CN204037899U - Solar power vertically taking off and landing flyer during long boat - Google Patents
Solar power vertically taking off and landing flyer during long boat Download PDFInfo
- Publication number
- CN204037899U CN204037899U CN201420091987.8U CN201420091987U CN204037899U CN 204037899 U CN204037899 U CN 204037899U CN 201420091987 U CN201420091987 U CN 201420091987U CN 204037899 U CN204037899 U CN 204037899U
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- CN
- China
- Prior art keywords
- boat
- solar power
- vertically taking
- landing flyer
- power vertically
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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
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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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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Abstract
The utility model relates to a kind of improvement of aircraft, particularly solar power vertically taking off and landing flyer during a kind of long boat, flight dynamic devices is four axle flying platform formula multi-rotor aerocrafts of Ultralight structure, be equipped with thin solar module at its rack upper surface, be provided with the equipment such as controller, storage battery, shooting, photography below.During the utility model long boat, solar power vertically taking off and landing flyer overcomes the shortcoming that the aircraft such as existing helicopter, fire balloon, dirigible can not fly for a long time aloft, has zero-emission Driven by Solar Energy, good airworthiness, low cost, operation of flying when fine day can grow boat, the advantage such as of many uses.
Description
Technical field:
The utility model relates to technical field of aerospace and technical field of new energies.
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 it all exists the shortcoming that can not fly for a long time aloft, there is 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
Problem during the above-mentioned short boat that the present utility model exists for existing various aircraft, provide a kind of structure simple, solar power vertically taking off and landing flyer when adopting solar powered length to navigate, its objective is the key issue of flight when the energy-saving and emission-reduction of solution multi-rotor aerocraft and long boat, improve solar power vertically taking off and landing flyer when a length of flying when can grow boat is navigated.
The utility model adopts following technical scheme to realize: solar power vertically taking off and landing flyer during long boat, it is made up of the multi-rotor aerocraft of Ultralight structure, thin solar module, controller, picture pick-up device, controller is connected with picture pick-up device, and the multi-rotor aerocraft of Ultralight structure is fixed on thin solar module both sides and described in the solar module relying on upper surface to lay, aircraft provides power source.
The utility model comprises (1). four axle flying platform formula multi-rotor aerocrafts of Ultralight structure; (2). thin solar module; (3). controller; (4). picture pick-up device.It is characterized in that: during fine day, rely on the frivolous solar module that upper surface is laid, for during long boat, solar power vertically taking off and landing flyer provides power source, fly during the long boat of solar power vertically taking off and landing flyer when making long boat and carry out making a video recording, photograph, detection etc.
The utility model has the advantages that: rely on solar power to provide power source, structure is simple, practicality easy to carry.
Accompanying drawing explanation
Solar power vertically taking off and landing flyer schematic diagram when Fig. 1 is the utility model length boat.
Reference numeral: 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, solar power vertically taking off and landing flyer during long boat, it is made up of four axle flying platform formula multi-rotor aerocrafts 1 of Ultralight structure, thin solar module 2, controller 3, picture pick-up device 4, controller 3 is connected with picture pick-up device 4, and the multi-rotor aerocraft 1 of Ultralight structure is fixed on thin solar module 2 both sides and described in the solar module relying on upper surface to lay, aircraft provides power source.The utility model 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 (1)
1. solar power vertically taking off and landing flyer during long boat, it is characterized in that being made up of four axle flying platform formulas multi-rotor aerocraft (1) of Ultralight structure, thin solar module (2), controller (3), picture pick-up device (4), controller (3) is connected with picture pick-up device (4), and the multi-rotor aerocraft (1) of Ultralight structure is fixed on thin solar module (2) both sides and described in the solar module relying on upper surface to lay, aircraft provides power source.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420091987.8U CN204037899U (en) | 2014-02-28 | 2014-02-28 | Solar power vertically taking off and landing flyer during long boat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420091987.8U CN204037899U (en) | 2014-02-28 | 2014-02-28 | Solar power vertically taking off and landing flyer during long boat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204037899U true CN204037899U (en) | 2014-12-24 |
Family
ID=52238594
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420091987.8U Expired - Fee Related CN204037899U (en) | 2014-02-28 | 2014-02-28 | Solar power vertically taking off and landing flyer during long boat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204037899U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104743114A (en) * | 2015-03-19 | 2015-07-01 | 陈英 | Aircraft |
| CN112977787A (en) * | 2021-03-11 | 2021-06-18 | 北京航天发射技术研究所 | Flexible fuselage wing aircraft |
| CN112977786A (en) * | 2021-03-11 | 2021-06-18 | 北京航天发射技术研究所 | Flexible tubular fuselage wing-group aircraft |
-
2014
- 2014-02-28 CN CN201420091987.8U patent/CN204037899U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104743114A (en) * | 2015-03-19 | 2015-07-01 | 陈英 | Aircraft |
| CN112977787A (en) * | 2021-03-11 | 2021-06-18 | 北京航天发射技术研究所 | Flexible fuselage wing aircraft |
| CN112977786A (en) * | 2021-03-11 | 2021-06-18 | 北京航天发射技术研究所 | Flexible tubular fuselage wing-group aircraft |
| CN112977786B (en) * | 2021-03-11 | 2023-02-21 | 北京航天发射技术研究所 | Flexible tubular fuselage wing-group aircraft |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141224 Termination date: 20160228 |