CN202264884U - Solar flying saucer device - Google Patents
Solar flying saucer device Download PDFInfo
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- CN202264884U CN202264884U CN2011203384984U CN201120338498U CN202264884U CN 202264884 U CN202264884 U CN 202264884U CN 2011203384984 U CN2011203384984 U CN 2011203384984U CN 201120338498 U CN201120338498 U CN 201120338498U CN 202264884 U CN202264884 U CN 202264884U
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- flying saucer
- solar
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Abstract
The utility model relates to a solar flying saucer device, which comprises a flying saucer machine cabin with a central controller and is characterized in that a rotating shaft capable of rotating driven by a motor is arranged on the flying saucer machine cabin, radial wings formed by a plurality of solar cell panels are connected onto the rotating shaft so as to convert solar energy to electric energy to supply power for the motor and drive the radial wings to rotate to generate upward lifting power. The external end portions of the radial wings are connected through an annular body, a plurality of universal air push-pull devices with power supplied by the electric energy converted from the solar energy are arranged on the annular body and connected with the annular body through universal joints, and working states of the universal air push-pull devices can be controlled by the central controller. An electricity storing device is further arranged on the flying saucer machine cabin so as to store the electric energy converted by the solar cell panels. The solar flying saucer device not only utilizes the solar energy to supply flying power to the flying saucer but also can flexibly control flying direction.
Description
Technical field
The utility model relates to a kind of solar power flying saucer device.
Background technology
Along with the develop rapidly of art such as communication, traffic, meteorology, more and more press for stable, the unrestricted aerial platform of channel capacity.Be engaged in the scientists of this aspect research and coincidentally eye invested advection layer, wait in expectation a kind of can in advection layer, the appearance by stable floating platform.Stratospheric space environment is between space and ground, and 18 kilometers to 50 kilometers of face of land height do not have the spatial domain restriction at present.Advection layer does not have steam basically, ceiling unlimited, and sunlight is strong, is confirmed as no life zone by aeronautics.Because the solar energy that advection layer is accepted is the several times of the earth, is that the research and development of the Helios of power source become new focus with the solar power.
The empty day aircraft of solar power has purposes widely in fields such as communication, meteorology, ground monitoring, national defence, as: communication repeating platform, atmospheric sampling and the battlefield surveillance of space tourism, aerial photography, the condition of a disaster monitoring, large-scale activity, target positioning, scouting or the like round the clock.But the function of this system's part instead of satellites more has superiority than satellite in the plurality of applications field.Because its flying height is well below satellite, its communication quality is better in communications applications, signal lag is shorter.
At present, countries in the world are all in the research of actively developing Helios.The Helios of states such as the U.S., Switzerland, Russia all successfully rises up into advection layer at present, and has carried out multinomial valuable experiment, and China also is being in the pri stage aspect the research of stratosphere flight device.
Summary of the invention
The purpose of the utility model is to provide a kind of solar power flying saucer device, and this device not only can utilize solar power for flying saucer flying power to be provided, and can control heading flexibly.
For realizing above-mentioned purpose; The technical scheme of the utility model is: a kind of solar power flying saucer device; Comprise the flying saucer cabin that is provided with central controller, it is characterized in that: said flying saucer cabin is provided with and can be connected with a plurality of radially wings that are made up of solar panel in the said rotating shaft by the rotating shaft of direct motor drive rotation; Can be said electrical motor power supply with conversion solar, drive said radially wing rotation and produce lift upwards; Said each radially outer end one annular solid of wing be connected; Said annular solid is provided with the universal blowing suction device that a plurality of electric energy that transformed by said solar panel provide power; Said universal blowing suction device is connected with said annular solid through universal-joint, and can be by said central controller controls operating attitude; Said flying saucer also is provided with electric storage device on the cabin, to store the electric energy that said solar panel transforms.
The beneficial effect of the utility model is the innovative design through solar power flying saucer structure; Utilize the electric energy of conversion of solar energy to drive radially wing rotation generation lift upwards; Thereby for solar power flying saucer device flying power is provided, but has realized that a stabilized flight is in stratospheric aerial platform.In addition, this device can be realized the flexible control of heading through the adjustment of universal blowing suction device operating attitude, and is practical.Therefore, the utlity model has wide application prospect.
Below in conjunction with accompanying drawing and specific embodiment the utility model is done further to specify.
Description of drawings
Fig. 1 is the plan structure scheme drawing of the utility model embodiment.
Fig. 2 is the side direction structural representation of the utility model embodiment.
Fig. 3 is the wing section scheme drawing of the radially wing of the utility model embodiment.
The specific embodiment
The solar power flying saucer device of the utility model; Like Fig. 1, shown in 2; Comprise the flying saucer cabin 1 that is provided with central controller, said flying saucer cabin 1 is provided with and can be connected with a plurality of radially wings 3 that are made up of solar panel in the said rotating shaft 2 by the rotating shaft 2 of direct motor drive rotation; Can be said electrical motor power supply with conversion solar, drive said radially wing 3 rotations and produce lift upwards; Said each radially outer end one annular solid 4 of wing 3 be connected; Said annular solid 4 is provided with the universal blowing suction device 5 that a plurality of electric energy that transformed by said solar panel provide power; Said universal blowing suction device 5 is connected with said annular solid 4 through universal-joint, and can be by said central controller controls operating attitude; Also be provided with electric storage device on the said flying saucer cabin 1, but said electric storage device comprises the device of storage of electrical energy such as storage battery, high energy nickel carbon cond, to store the electric energy that said solar panel transforms.
Fly in order to be beneficial in that advection layer is flat, as shown in Figure 3, the wing section of above-mentioned radially wing 3 is stream line pattern, and the leading edge 6 in said wing section is slick and sly shape and top arching, and the trailing edge 7 in said wing section is sharp thin shape, and the bottom 8 in said wing section is flats.
Fly in order to be beneficial in that advection layer is flat, as shown in Figure 2, the outward flange 9 of the radial section of above-mentioned annular solid 4 is slick and sly shape, and 10 arching bottoms 11, top are flat.
Also be provided with on the above-mentioned flying saucer cabin 1 a plurality of can be by the universal blowing suction device 5 of said central controller controls operating attitude.
More than be the preferred embodiment of the utility model, all changes of being done according to the utility model technical scheme when the function that is produced does not exceed the scope of the utility model technical scheme, all belong to the protection domain of the utility model.
Claims (4)
1. solar power flying saucer device; Comprise the flying saucer cabin that is provided with central controller; It is characterized in that: said flying saucer cabin is provided with can be by the rotating shaft of direct motor drive rotation; Be connected with a plurality of radially wings that constitute by solar panel in the said rotating shaft, can be said electrical motor power supply, drive said radially wing rotation and produce lift upwards with conversion solar; Said each radially outer end one annular solid of wing be connected; Said annular solid is provided with the universal blowing suction device that a plurality of electric energy that transformed by said solar panel provide power; Said universal blowing suction device is connected with said annular solid through universal-joint, and can be by said central controller controls operating attitude; Said flying saucer also is provided with electric storage device on the cabin, to store the electric energy that said solar panel transforms.
2. solar power flying saucer device according to claim 1; It is characterized in that: the wing section of said radially wing is stream line pattern; The leading edge in said wing section is slick and sly shape and top arching, and the trailing edge in said wing section is sharp thin shape, and the bottom in said wing section is flats.
3. solar power flying saucer device according to claim 1 is characterized in that: the outward flange of the radial section of said annular solid is slick and sly shape and arching bottom, top is flat.
4. solar power flying saucer device according to claim 1 is characterized in that: also be provided with on the said flying saucer cabin a plurality of can be by the universal blowing suction device of said central controller controls operating attitude.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011203384984U CN202264884U (en) | 2011-09-09 | 2011-09-09 | Solar flying saucer device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011203384984U CN202264884U (en) | 2011-09-09 | 2011-09-09 | Solar flying saucer device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202264884U true CN202264884U (en) | 2012-06-06 |
Family
ID=46155693
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011203384984U Expired - Fee Related CN202264884U (en) | 2011-09-09 | 2011-09-09 | Solar flying saucer device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202264884U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104309804A (en) * | 2014-10-22 | 2015-01-28 | 北京航空航天大学 | Novel disc type rotor wing layout solar aircraft |
| CN104340367A (en) * | 2013-08-02 | 2015-02-11 | 罗才德 | Flying saucer reconnaissance airplane |
| WO2017176174A1 (en) * | 2016-04-06 | 2017-10-12 | Bashayan Kholoud | Oxygen producing flying scooter |
-
2011
- 2011-09-09 CN CN2011203384984U patent/CN202264884U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104340367A (en) * | 2013-08-02 | 2015-02-11 | 罗才德 | Flying saucer reconnaissance airplane |
| CN104309804A (en) * | 2014-10-22 | 2015-01-28 | 北京航空航天大学 | Novel disc type rotor wing layout solar aircraft |
| WO2017176174A1 (en) * | 2016-04-06 | 2017-10-12 | Bashayan Kholoud | Oxygen producing flying scooter |
| US10960871B2 (en) | 2016-04-06 | 2021-03-30 | Kholoud Bashayan | Oxygen producing flying scooter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120606 Termination date: 20130909 |