CN105752346A - Solar unmanned aerial vehicle - Google Patents
Solar unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105752346A CN105752346A CN201610286199.8A CN201610286199A CN105752346A CN 105752346 A CN105752346 A CN 105752346A CN 201610286199 A CN201610286199 A CN 201610286199A CN 105752346 A CN105752346 A CN 105752346A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- solar
- solar energy
- aerial vehicle
- unmanned aerial
- 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
- 238000006243 chemical reaction Methods 0.000 claims abstract description 11
- 238000004891 communication Methods 0.000 claims abstract description 10
- 241001424688 Enceliopsis Species 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005286 illumination Methods 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Traffic Control Systems (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses a solar unmanned aerial vehicle which comprises an unmanned aerial vehicle body; a solar cell panel is arranged on the upper surface of the unmanned aerial vehicle body; a direction adjusting base is arranged under the solar cell panel; a photometric sensor is arranged at the front end of the solar cell panel; a control circuit is arranged inside the unmanned aerial vehicle; a photoelectric conversion component is arranged on one side of the control circuit; a large-capacity storage plate is arranged on the photoelectric conversion component. The solar unmanned aerial vehicle disclosed by the invention is simple in mounting and disassembly, the photometric sensor can sense solar rays and automatically adjust the direction of the solar cell panel, so that the collecting quantity of solar energy is increased; a communication device and a radar early warning device can increase safety coefficients and record flight lines in real time.
Description
Technical field
The present invention relates to a kind of solar energy unmanned plane.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself.Can be divided into from technical standpoint definition: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc..At present, the use scope of unmanned plane has widened military affairs, scientific research, civilian three big fields, specifically 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 very wide.
But the design hommization not enough of now traditional on the market unmanned plane, and need to be charged in use for some time, the energy needed for ability maintenance work, change battery not only to have high input but also the burden of environment can be increased, so can solar energy be referred on unmanned plane, but the work efficiency of existing solar energy unmanned plane is not high, and power is not high, so needing to improve.
Summary of the invention
For solving the problems referred to above, the present invention proposes a kind of solar energy unmanned plane.
Solar energy unmanned plane, including unmanned plane body, described unmanned plane body be provided above with solar panel；Described solar panel be arranged below direction adjusting base；The front end of described solar panel is provided with luminosity sensor；Described unmanned plane body be internally provided with control circuit；The side of described control circuit is provided with photoelectric conversion component；Described photoelectric conversion component is provided with Large Copacity savings plate.
Further, the middle part of described unmanned plane body is provided with flight controller.
Further, described direction adjusting base is provided with lowering or hoisting gear.
Further, it is provided with data-signal converter between described lowering or hoisting gear and luminosity sensor.
Further, the side of described flight controller is provided with communication device and early radar warning device.
Further, described unmanned plane body is provided with wing.
Further, described wing is provided with power spin oar.
nullThe present invention is compared with prior art，It has the advantages that the present invention is when coming into operation，Solar panel receives solar energy，The intensity of illumination that luminosity sensor will sense at that time，In real time the data sensed are transferred in data message transducer，Data according to luminosity regulate lowering or hoisting gear，Rising or decline along with lowering or hoisting gear，The direction of direction adjusting base can be changed，So that solar panel is able to receive that maximum light area，Increase the efficiency collecting energy，Convert light energy into electrical power storage again through photoelectric conversion component to save in plate at Large Copacity，Electric energy is passed to unmanned plane body and is powered by control circuit，Flight controller will control the flight course of unmanned plane，Communication device can real time record flight route，Early radar warning device can improve flight safety coefficient，Dynamic rotation oar on wing can provide power support for unmanned plane，The present invention installs simply，Dismounting is simple，Luminosity sensor sensing sunray can be automatically adjusted the direction of solar panel，Increase the collecting amount of solar energy，Communication device and early radar warning device can increase safety coefficient，Real time record flight path.
Accompanying drawing explanation
Fig. 1 is the section of structure of first embodiment of the invention；
Fig. 2 is the plan structure schematic diagram of first embodiment of the invention.
1-unmanned plane body 2-luminosity sensor 3-solar panel 4-power spin oar 5-wing 6-control circuit 7-photoelectric conversion component 8-Large Copacity savings plate 9-direction adjusting base 10-lowering or hoisting gear 11-flight controller 12-data-signal converter 13-communication device 14-early radar warning device.
Detailed description of the invention
As depicted in figs. 1 and 2, including unmanned plane body 1, described unmanned plane body 1 be provided above with solar panel 3；Described solar panel 3 be arranged below direction adjusting base 9；The front end of described solar panel 3 is provided with luminosity sensor 2；Described unmanned plane body 1 be internally provided with control circuit 6；The side of described control circuit 6 is provided with photoelectric conversion component 7；Described photoelectric conversion component 7 is provided with Large Copacity savings plate 8.
The middle part of described unmanned plane body 1 is provided with flight controller 11.
Described direction adjusting base 9 is provided with lowering or hoisting gear 10.
It is provided with data-signal converter 12 between described lowering or hoisting gear 10 and luminosity sensor 2.
The side of described flight controller 11 is provided with communication device 13 and early radar warning device 14.
Described unmanned plane body 1 is provided with wing 5.
Described wing 5 is provided with power spin oar 4.
nullThe present invention is compared with prior art，It has the advantages that the present invention is when coming into operation，Solar panel receives solar energy，The intensity of illumination that luminosity sensor will sense at that time，In real time the data sensed are transferred in data message transducer，Data according to luminosity regulate lowering or hoisting gear，Rising or decline along with lowering or hoisting gear，The direction of direction adjusting base can be changed，So that solar panel is able to receive that maximum light area，Increase the efficiency collecting energy，Convert light energy into electrical power storage again through photoelectric conversion component to save in plate at Large Copacity，Electric energy is passed to unmanned plane body and is powered by control circuit，Flight controller will control the flight course of unmanned plane，Communication device can real time record flight route，Early radar warning device can improve flight safety coefficient，Dynamic rotation oar on wing can provide power support for unmanned plane，The present invention installs simply，Dismounting is simple，Luminosity sensor sensing sunray can be automatically adjusted the direction of solar panel，Increase the collecting amount of solar energy，Communication device and early radar warning device can increase safety coefficient，Real time record flight path.
Embodiment described above is only that the preferred embodiment of the present invention is described, and not the spirit and scope of the present invention is defined.Under the premise without departing from design concept of the present invention; various modification that technical scheme is made by this area ordinary person and improvement; protection scope of the present invention all should be dropped into, the technology contents that the present invention is claimed, all record in detail in the claims.
Claims (7)
1. a solar energy unmanned plane, it is characterised in that: include unmanned plane body, described unmanned plane body be provided above with solar panel；Described solar panel be arranged below direction adjusting base；The front end of described solar panel is provided with luminosity sensor；Described unmanned plane body be internally provided with control circuit；The side of described control circuit is provided with photoelectric conversion component；Described photoelectric conversion component is provided with Large Copacity savings plate.
2. solar energy unmanned plane according to claim 1, it is characterised in that: the middle part of described unmanned plane body is provided with flight controller.
3. solar energy unmanned plane according to claim 1, it is characterised in that: described direction adjusting base is provided with lowering or hoisting gear.
4. solar energy unmanned plane according to claim 3, it is characterised in that: it is provided with data-signal converter between described lowering or hoisting gear and luminosity sensor.
5. solar energy unmanned plane according to claim 2, it is characterised in that: the side of described flight controller is provided with communication device and early radar warning device.
6. solar energy unmanned plane according to claim 1, it is characterised in that: described unmanned plane body is provided with wing.
7. solar energy unmanned plane according to claim 6, it is characterised in that: described wing is provided with power spin oar.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610286199.8A CN105752346A (en) | 2016-05-02 | 2016-05-02 | Solar unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610286199.8A CN105752346A (en) | 2016-05-02 | 2016-05-02 | Solar unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105752346A true CN105752346A (en) | 2016-07-13 |
Family
ID=56323258
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610286199.8A Pending CN105752346A (en) | 2016-05-02 | 2016-05-02 | Solar unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105752346A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043681A (en) * | 2016-08-15 | 2016-10-26 | 张崎 | Multi-rotor solar unmanned aerial vehicle |
| CN107972875A (en) * | 2017-11-22 | 2018-05-01 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of angle of solar cell panel regulating device of unmanned plane |
| CN109333538A (en) * | 2018-11-01 | 2019-02-15 | 北京万通易居环保设备科技有限公司 | A kind of control system of photovoltaic intelligent robot |
| CN109714577A (en) * | 2016-09-20 | 2019-05-03 | 张玲花 | Unmanned aerial vehicle control system, the video monitoring Skynet system based on recognition of face |
| CN109819223A (en) * | 2016-09-20 | 2019-05-28 | 朱海燕 | A kind of unmanned plane and the intelligent video monitoring system based on recognition of face |
| WO2019119183A1 (en) * | 2017-12-18 | 2019-06-27 | 深圳市大疆创新科技有限公司 | Agricultural drone flight control method , radar system, and agricultural drone |
| CN110816823A (en) * | 2018-08-08 | 2020-02-21 | 谭伊杰 | Many rotor unmanned aerial vehicle with smog recognition function |
-
2016
- 2016-05-02 CN CN201610286199.8A patent/CN105752346A/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043681A (en) * | 2016-08-15 | 2016-10-26 | 张崎 | Multi-rotor solar unmanned aerial vehicle |
| CN109714577A (en) * | 2016-09-20 | 2019-05-03 | 张玲花 | Unmanned aerial vehicle control system, the video monitoring Skynet system based on recognition of face |
| CN109819223A (en) * | 2016-09-20 | 2019-05-28 | 朱海燕 | A kind of unmanned plane and the intelligent video monitoring system based on recognition of face |
| CN107972875A (en) * | 2017-11-22 | 2018-05-01 | 安徽天鹰兄弟无人机科技创新有限公司 | A kind of angle of solar cell panel regulating device of unmanned plane |
| WO2019119183A1 (en) * | 2017-12-18 | 2019-06-27 | 深圳市大疆创新科技有限公司 | Agricultural drone flight control method , radar system, and agricultural drone |
| CN110816823A (en) * | 2018-08-08 | 2020-02-21 | 谭伊杰 | Many rotor unmanned aerial vehicle with smog recognition function |
| CN109333538A (en) * | 2018-11-01 | 2019-02-15 | 北京万通易居环保设备科技有限公司 | A kind of control system of photovoltaic intelligent robot |
| CN109333538B (en) * | 2018-11-01 | 2021-01-26 | 北京万通易居环保设备科技有限公司 | Control system of photovoltaic intelligent robot |
| CN112486069A (en) * | 2018-11-01 | 2021-03-12 | 北京万通易居环保设备科技有限公司 | Control system of photovoltaic intelligent robot |
| CN112486069B (en) * | 2018-11-01 | 2022-03-01 | 北京万通易居环保设备科技有限公司 | Control system of photovoltaic intelligent robot |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105752346A (en) | Solar unmanned aerial vehicle | |
| CN204250368U (en) | A kind of mini quadrotor of Intelligent aerial photography | |
| CN105913691B (en) | A kind of method that service is declared in flying area | |
| CN105516691B (en) | Long stagnant empty unmanned plane base station communication and monitoring system | |
| CN204415743U (en) | A kind of patrol monitoring unmanned vehicle system | |
| CN104044741B (en) | A kind of carry out solar energy tracking unmanned plane and fill can process | |
| CN204264449U (en) | A kind of line walking unmanned plane with infrared thermal imaging and aerial photography function | |
| CN206087353U (en) | For military use unmanned aerial vehicle with monitor function | |
| CN106394891A (en) | Anti-interference aerial photographic unmanned aerial vehicle powered by solar energy | |
| CN205139164U (en) | Particle image velocimetry detecting system based on unmanned aerial vehicle | |
| CN107390717A (en) | Patrol unmanned machine and system for power regulation station inspection | |
| CN105644760A (en) | Hydrogen suspending photovoltaic monitoring aircraft and manufacturing method thereof | |
| CN205044948U (en) | Solar energy unmanned aerial vehicle | |
| CN105882951A (en) | Multifunctional unmanned aerial vehicle | |
| CN209553482U (en) | Total lift body solar energy unmanned vehicle | |
| CN108674671A (en) | Solar cell module for unmanned aerial vehicle capable of vertically taking off and landing | |
| CN201914460U (en) | Novel rotor type disc aircraft | |
| CN204688419U (en) | A kind of unmanned plane | |
| CN204548507U (en) | A kind of Portable unmanned machine observation system | |
| CN113277080B (en) | Flapping wing platform for unmanned aerial vehicle charging and charging method thereof | |
| CN203902841U (en) | Unmanned aerial vehicle capable of performing solar energy tracking | |
| CN209192267U (en) | A kind of multi-rotor unmanned aerial vehicle is matched to be tethered at equipment | |
| CN204660017U (en) | A kind of kite assisting in flying device | |
| CN207346091U (en) | A kind of six rotor wing unmanned aerial vehicle system of long endurance | |
| CN208979092U (en) | A kind of mixed layout unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160713 |