CN104753144B - Rotor wing unmanned aerial vehicle charging pile and charging method thereof - Google Patents
Rotor wing unmanned aerial vehicle charging pile and charging method thereof Download PDFInfo
- Publication number
- CN104753144B CN104753144B CN201510183600.0A CN201510183600A CN104753144B CN 104753144 B CN104753144 B CN 104753144B CN 201510183600 A CN201510183600 A CN 201510183600A CN 104753144 B CN104753144 B CN 104753144B
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- Prior art keywords
- aerial vehicle
- unmanned aerial
- rotor wing
- wing unmanned
- charging
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Classifications
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0042—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries characterised by the mechanical construction
Abstract
A kind of rotor wing unmanned aerial vehicle charging pile and charging method, including electric pushrod, protruding and communication module, the charging panel of rotor wing unmanned aerial vehicle is fixed with projection, four projections are one group, constitute a square, and projection is covered with charging panel, constitutes multiple square；Telescopic electric pushrod is arranged on the surrounding of charging panel, and the sawtooth projection bottom bumper bracket embeds in the gap that charging panel convexes to form, and rotor wing unmanned aerial vehicle can not move horizontally；After rotor wing unmanned aerial vehicle stable landing is on charging panel, irrotationality Ji is man-machine sends signal to communication module, after charging module receives signal, sends instruction to electric pushrod, and electric pushrod stretches out, bottom the bumper bracket of fixing rotor wing unmanned aerial vehicle.Present configuration is simple, safe and reliable, can ensure that in charging process and will not depart from charging panel because of strong wind weather or other reasons rotor wing unmanned aerial vehicle.
Description
Technical field
The present invention relates to a kind of charging panel, be specifically related to the charging pile that a kind of rotor wing unmanned aerial vehicle that can make to drop to charge on it obtains fixing, and the method realizing charging.
Background technology
Rotor wing unmanned aerial vehicle is the rapidest as a kind of novel aircraft development in recent years.Rotor wing unmanned aerial vehicle mainly uses electric power as power at present, and in order to extend its voyage, a kind of method is to increase the carried charge of battery, and its shortcoming is the weight simultaneously adding battery, makes rotor wing unmanned aerial vehicle load become big.Therefore it has been proposed that use photovoltaic charged stake in the way that rotor wing unmanned aerial vehicle flies, rotor wing unmanned aerial vehicle to be charged, in addition to this charging pile photovoltaic power generation plate needed for general photovoltaic generation, accumulator, also needing to a charging panel stopped for rotor wing unmanned aerial vehicle, this charging panel takes the mode of wireless charging to be charged rotor wing unmanned aerial vehicle.
Existing charging panel surface is the most smooth, under the weather such as strong wind, it is impossible to the rotor wing unmanned aerial vehicle charged is played fixation, easily makes rotor wing unmanned aerial vehicle generation level and vertically moves, and even landing from charging panel causes the waste of energy loss and electric resources.
Summary of the invention
The present invention proposes rotor wing unmanned aerial vehicle charging pile and charging method thereof, and this charging pile can play fixation to dropping to rotor wing unmanned aerial vehicle thereon, makes rotor wing unmanned aerial vehicle will not produce level and vertical displacement in charging process.
The present invention is reached by following measure:
A kind of rotor wing unmanned aerial vehicle charging pile includes, including support bar, photovoltaic power generation plate and accumulator, and also electric pushrod, triangular pyramid projection and communication module.Being fixed with pyramid on the charging panel of rotor wing unmanned aerial vehicle protruding, four projections are one group, constitute a square, and projection is covered with charging panel, constitutes multiple square.Communication module is fixed on the support bar of charging pile.
Electric pushrod is arranged on the surrounding of charging panel, and the height of distance charging panel is higher than the bumper bracket height away from charging panel after rotor wing unmanned aerial vehicle landing, and scalable, after rotor wing unmanned aerial vehicle lands, push rod stretches out, and plays the effect of fixing rotor wing unmanned aerial vehicle bumper bracket.
When rotor wing unmanned aerial vehicle drops on charging panel, the sawtooth projection bottom bumper bracket embeds in the gap that charging panel convexes to form so that rotor wing unmanned aerial vehicle can not move horizontally.After rotor wing unmanned aerial vehicle stable landing is on charging panel, irrotationality Ji is man-machine sends signal to communication module, after charging module receives signal, instruction is sent to electric pushrod, electric pushrod stretches out, and plays the effect bottom fixing bumper bracket, makes bumper bracket to move up.
After rotor wing unmanned aerial vehicle is charged, the communication module on charging panel sends the signal of " charging complete ", and now communication module makes electric pushrod regain to electric pushrod transmission instruction, and rotor wing unmanned aerial vehicle automatic takeoff leaves charging panel.
And require that dropping to rotor wing unmanned aerial vehicle thereon need to be furnished with bumper bracket, has little jagged projection bottom bumper bracket.
The present invention uses specific surface texture and frame for movement, guarantee the rotor wing unmanned aerial vehicle charging process dropping on plank cannot move horizontally under Rhizoma Sparganii bores convex role, cannot move up in the case of electric pushrod stretches out, cause electric resources to waste so that it is guaranteed that charging process will not depart from charging panel because of strong wind weather or other reasons rotor wing unmanned aerial vehicle.After rotor wing unmanned aerial vehicle is charged, sending certain signal to charging device, electric pushrod is retracted automatically, so that rotor wing unmanned aerial vehicle can normally take off.Meanwhile, manufacturing process of the present invention is simple, and limitation is little, has wide applicability.
Accompanying drawing explanation
Fig. 1 is the top view of the charging panel of the present invention；
Fig. 2 is the polycrystalline substance schematic diagram of the rotor wing unmanned aerial vehicle bumper bracket that the present invention relates to.
It is embodied as implementing
Embodiment 1
When rotor wing unmanned aerial vehicle drops on charging panel, Fig. 2 sawtooth projection 4 embeds in the gap that Fig. 1 triangular pyramid protruding 1 is formed so that rotor wing unmanned aerial vehicle can not move horizontally.After rotor wing unmanned aerial vehicle stable landing is on charging panel, the communication module 2 installed on Fig. 1 charging panel sends signal, after charging module 2 receives signal, electric pushrod 3 sends instruction, electric pushrod stretches out, and plays the effect bottom fixing bumper bracket, makes bumper bracket to move up.
After rotor wing unmanned aerial vehicle is charged, the communication module 2 on Fig. 1 charging panel sends the signal of " charging complete ", and now communication module makes electric pushrod regain to electric pushrod transmission instruction, and rotor wing unmanned aerial vehicle automatic takeoff leaves charging panel.
Embodiment 2:
The involved projection of the present invention can be other shapes; use the projection of Rhizoma Sparganii cone-shaped in the aforementioned embodiment; it can also be conical protrusions; can also be other shapes; as long as fixing rotor wing unmanned aerial vehicle can be played make the function of rotor wing unmanned aerial vehicle not occurred level displacement, all within the scope of rights protection of the present invention.
After the present invention the most no matter rotor wing unmanned aerial vehicle landing, which direction head is directed at, and bumper bracket all can embed in the gap that charging panel Rhizoma Sparganii cone convexes to form, and plays the effect of fixing rotor wing unmanned aerial vehicle；The position distribution design of electric pushrod may insure that the push rod at least two groups of different directions successfully stretches out, and reaches good fixation.Meanwhile, practicality limitation of the present invention is little, has the good suitability.
Claims (1)
1. the method for a rotor wing unmanned aerial vehicle charging pile charging, it is characterized in that: rotor wing unmanned aerial vehicle charging pile includes support bar, photovoltaic power generation plate and accumulator, also have electric pushrod, protruding and communication module, the charging panel of charging pile is fixed with projection, four projections are one group, constituting a square, projection is covered with charging panel, constitutes multiple square；Telescopic electric pushrod is arranged on the surrounding of charging panel, and the height of distance charging panel is higher than the bumper bracket height away from charging panel after rotor wing unmanned aerial vehicle landing, and communication module is fixed on the support bar of charging pile；When rotor wing unmanned aerial vehicle drops on charging panel, the sawtooth projection bottom rotor wing unmanned aerial vehicle bumper bracket embeds in the gap that charging panel convexes to form, and rotor wing unmanned aerial vehicle can not move horizontally；After rotor wing unmanned aerial vehicle stable landing is on charging panel, rotation Ji unmanned plane sends signal to communication module, after communication module receives signal, instruction is sent to electric pushrod, electric pushrod stretches out, and bottom the bumper bracket of fixing rotor wing unmanned aerial vehicle, makes bumper bracket to move up；After rotor wing unmanned aerial vehicle is charged, the communication module on charging panel sends the signal of " charging complete ", and communication module sends instruction to electric pushrod and electric pushrod is regained, and rotor wing unmanned aerial vehicle automatic takeoff leaves charging panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510183600.0A CN104753144B (en) | 2015-04-19 | 2015-04-19 | Rotor wing unmanned aerial vehicle charging pile and charging method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510183600.0A CN104753144B (en) | 2015-04-19 | 2015-04-19 | Rotor wing unmanned aerial vehicle charging pile and charging method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104753144A CN104753144A (en) | 2015-07-01 |
| CN104753144B true CN104753144B (en) | 2016-11-30 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201510183600.0A Expired - Fee Related CN104753144B (en) | 2015-04-19 | 2015-04-19 | Rotor wing unmanned aerial vehicle charging pile and charging method thereof |
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Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9828093B2 (en) * | 2015-05-27 | 2017-11-28 | First Principles, Inc. | System for recharging remotely controlled aerial vehicle, charging station and rechargeable remotely controlled aerial vehicle, and method of use thereof |
| CN104979882B (en) * | 2015-07-30 | 2017-03-01 | 安徽啄木鸟无人机科技有限公司 | A kind of unmanned plane quick charging system and its charging method |
| WO2017109780A1 (en) * | 2015-12-21 | 2017-06-29 | Straus Itai | Autonomous docking station for drones |
| CN106203672B (en) * | 2016-06-21 | 2020-03-24 | 中南大学 | Charging pile layout method for unmanned aerial vehicle flying along mission air line |
| CN106127335B (en) * | 2016-06-21 | 2020-08-21 | 中南大学 | Battery replacement base station layout method for electric multi-rotor unmanned aerial vehicle flying at ultra-long distance |
| CN106026270B (en) * | 2016-06-28 | 2018-10-30 | 泉州台商投资区本盛机械科技有限公司 | A kind of photovoltaic charged equipment of multi-rotor unmanned aerial vehicle |
| CN106026313A (en) * | 2016-08-03 | 2016-10-12 | 安徽钰龙信息科技有限公司 | Charging device of shipborne unmanned aerial vehicle |
| CN106542109A (en) * | 2016-11-04 | 2017-03-29 | 上海云犀智能系统有限公司 | A kind of unmanned plane recharging platform |
| CN108237934B (en) | 2016-12-27 | 2021-02-26 | 财团法人工业技术研究院 | Charging station and charging station module |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101403713B1 (en) * | 2012-04-30 | 2014-06-05 | 엘아이지넥스원 주식회사 | Dmfc fuel cell system for supplying power in quadrotor and method thereof |
| CN202642094U (en) * | 2012-05-15 | 2013-01-02 | 南京信息工程大学 | Landing gear for unmanned aerial vehicle |
| CN102815397B (en) * | 2012-08-22 | 2016-01-13 | 华北电力大学 | Can the Miniature multi-rotor aircraft of land and water landing and recharging |
| CN104309801B (en) * | 2014-09-26 | 2016-02-03 | 金陵科技学院 | A kind of middle part is rotary wind type unmanned plane and the landing seat thereof of spherical solar catcher |
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| CN104753144A (en) | 2015-07-01 |
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| CB03 | Change of inventor or designer information |
Inventor after: Jiang Zhiyuan Inventor after: Liu Yifeng Inventor after: Wu Jun Inventor after: Liu Jinze Inventor after: Sun Yu Inventor after: Zou Huan Inventor after: Peng Chaiyang Inventor after: Zhang Heteng Inventor after: Lv Zhongyuan Inventor after: Peng Chunhua Inventor after: Jing Hang Inventor after: Wu Jing Inventor after: Liu Peisen Inventor after: Kou Hongbo Inventor after: Hu Junying Inventor after: Wei Hao Inventor after: Shen Boxing Inventor before: Jiang Zhiyuan Inventor before: Sun Yu Inventor before: Zou Huan Inventor before: Peng Chaiyang Inventor before: Zhang Heteng Inventor before: Lv Zhongyuan Inventor before: Wu Jing Inventor before: Liu Peisen Inventor before: Kou Hongbo Inventor before: Hu Junying Inventor before: Wei Hao Inventor before: Liu Yifeng Inventor before: Wu Jun Inventor before: Liu Jinze |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161130 Termination date: 20170419 |