CN205060008U - Four wing aircraft of solar energy - Google Patents
Four wing aircraft of solar energy Download PDFInfo
- Publication number
- CN205060008U CN205060008U CN201520753774.1U CN201520753774U CN205060008U CN 205060008 U CN205060008 U CN 205060008U CN 201520753774 U CN201520753774 U CN 201520753774U CN 205060008 U CN205060008 U CN 205060008U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- flying wing
- control box
- aircraft body
- support
- 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.)
- Expired - Fee Related
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Classifications
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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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The utility model relates to a four wing aircraft, more specifically the four wing aircraft of solar energy that says so, device are provided with four flight wings, receive the flight direction that slew velocity that control signal controlled each flight wing comes controlling means through the radio signal recepition ware, the device has the camera and can shoot the place of arrival to the wireless receiving arrangement of conveying stores, have emitting diode on the device, birds can be threatened to the light that sends, have avoided birds to be close to the destructor, the device absorbs solar energy transformation to be used for the electric energy, and the energy acquires the convenience for the device flight time is long. The camera is installed on the control box, and loudspeaker have four, and the equipartition is on the control box. Flight wing frame has four, and the equipartition is in the aircraft main part. Emitting diode installs on flight wing frame. The radio signal recepition ware has four, and the equipartition is in the aircraft main part, and the lower extreme of support II is connected with the aircraft bulk phase, and the upper end of support II is connected with solar cell panel.
Description
Technical field
The utility model relates to a kind of four rotor aircrafts, is a kind of solar power four rotor aircraft in particular.
Background technology
National strength except economical, political etc. topmost be exactly the power of military strength, the strong or weak relation of military strength is to a national national defence level, and aviation field is civilian or military all very important, the air material that current China is used for scientific research field is exactly small aircraft, so small aircraft send out the development contributing to scientific research, so design a kind of solar power four rotor aircraft.
Summary of the invention
The technical matters that the utility model mainly solves is to provide a kind of solar power four rotor aircraft, and device is provided with four flying wings, and the velocity of rotation controlling each flying wing by wireless signal receiver reception control signal carrys out the heading of control setup; Device can be taken place of arrival with camera, and is wirelessly transmitted to receiving device and stores; With light-emitting diode on device, the light sent can threaten birds, avoids birds near breaking plant; Device absorbs solar power and is converted into electric energy use, and the energy obtains convenient, makes the device flight time long.
For solving the problems of the technologies described above, the utility model relates to a kind of four rotor aircrafts, a kind of solar power four rotor aircraft in particular, comprise aircraft body, control box, control chip, conv, camera, battery, loudspeaker, support I, flying wing frame, light-emitting diode, electrical motor, retarder, fixing gusset I, coupler, fixing gusset II, flying wing, wireless signal receiver, support II and solar panel, device is provided with four flying wings, the velocity of rotation controlling each flying wing by wireless signal receiver reception control signal carrys out the heading of control setup, device can be taken place of arrival with camera, and is wirelessly transmitted to receiving device and stores, with light-emitting diode on device, the light sent can threaten birds, avoids birds near breaking plant, device absorbs solar power and is converted into electric energy use, and the energy obtains convenient, makes the device flight time long.
Control box is arranged in aircraft body, and is positioned at the bottom of aircraft body, and control chip, conv and battery are all arranged on the inside of control box, camera is arranged on control box, and be positioned at the bottom of control box, loudspeaker have four, are distributed on control box.Support I has four, is distributed in aircraft body, and is positioned at the bottom of aircraft body, and flying wing frame has four, is distributed in aircraft body.Light-emitting diode is arranged on flying wing frame, and is positioned at the bottom of flying wing frame, and one end of fixing gusset I is connected with flying wing frame, and the other end of fixing gusset I is connected with retarder, and electrical motor is arranged on retarder.One end of fixing gusset II is connected with flying wing frame, and the other end of fixing gusset II is connected with coupler, and flying wing is connected with retarder by coupler.Wireless signal receiver has four, is distributed in aircraft body, and is positioned at the top of aircraft body, and the lower end of support II is connected with aircraft body, and the upper end of support II is connected with solar panel.
As the further optimization of the technical program, aircraft body, control box, camera and the solar panel concentrically line described in a kind of solar power four of the utility model rotor aircraft.
As the further optimization of the technical program, the material of the flying wing described in a kind of solar power four of the utility model rotor aircraft is plastics.
As the further optimization of the technical program, electrical motor, retarder, coupler and flying wing described in a kind of solar power four of the utility model rotor aircraft all have four.
The beneficial effect of a kind of solar power four of the utility model rotor aircraft is:
A kind of solar power four rotor aircraft of the utility model, device is provided with four flying wings, and the velocity of rotation controlling each flying wing by wireless signal receiver reception control signal carrys out the heading of control setup; Device can be taken place of arrival with camera, and is wirelessly transmitted to receiving device and stores; With light-emitting diode on device, the light sent can threaten birds, avoids birds near breaking plant; Device absorbs solar power and is converted into electric energy use, and the energy obtains convenient, makes the device flight time long.
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 four of the utility model rotor aircraft.
In figure: aircraft body 1; Control box 2; Control chip 3; Conv 4; Camera 5; Battery 6; Loudspeaker 7; Support I 8; Flying wing frame 9; Light-emitting diode 10; Electrical motor 11; Retarder 12; Fixing gusset I 13; Coupler 14; Fixing gusset II 15; Flying wing 16; Wireless signal receiver 17; Support II 18; Solar panel 19.
Detailed description of the invention
Detailed description of the invention one:
Below in conjunction with Fig. 1, present embodiment is described, the utility model relates to a kind of four rotor aircrafts, a kind of solar power four rotor aircraft in particular, comprise aircraft body 1, control box 2, control chip 3, conv 4, camera 5, battery 6, loudspeaker 7, support I 8, flying wing frame 9, light-emitting diode 10, electrical motor 11, retarder 12, fixing gusset I 13, coupler 14, fixing gusset II 15, flying wing 16, wireless signal receiver 17, support II 18 and solar panel 19, device is provided with four flying wings, the velocity of rotation controlling each flying wing by wireless signal receiver reception control signal carrys out the heading of control setup, device can be taken place of arrival with camera, and is wirelessly transmitted to receiving device and stores, with light-emitting diode on device, the light sent can threaten birds, avoids birds near breaking plant, device absorbs solar power and is converted into electric energy use, and the energy obtains convenient, makes the device flight time long.
Control box 2 is arranged in aircraft body 1, and be positioned at the bottom of aircraft body 1, control chip 3, conv 4 and battery 6 are all arranged on the inside of control box 2, camera 5 is arranged on control box 2, and be positioned at the bottom of control box 2, loudspeaker 7 have four, be distributed on control box 2, control chip 3 is information processing cores of device, the luminous energy that conv 4 conversion solar energy cell panel 19 absorbs, and be stored in battery 6 and be used, battery 6 is powered to device, camera 5 is for taking place of arrival, and the picture photographed is sent to ground receiving wastewater facility by wireless signal receiver 17 receive, loudspeaker 17 are sounded, birds can be threatened, avoid birds near breaking plant.Support I 8 has four, is distributed in aircraft body 1, and is positioned at the bottom of aircraft body 1, and flying wing frame 9 has four, and be distributed in aircraft body 1, support I 8 is for the support of device.Light-emitting diode 10 is arranged on flying wing frame 9, and be positioned at the bottom of flying wing frame 9, one end of fixing gusset I 13 is connected with flying wing frame 9, the other end of fixing gusset I 13 is connected with retarder 12, electrical motor 11 is arranged on retarder 12, and the light that light-emitting diode 10 sends can threaten birds, avoids birds near breaking plant, fixing gusset I 13 is for the installation of retarder 12 and electrical motor 11, and electrical motor 11 provides power to the flight of device.One end of fixing gusset II 15 is connected with flying wing frame 9, and the other end of fixing gusset II 15 is connected with coupler 14, and flying wing 16 is connected with retarder 12 by coupler 14.Wireless signal receiver 17 has four, be distributed in aircraft body 1, and be positioned at the top of aircraft body 1, the lower end of support II 18 is connected with aircraft body 1, the upper end of support II 18 is connected with solar panel 19, wireless signal receiver 17 is for receiving and transmitting signal, support II 18 is for the support of solar panel 19, solar panel 19 is for absorbing luminous energy, and be converted to power storage in battery 6 by conv 4, save electric energy, make device aloft the flight time long.
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 aircraft body 1, control box 2, camera 5 and solar panel 19 concentrically line, make the good stability of device.
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 flying wing 16 is plastics.
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 electrical motor 11, retarder 12, coupler 14 and flying wing 16 all have four.
Certainly; 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 belongs to protection domain of the present utility model.
Claims (4)
1. solar power four rotor aircraft, comprises aircraft body (1), control box (2), control chip (3), conv (4), camera (5), battery (6), loudspeaker (7), support I (8), flying wing frame (9), light-emitting diode (10), electrical motor (11), retarder (12), fixing gusset I (13), coupler (14), fixing gusset II (15), flying wing (16), wireless signal receiver (17), support II (18) and solar panel (19), it is characterized in that: control box (2) is arranged in aircraft body (1), and be positioned at the bottom of aircraft body (1), control chip (3), conv (4) and battery (6) are all arranged on the inside of control box (2), camera (5) is arranged on control box (2), and be positioned at the bottom of control box (2), loudspeaker (7) have four, are distributed on control box (2), support I (8) has four, is distributed in aircraft body (1), and is positioned at the bottom of aircraft body (1), and flying wing frame (9) has four, is distributed in aircraft body (1), light-emitting diode (10) is arranged on flying wing frame (9), and be positioned at the bottom of flying wing frame (9), one end of fixing gusset I (13) is connected with flying wing frame (9), the other end of fixing gusset I (13) is connected with retarder (12), and electrical motor (11) is arranged on retarder (12), one end of fixing gusset II (15) is connected with flying wing frame (9), the other end of fixing gusset II (15) is connected with coupler (14), and flying wing (16) is connected with retarder (12) by coupler (14), wireless signal receiver (17) has four, be distributed in aircraft body (1), and be positioned at the top of aircraft body (1), the lower end of support II (18) is connected with aircraft body (1), and the upper end of support II (18) is connected with solar panel (19).
2. a kind of solar power four rotor aircraft according to claim 1, is characterized in that: described aircraft body (1), control box (2), camera (5) and solar panel (19) concentrically line.
3. a kind of solar power four rotor aircraft according to claim 1, is characterized in that: the material of described flying wing (16) is plastics.
4. a kind of solar power four rotor aircraft according to claim 1, is characterized in that: described electrical motor (11), retarder (12), coupler (14) and flying wing (16) all have four.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520753774.1U CN205060008U (en) | 2015-09-25 | 2015-09-25 | Four wing aircraft of solar energy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520753774.1U CN205060008U (en) | 2015-09-25 | 2015-09-25 | Four wing aircraft of solar energy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205060008U true CN205060008U (en) | 2016-03-02 |
Family
ID=55386595
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520753774.1U Expired - Fee Related CN205060008U (en) | 2015-09-25 | 2015-09-25 | Four wing aircraft of solar energy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205060008U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106016083A (en) * | 2016-08-01 | 2016-10-12 | 苏州光景照明科技有限公司 | Airport bird repelling system with LED lighting devices |
| CN106516089A (en) * | 2016-10-28 | 2017-03-22 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN108069026A (en) * | 2016-11-18 | 2018-05-25 | 天津毅搏云山科技有限公司 | A kind of new unmanned plane |
| 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 |
-
2015
- 2015-09-25 CN CN201520753774.1U patent/CN205060008U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106016083A (en) * | 2016-08-01 | 2016-10-12 | 苏州光景照明科技有限公司 | Airport bird repelling system with LED lighting devices |
| CN106516089A (en) * | 2016-10-28 | 2017-03-22 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| US10710707B2 (en) | 2016-10-28 | 2020-07-14 | Autel Robotics Co., Ltd | Unmanned aerial vehicle |
| CN108069026A (en) * | 2016-11-18 | 2018-05-25 | 天津毅搏云山科技有限公司 | A kind of new unmanned plane |
| 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 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160302 Termination date: 20160925 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |