CN103523236A - Unmanned aerial vehicle wind energy recycling device - Google Patents
Unmanned aerial vehicle wind energy recycling device Download PDFInfo
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- CN103523236A CN103523236A CN201310507107.0A CN201310507107A CN103523236A CN 103523236 A CN103523236 A CN 103523236A CN 201310507107 A CN201310507107 A CN 201310507107A CN 103523236 A CN103523236 A CN 103523236A
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- wind energy
- unmanned plane
- aerial vehicle
- unmanned aerial
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Abstract
The invention relates to an unmanned aerial vehicle assembly, in particular to an unmanned aerial vehicle wind energy recycling device. The unmanned aerial vehicle wind energy recycling device comprises a device body, an electronic device installed inside the device body and a first storage battery connected with the electronic device. The device body is provided with a blade assembly which is connected with a wind driven generator, the wind driven generator is connected with a second storage battery through a control circuit, and the first storage battery is connected to the control circuit and then is connected into the electronic device. According to the unmanned aerial vehicle wind energy recycling device, the electric energy produced by wind power when an unmanned aerial vehicle flies is stored and then is supplied to the electronic device on the unmanned aerial vehicle, and after the electric power is used up, an original battery of the unmanned aerial vehicle is used for supplying electricity, and charging is continuously carried out through the wind power. Therefore, the continuous journey mileage of the unmanned aerial vehicle is increased and continuous journey time is prolonged.
Description
Technical field
The present invention relates to a kind of unmanned plane assembly, especially a kind of unmanned plane wind energy regenerative apparatus.
Background technology
Robot airplane is called for short " unmanned plane ", is the not manned aircraft that utilizes radio robot and the process controller of providing for oneself to handle.On machine, without driving compartment, but the equipment such as autopilot, process controller are installed.On ground, naval vessels or machine tool command and control station personnel by equipment such as radars, to its follow the tracks of, location, remote control, remote measurement and digital communication.Can under radio telecommand, as conventional airplane, take off or launch with booster rocket, also can take aerial input to by machine tool and fly.During recovery, the available mode automatic Landing the same with conventional airplane landing mission, also can reclaim with parachute or block by remote control.
Unmanned plane is generally divided into two parts to the consumption of the energy, a part is for driving the consumption of power of unmanned plane during flying, a part is for communication and control the power consumption bringing, in existing unmanned plane, having the fuel oil of use is power fuel, battery is the design of electronic equipment power source, also there is full electric power energy, which kind of form no matter, because needing continual and ground to carry out communication, unmanned plane obtains orientation and control signal aloft, so its consumption of current is very big, the electric weight of battery is often not enough to maintain the long-time continuation of the journey of unmanned plane, makes the use of unmanned plane receive restriction.
Summary of the invention
The invention provides and a kind ofly can effectively improve the course continuation mileage of unmanned plane and the unmanned plane wind energy regenerative apparatus of time.
To achieve these goals, the present invention adopts following technical scheme:
The first storage battery that comprises fuselage, is located at the electronic machine in fuselage and is connected with electronic machine, described fuselage is provided with fan blade assembly, described fan blade assembly connects an aerogenerator, described aerogenerator connects the second storage battery by a control circuit, after the first described storage battery Access Control circuit, accesses electronic machine.
Preferably, described fan blade assembly is located at fuselage bottom.
Preferably, described control circuit comprises the first access module, the second access module; The first access module, the second access module connect one and switch switch module, and change-over switch module connects power supply output module.
Preferably, between the second described access module and change-over switch module, be provided with electric weight detection module.
Preferably, described fan blade assembly is comprised of one or more fan blades and anchor fitting.
Preferably, described fan blade vertically arranges.
Preferably, described anchor fitting is one to have the outwardly directed body of fuselage bottom.
Owing to having adopted said structure, unmanned plane wind energy regenerative apparatus of the present invention is powered to the electronic machine on unmanned plane after utilizing the wind-force of unmanned plane in flight course to produce electrical power storage, after power drain, using the original battery of unmanned plane to power, and continue to utilize wind-force charging, thereby realize, improve the course continuation mileage of unmanned plane and the object of time.
Accompanying drawing explanation
Fig. 1 is the perspective view of the embodiment of the present invention;
Fig. 2 is the overall circuit modular construction schematic diagram of the embodiment of the present invention;
Fig. 3 is the control circuit modular construction schematic diagram of the embodiment of the present invention.
The specific embodiment
As Figure 1-3, the first storage battery 3 that the unmanned plane wind energy regenerative apparatus of the present embodiment comprises fuselage 1, is located at the electronic machine 2 in fuselage 1 and is connected with electronic machine 2, described fuselage 1 is provided with fan blade assembly 4, described fan blade assembly 4 connects an aerogenerator 5, described aerogenerator 5 connects the second storage battery 7, the described rear access electronic machine 2 of the first storage battery 3 Access Control circuit 6 by a control circuit 6.
During work, aircraft flight produces air-flow, drive 4 rotations of fan blade assembly, fan blade assembly 4 drives aerogenerators 5 generatings, and the power storage of generation, in the second storage battery 7, is powered to electronic machine 2 after holding full electricity, electric weight deficiency is switched the first storage battery 3 power supplies by control circuit 6 afterwards, now, the second storage battery 7 continues charging, so circulation.
During due to aircraft flight, the air-flow of fuselage bottom is comparatively concentrated and is stable, and possesses enough propelling thrusts, so in the present embodiment, described fan blade assembly 4 is located at machine 1 body bottom.
Concrete, in the present embodiment, described control circuit 6 comprises the first access module 61, the second access module 62; The first access module 61, the second access module 62 connect one and switch switch module 63, and change-over switch module 63 connects power supply output module 64.During work, the first access module 61 connects the first storage battery 3, the second access module 62 and connects the second storage battery 7, power supply output module 64 connecting electronic equipment 2.
Interruption for fear of in handoff procedure, in the present embodiment, is provided with electric weight detection module 65 between the second described access module and change-over switch module.One threshold value is set in advance, when electric weight switches during lower than this threshold value, avoids electric weight to exhaust and while switching again, cause power failure.
In the present embodiment, described fan blade assembly 4 is comprised of one or more fan blades 41 and anchor fitting 42.
In the present embodiment, described fan blade vertically arranges; Described anchor fitting is one to have the outwardly directed body of fuselage bottom.
The foregoing is only the preferred embodiments of the present invention; not thereby limit the scope of the claims of the present invention; every equivalent structure or conversion of equivalent flow process that utilizes specification sheets of the present invention and accompanying drawing content to do; or be directly or indirectly used in other relevant technical fields, be all in like manner included in scope of patent protection of the present invention.
Claims (7)
1. unmanned plane wind energy regenerative apparatus, the first storage battery that comprises fuselage, is located at the electronic machine in fuselage and is connected with electronic machine, it is characterized in that: described fuselage is provided with fan blade assembly, described fan blade assembly connects an aerogenerator, described aerogenerator connects the second storage battery by a control circuit, after the first described storage battery Access Control circuit, accesses electronic machine.
2. unmanned plane wind energy regenerative apparatus as claimed in claim 1, is characterized in that: described fan blade assembly is located at fuselage bottom.
3. unmanned plane wind energy regenerative apparatus as claimed in claim 2, is characterized in that: described control circuit comprises the first access module, the second access module; The first access module, the second access module connect one and switch switch module, and change-over switch module connects power supply output module.
4. unmanned plane wind energy regenerative apparatus as claimed in claim 3, is characterized in that: between the second described access module and change-over switch module, be provided with electric weight detection module.
5. unmanned plane wind energy regenerative apparatus as claimed in claim 4, is characterized in that: described fan blade assembly is comprised of one or more fan blades and anchor fitting.
6. unmanned plane wind energy regenerative apparatus as claimed in claim 5, is characterized in that: described fan blade vertically arranges.
7. unmanned plane wind energy regenerative apparatus as claimed in claim 5, is characterized in that: described anchor fitting is one to have the outwardly directed body of fuselage bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
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| CN201310507107.0A CN103523236A (en) | 2013-10-25 | 2013-10-25 | Unmanned aerial vehicle wind energy recycling device |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201310507107.0A CN103523236A (en) | 2013-10-25 | 2013-10-25 | Unmanned aerial vehicle wind energy recycling device |
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| CN103523236A true CN103523236A (en) | 2014-01-22 |
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| CN201310507107.0A Pending CN103523236A (en) | 2013-10-25 | 2013-10-25 | Unmanned aerial vehicle wind energy recycling device |
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| CN104192308A (en) * | 2014-09-05 | 2014-12-10 | 上海理工大学 | Revolving wing flight power device capable of realizing charging and duration performance by wind power |
| CN106043719A (en) * | 2016-07-22 | 2016-10-26 | 珠海银通农业科技有限公司 | Self-powered unmanned aerial vehicle |
| CN109189101A (en) * | 2018-11-21 | 2019-01-11 | 武汉珈鹰智能科技有限公司 | A kind of length is taken photo by plane unmanned aerial vehicle control system |
| CN109889793A (en) * | 2016-08-30 | 2019-06-14 | 吴玉芳 | Cloud computing platform and can recognition of face video monitoring intelligence Skynet system |
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| WO2010041098A1 (en) * | 2008-10-09 | 2010-04-15 | Marco Antonio Caro Henriquez | Wind-powered aeroplane |
| CN101575007A (en) * | 2009-03-13 | 2009-11-11 | 黄灿荣 | Wind power generation electric plane |
| CN101758926A (en) * | 2009-03-13 | 2010-06-30 | 黄灿荣 | Wind energy and solar energy power generation electric airplane |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104192308A (en) * | 2014-09-05 | 2014-12-10 | 上海理工大学 | Revolving wing flight power device capable of realizing charging and duration performance by wind power |
| CN104192308B (en) * | 2014-09-05 | 2016-06-08 | 上海理工大学 | What utilize wind energy charging continuation of the journey rolls wing flight dynamic devices |
| CN106043719A (en) * | 2016-07-22 | 2016-10-26 | 珠海银通农业科技有限公司 | Self-powered unmanned aerial vehicle |
| CN106043719B (en) * | 2016-07-22 | 2023-08-29 | 珠海银通无人机科技有限公司 | Unmanned aerial vehicle of autologous power supply |
| CN109889793A (en) * | 2016-08-30 | 2019-06-14 | 吴玉芳 | Cloud computing platform and can recognition of face video monitoring intelligence Skynet system |
| CN109189101A (en) * | 2018-11-21 | 2019-01-11 | 武汉珈鹰智能科技有限公司 | A kind of length is taken photo by plane unmanned aerial vehicle control system |
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Application publication date: 20140122 |