CN105173105A - Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft - Google Patents
Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft Download PDFInfo
- Publication number
- CN105173105A CN105173105A CN201510469698.6A CN201510469698A CN105173105A CN 105173105 A CN105173105 A CN 105173105A CN 201510469698 A CN201510469698 A CN 201510469698A CN 105173105 A CN105173105 A CN 105173105A
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- mooring
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Abstract
The invention discloses an automatic cable coiling and uncoiling device used for a mooring unmanned plane aircraft. The device comprises a rotating arm and a cable disc. One end of the rotating arm is connected with a driving device. A cabling sleeve is arranged at the end of the outer side of the rotating arm. A cable is connected with the aircraft from the cable disc through the cabling sleeve. The cabling sleeve comprises a sleeve ring. A plurality of ball grooves used for installing balls are formed in the sleeve ring. The balls are installed inside the ball grooves. The balls are half exposed at openings of the ball grooves. According to the device, the rotating arm is driven by the driving device to rotate so that the cable in the cable disc can be coiled and uncoiled. The coiling efficiency of the rotating arm is high, and the coiling effect is good. The cable can be in sliding contact with the balls in the sleeve ring, so that the cable is prevented from being curled or getting stuck, and the coiling speed and uncoiling speed of the cable are improved.
Description
Technical field
The present invention relates to a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device.
Background technology
Mooring unmanned plane commercially occurs, also there is the take-up and pay-off device for mooring unmanned plane thereupon, the mooring unmanned plane take-up and pay-off device of current existence only can realize passive unwrapping wire along with unmanned plane during flying, and can not realize automatic takeup along with unmanned plane landing; When unmanned plane lands, take-up and pay-off device needs manual rotation's take-up to carry out take-up, works heavy, simultaneously when artificial not timely by unnecessary power cable income take-up and pay-off device time, unnecessary power cable very easily occurs that tangled up and knotted causes potential safety hazard; So need a kind of automatic lock take-up for mooring unmanned plane badly to solve the problem.
Summary of the invention
For above-mentioned prior art Problems existing, the invention provides a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device, realize the orderly folding and unfolding of cable, there is rationally distributed, compact conformation and safe and reliable.
To achieve these goals, the technical solution used in the present invention is: a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device, comprise pivot arm and cable disc, described one end connecting drive device, the outboard end of pivot arm has cabling sleeve, and cable connects aircraft by cabling sleeve from cable disc.
Described cabling sleeve comprises liner ring, and liner ring has the ball grooves of multiple installation ball, and ball is arranged in ball grooves, and ball is half naked state at the opening part of ball grooves.
This device also comprises induction installation, and induction installation comprises cable guide pulley, range finding guide wheel and pressure sensor guide wheel,
Cable is through cable guide pulley, range finding guide wheel and pressure sensor guide wheel, and cable is wrapped on pressure sensor guide wheel by cable guide pulley and forms a plumbness; Cable is walked around range finding guide wheel by pressure sensor guide wheel and is passed cabling sleeve and put in order in cable disc.
Described aircraft is many rotor wing unmanned aerial vehicles aircraft, and its rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
Also comprise controller, floor power supply device and mooring electric supply installation, controller carrys out accessory drive for computing information, signal,
Cable comprises two wires, the two ends of two wires respectively with floor power supply device and mooring electric supply installation; Described mooring electric supply installation is used for the later backup power of floor power supply device power-off, needs and power for position detecting device for forced landing.
It is simple that the automatic deploying and retracting line apparatus of mooring unmanned plane during flying device of the present invention has structure, reliability is high, hovering is stable, the feature such as easy to use and with low cost, mooring mode is applied to many rotor wing unmanned aerial vehicles, solve tethered platform in stability, erection comfort feature, use the ubiquitous problems in aspect such as alerting ability, in whole device, pivot arm is by actuating device driven rotary, carry out the folding and unfolding of cable in cable disc 3, the drum efficiency that arm rotates is high, and it is effective, cable 4 can be in moving contact with the ball in liner ring 21, prevent cable from occurring clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is pivot arm and cable disc constructional drawing.
Fig. 3 is induction installation structural representation.
In figure: 1, pivot arm, 2, cabling sleeve, 3, cable disc, 4, cable, 5, induction installation, 21, liner ring, 22, ball, 51, cable guide pulley, 52, range finding guide wheel, 53, pressure sensor guide wheel.
Detailed description of the invention
Below in conjunction with accompanying drawing, the invention will be further described.
As shown in Figure 1, a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device, comprise pivot arm 1 and cable disc 3, described pivot arm 1 one end connecting drive device, actuating device can be rotated by driven rotary arm, the outboard end of pivot arm 1 has cabling sleeve 2, and cable 4 connects aircraft by cabling sleeve 2 from cable disc.
Described cabling sleeve 2 comprises liner ring 21, liner ring 21 has the ball grooves of multiple installation ball, ball 22 is arranged in ball grooves, ball 22 is half naked state at the opening part of ball grooves and is free to slide, namely ball 22 protrudes from liner ring 21 inwall, make cable 4 can be in moving contact with the ball in liner ring 21 like this, prevent cable from occurring clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted.
This device also comprises induction installation 5, and induction installation comprises cable guide pulley 51, range finding guide wheel 52 and pressure sensor guide wheel 53,
Cable 4 is through cable guide pulley 51, range finding guide wheel 52 and pressure sensor guide wheel 53, and cable is wrapped on pressure sensor guide wheel by cable guide pulley and forms a plumbness; Cable is walked around range finding guide wheel by pressure sensor guide wheel and is passed cabling sleeve and put in order in cable disc.
In whole device, pivot arm 1 is by actuating device driven rotary, carry out the folding and unfolding of cable in cable disc 3, the drum efficiency that arm rotates is high, and it is effective, cable 4 can be in moving contact with the ball in liner ring 21, prevents cable from occurring clot or stuck phenomenon, and the folding and unfolding speed of the cable promoted.
Described aircraft is many rotor wing unmanned aerial vehicles aircraft, and its rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
Also comprise controller, floor power supply device and mooring electric supply installation, controller carrys out controller described in accessory drive for computing information, signal, adopts microcontroller, and Single Chip Microcomputer (SCM) system is formed, but is not limited to Single Chip Microcomputer (SCM) system.Controller employing wired mode respectively Bonding pressure sensor and photoelectric code disk also accepts the detection of unmanned plane elevation information at any time, and calculates the unwrapping wire distance required for mooring unmanned plane to specified altitude assignment according to all multi information.
Have controller in aircraft, controller has the effect of power-off protection, and when cable disconnects suddenly, controller can power-off immediately control take-up and pay-off device and carry out take-up.
Cable comprises two wires, the two ends of two wires respectively with floor power supply device and mooring electric supply installation; Described mooring electric supply installation is used for the later backup power of floor power supply device power-off, need for forced landing and power for position detecting device, a whole set of tethered platform can put into about 1 meter of cube of portable packing chest, together can be loaded in a miniature cross-country car with gen-set, have very strong manoevreability.
Four rotor wing unmanned aerial vehicle aircraft costs are lower, stable performance, easy to use, can be used for performing the multiple air taskings such as Data acquisition, coordinative command, search, measurement, communication, detection, scouting, have larger mission payload, stronger wind loading rating, outstanding gesture stability ability.Wherein mooring power and communication system no matter civilian or military in all there is very considerable application advance.
The above embodiment only represents several embodiments of invention, describes comparatively concrete and detailed, but can not be interpreted as limitation of the scope of the invention.It should be pointed out that for the person of ordinary skill of the art, without departing from the inventive concept of the premise, can also make some distortion and improvement, these all belong to scope.Therefore protection scope of the present invention should be as the criterion with described claim.
Claims (5)
1. the automatic deploying and retracting line apparatus for mooring unmanned plane during flying device, it is characterized in that, comprise pivot arm and cable disc, described pivot arm one end connecting drive device, the outboard end of pivot arm has cabling sleeve, and cable connects aircraft by cabling sleeve from cable disc.
2. a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device according to claim 1, it is characterized in that described cabling sleeve comprises liner ring, liner ring has multiple ball grooves, and ball is arranged in ball grooves, and ball is half naked state at the opening part of ball grooves.
3. a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device according to claim 1, is characterized in that, also comprise induction installation, and induction installation comprises cable guide pulley, range finding guide wheel and pressure sensor guide wheel,
Cable is through cable guide pulley, range finding guide wheel and pressure sensor guide wheel, and cable is wrapped on pressure sensor guide wheel by cable guide pulley and forms a plumbness; Cable is walked around range finding guide wheel by pressure sensor guide wheel and is passed cabling sleeve and put in order in cable disc.
4. a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device according to claim 1, is characterized in that described aircraft is many rotor wing unmanned aerial vehicles aircraft, and its rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
5. a kind of automatic deploying and retracting line apparatus for mooring unmanned plane during flying device according to claim 1, is characterized in that, also comprise controller, floor power supply device and mooring electric supply installation, and controller is used for computing information, signal carrys out accessory drive,
Cable comprises two wires, the two ends of two wires respectively with floor power supply device and mooring electric supply installation; Described mooring electric supply installation is used for the later backup power of floor power supply device power-off, needs and power for position detecting device for forced landing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510469698.6A CN105173105A (en) | 2015-08-04 | 2015-08-04 | Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft |
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| CN201510469698.6A CN105173105A (en) | 2015-08-04 | 2015-08-04 | Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft |
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| CN105173105A true CN105173105A (en) | 2015-12-23 |
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| CN201510469698.6A Pending CN105173105A (en) | 2015-08-04 | 2015-08-04 | Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft |
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Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105667834A (en) * | 2016-04-13 | 2016-06-15 | 云南电网有限责任公司电力科学研究院 | Device and method for testing unmanned aerial vehicle |
| CN105836153A (en) * | 2016-03-17 | 2016-08-10 | 北京大工科技有限公司 | Mooring system of unmanned aerial vehicle |
| CN106058783A (en) * | 2016-07-06 | 2016-10-26 | 合肥通鼎光电科技有限公司 | Communication cable coiling/uncoiling system for low-altitude sensing unmanned aerial vehicle |
| CN106274625A (en) * | 2016-08-29 | 2017-01-04 | 西安天鹰防务科技有限公司 | A kind of mechanical arm type unmanned plane hoistable platform |
| CN106995058A (en) * | 2017-05-25 | 2017-08-01 | 许启超 | A kind of manned semiclosed low flyer of use current collector system |
| CN107187961A (en) * | 2017-07-15 | 2017-09-22 | 珠海市双捷科技有限公司 | Automatic deploying and retracting line apparatus, system and its control method for being tethered at unmanned plane |
| CN107757942A (en) * | 2016-08-19 | 2018-03-06 | 深圳航天旭飞科技有限公司 | The electric power supply control system of unmanned plane |
| WO2018205099A1 (en) * | 2017-05-08 | 2018-11-15 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle protective device and method, unmanned aerial vehicle and flight field |
| CN109131863A (en) * | 2018-09-10 | 2019-01-04 | 哈尔滨工业大学 | The more rotors of culvert type are tethered at unmanned plane and its control system |
| CN109607331A (en) * | 2019-02-13 | 2019-04-12 | 深圳市赛为智能股份有限公司 | One kind being tethered at unmanned plane retractable cable buffer structure and its working method |
| CN109677627A (en) * | 2019-01-11 | 2019-04-26 | 苏州全波通信技术股份有限公司 | It is tethered at unmanned plane precision approach control system and method |
| CN109775481A (en) * | 2019-02-15 | 2019-05-21 | 湖南优加特装智能科技有限公司 | For being tethered at the take-up and pay-off device of unmanned plane |
| CN109895991A (en) * | 2018-12-12 | 2019-06-18 | 鲁金婵 | It is a kind of can wound wire collapsible unmanned plane |
| WO2020168631A1 (en) * | 2019-02-19 | 2020-08-27 | 深圳市赛为智能股份有限公司 | Intelligent take-up and pay-off device for tethered unmanned aerial vehicle, and operating method thereof |
| WO2021126071A1 (en) | 2019-12-18 | 2021-06-24 | Avetics Global Pte. Ltd. | A tether management system and method |
| CN116466734A (en) * | 2023-05-04 | 2023-07-21 | 山东御航智能科技有限公司 | Unmanned aerial vehicle threading method and system |
| CN118405546A (en) * | 2024-07-03 | 2024-07-30 | 凯姆乐(常州)电子有限公司 | Unmanned transplanter cable protection device |
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Cited By (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105836153A (en) * | 2016-03-17 | 2016-08-10 | 北京大工科技有限公司 | Mooring system of unmanned aerial vehicle |
| CN105667834A (en) * | 2016-04-13 | 2016-06-15 | 云南电网有限责任公司电力科学研究院 | Device and method for testing unmanned aerial vehicle |
| CN106058783A (en) * | 2016-07-06 | 2016-10-26 | 合肥通鼎光电科技有限公司 | Communication cable coiling/uncoiling system for low-altitude sensing unmanned aerial vehicle |
| CN107757942A (en) * | 2016-08-19 | 2018-03-06 | 深圳航天旭飞科技有限公司 | The electric power supply control system of unmanned plane |
| CN106274625A (en) * | 2016-08-29 | 2017-01-04 | 西安天鹰防务科技有限公司 | A kind of mechanical arm type unmanned plane hoistable platform |
| CN106274625B (en) * | 2016-08-29 | 2019-01-22 | 江苏艾格信航空科技有限公司 | A kind of mechanical arm type unmanned plane hoistable platform |
| WO2018205099A1 (en) * | 2017-05-08 | 2018-11-15 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle protective device and method, unmanned aerial vehicle and flight field |
| CN106995058A (en) * | 2017-05-25 | 2017-08-01 | 许启超 | A kind of manned semiclosed low flyer of use current collector system |
| CN107187961A (en) * | 2017-07-15 | 2017-09-22 | 珠海市双捷科技有限公司 | Automatic deploying and retracting line apparatus, system and its control method for being tethered at unmanned plane |
| CN109131863A (en) * | 2018-09-10 | 2019-01-04 | 哈尔滨工业大学 | The more rotors of culvert type are tethered at unmanned plane and its control system |
| CN109895991A (en) * | 2018-12-12 | 2019-06-18 | 鲁金婵 | It is a kind of can wound wire collapsible unmanned plane |
| CN109677627A (en) * | 2019-01-11 | 2019-04-26 | 苏州全波通信技术股份有限公司 | It is tethered at unmanned plane precision approach control system and method |
| CN109607331A (en) * | 2019-02-13 | 2019-04-12 | 深圳市赛为智能股份有限公司 | One kind being tethered at unmanned plane retractable cable buffer structure and its working method |
| CN109607331B (en) * | 2019-02-13 | 2024-02-27 | 深圳市赛为智能股份有限公司 | Tethered unmanned aerial vehicle coiling and uncoiling line buffer structure and working method thereof |
| CN109775481A (en) * | 2019-02-15 | 2019-05-21 | 湖南优加特装智能科技有限公司 | For being tethered at the take-up and pay-off device of unmanned plane |
| WO2020168631A1 (en) * | 2019-02-19 | 2020-08-27 | 深圳市赛为智能股份有限公司 | Intelligent take-up and pay-off device for tethered unmanned aerial vehicle, and operating method thereof |
| WO2021126071A1 (en) | 2019-12-18 | 2021-06-24 | Avetics Global Pte. Ltd. | A tether management system and method |
| EP4077199A4 (en) * | 2019-12-18 | 2023-09-06 | Avetics Global Pte. Ltd. | A tether management system and method |
| CN116466734A (en) * | 2023-05-04 | 2023-07-21 | 山东御航智能科技有限公司 | Unmanned aerial vehicle threading method and system |
| CN116466734B (en) * | 2023-05-04 | 2024-02-06 | 山东御航智能科技有限公司 | Unmanned aerial vehicle threading method and system |
| CN118405546A (en) * | 2024-07-03 | 2024-07-30 | 凯姆乐(常州)电子有限公司 | Unmanned transplanter cable protection device |
| CN118405546B (en) * | 2024-07-03 | 2024-09-20 | 凯姆乐(常州)电子有限公司 | Unmanned transplanter cable protection device |
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