CN104326080A - Full-solar vertical taking-off and landing flying satellite platform - Google Patents
Full-solar vertical taking-off and landing flying satellite platform Download PDFInfo
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- CN104326080A CN104326080A CN201410531299.3A CN201410531299A CN104326080A CN 104326080 A CN104326080 A CN 104326080A CN 201410531299 A CN201410531299 A CN 201410531299A CN 104326080 A CN104326080 A CN 104326080A
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Abstract
The invention discloses a full solar vertical taking-off and landing flying satellite platform mainly including multi-rotor wing aircrafts with a super-light-weight structure, a thin solar cell assembly, a controller and a camera device; the light thin solar cell assembly is laid on the upper surface of the flying satellite platform; the upper end of the flying satellite platform is provided with the controller, and the lower end is provided with the camera device; the flying satellite platform is square in shape, and the circumference is provided with the multi-rotor wing aircrafts. The flying satellite platform has the advantages that the flying satellite platform relies on solar energy for supplying power energy, has a simple structure, is convenient and practical to carry, and solves the multi-rotor wing aircraft key problems of energy-saving emission reduction and long-navigation flight.
Description
Technical field
The present invention relates to technical field of aerospace and technical field of new energies, be specifically related to a kind of full solar power vertical takeoff and landing flight satellite platform.
Technical background
At present; market adopts usually the aircraft such as helicopter, fire balloon, dirigible carry out taking photo by plane, explore, investigate, survey and draw, meteorological, environmental protection; but all there is the shortcoming that can not fly for a long time aloft in it; there is no a kind of full solar power vertical takeoff and landing flight satellite platform on the market; can overcome the shortcoming that the aircraft such as existing helicopter, fire balloon, dirigible can not fly for a long time aloft, it has zero-emission Driven by Solar Energy, good airworthiness, low cost, fly when fine day can grow boat operation, the advantage such as of many uses.
Summary of the invention
The present invention is directed to problem during the above-mentioned short boat of existing various aircraft existence, provide a kind of structure simple, adopt solar powered full solar power vertical takeoff and landing flight satellite platform, its objective is the key issue of flight when the energy-saving and emission-reduction and long boat that solve multi-rotor aerocraft, improve a full solar power vertical takeoff and landing flight satellite platform flown when can grow boat.
The present invention adopts following technical scheme to realize, and full solar power vertical takeoff and landing flight satellite platform, mainly comprises the multi-rotor aerocraft of Ultralight structure, thin solar module, controller and picture pick-up device; It is characterized in that: flight satellite platform upper surface lays frivolous solar module, flight satellite platform upper end is provided with controller, lower end is provided with picture pick-up device, and described flight satellite platform shape is square, and its surrounding arranges and is provided with multi-rotor aerocraft.
The multi-rotor aerocraft of Ultralight structure of the present invention is the flight dynamic devices of flight satellite platform.
Flight satellite platform of the present invention is equipped with thin solar module at its rack upper surface, for full solar power vertical takeoff and landing flight satellite platform provides power source, makes to fly when full solar power vertical takeoff and landing flight satellite platform is long to navigate.
Flight satellite platform of the present invention can be provided with the equipment such as controller, storage battery, shooting, photography.
Picture pick-up device of the present invention is rotatable, carries out making a video recording, photographs, detection etc. for full solar power vertical takeoff and landing flight satellite platform.
Advantage of the present invention is: (1) flight satellite platform relies on solar power to provide power source, structure is simple, practicality easy to carry, has zero-emission Driven by Solar Energy, good airworthiness, low cost, fly when fine day can grow boat operation, the advantage such as of many uses.(2) fly that satellite platform is light to be small and exquisitely easy to carry, can vertical takeoff and landing be realized, the flying methods such as hovering simultaneously.(3) flying below satellite platform can the equipment such as camera, pick up camera of carrying portable, can be widely used in take photo by plane, explore, investigate, survey and draw, meteorology, environmental protection etc.
Accompanying drawing explanation
Fig. 1 is structural representation one of the present invention.
Fig. 2 is structural representation two of the present invention.
In the drawings, the multi-rotor aerocraft of (1) Ultralight structure; (2) thin solar module; (3) controller; (4) picture pick-up device.
Detailed description of the invention
As shown in Figure 1 and Figure 2, the present invention is achieved like this, and full solar power vertical takeoff and landing flight satellite platform, mainly comprises the multi-rotor aerocraft 1 of Ultralight structure, thin solar module 2, controller 3 and picture pick-up device 4; It is characterized in that: flight satellite platform upper surface lays frivolous solar module 2, flight satellite platform upper end is provided with controller 3, lower end is provided with picture pick-up device 4, and described flight satellite platform shape is square, and its surrounding arranges and is provided with multi-rotor aerocraft 1.
The present invention utilizes frivolous solar module to accept solar energy to generate electricity and the motor supplying multi-rotor aerocraft makes screw propeller rotate produces flying power multiaxis class rotor craft is aloft flown, and control multi-rotor aerocraft heading by ground control break pitch, on multi-rotor aerocraft take photo by plane and miscellaneous equipment can carry out taking photo by plane, makes a video recording, investigates, exploration etc.
Principle of work: accept solar energy generating by solar module, and charge to energy-storage travelling wave tube and power to the motor of multi-rotor aerocraft, making driven by motor screw propeller rotate generation flying power makes multi-rotor aerocraft fly aloft, and control multi-rotor aerocraft heading by ground control break pitch, on multi-rotor aerocraft take photo by plane and miscellaneous equipment can carry out taking photo by plane, makes a video recording, investigates, exploration etc.
Claims (3)
1. full solar power vertical takeoff and landing flight satellite platform, mainly comprises the multi-rotor aerocraft of Ultralight structure, thin solar module, controller and picture pick-up device; It is characterized in that: flight satellite platform upper surface lays frivolous solar module, flight satellite platform upper end is provided with controller, lower end is provided with picture pick-up device, and described flight satellite platform shape is square, and its surrounding arranges and is provided with multi-rotor aerocraft.
2. full solar power vertical takeoff and landing flight satellite platform according to claim 1, is characterized in that: described multi-rotor aerocraft is the flight dynamic devices of flight satellite platform.
3. full solar power vertical takeoff and landing flight satellite platform according to claim 1, is characterized in that: described flight satellite platform is equipped with thin solar module at its rack upper surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410531299.3A CN104326080A (en) | 2014-10-11 | 2014-10-11 | Full-solar vertical taking-off and landing flying satellite platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410531299.3A CN104326080A (en) | 2014-10-11 | 2014-10-11 | Full-solar vertical taking-off and landing flying satellite platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104326080A true CN104326080A (en) | 2015-02-04 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410531299.3A Pending CN104326080A (en) | 2014-10-11 | 2014-10-11 | Full-solar vertical taking-off and landing flying satellite platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104326080A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107364577A (en) * | 2017-08-17 | 2017-11-21 | 西安航空学院 | Solar energy VTOL reconnaissance patrol device |
-
2014
- 2014-10-11 CN CN201410531299.3A patent/CN104326080A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107364577A (en) * | 2017-08-17 | 2017-11-21 | 西安航空学院 | Solar energy VTOL reconnaissance patrol device |
| CN107364577B (en) * | 2017-08-17 | 2023-04-07 | 西安航空学院 | Solar vertical take-off and landing reconnaissance patrol aircraft |
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| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150204 |