CN105668350A - Automatic take-up and payoff device and method for mooring unmanned aerial vehicle - Google Patents
Automatic take-up and payoff device and method for mooring unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105668350A CN105668350A CN201610248942.0A CN201610248942A CN105668350A CN 105668350 A CN105668350 A CN 105668350A CN 201610248942 A CN201610248942 A CN 201610248942A CN 105668350 A CN105668350 A CN 105668350A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- reel
- guide wheel
- power cable
- power
- 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.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 12
- 230000007246 mechanism Effects 0.000 claims abstract description 31
- 238000004804 winding Methods 0.000 claims abstract description 8
- 244000309464 bull Species 0.000 claims description 19
- 230000007423 decrease Effects 0.000 claims description 9
- 230000003287 optical effect Effects 0.000 claims description 9
- 238000007667 floating Methods 0.000 claims description 3
- 230000006870 function Effects 0.000 description 4
- 230000007547 defect Effects 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 230000008447 perception Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
- B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
- B65H75/34—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables
- B65H75/38—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material
- B65H75/40—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material mobile or transportable
- B65H75/42—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material mobile or transportable attached to, or forming part of, mobile tools, machines or vehicles
-
- 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
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
- B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
- B65H75/34—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables
- B65H75/38—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material
- B65H75/44—Constructional details
- B65H75/48—Automatic re-storing devices
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electric Cable Installation (AREA)
Abstract
The invention discloses an automatic take-up and payoff device and method for a mooring unmanned aerial vehicle. The automatic take-up and payoff device comprises a base, a winding reel, a guide wheel, a distance sensing mechanism, a power mechanism and a belt pulley mechanism, wherein the winding reel is fixed on the base by virtue of a winding reel vertical column; the guide wheel is positioned in the distance sensing mechanism; a power cable is wound around the winding reel; the guiding wheel is used for controlling the guiding of the power cable; the distance sensing mechanism comprises a screw rod, a polish rod, a guide wheel casing and distance sensors; the screw rod is rotationally connected to the screw rod vertical column on the base; the screw rod is fixedly connected with the guide wheel casing; the guide wheel is rotationally arranged in the guide wheel casing by virtue of the polish rod; a wire-pulling rotating rod is fixedly connected between the screw rod and the polish rod, and is connected with the distance sensors; the distance sensor is in signal connection with the power mechanism; power is transmitted to the power mechanism, the winding reel and the distance sensors through the belt pulley mechanism.
Description
Technical field
The present invention relates to a kind of mooring unmanned plane automatic deploying and retracting line apparatus, automatic deploying and retracting line method.
Background technology
Mooring unmanned plane commercially occurs, and is known by masses, along with the application of mooring unmanned plane, consequently also occurs in that the take-up and pay-off device for mooring unmanned plane, utilizes take-up and pay-off device just can easily mooring unmanned plane be controlled.
But, the mooring unmanned plane wire coiling and releasing that presently, there are is set to manual type, function is more single and traditional, it is only capable of along with unmanned plane during flying realizes passive unwrapping wire, and automatic takeup can not be realized along with unmanned plane landing, when unmanned plane lands, need to rotate take-up manually and carry out take-up, this has resulted in the shortcoming that take-up work is heavy, simultaneously when manually in time unnecessary power cable not being taken in take-up and pay-off device, very easily there is the situation of tangled up and knotted in unnecessary power cable, easily cause potential safety hazard, so, ensure that power cable take-up is easy, safety is the short slab of existing mooring unmanned plane take-up and pay-off device.
So, need badly and develop a kind of automatic deploying and retracting line apparatus for mooring unmanned plane, to solve above-mentioned technical problem.
Summary of the invention
Present invention aim to address in prior art, mooring unmanned plane from take-up and pay-off device troublesome poeration, safety is low, do not possess the defect of automation function.
In order to solve above-mentioned technical problem, this application provides following technical scheme:
A kind of mooring unmanned plane automatic deploying and retracting line apparatus, including base, reel, guide wheel, Distance-sensing mechanism, actuating unit and belt wheel mechanism;
Described reel is fixed on described base by reel column, and described guide wheel is positioned at described Distance-sensing mechanism, and described reel is used for winding power cable, and described guide wheel is for controlling the guiding of power cable;
Described Distance-sensing mechanism includes leading screw, polished rod, guide wheel cover and range sensor;
Described screw turns is connected to the leading screw column being fixed on described base, and described leading screw is also fixing connects guide wheel cover, and described guide wheel is rotated by described polished rod and is arranged in described guide wheel cover;
Be fixedly connected with, between described leading screw and described polished rod, bull stick of pulling strings, described in bull stick of pulling strings be connected with described range sensor;
Described range sensor is connected with described actuating unit signal;
Described actuating unit, described reel and described Distance-sensing are inter-agency transmits power by described belt wheel mechanism.
Further, in one embodiment, described base is provided with optical track column, this optical track column is provided with the slideway suitable with described polished rod.
Further, in one embodiment, described belt wheel mechanism includes two power belt wheels, four reel belt wheels and two screw pulley;
Two described powered belt wheel is rotationally connected with in described actuating unit the outfan of motor both sides;
Two described screw pulley are fixedly connected on the two ends of described leading screw.
Further, in one embodiment, four described reel belt wheels include two the first reel belt wheels and two the second reel belt wheels;
Two described first reel belt wheels are fixedly connected on the two ends of described reel;
Two described second reel belt wheels are positioned at the both sides of described reel column, for transmitting the power between described power belt wheel and described first reel belt wheel.
Further, in one embodiment, described range sensor includes piano wire, described in bull stick of pulling strings be connected with described piano wire.
A kind of automatic deploying and retracting line method based on described mooring unmanned plane automatic deploying and retracting line apparatus, the stressing conditions of power cable is monitored by described polished rod, and described stressing conditions is passed to described range sensor, the lifting situation of unmanned plane is judged by range sensor;
When judging that unmanned plane is in propradation, transmit the signal of automatic unwrapping wire to actuating unit;
When judging that unmanned plane is in decline state, transmit the signal of automatic takeup to actuating unit.
Further, in one embodiment, described stressing conditions includes: by accelerating pulling force, being subject to fixing pulling force and by pulling force.
Further, in one embodiment, described stressing conditions corresponds to the kinestate of unmanned plane:
When power cable is by when accelerating pulling force, unmanned plane is in propradation;
When power cable is by fixing pulling force, unmanned plane is in floating state;
When power cable is not by pulling force, unmanned plane is in decline state.
According to technique scheme, this technical scheme can pass through Distance-sensing mechanism and actuating unit automatically detects and judges the lifting situation of unmanned plane, the retractable cable state of the lifting situation motivation of adjustment mechanism according to unmanned plane, it is made to possess the function of automatic deploying and retracting line, then pass through reel, the cooperation of guide wheel and belt wheel mechanism, the lifting situation automatic deploying and retracting power cable of unmanned plane can be coordinated, the twisted and released of the cable making mooring unmanned plane realizes automatization, ensure that the convenience of mooring unmanned plane cable power twisted and released of the cable, safety and efficiency, and described mooring unmanned plane automatic deploying and retracting line apparatus simple in construction, reliability is high, hovering is stable.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present application or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, the accompanying drawing that the following describes is only some embodiments recorded in the application, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the structural representation of mooring unmanned plane automatic deploying and retracting line apparatus described herein.
Detailed description of the invention
In order to make those skilled in the art be more fully understood that the present invention program, below in conjunction with the accompanying drawing in the embodiment of the present invention, technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is only a part of embodiment of the present invention, rather than whole embodiments. Based on the embodiment in the present invention, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of protection of the invention.
In order to solve in prior art mooring unmanned plane from take-up and pay-off device troublesome poeration, safety is low, do not possess the defect of automation function, this application provides a kind of mooring unmanned plane automatic deploying and retracting line apparatus, including base 1, reel 6, guide wheel 10, Distance-sensing mechanism, actuating unit and belt wheel mechanism; Described base 1 is fixed on unmanned aerial vehicle platform, for fixing overall mooring unmanned plane automatic deploying and retracting line apparatus, it is achieved the retractable cable on ground, controls the flight of unmanned plane.
Described reel 6 is fixed on described base 1 by reel column 61, and described guide wheel 10 is positioned at described Distance-sensing mechanism, and described reel 6 is for winding power cable, and described guide wheel 10 is for controlling the guiding of power cable; Being wrapped in by the power cable of Len req on described reel 6, power cable walks around guide wheel 10 for the one end connecting unmanned plane, is connected with unmanned plane through guide wheel 10 guiding;
Described Distance-sensing mechanism includes leading screw 8, polished rod 11, guide wheel cover 9 and range sensor 2; Distance-sensing mechanism is for detecting the lifting situation of unmanned plane, and the lifting situation according to unmanned plane passes to the corresponding signal of actuating unit, makes actuating unit automatically make the action of retractable cable, it is achieved the retractable cable of power cable.
Concrete, as shown in Figure 1, described leading screw 8 is rotationally connected with the leading screw column 81 being fixed on described base 1, described leading screw 8 is also fixing connects guide wheel cover 9, described guide wheel 10 is rotated by described polished rod 11 and is arranged in described guide wheel cover 9, is fixedly connected with, between described leading screw 8 and described polished rod 11, bull stick 13 of pulling strings; Owing to guide wheel 10 and guide wheel cover 9 one end are fixed on leading screw 8, the other end is fixed on polished rod 11, bull stick 13 one end of pulling strings is fixed on leading screw 8, the other end is fixed on polished rod 11, the bull stick 13 that so can make to pull strings keeps the consistent of motion with guide wheel 10 and guide wheel cover 9, and along with receiving the difference of power cable pull, polished rod 11 can on optical track column 12 back and forth movement.
Described bull stick 13 of pulling strings is connected with described range sensor 2; When bull stick 13 of pulling strings moves up and down along with guide wheel 10 and guide wheel cover 9, the variable quantity of range sensor 2 perceived distance, described range sensor 2 is connected with described actuating unit signal, to signal, range sensor perception can be fed back to motor.
Described actuating unit, described reel 6 and described Distance-sensing are inter-agency transmits power by described belt wheel mechanism. As it is shown in figure 1, described belt wheel mechanism includes 3, four reel belt wheels of two power belt wheels and two screw pulley 7; The outfan of the motor both sides that two described power belt wheels 3 are rotationally connected with in described actuating unit; Two described screw pulley 7 are fixedly connected on the two ends of described leading screw 8. Four described reel belt wheels include two the first reel belt wheels 5 and two the second reel belt wheels 4; Two described first reel belt wheels 5 are fixedly connected on the two ends of described reel 6; Two described second reel belt wheels are positioned at the both sides of described reel column 61, for transmitting the power between described power belt wheel 3 and described first reel belt wheel 5.
Wherein, the power belt wheel 3 connecting motor is connected by Timing Belt and the second reel belt wheel 4, second reel belt wheel 4 includes inner side belt wheel and outside belt wheel, inner side belt wheel and outside belt wheel synchronous axial system, described outside belt wheel is for being connected with power belt wheel 3 by Timing Belt, described inner side belt wheel and outside belt wheel synchronous axial system, and connected by Timing Belt and the first reel belt wheel 5, further, first reel belt wheel 5 is connected with screw pulley 7 by Timing Belt, so that the power of actuating unit is delivered on screw pulley 7 by Timing Belt, and drive screw turns.
Further, in one embodiment, described base 1 is provided with optical track column 12, this optical track column 12 is provided with the slideway 14 suitable with described polished rod 11. Owing to pulling strings, bull stick 13 keeps the consistent of motion with guide wheel 10 and guide wheel cover 9, and along with receiving the difference of power cable pull, described polished rod 11 can back and forth movement in the slideway on optical track column 12, slideway 14 is for controlling the back and forth movement degree of polished rod 11, it is to avoid unmanned plane pulls the pulling force of guide wheel 10 to cross ambassador's failure of apparatus by power cable.
Further, in one embodiment, described range sensor 2 includes piano wire, described in bull stick 13 of pulling strings be connected with described piano wire. When guide wheel 10 rises or falls, bull stick 13 of pulling strings increases or reduction apart from D with underframe 1, and piano wire is pulled out from range sensor 2 or regains by bull stick 13 of simultaneously pulling strings, after range sensor 2 detects that piano wire is drawn out or regains, the lifting situation of unmanned plane can be judged, signal is fed back to motor.
A kind of automatic deploying and retracting line method based on described mooring unmanned plane automatic deploying and retracting line apparatus, the stressing conditions of power cable is monitored by described polished rod 11, and described stressing conditions is passed to described range sensor 2, the lifting situation of unmanned plane is judged by range sensor 2;
When judging that unmanned plane is in propradation, transmit the signal of automatic unwrapping wire to actuating unit;
When judging that unmanned plane is in decline state, transmit the signal of automatic takeup to actuating unit.
Further, in one embodiment, described stressing conditions includes: by accelerating pulling force, being subject to fixing pulling force and by pulling force.
Further, in one embodiment, described stressing conditions corresponds to the kinestate of unmanned plane:
When power cable is by when accelerating pulling force, unmanned plane is in propradation;
When power cable is by fixing pulling force, unmanned plane is in floating state;
When power cable is not by pulling force, unmanned plane is in decline state.
Its operation principle is: when unmanned plane is in propradation, and power cable pulling force continues to increase, and now power cable is by accelerating pulling force, drives guide wheel 10 to rise; Guide wheel 10 rises, bull stick 13 of pulling strings increases apart from D with underframe 1, piano wire is pulled out by bull stick 13 of simultaneously pulling strings from range sensor 2, range sensor 2 detects that signal is fed back to motor after being drawn out by piano wire, driven by motor reel 6 starts to rotate unwrapping wire therewith, simultaneously, reel 6 coordinates Timing Belt to drive leading screw 8 to rotate by belt wheel mechanism, leading screw 8 rotates and drives band guide wheel 10 and guide wheel cover 9, driving polished rod 11 to do back and forth movement in the slideway 14 of optical track column, its round trip cycle is just consistent with the reel 6 retractable cable cycle simultaneously.
When the unmanned plane rate of climb reduces until when hovering, power cable tension reduces therewith, guide wheel 10 is driven to decline; Bull stick 13 of pulling strings reduces apart from D with underframe 1, and signal is fed back to motor by range sensor 2, and motor speed starts to reduce until stopping operating therewith.
When unmanned plane is in the decline stage, power cable tension continues to reduce, and guide wheel 10 by the pulling force of power cable, does not decline due to gravity. Bull stick 13 of pulling strings reduces apart from D with underframe 1, and signal is fed back to motor by range sensor 2, and motor starts to reversely rotate, reel 6 take-up therewith.
Above mooring unmanned plane automatic deploying and retracting line apparatus provided by the present invention, automatic deploying and retracting line method are described in detail. Principles of the invention and embodiment are set forth by specific case used herein, and the explanation of above example is only intended to help to understand method and the core concept thereof of the present invention. It should be pointed out that, for those skilled in the art, under the premise without departing from the principles of the invention, it is also possible to the present invention carries out some improvement and modification, these improve and modify in the protection domain also falling into the claims in the present invention.
Claims (8)
1. a mooring unmanned plane automatic deploying and retracting line apparatus, it is characterised in that include base, reel, guide wheel, Distance-sensing mechanism, actuating unit and belt wheel mechanism;
Described reel is fixed on described base by reel column, and described guide wheel is positioned at described Distance-sensing mechanism, and described reel is used for winding power cable, and described guide wheel is for controlling the guiding of power cable;
Described Distance-sensing mechanism includes leading screw, polished rod, guide wheel cover and range sensor;
Described screw turns is connected to the leading screw column being fixed on described base, and described leading screw is also fixing connects guide wheel cover, and described guide wheel is rotated by described polished rod and is arranged in described guide wheel cover;
Be fixedly connected with, between described leading screw and described polished rod, bull stick of pulling strings, described in bull stick of pulling strings be connected with described range sensor;
Described range sensor is connected with described actuating unit signal;
Described actuating unit, described reel and described Distance-sensing are inter-agency transmits power by described belt wheel mechanism.
2. mooring unmanned plane automatic deploying and retracting line apparatus as claimed in claim 1, it is characterised in that be provided with optical track column on described base, this optical track column is provided with the slideway suitable with described polished rod.
3. mooring unmanned plane automatic deploying and retracting line apparatus as claimed in claim 2, it is characterised in that described belt wheel mechanism includes two power belt wheels, four reel belt wheels and two screw pulley;
Two described powered belt wheel is rotationally connected with in described actuating unit the outfan of motor both sides;
Two described screw pulley are fixedly connected on the two ends of described leading screw.
4. mooring unmanned plane automatic deploying and retracting line apparatus as claimed in claim 3, it is characterised in that four described reel belt wheels include two the first reel belt wheels and two the second reel belt wheels;
Two described first reel belt wheels are fixedly connected on the two ends of described reel;
Two described second reel belt wheels are positioned at the both sides of described reel column, for transmitting the power between described power belt wheel and described first reel belt wheel.
5. mooring unmanned plane automatic deploying and retracting line apparatus as claimed in claim 4, it is characterised in that described range sensor includes piano wire, described in bull stick of pulling strings be connected with described piano wire.
6. the automatic deploying and retracting line method based on the mooring unmanned plane automatic deploying and retracting line apparatus described in any one of claim 1-5, it is characterized in that, the stressing conditions of power cable is monitored by described polished rod, and described stressing conditions is passed to described range sensor, the lifting situation of unmanned plane is judged by range sensor;
When judging that unmanned plane is in propradation, transmit the signal of automatic unwrapping wire to actuating unit;
When judging that unmanned plane is in decline state, transmit the signal of automatic takeup to actuating unit.
7. automatic deploying and retracting line method as claimed in claim 6, it is characterised in that described stressing conditions includes: by accelerating pulling force, being subject to fixing pulling force and not by pulling force.
8. automatic deploying and retracting line method as claimed in claim 7, it is characterised in that the kinestate of described stressing conditions and unmanned plane corresponds to:
When power cable is by when accelerating pulling force, unmanned plane is in propradation;
When power cable is by fixing pulling force, unmanned plane is in floating state;
When power cable is not by pulling force, unmanned plane is in decline state.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610248942.0A CN105668350A (en) | 2016-04-20 | 2016-04-20 | Automatic take-up and payoff device and method for mooring unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610248942.0A CN105668350A (en) | 2016-04-20 | 2016-04-20 | Automatic take-up and payoff device and method for mooring unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105668350A true CN105668350A (en) | 2016-06-15 |
Family
ID=56215630
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610248942.0A Pending CN105668350A (en) | 2016-04-20 | 2016-04-20 | Automatic take-up and payoff device and method for mooring unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105668350A (en) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005450A (en) * | 2016-06-27 | 2016-10-12 | 北京深远世宁科技有限公司 | Anti-electromagnetic method for mooring unmanned aerial vehicle and anti-electromagnetic structure of mooring unmanned aerial vehicle |
| CN106075765A (en) * | 2016-08-05 | 2016-11-09 | 杨勇 | A kind of hydrodynamic force fire-fighting aircraft |
| 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 |
| CN107128750A (en) * | 2017-06-28 | 2017-09-05 | 北京石油化工学院 | Novel robot umbilical cables reeling-up reeling-out device |
| CN107187960A (en) * | 2017-07-06 | 2017-09-22 | 西安科技大学 | Wired control machine people cable winding apparatus and drawing cable method |
| 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 |
| CN107238907A (en) * | 2017-07-18 | 2017-10-10 | 沈阳亨通光通信有限公司 | Aerial optical cable laying system and aerial optical cable laying method |
| CN108190657A (en) * | 2018-01-09 | 2018-06-22 | 深圳市科卫泰实业发展有限公司 | One kind is tethered at unmanned plane cable tension control device and method |
| CN108565816A (en) * | 2018-03-23 | 2018-09-21 | 北京化工大学 | Bobbin winder device between a kind of primary and secondary unmanned plane |
| CN108821036A (en) * | 2018-07-02 | 2018-11-16 | 合肥瀚翔智能科技有限公司 | One kind being tethered at unmanned plane with full-automatic hawser draw off gear |
| CN108910624A (en) * | 2018-06-05 | 2018-11-30 | 中国人民解放军第六九O五工厂 | It is tethered at unmanned plane folding and unfolding line method |
| CN108928686A (en) * | 2017-05-26 | 2018-12-04 | 东莞前沿技术研究院 | The control system and control method of hawser recycling |
| CN109704155A (en) * | 2018-10-11 | 2019-05-03 | 深圳市科卫泰实业发展有限公司 | A kind of simple type is tethered at unmanned plane automatic deploying and retracting line apparatus |
| WO2019095260A1 (en) * | 2017-11-17 | 2019-05-23 | 深圳市科比特航空科技有限公司 | Control apparatus for cable winding and unwinding and apparatus for cable winding and unwinding |
| CN111232767A (en) * | 2020-03-26 | 2020-06-05 | 秦皇岛港股份有限公司 | Walking positioning device for port mechanical equipment |
| CN112158683A (en) * | 2020-09-29 | 2021-01-01 | 西安应用光学研究所 | Automatic winding and unwinding device and method for photoelectric composite cable of miniaturized mooring unmanned aerial vehicle |
| CN113001352A (en) * | 2021-03-22 | 2021-06-22 | 吾尚良品环境服务(上海)有限公司 | A spooler for stone material is polished |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4825986A (en) * | 1983-09-02 | 1989-05-02 | Wyle Laboratories | Remotely controllable cable assembly |
| CN201927943U (en) * | 2011-01-13 | 2011-08-10 | 杨苡 | Onboard electric stringing device for unmanned air vehicle |
| CN203589583U (en) * | 2013-11-05 | 2014-05-07 | 国家电网公司 | Pay-off rack used for flight stringing |
| CN204079334U (en) * | 2014-09-04 | 2015-01-07 | 安徽民生信息股份有限公司 | A kind of electric winch for mooring unmanned vehicle |
| CN204999444U (en) * | 2015-08-04 | 2016-01-27 | 徐州创航科技有限公司 | Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft |
| CN205011173U (en) * | 2015-09-02 | 2016-02-03 | 深圳九星智能航空科技有限公司 | Power supply of staying unmanned aerial vehicle automatic paying out machine that receives construct |
| CN205555756U (en) * | 2016-04-20 | 2016-09-07 | 北京深远世宁科技有限公司 | Automatic coiling and uncoiling device of staying unmanned aerial vehicle |
-
2016
- 2016-04-20 CN CN201610248942.0A patent/CN105668350A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4825986A (en) * | 1983-09-02 | 1989-05-02 | Wyle Laboratories | Remotely controllable cable assembly |
| CN201927943U (en) * | 2011-01-13 | 2011-08-10 | 杨苡 | Onboard electric stringing device for unmanned air vehicle |
| CN203589583U (en) * | 2013-11-05 | 2014-05-07 | 国家电网公司 | Pay-off rack used for flight stringing |
| CN204079334U (en) * | 2014-09-04 | 2015-01-07 | 安徽民生信息股份有限公司 | A kind of electric winch for mooring unmanned vehicle |
| CN204999444U (en) * | 2015-08-04 | 2016-01-27 | 徐州创航科技有限公司 | Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft |
| CN205011173U (en) * | 2015-09-02 | 2016-02-03 | 深圳九星智能航空科技有限公司 | Power supply of staying unmanned aerial vehicle automatic paying out machine that receives construct |
| CN205555756U (en) * | 2016-04-20 | 2016-09-07 | 北京深远世宁科技有限公司 | Automatic coiling and uncoiling device of staying unmanned aerial vehicle |
Cited By (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005450A (en) * | 2016-06-27 | 2016-10-12 | 北京深远世宁科技有限公司 | Anti-electromagnetic method for mooring unmanned aerial vehicle and anti-electromagnetic structure of mooring unmanned aerial vehicle |
| CN106005450B (en) * | 2016-06-27 | 2018-07-10 | 北京深远世宁科技有限公司 | A kind of method for being tethered at the anti-electromagnetism of unmanned plane and it is tethered at the anti-electromagnetic structure of unmanned plane |
| 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 |
| CN106075765A (en) * | 2016-08-05 | 2016-11-09 | 杨勇 | A kind of hydrodynamic force fire-fighting aircraft |
| CN108928686A (en) * | 2017-05-26 | 2018-12-04 | 东莞前沿技术研究院 | The control system and control method of hawser recycling |
| CN108928686B (en) * | 2017-05-26 | 2024-06-11 | 深圳光启空间技术有限公司 | Control system and control method for cable recovery |
| CN107128750A (en) * | 2017-06-28 | 2017-09-05 | 北京石油化工学院 | Novel robot umbilical cables reeling-up reeling-out device |
| CN107187960A (en) * | 2017-07-06 | 2017-09-22 | 西安科技大学 | Wired control machine people cable winding apparatus and drawing cable method |
| CN107187960B (en) * | 2017-07-06 | 2018-09-21 | 西安科技大学 | Wired control robot cable winding apparatus and drawing cable method |
| 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 |
| CN107238907A (en) * | 2017-07-18 | 2017-10-10 | 沈阳亨通光通信有限公司 | Aerial optical cable laying system and aerial optical cable laying method |
| CN107238907B (en) * | 2017-07-18 | 2024-05-10 | 沈阳亨通光通信有限公司 | Aerial optical cable laying system and aerial optical cable laying method |
| WO2019095260A1 (en) * | 2017-11-17 | 2019-05-23 | 深圳市科比特航空科技有限公司 | Control apparatus for cable winding and unwinding and apparatus for cable winding and unwinding |
| CN108190657A (en) * | 2018-01-09 | 2018-06-22 | 深圳市科卫泰实业发展有限公司 | One kind is tethered at unmanned plane cable tension control device and method |
| CN108190657B (en) * | 2018-01-09 | 2019-10-15 | 深圳市科卫泰实业发展有限公司 | One kind being tethered at unmanned plane cable tension control device and method |
| CN108565816A (en) * | 2018-03-23 | 2018-09-21 | 北京化工大学 | Bobbin winder device between a kind of primary and secondary unmanned plane |
| CN108565816B (en) * | 2018-03-23 | 2023-08-29 | 北京化工大学 | Winding device between primary and secondary unmanned aerial vehicle |
| CN108910624A (en) * | 2018-06-05 | 2018-11-30 | 中国人民解放军第六九O五工厂 | It is tethered at unmanned plane folding and unfolding line method |
| CN108821036A (en) * | 2018-07-02 | 2018-11-16 | 合肥瀚翔智能科技有限公司 | One kind being tethered at unmanned plane with full-automatic hawser draw off gear |
| CN109704155A (en) * | 2018-10-11 | 2019-05-03 | 深圳市科卫泰实业发展有限公司 | A kind of simple type is tethered at unmanned plane automatic deploying and retracting line apparatus |
| CN111232767A (en) * | 2020-03-26 | 2020-06-05 | 秦皇岛港股份有限公司 | Walking positioning device for port mechanical equipment |
| CN112158683A (en) * | 2020-09-29 | 2021-01-01 | 西安应用光学研究所 | Automatic winding and unwinding device and method for photoelectric composite cable of miniaturized mooring unmanned aerial vehicle |
| CN113001352A (en) * | 2021-03-22 | 2021-06-22 | 吾尚良品环境服务(上海)有限公司 | A spooler for stone material is polished |
| CN113001352B (en) * | 2021-03-22 | 2022-02-22 | 吾尚良品环境服务(上海)有限公司 | A spooler for stone material is polished |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105668350A (en) | Automatic take-up and payoff device and method for mooring unmanned aerial vehicle | |
| CN205555756U (en) | Automatic coiling and uncoiling device of staying unmanned aerial vehicle | |
| CN104743129B (en) | For being tethered at the automatic lock take-up and pay-off device of unmanned plane | |
| CN204999444U (en) | Automatic coiling and uncoiling device of unmanned aerial vehicle aircraft | |
| CN202670911U (en) | Rewinding device | |
| CN106005462A (en) | Retraction system for mooring unmanned aerial vehicle and method for deploying and retracting mooring unmanned aerial vehicle with same | |
| CN102135651B (en) | Optical fiber micro cable withdrawing and releasing winch | |
| CA2935496C (en) | Lifting apparatus for highly mounted equipment | |
| CN105967002B (en) | Hawser extension and retraction system | |
| CN205294508U (en) | Power supply of staying unmanned aerial vehicle automatic paying out machine that receives construct | |
| WO2019015086A1 (en) | Automatic take-up and pay-off device and system for moored unmanned aerial vehicle and control method thereof | |
| CN105947917A (en) | Towing winch for ground mooring of aerostat | |
| CN108249231A (en) | It is tethered at the change torque cable winding apparatus of unmanned plane and its folding and unfolding cable method | |
| CN112408226A (en) | Winding device and parachute system adopting same | |
| CN107732669B (en) | Intelligent full-automatic lifting lightning protection equipment | |
| CN108892007A (en) | A kind of hawser draw off gear | |
| CN203199792U (en) | Control device of wire arranging flatness for take-up machine | |
| JP7048082B2 (en) | Pilot rope wire drawing and recovery device | |
| CN205114915U (en) | Hoist cable drum cable protection device | |
| CN205931306U (en) | Unmanned aerial vehicle's power supply control system | |
| CN105584639B (en) | A kind of integrated disc type carrier landing stopping device and its method for arresting with clutch | |
| CN108439088B (en) | Wire rope winding and unwinding device and wire rope winding and unwinding method | |
| CN110467053A (en) | A kind of galvanized wire wrap-up | |
| CN206116100U (en) | Around automatic pay -off of chartered plane | |
| CN215974442U (en) | Reciprocating winding mechanism of winch for hydraulic culvert detection vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160615 |
|
| WD01 | Invention patent application deemed withdrawn after publication |