CN108248888A - For being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device - Google Patents
For being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device Download PDFInfo
- Publication number
- CN108248888A CN108248888A CN201711424373.1A CN201711424373A CN108248888A CN 108248888 A CN108248888 A CN 108248888A CN 201711424373 A CN201711424373 A CN 201711424373A CN 108248888 A CN108248888 A CN 108248888A
- Authority
- CN
- China
- Prior art keywords
- cable
- tethered
- unmanned plane
- guide wheel
- ball
- Prior art date
- 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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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
Abstract
The present invention provides a kind of automatic deploying and retracting line apparatus for being used to be tethered at unmanned plane during flying device, including rotating arm and cable disc, rotating arm one end connection driving device, the outboard end of rotating arm has cabling sleeve, cable connects aircraft by cabling sleeve from cable disc, and the cabling sleeve includes liner ring, and liner ring has the ball grooves of multiple installation balls, ball is mounted in ball grooves, and ball is in half naked state in the opening of ball grooves.In the present invention, rotating arm is driven by driving device to be rotated, to complete the folding and unfolding of cable in cable disc, the drum of arm rotation is efficient, and effect is good, cable is at sliding contact with the ball in liner ring, prevents cable from clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted occur.
Description
Technical field
The present invention relates to a kind of for being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device.
Background technology
It is tethered at unmanned plane on the market to occur, the take-up and pay-off device for being tethered at unmanned plane consequently also occurs, at present
The existing unmanned plane take-up and pay-off device that is tethered at is only capable of realizing passive unwrapping wire with unmanned plane during flying, and cannot be dropped with unmanned plane
Implement existing automatic takeup；When unmanned plane lands, take-up and pay-off device needs manual rotation's take-up to carry out take-up, and work is numerous
Weight, while when extra power cable manually is not taken in take-up and pay-off device in time, extra power cable easily twines
Cause security risk around knotting；So there is an urgent need for a kind of automatic lock take-ups for being used to be tethered at unmanned plane to solve the above problems.
Invention content
In view of the above existing problems in the prior art, the present invention provides a kind of for being tethered at the automatic receipts of unmanned plane during flying device
Actinobacillus device realizes the orderly folding and unfolding of cable, has rationally distributed, compact-sized and safe and reliable.
To achieve these goals, the technical solution adopted by the present invention is：It is a kind of for be tethered at unmanned plane during flying device from
Dynamic take-up and pay-off device, including rotating arm and cable disc, described one end connection driving device, the outboard end of rotating arm has
Line sleeve, cable connect aircraft by cabling sleeve from cable disc.
The cabling sleeve includes liner ring, and liner ring has the ball grooves of multiple installation balls, and ball is mounted on rolling
In pearl slot, ball is in half naked state in the opening of ball grooves.
The present apparatus further includes sensing device, and sensing device includes cable guide pulley, ranging guide wheel and pressure sensor guide wheel,
Cable passes through cable guide pulley, ranging guide wheel and pressure sensor guide wheel, cable to be wrapped in by cable guide pulley
A plumbness is formed on pressure sensor guide wheel；Cable around ranging guide wheel and is passed through by pressure sensor guide wheel
Cabling sleeve is simultaneously put in order in cable disc.
The aircraft is multi-rotor unmanned aerial vehicle aircraft, and rotor quantity is quadrotor, six rotors, eight rotors or ten
Six rotors.
It further includes controller, floor power supply device and is tethered at for electric installation, controller is used to calculate information, signal to control
Driving device,
Cable includes two conducting wires, and the both ends of two conducting wires are respectively with floor power supply device and being tethered at for electric installation；Institute
It states to be tethered at and later stand-by power supply is powered off for floor power supply device for electric installation, for forced landing needs and be position detection
Device is powered.
The present invention be tethered at unmanned plane during flying device automatic deploying and retracting line apparatus have it is simple in structure, reliability is high, hovering is stable,
The features such as easy to use and of low cost, will be tethered at mode applied to multi-rotor unmanned aerial vehicle, solve tethered platform stability,
Set up convenience, using flexible etc. common problem, in whole device, rotating arm passes through driving device and drives rotation
Turn, to complete the folding and unfolding of cable in cable disc 3, the drum of arm rotation is efficient, and effect is good, cable 4 and liner ring
Ball in 21 is at sliding contact, prevents cable from clot or stuck phenomenon occur, and the cable promoted
Folding and unfolding speed.
Description of the drawings
Fig. 1 is the structure diagram of the present invention.
Fig. 2 is cabling sleeve and cable disc structure chart.
Fig. 3 is sensing device structure diagram.
In figure：1st, rotating arm, 2, cabling sleeve, 3, cable disc, 4, cable, 5, sensing device, 21, liner ring, 22, rolling
Pearl, 51, cable guide pulley, 52, ranging guide wheel, 53, pressure sensor guide wheel.
Specific embodiment
The invention will be further described below in conjunction with the accompanying drawings.
As shown in Figure 1, it is a kind of for being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device, including rotating arm 1 and cable
Disk 3, described 1 one end of rotating arm connection driving device so that driving device can drive rotating arm to rotate, outside rotating arm 1
Side end has cabling sleeve 2, and cable 4 connects aircraft by cabling sleeve 2 from cable disc.
The cabling sleeve 2 includes liner ring 21, and liner ring 21 has the ball grooves of multiple installation balls, and ball 22 is pacified
In ball grooves, ball 22 in half naked state and be free to slide in the opening of ball grooves, i.e., ball 22 is prominent
For 21 inner wall of liner ring, so that cable 4 is at sliding contact with the ball in liner ring 21, prevents cable
There is clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted.
The present apparatus further includes sensing device 5, and sensing device is led including cable guide pulley 51, ranging guide wheel 52 and pressure sensor
Wheel 53,
Cable 4 passes through cable guide pulley 51, ranging guide wheel 52 and pressure sensor guide wheel 53, and cable passes through cable guide pulley
It is wrapped in one plumbness of formation on pressure sensor guide wheel；Cable bypasses ranging guide wheel simultaneously by pressure sensor guide wheel
And it across cabling sleeve and puts in order in cable disc.
In whole device, rotating arm 1 is driven by driving device to be rotated, to complete the folding and unfolding of cable in cable disc 3, arm
The drum of rotation is efficient, and effect is good, and cable 4 is at sliding contact with the ball in liner ring 21, prevents electricity
There is clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted in cable.
The aircraft is multi-rotor unmanned aerial vehicle aircraft, and rotor quantity is quadrotor, six rotors, eight rotors or ten
Six rotors.
It further includes controller, floor power supply device and is tethered at for electric installation, controller is used to calculate information, signal to control
Controller described in driving device, using microcontroller, SCM system is formed, but is not limited to SCM system.Controller
Pressure sensor and photoelectric code disk are connected using wired mode respectively and receive the detection of unmanned plane elevation information at any time, and according to all
Multi information calculating is tethered at unmanned plane to the required unwrapping wire distance of specified altitude assignment.
There is controller, controller has the function of power-off protection, and when cable disconnects suddenly, controller can in aircraft
To power off and control take-up and pay-off device to carry out take-up immediately.
Cable includes two conducting wires, and the both ends of two conducting wires are respectively with floor power supply device and being tethered at for electric installation；Institute
It states to be tethered at and later stand-by power supply is powered off for floor power supply device for electric installation, for forced landing needs and be position detection
Device power supply the whole series tethered platform can be put into an about 1 meter cube portable packing case, can be loaded together with gen-set
In a miniature cross-country vehicle, there is very strong mobility.
Quadrotor unmanned plane during flying device cost is relatively low, performance is stable, easy to use, available for performing data collection, coordinating
Commander, search, measure, communication, detection, scout etc. a variety of air taskings, possess larger mission payload, stronger wind resistance energy
Power, outstanding gesture stability ability.Power supply and communication system is wherein tethered to be respectively provided with very at civilian or military aspect
Considerable application is advanced.
Embodiment described above only represents the several embodiments of invention, and description is more specific and detailed, but can not manage
It solves as limitation of the scope of the invention.It should be pointed out that for those of ordinary skill in the art, this hair is not being departed from
Under the premise of bright design, various modifications and improvements can be made, these belong to the scope of the present invention.Therefore the present invention
Protection domain should be subject to the claim.
Claims (5)
- It is 1. a kind of for being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device, which is characterized in that including rotating arm and cable disc, Rotating arm one end connection driving device, the outboard end of rotating arm have cabling sleeve, and cable passes through cabling sleeve Aircraft is connected from cable disc.
- 2. a kind of automatic deploying and retracting line apparatus for being used to be tethered at unmanned plane during flying device according to claim 1, it is characterised in that The cabling sleeve includes liner ring, and liner ring has multiple ball grooves, and ball is mounted in ball grooves, and ball is in ball grooves Opening be in half naked state.
- 3. a kind of automatic deploying and retracting line apparatus for being used to be tethered at unmanned plane during flying device according to claim 1, which is characterized in that Sensing device is further included, sensing device includes cable guide pulley, ranging guide wheel and pressure sensor guide wheel,Cable passes through cable guide pulley, ranging guide wheel and pressure sensor guide wheel, cable to be wrapped in pressure by cable guide pulley A plumbness is formed on sensor guide wheel；Cable around ranging guide wheel and passes through cabling by pressure sensor guide wheel Sleeve is simultaneously put in order in cable disc.
- 4. a kind of automatic deploying and retracting line apparatus for being used to be tethered at unmanned plane during flying device according to claim 1, it is characterised in that The aircraft is multi-rotor unmanned aerial vehicle aircraft, and rotor quantity is quadrotor, six rotors, eight rotors or 16 rotors.
- 5. a kind of automatic deploying and retracting line apparatus for being used to be tethered at unmanned plane during flying device according to claim 1, which is characterized in that It further includes controller, floor power supply device and is tethered at for electric installation, controller fills for calculating information, signal to control to drive It puts, cable includes two conducting wires, and the both ends of two conducting wires are respectively with floor power supply device and being tethered at for electric installation；It is described to be tethered at Later stand-by power supply is powered off for floor power supply device for electric installation, needed for forced landing and is supplied for position detecting device Electricity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711424373.1A CN108248888A (en) | 2017-12-25 | 2017-12-25 | For being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711424373.1A CN108248888A (en) | 2017-12-25 | 2017-12-25 | For being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108248888A true CN108248888A (en) | 2018-07-06 |
Family
ID=62723860
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711424373.1A Pending CN108248888A (en) | 2017-12-25 | 2017-12-25 | For being tethered at the automatic deploying and retracting line apparatus of unmanned plane during flying device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108248888A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109005344A (en) * | 2018-08-08 | 2018-12-14 | 哈尔滨工业大学 | Multiple degrees of freedom is tethered at monitor supervision platform |
| CN109895991A (en) * | 2018-12-12 | 2019-06-18 | 鲁金婵 | It is a kind of can wound wire collapsible unmanned plane |
| CN110182379A (en) * | 2019-06-03 | 2019-08-30 | 深圳市贝贝特科技实业有限公司 | There is synchronizing for line traffic control to be tethered at UAV system and unmanned plane |
| CN110611270A (en) * | 2019-09-04 | 2019-12-24 | 国网河南省电力公司三门峡供电公司 | Stringing method and stringing track aircraft thereof |
| CN114955747A (en) * | 2022-07-27 | 2022-08-30 | 北京卓翼智能科技有限公司 | Automatic winding displacement device and mooring unmanned aerial vehicle system comprising same |
| CN110611270B (en) * | 2019-09-04 | 2024-04-26 | 国网河南省电力公司三门峡供电公司 | Stringing method and stringing orbital aircraft |
-
2017
- 2017-12-25 CN CN201711424373.1A patent/CN108248888A/en active Pending
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109005344A (en) * | 2018-08-08 | 2018-12-14 | 哈尔滨工业大学 | Multiple degrees of freedom is tethered at monitor supervision platform |
| CN109005344B (en) * | 2018-08-08 | 2020-09-01 | 哈尔滨工业大学 | Multi-degree-of-freedom mooring monitoring platform |
| CN109895991A (en) * | 2018-12-12 | 2019-06-18 | 鲁金婵 | It is a kind of can wound wire collapsible unmanned plane |
| CN110182379A (en) * | 2019-06-03 | 2019-08-30 | 深圳市贝贝特科技实业有限公司 | There is synchronizing for line traffic control to be tethered at UAV system and unmanned plane |
| CN110611270A (en) * | 2019-09-04 | 2019-12-24 | 国网河南省电力公司三门峡供电公司 | Stringing method and stringing track aircraft thereof |
| CN110611270B (en) * | 2019-09-04 | 2024-04-26 | 国网河南省电力公司三门峡供电公司 | Stringing method and stringing orbital aircraft |
| CN114955747A (en) * | 2022-07-27 | 2022-08-30 | 北京卓翼智能科技有限公司 | Automatic winding displacement device and mooring unmanned aerial vehicle system comprising same |
| CN114955747B (en) * | 2022-07-27 | 2022-11-08 | 北京卓翼智能科技有限公司 | Automatic winding displacement device and mooring unmanned aerial vehicle system comprising same |
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Legal Events
| Date | Code | Title | Description |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180706 |
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| WD01 | Invention patent application deemed withdrawn after publication |