CN106033826A - Multi-rotary-wing unmanned aerial vehicle returning automatic charging method - Google Patents
Multi-rotary-wing unmanned aerial vehicle returning automatic charging method Download PDFInfo
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- CN106033826A CN106033826A CN201510115721.1A CN201510115721A CN106033826A CN 106033826 A CN106033826 A CN 106033826A CN 201510115721 A CN201510115721 A CN 201510115721A CN 106033826 A CN106033826 A CN 106033826A
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
Abstract
The invention discloses a multi-rotary-wing unmanned aerial vehicle returning automatic charging method, which comprises: (1) arranging a takeoff and landing platform for a multi-rotary-wing unmanned aerial vehicle at a designated landing place, wherein direct current positive electrodes and direct current negative electrodes are alternately and completely paved on the whole takeoff and landing platform; (2) additionally arranging electric conduction contact electrodes at four corners of the under carriage of the multi-rotary-wing unmanned aerial vehicle, wherein the electric conduction contact electrode is used for contacting the electrode arranged on the takeoff and landing platform; and (3) using a bridge type rectification circuit behind each contact point of the multi-rotary-wing unmanned aerial vehicle, wherein the bridge type rectification circuit is used for resolving the positive electrode and the negative electrode, and connecting the electrode to the correct electrode at the battery charging interface. With the multi-rotary-wing unmanned aerial vehicle returning automatic charging method of the present invention, the charging process does not need manual participation, the automatic returning charging of the multi-rotary-wing unmanned aerial vehicle can be achieved in the unattended case, and the application range of the multi-rotary-wing unmanned aerial vehicle is substantially expanded.
Description
Technical field
The present invention relates to a kind of many rotor unmanned aircrafts make a return voyage automatic recharging method.
Background technology
Multi-rotor aerocraft is just being widely used in the fields such as aerial photographing, environment measuring, traffic supervision, electric power inspection and field rescue, has wide military and civilian prospect.But it is limited by the shortcoming that multi-rotor aerocraft endurance distance is short, completes long job demand and carry out charging of making a return voyage repeatedly.The most quickly and complete charging of making a return voyage automatically, then become this area institute problem in urgent need to solve.
Current existing charging scheme, almost all needs artificial participation, if it is possible to realizes the charging of automatically making a return voyage of many rotor wing unmanned aerial vehicles in the case of unmanned, will extend the range of application of many rotor wing unmanned aerial vehicles greatly.
Battery capacity entrained by many rotor unmanned aircrafts is much larger than general portable electric appts, and current wireless charging technology cannot meet the high-power charge requirement of aircraft battery.
Summary of the invention
The technical problem to be solved in the present invention is the defect overcoming prior art, it is provided that a kind of many rotor unmanned aircrafts make a return voyage automatic recharging method.
In order to solve above-mentioned technical problem, the invention provides following technical scheme:
A kind of many rotor unmanned aircrafts of the present invention make a return voyage automatic recharging method, and it comprises the following steps:
(1) it is that many rotor unmanned aircrafts are specifying landing erection site landing platform, landing platform is alternately paved with whole landing platform with galvanic positive and negative electrode；
(2) four angles of undercarriage at many rotor unmanned aircrafts install conductive pole contact additional, and described conductive pole contact is used for and the electrode contact being arranged on described landing platform；
(3) all using a bridge rectifier behind each contact of many rotor unmanned aircrafts, described bridge rectifier is for differentiating the positive and negative of electrode and being connected by the electrode that it is correct with battery charging inlet.
Further, the electrode of landing platform is set to square, and the undercarriage of described many rotor unmanned aircrafts is sized slightly larger than the square dimensions of each electrode.Owing to therefore the undercarriage size of many rotor unmanned aircrafts can ensure that the tactile pole on four angles of many rotor unmanned aircrafts at least must can touch on undercarriage positive one negative slightly larger than the size of each electrode.
After many rotor unmanned aircrafts drop to landing platform and contact with electrode, the automatic charging process to many rotor unmanned aircrafts battery can be started.
Further, if there is the situation of electrode loose contact, many rotor unmanned aircrafts pass through airborne computer monitor cell voltage, if the voltage of battery does not rise in one minute, airborne computer thinks that charging does not starts to, and many rotor unmanned aircrafts can the most again take off and reattempt to and drop to specify on platform.
The present invention is reached to provide the benefit that:
Many rotor unmanned aircrafts that the present invention provides make a return voyage automatic recharging method, and charging process need not artificial participation, it is possible to realize the charging of automatically making a return voyage of many rotor wing unmanned aerial vehicles in the case of unmanned, extend the range of application of many rotor wing unmanned aerial vehicles greatly.
Accompanying drawing explanation
Accompanying drawing is for providing a further understanding of the present invention, and constitutes a part for description, is used for together with embodiments of the present invention explaining the present invention, is not intended that limitation of the present invention.In the accompanying drawings:
Fig. 1 is the present invention many rotor unmanned aircrafts landing platform schematic diagram；
Fig. 2 is the schematic diagram of the polarity of the electrode of the platform that rises and falls being judged contact by bridge rectifier；
Fig. 3 is the automatic charger structural representation of many rotor unmanned aircrafts；
Fig. 4 is the structural representation of the present invention.
Detailed description of the invention
Below in conjunction with accompanying drawing, the preferred embodiments of the present invention are illustrated, it will be appreciated that preferred embodiment described herein is merely to illustrate and explains the present invention, is not intended to limit the present invention.
As Figure 1-4, a kind of many rotor unmanned aircrafts of the present invention make a return voyage automatic recharging method, and it comprises the following steps:
(1) it is that many rotor unmanned aircrafts are specifying landing erection site landing platform 1, landing platform 1 is alternately paved with whole landing platform 1 with galvanic positive and negative electrode；
(2) 2 four angles of undercarriage at many rotor unmanned aircrafts install conductive pole contact 3 additional, and described conductive pole contact 3 is used for and the electrode contact being arranged on described landing platform；
(3) all using a bridge rectifier after each conductive pole contact 3 of many rotor unmanned aircrafts, described bridge rectifier is for differentiating the positive and negative of electrode and being connected by the electrode that it is correct with battery charging inlet.
Further, the electrode of landing platform is set to square, and the undercarriage of described many rotor unmanned aircrafts is sized slightly larger than the square dimensions of each electrode.Owing to therefore the undercarriage size of many rotor unmanned aircrafts can ensure that the tactile pole on four angles of many rotor unmanned aircrafts at least must can touch on undercarriage positive one negative slightly larger than the size of each electrode.
After many rotor unmanned aircrafts drop to landing platform and contact with electrode, the automatic charging process to many rotor unmanned aircrafts battery can be started.
Further, if there is the situation of electrode loose contact, many rotor unmanned aircrafts pass through airborne computer monitor cell voltage, if the voltage of battery does not rise in one minute, airborne computer thinks that charging does not starts to, and many rotor unmanned aircrafts can the most again take off and reattempt to and drop to specify on platform.
The present invention is reached to provide the benefit that:
Many rotor unmanned aircrafts that the present invention provides make a return voyage automatic recharging method, and charging process need not artificial participation, it is possible to realize the charging of automatically making a return voyage of many rotor wing unmanned aerial vehicles in the case of unmanned, extend the range of application of many rotor wing unmanned aerial vehicles greatly.
Last it is noted that the foregoing is only the preferred embodiments of the present invention, it is not limited to the present invention, although the present invention being described in detail with reference to previous embodiment, for a person skilled in the art, technical scheme described in foregoing embodiments still can be modified by it, or wherein portion of techniques feature is carried out equivalent.All within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. made, should be included within the scope of the present invention.
Claims (3)
1. rotor unmanned aircraft more than a kind makes a return voyage automatic recharging method, it is characterised in that comprise the following steps:
(1) it is that many rotor unmanned aircrafts are specifying landing erection site landing platform, landing platform is alternately paved with whole landing platform with galvanic positive and negative electrode；
(2) four angles of undercarriage at many rotor unmanned aircrafts install conductive pole contact additional, and described conductive pole contact is used for and the electrode contact being arranged on described landing platform；
(3) all using a bridge rectifier behind each contact of many rotor unmanned aircrafts, described bridge rectifier is for differentiating the positive and negative of electrode and being connected by the electrode that it is correct with battery charging inlet.
The many rotor unmanned aircrafts of one the most according to claim 1 make a return voyage automatic recharging method, it is characterised in that the electrode of landing platform is set to square, and the undercarriage of described many rotor unmanned aircrafts is sized slightly larger than the square dimensions of each electrode.
The many rotor unmanned aircrafts of one the most according to claim 1 make a return voyage automatic recharging method, it is characterized in that, if there is the situation of electrode loose contact, many rotor unmanned aircrafts pass through airborne computer monitor cell voltage, if the voltage of battery does not rise in one minute, airborne computer thinks that charging does not starts to, and many rotor unmanned aircrafts can the most again take off and reattempt to and drop to specify on platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510115721.1A CN106033826A (en) | 2015-03-17 | 2015-03-17 | Multi-rotary-wing unmanned aerial vehicle returning automatic charging method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510115721.1A CN106033826A (en) | 2015-03-17 | 2015-03-17 | Multi-rotary-wing unmanned aerial vehicle returning automatic charging method |
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| CN106033826A true CN106033826A (en) | 2016-10-19 |
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| CN201510115721.1A Pending CN106033826A (en) | 2015-03-17 | 2015-03-17 | Multi-rotary-wing unmanned aerial vehicle returning automatic charging method |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106992573A (en) * | 2017-05-18 | 2017-07-28 | 北京科技大学 | Multi-rotor unmanned aerial vehicle charging system and method |
| CN107128203A (en) * | 2017-06-02 | 2017-09-05 | 南宁市第二中学 | Portable unmanned plane charging station |
| CN108215817A (en) * | 2016-12-15 | 2018-06-29 | 比亚迪股份有限公司 | Charging system and a kind of vehicles for the vehicles |
| CN108923492A (en) * | 2018-08-12 | 2018-11-30 | 南京云睿航天科技有限公司 | A kind of unmanned plane single-contact charging plate |
| CN109050885A (en) * | 2018-08-12 | 2018-12-21 | 南京云睿航天科技有限公司 | A kind of unmanned plane Multi-contact charging plate |
| CN110901426A (en) * | 2019-12-09 | 2020-03-24 | 北京京东乾石科技有限公司 | Charging device, unmanned aerial vehicle, charging panel and unmanned aerial vehicle charging system |
| CN113928144A (en) * | 2021-04-22 | 2022-01-14 | 南京韬讯航空科技有限公司 | Mobile unmanned aerial vehicle take-off and landing platform and take-off and landing control method |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202929383U (en) * | 2012-09-11 | 2013-05-08 | 深圳一电科技有限公司 | Unmanned plane and automatic charging system thereof |
| US20140015493A1 (en) * | 2012-07-13 | 2014-01-16 | Ben WIRZ | Self-optimizing power transfer |
| CN204068303U (en) * | 2014-06-12 | 2014-12-31 | 深圳市大疆创新科技有限公司 | A kind of charging system, electric supply installation and aircraft |
-
2015
- 2015-03-17 CN CN201510115721.1A patent/CN106033826A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140015493A1 (en) * | 2012-07-13 | 2014-01-16 | Ben WIRZ | Self-optimizing power transfer |
| CN202929383U (en) * | 2012-09-11 | 2013-05-08 | 深圳一电科技有限公司 | Unmanned plane and automatic charging system thereof |
| CN204068303U (en) * | 2014-06-12 | 2014-12-31 | 深圳市大疆创新科技有限公司 | A kind of charging system, electric supply installation and aircraft |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108215817A (en) * | 2016-12-15 | 2018-06-29 | 比亚迪股份有限公司 | Charging system and a kind of vehicles for the vehicles |
| CN106992573A (en) * | 2017-05-18 | 2017-07-28 | 北京科技大学 | Multi-rotor unmanned aerial vehicle charging system and method |
| CN106992573B (en) * | 2017-05-18 | 2023-06-20 | 北京科技大学 | Multi-rotor unmanned aerial vehicle charging system and method |
| CN107128203A (en) * | 2017-06-02 | 2017-09-05 | 南宁市第二中学 | Portable unmanned plane charging station |
| CN108923492A (en) * | 2018-08-12 | 2018-11-30 | 南京云睿航天科技有限公司 | A kind of unmanned plane single-contact charging plate |
| CN109050885A (en) * | 2018-08-12 | 2018-12-21 | 南京云睿航天科技有限公司 | A kind of unmanned plane Multi-contact charging plate |
| CN110901426A (en) * | 2019-12-09 | 2020-03-24 | 北京京东乾石科技有限公司 | Charging device, unmanned aerial vehicle, charging panel and unmanned aerial vehicle charging system |
| CN110901426B (en) * | 2019-12-09 | 2021-05-25 | 北京京东乾石科技有限公司 | Charging device, unmanned aerial vehicle, charging panel and unmanned aerial vehicle charging system |
| CN113928144A (en) * | 2021-04-22 | 2022-01-14 | 南京韬讯航空科技有限公司 | Mobile unmanned aerial vehicle take-off and landing platform and take-off and landing control method |
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Application publication date: 20161019 |