CN105480422A - Solar unmanned aerial vehicle - Google Patents
Solar unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105480422A CN105480422A CN201510980678.5A CN201510980678A CN105480422A CN 105480422 A CN105480422 A CN 105480422A CN 201510980678 A CN201510980678 A CN 201510980678A CN 105480422 A CN105480422 A CN 105480422A
- Authority
- CN
- China
- Prior art keywords
- apparatus body
- solar
- support
- device body
- solar panel
- 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
- 239000000463 material Substances 0.000 claims description 3
- 239000010935 stainless steel Substances 0.000 claims description 3
- 238000011161 development Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 238000005457 optimization Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000010365 information processing Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000009972 noncorrosive effect Effects 0.000 description 1
- 238000007634 remodeling Methods 0.000 description 1
Classifications
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention relates to an unmanned aerial vehicle, in particular to a solar unmanned aerial vehicle. The solar unmanned aerial vehicle comprises a device body, signal transceivers, rotors, a solar panel bracket, a solar panel, a control box, a bracket, an accumulator, a control chip, a camcorder lens and a converter. The solar unmanned aerial vehicle is provided with the solar panel which can absorb light energy and can convert the light energy into electric energy for use, so that the electric energy is saved. The signal transceivers are mounted on the device body and are positioned at the top end of the device body; the rotors are mounted on the device body and are positioned at the top end of the device body; the lower end of the solar panel bracket is connected with the device body, and the upper end of the solar panel bracket is connected with the solar panel; the control box is mounted on the device body and is positioned at the bottom end of the device body; the accumulator, the control chip and the converter are all arranged in the control box; the bracket is mounted on the device body and is positioned at the bottom end of the device body; the camcorder lens is mounted on the bracket.
Description
Technical field
The present invention relates to a kind of unmanned plane, is more particularly a kind of solar power unmanned plane.
Background technology
The progress and development of science and technology drives expanding economy, and unmanned plane is a part for development in science and technology, and the development of unmanned plane drives a major project of economic development beyond doubt, therefore, designs a kind of solar power unmanned plane and is necessary.
Summary of the invention
The technical matters that the present invention mainly solves is to provide a kind of solar power unmanned plane, and device, with solar panel, can absorb luminous energy, and is converted to electric energy use, saves electric energy.
For solving the problems of the technologies described above, the present invention relates to a kind of unmanned plane, it is more particularly a kind of solar power unmanned plane, comprise apparatus body, signal transceiver, rotor, solar-cell panel support, solar panel, control box, support, storage battery, control chip, camera and conv, device is with solar panel, can luminous energy be absorbed, and be converted to electric energy use, save electric energy.
Signal transceiver is arranged on apparatus body, and is positioned at the top of apparatus body, and rotor is arranged on apparatus body, and is positioned at the top of apparatus body.The lower end of solar-cell panel support is connected with apparatus body, and is positioned at the top of apparatus body, and the upper end of solar-cell panel support is connected with solar panel.Control box is arranged on apparatus body, and is positioned at the bottom of apparatus body, and storage battery, control chip and conv are all arranged on the inside of control box.Support installing on apparatus body, and is positioned at the bottom of apparatus body, and camera is rack-mount.
As the further optimization of the technical program, the rotor described in a kind of solar power unmanned plane of the present invention has four.
As the further optimization of the technical program, the material of the support described in a kind of solar power unmanned plane of the present invention is corrosion-resistant steel.
As the further optimization of the technical program, apparatus body, solar panel, control box, support and the camera concentrically line described in a kind of solar power unmanned plane of the present invention.
The beneficial effect of a kind of solar power unmanned plane of the present invention is:
A kind of solar power unmanned plane of the present invention, device, with solar panel, can absorb luminous energy, and is converted to electric energy use, saves electric energy.
Accompanying drawing explanation
Below in conjunction with accompanying drawing and specific implementation method, the present invention will be further described in detail.
Fig. 1 is the structural representation of a kind of solar power unmanned plane of the present invention.
In figure: apparatus body 1; Signal transceiver 2; Rotor 3; Solar-cell panel support 4; Solar panel 5; Control box 6; Support 7; Storage battery 8; Control chip 9; Camera 10; Conv 11.
Detailed description of the invention
Detailed description of the invention one:
Below in conjunction with Fig. 1, present embodiment is described, the present invention relates to a kind of unmanned plane, it is more particularly a kind of solar power unmanned plane, comprise apparatus body 1, signal transceiver 2, rotor 3, solar-cell panel support 4, solar panel 5, control box 6, support 7, storage battery 8, control chip 9, camera 10 and conv 11, device is with solar panel, can luminous energy be absorbed, and be converted to electric energy use, save electric energy.
Signal transceiver 2 is arranged on apparatus body 1, and be positioned at the top of apparatus body 1, rotor 3 is arranged on apparatus body 1, and be positioned at the top of apparatus body 1, signal transceiver 2 is for receiving and sending signal, make people can remote control, rotor 3 for the flight of device, and carrys out the service direction of control apparatus by the control of each rotor 3 speed.
The lower end of solar-cell panel support 4 is connected with apparatus body 1, and be positioned at the top of apparatus body 1, the upper end of solar-cell panel support 4 is connected with solar panel 5, solar-cell panel support 4 is for the support of solar panel 5, solar panel 5 is for absorbing luminous energy, and be converted to electric energy by conv 11 to use, save electric energy, increase the time of device follow-on mission.
Control box 6 is arranged on apparatus body 1, and is positioned at the bottom of apparatus body 1, and storage battery 8, control chip 9 and conv 11 are all arranged on the inside of control box 6, and storage battery 8 is powered to device, and control chip 9 is information processing cores of device.Support 7 is arranged on apparatus body 1, and is positioned at the bottom of apparatus body 1, and camera 10 is arranged on support 7, and support 7 is for the support of device, and camera 10 is for video recording.
Detailed description of the invention two:
Below in conjunction with Fig. 1, present embodiment is described, present embodiment is described further embodiment one, and described rotor 3 has four.
Detailed description of the invention three:
Below in conjunction with Fig. 1, present embodiment is described, present embodiment is described further embodiment one, and the material of described support 7 is corrosion-resistant steel, and stainless intensity is large, and load ability is strong, and non-corrosive, keep good outward appearance always.
Detailed description of the invention four:
Below in conjunction with Fig. 1, present embodiment is described, present embodiment is described further embodiment one, and described apparatus body 1, solar panel 5, control box 6, support 7 and camera 10 concentrically line, make the good stability of device.
Certain above-mentioned explanation is not limitation of the present invention, and the present invention is also not limited only to above-mentioned citing, and the change that those skilled in the art make in essential scope of the present invention, remodeling, interpolation or replacement, also belong to protection scope of the present invention.
Claims (4)
1. a solar power unmanned plane, comprise apparatus body (1), signal transceiver (2), rotor (3), solar-cell panel support (4), solar panel (5), control box (6), support (7), storage battery (8), control chip (9), camera (10) and conv (11), it is characterized in that: signal transceiver (2) is arranged on apparatus body (1), and be positioned at the top of apparatus body (1), rotor (3) is arranged on apparatus body (1), and be positioned at the top of apparatus body (1), the lower end of solar-cell panel support (4) is connected with apparatus body (1), and be positioned at the top of apparatus body (1), the upper end of solar-cell panel support (4) is connected with solar panel (5), control box (6) is arranged on apparatus body (1), and be positioned at the bottom of apparatus body (1), storage battery (8), control chip (9) and conv (11) are all arranged on the inside of control box (6), support (7) is arranged on apparatus body (1), and is positioned at the bottom of apparatus body (1), and camera (10) is arranged on support (7).
2. a kind of solar power unmanned plane according to claim 1, is characterized in that: described rotor (3) has four.
3. a kind of solar power unmanned plane according to claim 1, is characterized in that: the material of described support (7) is corrosion-resistant steel.
4. a kind of solar power unmanned plane according to claim 1, is characterized in that: described apparatus body (1), solar panel (5), control box (6), support (7) and camera (10) concentrically line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510980678.5A CN105480422A (en) | 2015-12-22 | 2015-12-22 | Solar unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510980678.5A CN105480422A (en) | 2015-12-22 | 2015-12-22 | Solar unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105480422A true CN105480422A (en) | 2016-04-13 |
Family
ID=55667775
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510980678.5A Pending CN105480422A (en) | 2015-12-22 | 2015-12-22 | Solar unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105480422A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818984A (en) * | 2016-05-16 | 2016-08-03 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle satellite intercom with robot device |
| CN108263605A (en) * | 2018-01-31 | 2018-07-10 | 芜湖市海联机械设备有限公司 | A kind of high continuation of the journey multi-rotor unmanned aerial vehicle |
| CN115675874A (en) * | 2022-12-12 | 2023-02-03 | 西南大学 | Unmanned aerial vehicle for spraying pesticides |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060060693A1 (en) * | 2004-03-10 | 2006-03-23 | Poltorak Alexander I | Rotating wing aircraft with tip-driven rotor and rotor guide-ring |
| CN104787314A (en) * | 2015-04-17 | 2015-07-22 | 南昌航空大学 | Dismountable solar cell panel four-axis aircraft |
| CN104943858A (en) * | 2015-07-03 | 2015-09-30 | 广西大学 | Multifunctional coaxial double-rotor-wing four-shaft aircraft |
-
2015
- 2015-12-22 CN CN201510980678.5A patent/CN105480422A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060060693A1 (en) * | 2004-03-10 | 2006-03-23 | Poltorak Alexander I | Rotating wing aircraft with tip-driven rotor and rotor guide-ring |
| CN104787314A (en) * | 2015-04-17 | 2015-07-22 | 南昌航空大学 | Dismountable solar cell panel four-axis aircraft |
| CN104943858A (en) * | 2015-07-03 | 2015-09-30 | 广西大学 | Multifunctional coaxial double-rotor-wing four-shaft aircraft |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818984A (en) * | 2016-05-16 | 2016-08-03 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle satellite intercom with robot device |
| CN108263605A (en) * | 2018-01-31 | 2018-07-10 | 芜湖市海联机械设备有限公司 | A kind of high continuation of the journey multi-rotor unmanned aerial vehicle |
| CN115675874A (en) * | 2022-12-12 | 2023-02-03 | 西南大学 | Unmanned aerial vehicle for spraying pesticides |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160413 |
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| RJ01 | Rejection of invention patent application after publication |