CN205044948U - Solar energy unmanned aerial vehicle - Google Patents

Solar energy unmanned aerial vehicle Download PDF

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Publication number
CN205044948U
CN205044948U CN201520728151.9U CN201520728151U CN205044948U CN 205044948 U CN205044948 U CN 205044948U CN 201520728151 U CN201520728151 U CN 201520728151U CN 205044948 U CN205044948 U CN 205044948U
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CN
China
Prior art keywords
unmanned plane
aerial vehicle
unmanned aerial
solar
sets
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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.)
Expired - Fee Related
Application number
CN201520728151.9U
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Chinese (zh)
Inventor
钟少央
王仁锋
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Wenzhou Lexiang Technology Information Co Ltd
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Wenzhou Lexiang Technology Information Co Ltd
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Priority to CN201520728151.9U priority Critical patent/CN205044948U/en
Application granted granted Critical
Publication of CN205044948U publication Critical patent/CN205044948U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/50On board measures aiming to increase energy efficiency

Abstract

The utility model relates to an unmanned aerial vehicle, the more specifically solar energy unmanned aerial vehicle that says so adopts the structure of three rotors for unmanned aerial vehicle's flight performance is more stable, and the combination of solar cell panel and battery has simultaneously ensured unmanned aerial vehicle's duration, and the practicality obtains the reinforcing. Solar cell panel fixed mounting is on the top of unmanned aerial vehicle body, the mounting bracket has threely, the equipartition sets up the top at the unmanned aerial vehicle body, and be located the edge of unmanned aerial vehicle body, steering wheel fixed mounting is in the inside of mounting bracket, the connecting axle sets up between steering wheel and flabellum, the flabellum sets up the top at the connecting axle, the fixed inside that sets up at the unmanned aerial vehicle body of control box, battery fixed mounting is in the bottom of control box, discharge controller of solar sets up the left end at the control box, navigational positioning module setting is at the left end of control box, the fixed right side that sets up at discharge controller of solar of little the control unit, the fixed right side that sets up at the battery of wireless communication module.

Description

A kind of solar power unmanned plane
Technical field
The utility model relates to a kind of unmanned plane, is more particularly a kind of solar power unmanned plane.
Background technology
Robot airplane, is called for short unmanned plane, is a kind ofly to be in the equipment of the new concept weapon in developing rapidly, its have maneuverability, reaction fast, unmanned flight, advantage that operation requirements is low.Unmanned plane, by carrying multiclass sensor, can realize image real-time Transmission, high-risk areas detecting function, is that satellite remote sensing and the strong of traditional air remote sensing supplement.At present, the range of use of unmanned plane has widened military affairs, scientific research, civilian three large fields, specifically in electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the field application such as public security anti-terrorism be very wide.
At present, general monitoring unmanned plane is all use storage battery to provide electric energy for unmanned plane, quite waste energy, before use storage battery is charged, because the electricity of storage battery is limited, can not long-time continuous carry out policer operation, otherwise it is not enough just may to appear in flight course electricity, causes the situations such as unmanned plane crash to occur.
Summary of the invention
The technical matters that the utility model mainly solves is to provide a kind of solar power unmanned plane, adopt the structure of three rotors, make the airworthiness of unmanned plane more stable, the combination of solar panel and storage battery has simultaneously ensured the flying power of unmanned plane, and practicality is enhanced.
For solving the problems of the technologies described above, the utility model relates to a kind of unmanned plane, it is more particularly a kind of solar power unmanned plane, comprise unmanned plane body, solar panel, erecting frame, steering wheel, adapter shaft, flabellum, control capsule, storage battery, solar charging/discharging controller, navigation positioning module, micro-control unit, wireless communication module and alighting carriage, adopt the structure of three rotors, make the airworthiness of unmanned plane more stable, the combination of solar panel and storage battery has simultaneously ensured the flying power of unmanned plane, and practicality is enhanced.
Solar panel is fixedly mounted on unmanned plane body, and is positioned at the top of unmanned plane body.Erecting frame has three, the uniform top being arranged on unmanned plane body, and is positioned at the edge of unmanned plane body.Steering wheel is fixedly mounted on the inside of erecting frame, and is positioned at the centre of erecting frame.Adapter shaft is arranged on the top of steering wheel, and between steering wheel and flabellum.Flabellum is arranged on the top of adapter shaft.Control capsule is fixedly installed on the inside of unmanned plane body, and is positioned at the centre of unmanned plane body.Storage battery is fixedly mounted on the bottom of control capsule, and is positioned at the centre of control capsule.Solar charging/discharging controller is arranged on the left end of control capsule, and is positioned at the top of storage battery.Navigation positioning module is arranged on the left end of control capsule, and is positioned at the left side of storage battery.Micro-control unit is fixedly installed on the top of control capsule, and is positioned at the right side of solar charging/discharging controller.Wireless communication module is fixedly installed on the right-hand member of control capsule, and is positioned at the right side of storage battery.Alighting carriage has three, the uniform bottom being arranged on unmanned plane body.
As the further optimization of the technical program, the unmanned plane body described in a kind of solar power unmanned plane of the utility model and the material of erecting frame are carbon fiber composite material.
As the further optimization of the technical program, the navigation positioning module described in a kind of solar power unmanned plane of the utility model and steering wheel are electrically connected.
As the further optimization of the technical program, the adapter shaft described in a kind of solar power unmanned plane of the utility model and flabellum all have three.
The beneficial effect of a kind of solar power unmanned plane of the utility model is:
A kind of solar power unmanned plane of the utility model, adopts the structure of three rotors, makes the airworthiness of unmanned plane more stable, and the combination of solar panel and storage battery has simultaneously ensured the flying power of unmanned plane, and practicality is enhanced.
Accompanying drawing explanation
Below in conjunction with accompanying drawing and specific implementation method, the utility model is described in more detail.
Fig. 1 is the structural representation of a kind of solar power unmanned plane of the utility model.
Fig. 2 is the birds-eye view of a kind of solar power unmanned plane of the utility model.
In figure: unmanned plane body 1; Solar panel 2; Erecting frame 3; Steering wheel 4; Adapter shaft 5; Flabellum 6; Control capsule 7; Storage battery 8; Solar charging/discharging controller 9; Navigation positioning module 10; Micro-control unit 11; Wireless communication module 12; Alighting carriage 13.
Detailed description of the invention
Detailed description of the invention one:
Below in conjunction with Fig. 1, 2 illustrate present embodiment, the utility model relates to a kind of unmanned plane, it is more particularly a kind of solar power unmanned plane, comprise unmanned plane body 1, solar panel 2, erecting frame 3, steering wheel 4, adapter shaft 5, flabellum 6, control capsule 7, storage battery 8, solar charging/discharging controller 9, navigation positioning module 10, micro-control unit 11, wireless communication module 12 and alighting carriage 13, adopt the structure of three rotors, make the airworthiness of unmanned plane more stable, the combination of solar panel and storage battery has simultaneously ensured the flying power of unmanned plane, practicality is enhanced.
Solar panel 2 is fixedly mounted on unmanned plane body 1, and is positioned at the top of unmanned plane body 1, and solar panel 2 provides flying power for unmanned plane.Erecting frame 3 has three, the uniform top being arranged on unmanned plane body 1, and is positioned at the edge of unmanned plane body 1, and erecting frame 3 facilitates the installation of steering wheel 4 and flabellum 6.Steering wheel 4 is fixedly mounted on the inside of erecting frame 3, and is positioned at the centre of erecting frame 3, and steering wheel 4 provides power for flabellum 6.Adapter shaft 5 is arranged on the top of steering wheel 4, and between steering wheel 4 and flabellum 6.Flabellum 6 is arranged on the top of adapter shaft 5.Control capsule 7 is fixedly installed on the inside of unmanned plane body 1, and is positioned at the centre of unmanned plane body 1, and control capsule 7 is convenient to the centralized control to unmanned plane.Storage battery 8 is fixedly mounted on the bottom of control capsule 7, and is positioned at the centre of control capsule 7, and storage battery 8 provides electric energy for unmanned plane, stores the electric energy that solar panel 2 produces.Solar charging/discharging controller 9 is arranged on the left end of control capsule 7, and is positioned at the top of storage battery 8.Navigation positioning module 10 is arranged on the left end of control capsule 7, and is positioned at the left side of storage battery 8, and navigation positioning module 10 is convenient to location to unmanned plane and control.Micro-control unit 11 is fixedly installed on the top of control capsule 7, and is positioned at the right side of solar charging/discharging controller 9, and micro-control unit 11 is the control core of unmanned plane.Wireless communication module 12 is fixedly installed on the right-hand member of control capsule 7, and is positioned at the right side of storage battery 8.Alighting carriage 13 has three, and the uniform bottom being arranged on unmanned plane body 1, alighting carriage 13 facilitates the landing of unmanned plane.
Detailed description of the invention two:
Below in conjunction with Fig. 1,2, present embodiment is described, present embodiment is described further embodiment one, and described unmanned plane body 1 and the material of erecting frame 3 are carbon fiber composite material, have the characteristic that intensity is high, quality is light.
Detailed description of the invention three:
Below in conjunction with Fig. 1,2, present embodiment is described, present embodiment is described further embodiment one, and described navigation positioning module 10 is electrically connected with steering wheel 4, the reliability of assurance device.
Detailed description of the invention four:
Below in conjunction with Fig. 1,2, present embodiment is described, present embodiment is described further embodiment one, and described adapter shaft 5 and flabellum 6 all have three.
Certain above-mentioned explanation is not limitation of the utility model; the utility model is also not limited only to above-mentioned citing; the change that those skilled in the art make in essential scope of the present utility model, remodeling, interpolation or replacement, also belong to protection domain of the present utility model.

Claims (4)

1. a solar power unmanned plane, comprise unmanned plane body (1), solar panel (2), erecting frame (3), steering wheel (4), adapter shaft (5), flabellum (6), control capsule (7), storage battery (8), solar charging/discharging controller (9), navigation positioning module (10), micro-control unit (11), wireless communication module (12) and alighting carriage (13), it is characterized in that: solar panel (2) is fixedly mounted on unmanned plane body (1), and be positioned at the top of unmanned plane body (1), erecting frame (3) has three, the uniform top being arranged on unmanned plane body (1), and is positioned at the edge of unmanned plane body (1), steering wheel (4) is fixedly mounted on the inside of erecting frame (3), and is positioned at the centre of erecting frame (3), adapter shaft (5) is arranged on the top of steering wheel (4), and is positioned between steering wheel (4) and flabellum (6), flabellum (6) is arranged on the top of adapter shaft (5), control capsule (7) is fixedly installed on the inside of unmanned plane body (1), and is positioned at the centre of unmanned plane body (1), storage battery (8) is fixedly mounted on the bottom of control capsule (7), and is positioned at the centre of control capsule (7), solar charging/discharging controller (9) is arranged on the left end of control capsule (7), and is positioned at the top of storage battery (8), navigation positioning module (10) is arranged on the left end of control capsule (7), and is positioned at the left side of storage battery (8), micro-control unit (11) is fixedly installed on the top of control capsule (7), and is positioned at the right side of solar charging/discharging controller (9), wireless communication module (12) is fixedly installed on the right-hand member of control capsule (7), and is positioned at the right side of storage battery (8), alighting carriage (13) has three, the uniform bottom being arranged on unmanned plane body (1).
2. a kind of solar power unmanned plane according to claim 1, is characterized in that: described unmanned plane body (1) and the material of erecting frame (3) are carbon fiber composite material.
3. a kind of solar power unmanned plane according to claim 1, is characterized in that: described navigation positioning module (10) and steering wheel (4) are electrically connected.
4. a kind of solar power unmanned plane according to claim 1, is characterized in that: described adapter shaft (5) and flabellum (6) all have three.
CN201520728151.9U 2015-09-21 2015-09-21 Solar energy unmanned aerial vehicle Expired - Fee Related CN205044948U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520728151.9U CN205044948U (en) 2015-09-21 2015-09-21 Solar energy unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520728151.9U CN205044948U (en) 2015-09-21 2015-09-21 Solar energy unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN205044948U true CN205044948U (en) 2016-02-24

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CN (1) CN205044948U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105836144A (en) * 2016-05-19 2016-08-10 郑琳琳 Novel airborne power supply system of multi-rotor unmanned aerial vehicle
CN105947191A (en) * 2016-05-19 2016-09-21 郑琳琳 Novel multi-rotor unmanned aerial vehicle
CN109383816A (en) * 2017-08-04 2019-02-26 中交遥感载荷(北京)科技有限公司 A kind of solar energy unmanned plane operating method
CN111414008A (en) * 2020-04-08 2020-07-14 中国地质大学(武汉) Unmanned aerial vehicle bootstrap system based on visual transmission design

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105836144A (en) * 2016-05-19 2016-08-10 郑琳琳 Novel airborne power supply system of multi-rotor unmanned aerial vehicle
CN105947191A (en) * 2016-05-19 2016-09-21 郑琳琳 Novel multi-rotor unmanned aerial vehicle
CN109383816A (en) * 2017-08-04 2019-02-26 中交遥感载荷(北京)科技有限公司 A kind of solar energy unmanned plane operating method
CN111414008A (en) * 2020-04-08 2020-07-14 中国地质大学(武汉) Unmanned aerial vehicle bootstrap system based on visual transmission design

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160224

Termination date: 20160921

CF01 Termination of patent right due to non-payment of annual fee