CN204999444U - Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft - Google Patents
Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft Download PDFInfo
- Publication number
- CN204999444U CN204999444U CN201520577269.6U CN201520577269U CN204999444U CN 204999444 U CN204999444 U CN 204999444U CN 201520577269 U CN201520577269 U CN 201520577269U CN 204999444 U CN204999444 U CN 204999444U
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- capstan winch
- winch
- hydraulic pressure
- unmanned plane
- rotors
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Abstract
The utility model discloses an automatic coiling and uncoiling device of unmanned aerial vehicle aircraft, include capstan winch, capstan winch frame, install the hydraulic pressure stroke device in capstan winch frame top, hydraulic pressure stroke device include the hydraulic pressure slide bar with can be along the gliding sensor mechanism of hydraulic pressure slide bar, rubber wheel mechanism include pressure sensor guide pulley, range finding guide pulley, winding displacement guide pulley, the motor is connected to the capstan winch, capstan winch rest base portion install walking wheel, the capstan winch on have a photoelectric cables. The utility model has the characteristics of simple structure, reliability be high, hover stably, convenient to use and low cost etc. In the whole device, can intelligent realization cable receive and release in order, have rationally distributed, the mechanism is compact and safe and reliable etc, photoelectric cables and the intra -annular ball of sleeve can be in sliding contact, prevent that beating from appearing in the cable conductor to roll up or block dead phenomenon, the cable conductor that promotes moreover receive and release speed.
Description
Technical field
The utility model relates to a kind of automatic deploying and retracting line apparatus of 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 utility model provides a kind of automatic deploying and retracting line apparatus of unmanned plane during flying device, realizes the orderly folding and unfolding of cable, has rationally distributed, compact conformation and safe and reliable.
To achieve these goals, the technical solution adopted in the utility model is: a kind of automatic deploying and retracting line apparatus of unmanned plane during flying device, it is characterized in that comprising capstan winch, winch rack, be arranged on hydraulic stroke device above winch rack, described hydraulic stroke device comprises hydraulic pressure slide bar and can along the guide wheel mechanism of hydraulic pressure sliding bar, described guide wheel mechanism comprises pressure sensor guide wheel, range finding guide wheel, cable guide pulley, capstan winch connects motor
Bottom described winch rack, road wheel is installed, described capstan winch has photoelectric compound cable.
Described capstan winch spindle central has cabling sleeve, and cabling sleeve comprises liner ring, and 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.
Bottom described winch rack, road wheel is installed.
Also comprise controller, described controller is positioned at winch rack, and is connected with motor.
Described aircraft is many rotor wing unmanned aerial vehicles aircraft, and its rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
It is simple that the utility model 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, intelligent can realize the orderly folding and unfolding of cable, have rationally distributed, the features such as mechanism is compact and safe and reliable, ball in photoelectric compound cable and liner ring can be in moving contact, 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 utility model.
Fig. 2 is the utility model lateral plan.
Fig. 3 is wiring sleeve barrel structure figure.
In figure: 1, capstan winch, 2, winch rack, 3, hydraulic stroke device, 4, cable guide pulley, 5 range finding guide wheels, 6, pressure sensor guide wheel, 7, road wheel, 8, pull bar, 9, cabling sleeve, 91, liner ring, 92, ball.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail.
As shown in Figure 1, a kind of automatic deploying and retracting line apparatus of unmanned plane during flying device, it is characterized in that comprising capstan winch 1, winch rack 2, be arranged on hydraulic stroke device 3 above winch rack 2, described hydraulic stroke device 3 comprises hydraulic pressure slide bar and can along the guide wheel mechanism of hydraulic pressure sliding bar, described guide wheel mechanism comprises pressure sensor guide wheel 6, range finding guide wheel 5, cable guide pulley 4, capstan winch 1 connects motor, hydraulic stroke device 3 slowly can change the position of guide wheel mechanism, facilitates the retractable cable of photoelectric compound cable.
Bottom described winch rack 2, road wheel 7 is installed, described capstan winch 1 has photoelectric compound cable.
Described capstan winch 1 spindle central has cabling sleeve 9, cabling sleeve 9 comprises liner ring 91, liner ring 91 has multiple ball grooves, ball 92 is arranged in ball grooves, ball 92 is half naked state at the opening part of ball grooves, such photoelectric compound cable all the time with ball 92 moving contact, make photoelectric compound cable to produce stuck phenomenon.
Bottom described winch rack 2, road wheel 7 is installed.
Also comprise controller, described controller is positioned at capstan winch support, and is connected with motor.
Winch rack 2 side is also provided with pull bar 8, is convenient to mobile.
Guide wheel becomes set composite with pressure sensor with photoelectric code disk, and its device can by information, data transmission to controller; Composite cable passes guide wheel and coils through strand oscillator and is connected with capstan winch, forms certain angular distance power and composite cable is closely wrapped on strand oscillator; Controller by signal and information transmission for driving and controlling rotating speed and the rotating of buncher;
Described aircraft is many rotor wing unmanned aerial vehicles aircraft, and its rotor quantity is four rotors, six rotors, eight rotors or 16 rotors.
The above embodiment only represents several embodiments of utility model, describes comparatively concrete and detailed, but can not be interpreted as the restriction to the utility model scope.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 domain of the present utility model should be as the criterion with described claim.
Claims (4)
1. the automatic deploying and retracting line apparatus of a unmanned plane during flying device, it is characterized in that comprising capstan winch, winch rack, be arranged on hydraulic stroke device above winch rack, described hydraulic stroke device comprises hydraulic pressure slide bar and can along the guide wheel mechanism of hydraulic pressure sliding bar, described guide wheel mechanism comprises pressure sensor guide wheel, range finding guide wheel, cable guide pulley, capstan winch connects motor
Bottom described winch rack, road wheel is installed, described capstan winch has photoelectric compound cable,
The described capstan winch center of walking around has cabling sleeve, and cabling sleeve comprises liner ring, and 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.
2. the automatic deploying and retracting line apparatus of a kind of unmanned plane during flying device according to claim 1, is characterized in that being provided with road wheel bottom described winch rack.
3. the automatic deploying and retracting line apparatus of a kind of unmanned plane during flying device according to claim 1, it is characterized in that, also comprise controller, described controller is positioned at winch rack, and is connected with motor.
4. the automatic deploying and retracting line apparatus of a kind of 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.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520577269.6U CN204999444U (en) | 2015-08-04 | 2015-08-04 | Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520577269.6U CN204999444U (en) | 2015-08-04 | 2015-08-04 | Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204999444U true CN204999444U (en) | 2016-01-27 |
Family
ID=55156341
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520577269.6U Expired - Fee Related CN204999444U (en) | 2015-08-04 | 2015-08-04 | Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft |
Country Status (1)
| Country | Link |
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| CN (1) | CN204999444U (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105173105A (en) * | 2015-08-04 | 2015-12-23 | 徐州创航科技有限公司 | Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft |
| 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 |
| CN105668350A (en) * | 2016-04-20 | 2016-06-15 | 北京深远世宁科技有限公司 | Automatic take-up and payoff device and method for mooring 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 |
| CN106144926A (en) * | 2016-07-07 | 2016-11-23 | 衢州赋腾信息科技有限公司 | A kind of winch for unmanned plane |
| CN106516151A (en) * | 2016-12-07 | 2017-03-22 | 青海利高智能设备有限公司 | Unmanned aerial vehicle mooring base |
| CN107284689A (en) * | 2017-06-20 | 2017-10-24 | 安徽博识电子科技有限公司 | A kind of automatically controlled packaged type unmanned plane draw off gear |
| CN107298184A (en) * | 2017-06-20 | 2017-10-27 | 安徽博识电子科技有限公司 | A kind of protection type unmanned plane draw off gear |
| CN109748158A (en) * | 2017-11-02 | 2019-05-14 | 天津职业技术师范大学 | A kind of unmanned plane cable automatic retraction device |
| CN110240022A (en) * | 2019-07-19 | 2019-09-17 | 青岛大学附属医院 | A kind of Intensive Care Unit equipment conducting wire auto take-up |
| CN110406402A (en) * | 2018-12-10 | 2019-11-05 | 乌鲁木齐爱思特专利转让服务有限责任公司 | A kind of long-distance flight system |
-
2015
- 2015-08-04 CN CN201520577269.6U patent/CN204999444U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105173105A (en) * | 2015-08-04 | 2015-12-23 | 徐州创航科技有限公司 | Automatic cable coiling and uncoiling device used for mooring unmanned plane aircraft |
| 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 |
| CN105668350A (en) * | 2016-04-20 | 2016-06-15 | 北京深远世宁科技有限公司 | Automatic take-up and payoff device and method for mooring 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 |
| CN106144926A (en) * | 2016-07-07 | 2016-11-23 | 衢州赋腾信息科技有限公司 | A kind of winch for unmanned plane |
| CN106516151A (en) * | 2016-12-07 | 2017-03-22 | 青海利高智能设备有限公司 | Unmanned aerial vehicle mooring base |
| CN107284689A (en) * | 2017-06-20 | 2017-10-24 | 安徽博识电子科技有限公司 | A kind of automatically controlled packaged type unmanned plane draw off gear |
| CN107298184A (en) * | 2017-06-20 | 2017-10-27 | 安徽博识电子科技有限公司 | A kind of protection type unmanned plane draw off gear |
| CN109748158A (en) * | 2017-11-02 | 2019-05-14 | 天津职业技术师范大学 | A kind of unmanned plane cable automatic retraction device |
| CN110406402A (en) * | 2018-12-10 | 2019-11-05 | 乌鲁木齐爱思特专利转让服务有限责任公司 | A kind of long-distance flight system |
| CN110406402B (en) * | 2018-12-10 | 2023-10-03 | 乌鲁木齐爱思特专利转让服务有限责任公司 | Remote flight system |
| CN110240022A (en) * | 2019-07-19 | 2019-09-17 | 青岛大学附属医院 | A kind of Intensive Care Unit equipment conducting wire auto take-up |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160127 Termination date: 20160804 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |