CN110155331A - A kind of attachment device and its application method of connection unmanned plane and throwing hang device - Google Patents
A kind of attachment device and its application method of connection unmanned plane and throwing hang device Download PDFInfo
- Publication number
- CN110155331A CN110155331A CN201910003283.8A CN201910003283A CN110155331A CN 110155331 A CN110155331 A CN 110155331A CN 201910003283 A CN201910003283 A CN 201910003283A CN 110155331 A CN110155331 A CN 110155331A
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- unmanned plane
- mainboard
- snap
- gauge
- throwing
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- 238000000034 method Methods 0.000 title claims description 10
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 35
- 241000883966 Astrophytum capricorne Species 0.000 claims description 6
- 238000012423 maintenance Methods 0.000 abstract description 6
- 239000003973 paint Substances 0.000 abstract description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 5
- 238000009434 installation Methods 0.000 description 5
- 238000007689 inspection Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000008439 repair process Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000010079 rubber tapping Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
Abstract
The present disclosure discloses the attachment devices of a kind of connection unmanned plane and throwing hang device, including mainboard, the throwing hang device connecting component that mainboard lower surface is arranged in and the unmanned plane connecting component that mainboard upper surface is arranged, the unmanned plane connecting component includes the first snap-gauge and the second snap-gauge that mainboard both ends are arranged in, first snap-gauge forms the first card slot after connecting with mainboard, second snap-gauge forms the second card slot after connecting with mainboard, wherein the second snap-gauge and the movable connection of mainboard.The attachment device structure of the disclosure is simple, it can be realized and throw being rapidly assembled and disassembled for hang device and unmanned plane, on the basis of not changing unmanned plane original structure, it realizes the connection on the unmanned plane of no hanging point and throws hang device, and the fuselage exterior paint that will not collide with does not have any damage to unmanned aerial vehicle body, the utilization rate for improving unmanned plane, reduces maintenance cost.
Description
Technical field
This disclosure relates to electric inspection process correlative technology field, in particular to a kind of connection unmanned plane is mounted with throwing
The attachment device and its application method set.
Background technique
Only there is provided background technical informations relevant to the disclosure for the statement of this part, it is not necessary to so constitute first skill
Art.
Unmanned plane is used as the main force of daily power system inspection, and airframe structure, size, performance etc. are suitble to daily
Electric inspection process requirement.The work of electric power transmission fortune inspection room has transmission of electricity maintenance and livewire work work, this two work often need
Artificial throwing traction rope is wanted, the efficiency and accuracy of artificial throwing traction rope are relatively low, and there is also some potential safety problemss.
Present Development of UAV is rapid, and many industries use unmanned operation, greatly improves work efficiency and quality, now
Unmanned plane throws hang device sale on the market, but the use that unmanned plane throws hang device has certain requirement to unmanned plane: first is that
Mounted unmanned plane flies control and opens, do not have shell seal, is attached and communicates with unmanned plane convenient for throwing hang device；Second is that should
There is the hanging point for facilitating installation to throw hang device on unmanned plane.Many unmanned planes do not have the condition of above-mentioned these two aspects, and such as big deadlock realizes 2
Unmanned plane throws hang device needs if necessary to setting and mounting hole is arranged on fuselage, produce for being not provided with the unmanned plane of hanging point
The guarantee regulation of product due to artificial origin damage or change has been done to product cannot guarantee to keep in good repair, the product artificially dismantled is not yet
In warranty coverage, it is seen then that after mounting hole is arranged in unmanned plane, so that unmanned plane can not carry out the guarantee in later period, throwing can not be assembled
Hang device limits the use scope of unmanned plane, causes the utilization rate of unmanned plane, reequips to the unmanned plane of not hanging point
Increase the maintenance cost of maintenance.
Summary of the invention
The disclosure to solve the above-mentioned problems, proposes the attachment device and use of a kind of connection unmanned plane and throwing hang device
Method is provided with and throws hang device connecting component and unmanned plane connecting component, and the attachment device structure of the disclosure is simple, Neng Goushi
Being rapidly assembled and disassembled for hang device and unmanned plane is now thrown, on the basis of not changing unmanned plane original structure, is realized
Hang device, and the fuselage exterior paint that will not collide with are thrown in connection on the unmanned plane of no hanging point, do not have any damage to unmanned aerial vehicle body,
The utilization rate for improving unmanned plane, reduces maintenance cost.
To achieve the goals above, the disclosure adopts the following technical scheme that
One or more embodiments provide a kind of connection unmanned plane and throw the attachment device of hang device, including mainboard, set
Set the unmanned plane connecting component thrown hang device connecting component and mainboard upper surface is set in mainboard lower surface, the unmanned plane
Connecting component includes the first snap-gauge and the second snap-gauge that mainboard both ends are arranged in, and first snap-gauge forms after connecting with mainboard
One card slot, second snap-gauge form the second card slot after connecting with mainboard, wherein the second snap-gauge and the movable connection of mainboard.
Further, the first snap-gauge be straight panel, be fixedly connected on mainboard by the first pedestal, the height of the first pedestal with
The wedging position thickness of unmanned plane matches.
Further, the second snap-gauge is straight panel, is connected on mainboard by the way that the second pedestal is movable, the height of the second pedestal
Match with the wedging position thickness of unmanned plane.
It further, further include take-up, take-up connection mainboard and the second snap-gauge, one end of the second pedestal are fixed
The second snap-gauge is connected, the other end of second pedestal is fixedly installed pin shaft, pin shaft hole is arranged on mainboard, pin shaft and pin shaft hole can
It is flexibly connected.
Further, the take-up include goat's horn screw rod and with the matched nut of goat's horn screw rod.
Further, one end of second pedestal is fixedly connected with the second snap-gauge, and screw thread is arranged in the other end of the second pedestal
Hole passes through bolt and the movable connection of mainboard.
Further, the table connecting on the surface and unmanned plane connecting component of unmanned plane side with unmanned plane is connected on mainboard
Resilient cushion is arranged in face.
Based on a kind of above-mentioned application method of connection unmanned plane and the attachment device for throwing hang device, include the following steps:
Hang device will be thrown to connect by throwing hang device connecting component with attachment device；
It removes and send take-up；
The second snap-gauge is rotated, the first card slot is connected to the clamping position of unmanned plane；
Second snap-gauge is gone back into original position, the second card slot is connected to another clamping position of unmanned plane；
Take-up is installed, the second snap-gauge is fastened.
Compared with prior art, the disclosure has the beneficial effect that
(1) attachment device of the disclosure, which is provided with, throws hang device connecting component and unmanned plane connecting component, attachment device
Structure is simple, can be realized and throws being rapidly assembled and disassembled for hang device and unmanned plane, is not changing the original structure of unmanned plane
On the basis of, it realizes the connection on the unmanned plane of no hanging point and throws hang device, and the fuselage exterior paint that will not collide with, to unmanned aerial vehicle body
There is no any damage, improves the utilization rate of unmanned plane, reduce maintenance cost.
(2) take-up of disclosure setting, realizes the positioning of the second snap-gauge, will not rotate in stress, energy after fastening
The wedging position of enough reliable grip unmanned planes, improves the reliability of attachment device.
Detailed description of the invention
The accompanying drawings constituting a part of this application is used to provide further understanding of the present application, and the application's shows
Meaning property embodiment and its explanation do not constitute the restriction to the application for explaining the application.
Fig. 1 is the structural schematic diagram of attachment device；
Wherein: 1, first snap-gauge, 1-1, the first card slot, the 2, first pedestal, 3, mainboard, the 4, second pedestal, the 5, second snap-gauge,
5-1, the second card slot, 6, goat's horn screw rod, 7, installation screw rod, 8, pin shaft, 9, nut.
Specific embodiment:
The disclosure is described further with embodiment with reference to the accompanying drawing.
It is noted that described further below be all exemplary, it is intended to provide further instruction to the application.Unless another
It indicates, all technical and scientific terms used herein has usual with the application person of an ordinary skill in the technical field
The identical meanings of understanding.
It should be noted that term used herein above is merely to describe specific embodiment, and be not intended to restricted root
According to the illustrative embodiments of the application.As used herein, unless the context clearly indicates otherwise, otherwise singular
Also it is intended to include plural form, additionally, it should be understood that, when in the present specification using term "comprising" and/or " packet
Include " when, indicate existing characteristics, step, operation, device, component and/or their combination.It should be noted that not conflicting
In the case where, the features in the embodiments and the embodiments of the present application can be combined with each other.Below in conjunction with attached drawing to embodiment
It is described in detail.
In the technical solution disclosed in one or more embodiments, as shown in Figure 1, a kind of connection unmanned plane and throwing are hung
Including mainboard 3, table in the throwing hang device connecting component and setting mainboard of 3 lower surface of mainboard is arranged in the attachment device of device
The unmanned plane connecting component in face, the throwing hang device connecting component throw hang device for connecting, and the unmanned plane connecting component is used
In connection unmanned plane.The hang device connecting component of throwing matches with the existing mounting means for throwing hang device and installation site,
It is to be threadedly coupled that majority, which throws the mounting means of hang devices, in the market, is provided with mounting hole, in the throwing hang device connecting component
Corresponding position setting screw rod or nut can realize connection, and some throwing hanging devices are provided with 6 mounting holes, can be in institute
It states to throw that 6 installation screw rods 7 are arranged in hang device connecting component and configure the nut to match and connection can be realized.
The unmanned plane connecting component includes the first snap-gauge 1 and the second snap-gauge 5 that mainboard both ends are arranged in, first card
Plate 1 forms the first card slot 1-1 after connecting with mainboard 3, second snap-gauge 5 forms the second card slot 5-1 after connecting with mainboard 3,
In the second snap-gauge 5 and the movable connection of mainboard 3.The distance of first card slot 1-1 and the second card slot 5-1 are according to the specific outer of unmanned plane
The matching of shape size item, the bottom surface as big deadlock realizes 2 unmanned planes are won in succession in the case where horn goes up and down and has been fixedly connected below steering engine, horn liter
Drop steering engine wins in succession to form an inverse-T-shaped structure under, and lifting steering engine two sides are empty on lower linking plate, can be used for and first
Card slot and the clamping of the second card slot are attached, for winning in succession and having the unmanned plane of clamping position can be using this comprising under
Disclosed attachment device, or the support rod with leakage and the connection that there is the type of clamping position can also use the disclosure
Device, size can carry out selection setting according to specific type.
First snap-gauge 1 may be set to be to be fixedly connected with mainboard, or movable connection, the side of movable connection
Formula can be identical as the connection type of the second snap-gauge 5.1 first snap-gauge 1 of the present embodiment as shown in Figure 1 can appointing for the prior art
Meaning shape, such as L shape plate, straight panel, trapezoidal plate, the present embodiment can be straight panel, be fixedly connected on mainboard 3 by the first pedestal 2
On, it is fixedly connected including riveting, welding or for casting integrated connection.The height of first pedestal 2 and the wedging position of unmanned plane
Thickness matches.Two the second pedestals 2 can also be set while connecting the reliability that the first snap-gauge 1 is used to enhance the first snap-gauge 1,
When clamping unmanned plane, the first snap-gauge 1 is not easy to slide, and one end is fixedly connected with the stability that connection can be improved, and reduces card
Connect the probability of slippage.First pedestal, 2 cross section can have any shape, and can be circle, quadrangle, semi-circular shape, can be with
It is hollow.
Fig. 1 is a kind of mode that the second snap-gauge 5 realizes movable connection with mainboard 3, and the second snap-gauge 5 can be the prior art
Arbitrary shape, such as L shape plate, straight panel, trapezoidal plate, the present embodiment can be straight panel, be connected to by the way that the second pedestal 4 is movable
On mainboard 3, the height of the second pedestal 4 and the wedging position thickness of unmanned plane match.Second pedestal, 4 cross section can be any
Shape can be circle, quadrangle, semi-circular shape, can also be hollow.Second snap-gauge 5 passes through the movable company of the second pedestal 4
It connects on mainboard 3, can be movable at least there are two between for the second snap-gauge 5, the second pedestal 4 and mainboard 1 these three components
Connection, it is described it is movable can for rotation and it is up and down.One end of second pedestal 4 can be fixedly connected with the second snap-gauge 5, institute
The other end fixed setting pin shaft 8 of the second pedestal 4 is stated, pin shaft hole is set on mainboard, is realized by pin shaft 8 and pin shaft hole movable
Connection, both can be up and down relative to mainboard 3 or relative to the rotation of mainboard 3.It can also be by the fixed company in one end of the second pedestal 4
Connect the second snap-gauge 5, rivet is fixedly installed in the other end of second pedestal 4, and through-hole is arranged on mainboard, and rivet can be after connection
It is up and down in through-hole, movable connection is realized by rivet and through-hole, it both can be up and down with respect to mainboard 3 or opposite
Mainboard 3 rotates.The attachment device of the present embodiment further includes take-up, and take-up is used to connect mainboard 3 and the second snap-gauge 5,
The wedging position fixed on the second snap-gauge 5 compression unmanned plane is adjusted when for the present apparatus to be connect with unmanned plane.The elastic dress
Set can be set to include screw rod and with the matched nut 9 of screw rod, screw rod can be set as goat's horn for the ease of Fast Installation
Screw rod 6.It is provided with the fixed form of take-up and the second pedestal 4 simultaneously, it will not be by two fixed second snap-gauge after fastening
It is rotated under the action of external force, improves the reliability of device.
As a further improvement, the disclosure provides another realization side that the second snap-gauge 5 realizes movable connection with mainboard 3
Formula, one end of second pedestal 4 are fixedly connected with the second snap-gauge 5, and the other end of the second pedestal 4 is arranged threaded hole, passes through bolt
With the movable connection of mainboard 3, through-hole or threaded hole can be set on mainboard, bolt passes through the screw thread of mainboard and the second pedestal 4
Hole connection is tightened and is unclamped the movable connection of realization by screw thread, moving up and down for the second snap-gauge 5 may be implemented, can also be with
Realize the rotation of the second snap-gauge 5.This implementation realizes the function of movable connection and elastic fixation, this implementation simultaneously
Take-up can be set, take-up can also be not provided with.The structure of take-up can be identical as a upper implementation.
The surface that the surface of mainboard connection unmanned plane side and unmanned plane connecting component are contacted with unmanned plane can also be arranged
Resilient cushion can be high density EVA sponge plate for reducing or avoiding the damage such as scuffing of colliding with of unmanned aerial vehicle body.Thickness
It can be set to be greater than 2mm.
It is illustrated below with the attachment device for realizing 2 unmanned planes for connecting big deadlock, the lower plate that big deadlock realizes 2 unmanned planes is
Symmetrically, the left and right sides have respectively can place the first snap-gauge 1 and second win in succession 5 space.Big deadlock realizes the lower company of 2 unmanned planes
Pull be respectively for the left and right sides attachment device clamping position.The mainboard that 2 unmanned plane attachment devices are realized for connecting big deadlock can be with
For 3-5mm thickness, the aluminum alloy plate materials of 12-18mm wide, 100-130mm long, aluminum alloy plate materials are light-weight, and can reach needed for use
The hardness wanted.First snap-gauge 1 can be 3-5mm thickness, the aluminum alloy plate materials of 12-18mm wide, 17-19mm long, and second wins in succession 5 can be with
For 3-5mm thickness, the aluminum alloy plate materials of 12-18mm wide, 27-29mm long, the first pedestal and the second pedestal can using internal diameter 3mm,
Outer diameter 8mm, long 12mm aluminum alloy materials, needing to be arranged threaded hole is that can be realized with welded nut or tapping.
The application method of above-mentioned a kind of connection unmanned plane and the attachment device for throwing hang device, includes the following steps:
Hang device will be thrown to connect by throwing hang device connecting component with attachment device；
Remove take-up；After removing, the second snap-gauge can be freely rotated, so as to go to the second snap-gauge and nothing
The man-machine position that do not interfere；
Rotate the position that the second snap-gauge and unmanned plane are not interfered；First card slot is connected to the clamping position of unmanned plane；
Second snap-gauge is gone back into original position, the second card slot is connected to another clamping position of unmanned plane；
Take-up is installed, the second snap-gauge is fastened.
The foregoing is merely preferred embodiment of the present application, are not intended to limit this application, for the skill of this field
For art personnel, various changes and changes are possible in this application.Within the spirit and principles of this application, made any to repair
Change, equivalent replacement, improvement etc., should be included within the scope of protection of this application.
Although above-mentioned be described in conjunction with specific embodiment of the attached drawing to the disclosure, model not is protected to the disclosure
The limitation enclosed, those skilled in the art should understand that, on the basis of the technical solution of the disclosure, those skilled in the art are not
Need to make the creative labor the various modifications or changes that can be made still within the protection scope of the disclosure.
Claims (8)
1. a kind of connection unmanned plane and the attachment device for throwing hang device, it is characterized in that: including mainboard, mainboard lower surface being arranged in
It throws hang device connecting component and the unmanned plane connecting component of mainboard upper surface is set, the unmanned plane connecting component includes setting
The first snap-gauge and the second snap-gauge at mainboard both ends, first snap-gauge form the first card slot after connecting with mainboard, and described second
Snap-gauge forms the second card slot after connecting with mainboard, wherein the second snap-gauge and the movable connection of mainboard.
2. a kind of connection unmanned plane as described in claim 1 and the attachment device for throwing hang device, it is characterized in that: the first snap-gauge is
Straight panel is fixedly connected on mainboard by the first pedestal, and the height of the first pedestal and the wedging position thickness of unmanned plane match.
3. a kind of connection unmanned plane as described in claim 1 and the attachment device for throwing hang device, it is characterized in that: the second snap-gauge is
Straight panel is connected on mainboard by the way that the second pedestal is movable, the height and the wedging position thickness phase of unmanned plane of the second pedestal
Match.
4. a kind of connection unmanned plane as claimed in claim 3 and the attachment device for throwing hang device, it is characterized in that: further including elastic
Device, take-up connection mainboard and the second snap-gauge, one end of the second pedestal are fixedly connected with the second snap-gauge, second pedestal
Pin shaft is fixedly installed in the other end, and pin shaft hole, pin shaft and the movable connection of pin shaft hole is arranged on mainboard.
5. a kind of connection unmanned plane as claimed in claim 4 and the attachment device for throwing hang device, it is characterized in that: the elastic dress
Set including goat's horn screw rod and with the matched nut of goat's horn screw rod.
6. a kind of connection unmanned plane as claimed in claim 3 and the attachment device for throwing hang device, it is characterized in that: described second connects
One end of column is fixedly connected with the second snap-gauge, and the other end of the second pedestal is arranged threaded hole, passes through bolt and the movable connection of mainboard.
7. a kind of connection unmanned plane as described in claim 1 and the attachment device for throwing hang device, it is characterized in that: being connected on mainboard
The surface setting resilient cushion being connect on the surface of unmanned plane side and unmanned plane connecting component with unmanned plane.
8. based on a kind of described in any item users of connection unmanned plane and the attachment device for throwing hang device of claim 1-7
Method, characterized in that include the following steps:
Hang device will be thrown to connect by throwing hang device connecting component with attachment device；
It removes and send take-up；
The second snap-gauge is rotated, the first card slot is connected to the clamping position of unmanned plane；
Second snap-gauge is gone back into original position, the second card slot is connected to another clamping position of unmanned plane；
Take-up is installed, the second snap-gauge is fastened.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910003283.8A CN110155331B (en) | 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 | Connecting device for connecting unmanned aerial vehicle and throwing and hanging device and using method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110155331A true CN110155331A (en) | 2019-08-23 |
| CN110155331B CN110155331B (en) | 2024-05-17 |
Family
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| 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 |
| US20180237158A1 (en) * | 2015-10-28 | 2018-08-23 | Autel Robotics Co., Ltd. | Gimbal quick assembly/disassembly apparatus and unmanned aerial vehicle having the same |
| 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 |
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20180237158A1 (en) * | 2015-10-28 | 2018-08-23 | Autel Robotics Co., Ltd. | Gimbal quick assembly/disassembly apparatus and unmanned aerial vehicle having the same |
| 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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