 1 forms first draw-in groove 1-1 after being connected with mainboard 3, second cardboard 5 forms second draw-in groove 5-1 after being connected with mainboard 3, but wherein second cardboard 5 and mainboard 3 swing joint. The distance between the first clamping groove 1-1 and the second clamping groove 5-1 is matched according to the specific overall dimension item of the unmanned aerial vehicle, if the lower connecting plate is fixedly connected with the bottom surface of the unmanned aerial vehicle below the horn lifting steering engine, the horn lifting steering engine and the lower connecting plate form an inverted T-shaped structure, the two sides of the horn lifting steering engine on the lower connecting plate are empty and can be used for being connected with the first clamping groove and the second clamping groove in a clamping manner, the connecting device of the disclosure can be adopted for the unmanned aerial vehicle comprising the lower connecting plate and having the clamping position, or the connecting device of the disclosure can be adopted for the unmanned aerial vehicle with the leaked supporting rod and having the clamping position, and the size can be selected and set according to the specific model.
The first clamping plate 1 can be fixedly connected with the main board, can be movably connected, and can be connected in the same manner as the second clamping plate 5. As shown in fig. 1, in this embodiment 1, the first clamping plate 1 may be any shape in the prior art, such as an L-shaped plate, a straight plate, or a trapezoid plate, and in this embodiment may be a straight plate, and is fixedly connected to the main plate 3 through the first connecting column 2, where the fixed connection includes riveting, welding, or integrally casting. The height of the first connecting column 2 is matched with the thickness of the clamping part of the unmanned aerial vehicle. Two second even posts 2 can also be set up and first cardboard 1 is used for reinforcing first cardboard 1's reliability is connected simultaneously, and first cardboard 1 is difficult to slide when pressing from both sides tight unmanned aerial vehicle to one end fixed connection can improve the stability of connection, reduces the probability of joint slippage. The cross section of the first connecting column 2 can be any shape, can be round, quadrilateral, semicircular, or hollow.
Fig. 1 is a mode of realizing movable connection between the second clamping plate 5 and the main board 3, where the second clamping plate 5 may be any shape in the prior art, such as an L-shaped plate, a straight plate, and a trapezoid plate, and this embodiment may be a straight plate, and the second connecting column 4 is movably connected to the main board 3, and the height of the second connecting column 4 is matched with the thickness of the clamping part of the unmanned aerial vehicle. The cross section of the second connecting column 4 can be any shape, can be round, quadrilateral, semicircular, or hollow. The second clamping plate 5 is movably connected to the main board 3 through the second connecting column 4, and can be movably connected between at least two of the second clamping plate 5, the second connecting column 4 and the main board 1, and the movable part can rotate and move up and down. One end of the second connecting column 4 can be fixedly connected with the second clamping plate 5, the other end of the second connecting column 4 is fixedly provided with a pin shaft 8, a pin shaft hole is formed in the main board, movable connection is realized through the pin shaft 8 and the pin shaft hole, and the second clamping plate can move up and down relative to the main board 3 and also can rotate relative to the main board 3. One end of the second connecting column 4 can be fixedly connected with the second clamping plate 5, the other end of the second connecting column 4 is fixedly provided with a rivet, a through hole is formed in the main board, the rivet can move up and down in the through hole after connection, movable connection is realized through the rivet and the through hole, and the rivet can move up and down relative to the main board 3 and also can rotate relative to the main board 3. The connecting device of this embodiment still includes the elasticity device, and the elasticity device is used for connecting mainboard 3 and second cardboard 5 for adjust when being connected this device and unmanned aerial vehicle and fix the joint position on the second cardboard 5 compress tightly unmanned aerial vehicle. The tightening device may be provided to include a screw and a nut 9 matching the screw, which may be set as a claw screw 6 for quick installation. Meanwhile, the fixing mode of the elastic device and the second connecting column 4 is set, and the second clamping plate is fixed by two points after fastening and cannot rotate under the action of external force, so that the reliability of the device is improved.
As a further improvement, the present disclosure provides another implementation manner in which the second clamping plate 5 and the main board 3 are movably connected, one end of the second connecting column 4 is fixedly connected with the second clamping plate 5, the other end of the second connecting column 4 is provided with a threaded hole, the second clamping plate is movably connected with the main board 3 through a bolt, a through hole or a threaded hole can be formed in the main board, the bolt is connected with the threaded hole of the second connecting column 4 through the main board, the movable connection is realized through tightening and loosening of the threads, the up-and-down movement of the second clamping plate 5 can be realized, and the rotation of the second clamping plate 5 can also be realized. The realization mode simultaneously realizes the functions of movable connection and tightness fixation, and the realization mode can be provided with or without a tightness device. The structure of the elastic device can be the same as the previous implementation.
The surface of unmanned aerial vehicle one side and the surface of unmanned aerial vehicle connecting piece and unmanned aerial vehicle contact can also set up the shock pad for reduce or avoid damage such as the fish tail that collides with of unmanned aerial vehicle fuselage, can be high density EVA sponge board. The thickness may be set to be greater than 2mm.
The following is specifically explained with a connecting device for connecting the beauvely 2 unmanned aerial vehicle, the lower connecting plate of the beauvely 2 unmanned aerial vehicle is bilateral symmetry, and the left and right sides respectively have the space that can place first cardboard 1 and second even pull 5. The lower connecting plate of the beauvely 2 unmanned aerial vehicle is a clamping position with the left side and the right side of the connecting device respectively. The main board for connecting the beauvely 2 unmanned aerial vehicle connecting device can be an aluminum alloy plate material with the thickness of 3-5mm, the width of 12-18mm and the length of 100-130mm, and the aluminum alloy plate material has light weight and can reach the hardness required by use. The first clamping plate 1 can be an aluminum alloy plate with the thickness of 3-5mm, the width of 12-18mm and the length of 17-19mm, the second connecting plate 5 can be an aluminum alloy plate with the thickness of 3-5mm, the width of 12-18mm and the length of 27-29mm, the first connecting column and the second connecting column can be made of aluminum alloy materials with the inner diameter of 3mm, the outer diameter of 8mm and the length of 12mm, and the threaded holes can be welded nuts or tapped by arranging.
The application method of the connecting device for connecting the unmanned aerial vehicle and the throwing and hanging device comprises the following steps:
the throwing and hanging device is connected with the connecting device through a connecting part of the throwing and hanging device;
Removing the elastic device; after the second clamping plate is detached, the second clamping plate can freely rotate, so that the second clamping plate can be rotated to a position which does not interfere with the unmanned aerial vehicle;
rotating the position where the second clamping plate does not interfere with the unmanned aerial vehicle; the first clamping groove is clamped at the clamping position of the unmanned aerial vehicle;
The second clamping plate is turned back to the original position, and the second clamping groove is clamped at the other clamping position of the unmanned aerial vehicle;
And installing an elastic device to fasten the second clamping plate.
The above description is only of the preferred embodiments of the present application and is not intended to limit the present application, but various modifications and variations can be made to the present application by those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application should be included in the protection scope of the present application.
While the specific embodiments of the present disclosure have been described above with reference to the drawings, it should be understood that the present disclosure is not limited to the embodiments, and that various modifications and changes can be made by one skilled in the art without inventive effort on the basis of the technical solutions of the present disclosure while remaining within the scope of the present disclosure.
Claims (4)
1. A connecting device for connecting unmanned aerial vehicle and throwing-hanging device, which is characterized in that: the unmanned aerial vehicle comprises a main board, a throwing and hanging device connecting part arranged on the lower surface of the main board and an unmanned aerial vehicle connecting part arranged on the upper surface of the main board, wherein the unmanned aerial vehicle connecting part comprises a first clamping plate and a second clamping plate which are arranged at two ends of the main board, a first clamping groove is formed after the first clamping plate is connected with the main board, a second clamping groove is formed after the second clamping plate is connected with the main board, and the second clamping plate is movably connected with the main board;
the first clamping plate is a straight plate and is fixedly connected to the main plate through a first connecting column, and the height of the first connecting column is matched with the thickness of the clamping part of the unmanned aerial vehicle;
the second clamping plate is a straight plate and can be movably connected to the main plate through a second connecting column, and the height of the second connecting column is matched with the thickness of the clamping part of the unmanned aerial vehicle;
Unmanned aerial vehicle adapting unit still includes the elastic device, and mainboard and second cardboard are connected to the elastic device, and the one end fixed connection second cardboard of second even post, the other end fixed setting round pin axle of second even post is epaxial, sets up the round pin shaft hole on the mainboard, but round pin axle and round pin shaft hole swing joint.
2. A connection device for connecting a drone to a slinging device as claimed in claim 1, wherein: the tightness device comprises a claw screw and a nut matched with the claw screw.
3. A connection device for connecting a drone to a slinging device as claimed in claim 1, wherein: the surface of connecting unmanned aerial vehicle one side on the mainboard and the surface of being connected with unmanned aerial vehicle on the unmanned aerial vehicle connecting piece set up the shock pad.
4. A method of using a connection device for connecting a drone to a slinger device according to any one of claims 1 to 3, comprising the steps of:
the throwing and hanging device is connected with the connecting device through a connecting part of the throwing and hanging device;
Removing the elastic device;
rotating the second clamping plate to clamp the first clamping groove at the clamping position of the unmanned aerial vehicle;
The second clamping plate is turned back to the original position, and the second clamping groove is clamped at the other clamping position of the unmanned aerial vehicle;
And installing an elastic device to fasten the second clamping plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910003283.8A CN110155331B (en) | 2019-01-03 | 2019-01-03 | Connecting device for connecting unmanned aerial vehicle and throwing and hanging device and using method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910003283.8A CN110155331B (en) | 2019-01-03 | 2019-01-03 | Connecting device for connecting unmanned aerial vehicle and throwing and hanging device and using method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110155331A CN110155331A (en) | 2019-08-23 |
| CN110155331B true CN110155331B (en) | 2024-05-17 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201910003283.8A Active CN110155331B (en) | 2019-01-03 | 2019-01-03 | Connecting device for connecting unmanned aerial vehicle and throwing and hanging device and using method thereof |
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| CN106892119A (en) * | 2016-10-21 | 2017-06-27 | 北京京东尚科信息技术有限公司 | Automatic unloading carrier and unmanned plane |
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| CN206984341U (en) * | 2017-06-29 | 2018-02-09 | 昊翔电能运动科技(昆山)有限公司 | Rotor wing unmanned aerial vehicle |
| CN207225684U (en) * | 2017-09-18 | 2018-04-13 | 上海拓攻航空科技有限公司 | A kind of fast disassembly type is taken photo by plane unmanned plane |
| CN210126640U (en) * | 2019-01-03 | 2020-03-06 | 国网山东省电力公司济宁供电公司 | Connecting device for connecting unmanned aerial vehicle and throwing hanging device |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205076056U (en) * | 2015-10-28 | 2016-03-09 | 深圳市道通智能航空技术有限公司 | Cloud platform is installed and removed device fast and is had its unmanned aerial vehicle |
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2019
- 2019-01-03 CN CN201910003283.8A patent/CN110155331B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892119A (en) * | 2016-10-21 | 2017-06-27 | 北京京东尚科信息技术有限公司 | Automatic unloading carrier and unmanned plane |
| WO2018072654A1 (en) * | 2016-10-21 | 2018-04-26 | 北京京东尚科信息技术有限公司 | Automatic unloading carrier and unmanned aerial vehicle |
| CN206590119U (en) * | 2017-03-16 | 2017-10-27 | 普宙飞行器科技（深圳）有限公司 | Uas |
| CN206984341U (en) * | 2017-06-29 | 2018-02-09 | 昊翔电能运动科技(昆山)有限公司 | Rotor wing unmanned aerial vehicle |
| CN207225684U (en) * | 2017-09-18 | 2018-04-13 | 上海拓攻航空科技有限公司 | A kind of fast disassembly type is taken photo by plane unmanned plane |
| CN210126640U (en) * | 2019-01-03 | 2020-03-06 | 国网山东省电力公司济宁供电公司 | Connecting device for connecting unmanned aerial vehicle and throwing hanging device |
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| Publication number | Publication date |
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| CN110155331A (en) | 2019-08-23 |
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