CN107416231A - Pneumatic-control type thin film solar windsurfing and its accommodation method - Google Patents
Pneumatic-control type thin film solar windsurfing and its accommodation method Download PDFInfo
- Publication number
- CN107416231A CN107416231A CN201710507689.0A CN201710507689A CN107416231A CN 107416231 A CN107416231 A CN 107416231A CN 201710507689 A CN201710507689 A CN 201710507689A CN 107416231 A CN107416231 A CN 107416231A
- Authority
- CN
- China
- Prior art keywords
- film solar
- thin film
- solar energy
- windsurfing
- cluster
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/42—Arrangements or adaptations of power supply systems
- B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
- B64G1/443—Photovoltaic cell arrays
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Winding Of Webs (AREA)
Abstract
The invention discloses a kind of Pneumatic-control type thin film solar windsurfing and its accommodation method, it includes some cluster film solar energy sailboards, the both sides per cluster film solar energy sailboard are respectively equipped with a bronchus, the connection of some cluster film solar energy sailboards is integral by array connect band between described some cluster film solar energy sailboards, one end of some cluster film solar energy sailboards is additionally provided with a main tracheae, the bronchus respectively with every cluster film solar energy sailboard both sides of the main tracheae is connected, and UNICOM；Place is additionally provided with air inlet electromagnetic valve below among the described main tracheae, some cluster film solar energy sailboard both sides it is bronchial above and below be respectively equipped with several exhaust solenoid valves；The thin film solar windsurfing is simple and reliable for structure, and not only storage is convenient, and developed area is bigger than traditional outspreading sailboard area, and the present invention can realize that left rotation and right rotation is adjusted, and can also realize that tilting forward and back angle is adjusted by gas control.
Description
Technical field
The present invention relates to technical field of solar, and in particular to a kind of Pneumatic-control type thin film solar windsurfing and its storage side
Method.
Background technology
Concern of the countries in the world man for aerospace industry in recent years is increasing, and the research of spacecraft is also more and more extensive,
And the solar battery array as the main stream feed system of spacecraft also constantly gets a promotion in technology, structure etc.,
Progressively adapt to various highly difficult complicated space flight requirements.Solar battery array is the main power-supply system of in-orbit spacecraft.Sun electricity
Chi Zhen is arranged and formed in length and breadth by the solar cell for being connected into certain circuit, using the sunlight direct generation of electricity without chemical process.In the sun
In the development course of cell array, its configuration constantly develops, become it is increasingly advanced with it is perfect.Nowadays the design of solar battery array is more
Involvement divergent thinking and innovative thinking, stepped into new step, to meet increasingly complex space mission.
However, just from the point of view of current existing technology, solar energy sailboard is when being loaded in spacecraft due to spacecraft space
It is limited, and traditional solar energy sailboard is all to be loaded into using bulk form in spacecraft, therefore, when solar energy sailboard is excessive
When, spacecraft can not deliver；And the electric energy supply of space station can not be met when too small.In addition, existing solar energy sailboard exists
Needed in space according to the angle of solar energy sailboard is adjusted to day, just at present, existing solar energy sailboard is all to use
Finely tune to realize to day left and right.And those of skill in the art understand, a suspended state is in too aerial object, because
This, often because displacement can be produced by suspending, causes sunray not to be radiated on solar energy sailboard correctly.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of Pneumatic-control type thin film solar windsurfing and its accommodation method,
The thin film solar windsurfing is simple and reliable for structure, and not only storage is convenient, and developed area is than traditional outspreading sailboard area
Big, the present invention can realize that left rotation and right rotation is adjusted, and can also realize that tilting forward and back angle is adjusted by gas control.
The technical problems to be solved by the invention are realized using following technical scheme：
A kind of Pneumatic-control type thin film solar windsurfing, it includes some cluster film solar energy sailboards, described per the cluster film sun
The both sides of energy windsurfing are respectively equipped with a bronchus, pass through array connect band between described some cluster film solar energy sailboards
The connection of some cluster film solar energy sailboards is integral, one end of some cluster film solar energy sailboards is additionally provided with a master
Tracheae, the bronchus respectively with every cluster film solar energy sailboard both sides of the main tracheae is connected, and UNICOM；
Place is additionally provided with air inlet electromagnetic valve below among the described main tracheae, in some cluster film solar energy sailboards two
The bronchial top of side is provided with several upward exhaust solenoid valves, sets also be provided with several exhaust electromagnetism downwards thereunder
Valve；
The application also includes control system and gas generator, and described control system connects with described gas generator
Connect, and control the air demand of gas generator in real time by control system, described gas generator is by pipeline and enters pneumoelectric
Magnet valve connect, provide source of the gas in real time to main tracheae by gas generator, described control system also respectively with bronchus
Upward exhaust solenoid valve is connected with downward exhaust solenoid valve, and intrabronchial air pressure is adjusted by control system.
As the present invention further improvement is that：Described main tracheae middle position is additionally provided with one and is connected with spacecraft
There is active connection.
As the present invention further improvement is that：Described active connection includes being used to consolidate with what main tracheae was fixedly connected
Reservation, and two groups of hangers being arranged in fixed seat, a connecting hole is had on two groups of hangers, and described
A movable axis is provided with connecting hole, described movable axis has a linking arm being connected with spacecraft rotating mechanism.
As the present invention further improvement is that：The spacing of the array connect band is equal.
As the present invention further improvement is that：The connect band use make with the strong nonmetallic materials of toughness and
Into.
As the present invention further improvement is that：The quantity of the thin film solar windsurfing is odd number.
As the present invention further improvement is that：Described main trachea and bronchus is air bag.
Another object of the present invention is to additionally provide a kind of accommodation method of Pneumatic-control type thin film solar windsurfing, its feature
It is, it is comprised the following steps that：
Step S1, winding prepares
The gas in main trachea and bronchus is extracted out first, several thin film solar windsurfings is lost tension, then
According to the distance between connect band and connect band, the girth that will some cluster film solar energy sailboards often be enclosed with winding is calculated, is made
Equal with the spacing of connect band per circumference length, it is overlapping with connect band to reach connect band, and by some cluster film solar energy sails
Coiled sheet is coiled into cylindrical shape；
Step S2, fold and prepare
After some cluster film solar energy sailboards are wound into cylindrical shape, rolled up with a most middle cluster film solar energy sailboard
Centered on group, other volume groups at its both ends are close to a cluster film solar energy sailboard volume group of centre successively, make to be integrally formed
One thin film solar windsurfing packaging container being made up of multiple cylinders；
Step S3, store
Because spacecraft shape is usually a cylindrical structure, the thin film solar windsurfing packaging container in step S2 is filled
Enter in spacecraft storage storehouse, thin film solar windsurfing packaging container surrounding is affixed with space flight storage storehouse inwall, so as to save sky
Between area occupied.
The beneficial effects of the invention are as follows：
1) present invention forms an entirety using some cluster film solar energy sailboards by connect band, not only increases the sun
The collection rate of energy, and the present invention is stored by volume group and after folding, and area occupied and the carrying for reducing spacecraft are heavy
Amount；
2) present invention uses air pressure mode to realize the expansion to thin film solar windsurfing, meanwhile, the present invention can not only realize
Leftward/rightward rotating is adjusted, but also can tilt forward and back angle regulation to thin film solar windsurfing by gas control mode, so as to
Solve various solar radiation angles.
Brief description of the drawings
Fig. 1 is positive structure schematic of the present invention；
Fig. 2 is structure schematic diagram of the present invention；
Fig. 3 is A-A direction structure schematic diagrames in Fig. 1；
Fig. 4 is B-B direction structure schematic diagrames in Fig. 1；
Fig. 5 is control system architecture schematic diagram of the present invention；
Fig. 6 is Moveable connecting piece structure schematic diagram in the present invention；
Fig. 7 is structural representation after thin film solar windsurfing volume group of the present invention；
Fig. 8 is C portion structure enlargement diagram in Fig. 7；
Fig. 9 be volume group of the present invention after fold schematic flow sheet；
Figure 10 folds rear end face structural representation for the present invention；
Figure 11 is thin film solar windsurfing tilt adjustment view to the right in the embodiment of the present invention one；
Figure 12 is thin film solar windsurfing tilt adjustment view to the left in the embodiment of the present invention one；
Figure 13 is thin film solar windsurfing tilt adjustment view forwards in the embodiment of the present invention one；
Figure 14 is thin film solar windsurfing rearward tilt adjustment view in the embodiment of the present invention one.
Embodiment
In order that the technical means, the inventive features, the objects and the advantages of the present invention are easy to understand, tie below
Conjunction is specifically illustrating and embodiment, and the present invention is expanded on further.
As shown in figures 1 to 6, a kind of Pneumatic-control type thin film solar windsurfing, it includes some cluster film solar energy sailboards 100, often
The both sides of cluster film solar energy sailboard 100 are respectively equipped with a bronchus 300, in described some cluster film solar energy sailboards
The connection of some cluster film solar energy sailboards 100 is integral by array connect band 200 between 100, some cluster film sun
Can one end of windsurfing 100 be additionally provided with a main tracheae 400, the main tracheae 400 respectively with every both sides of cluster film solar energy sailboard 100
Bronchus 300 be connected, and UNICOM；
Place is additionally provided with air inlet electromagnetic valve 401 below the main centre of tracheae 400, in some 100 liang of cluster film solar energy sailboards
The top of the bronchus 300 of side is provided with several upward exhaust solenoid valve 30a, sets also be provided with several exhausts downwards thereunder
Magnetic valve 30b；
The application also includes control system 500 and gas generator 600, and control system 500 connects with gas generator 600
Connect, and control the air demand of gas generator 600 in real time by control system 500, gas generator 600 passes through pipeline and air inlet
Magnetic valve 401 is connected, and source of the gas is provided main tracheae 400 in real time by gas generator 600, control system 500 also respectively with branch gas
Downward exhaust solenoid valve 30b on pipe 300 connects with upward exhaust solenoid valve 30a, by control system 500 to bronchus 300
Interior air pressure is adjusted.Some cluster film solar energy sailboards 100 are tilted forward or backward to realize.
An active connection being connected with spacecraft 700 is additionally provided with the main middle position of tracheae 400.Active connection
700 fixed seats 70 including being used to be fixedly connected with main tracheae 400, and two groups of hangers 71 being arranged in fixed seat 70, two
A connecting hole 72 is had on group hanger 71, and a movable axis 73 is provided with connecting hole 72, movable axis 73 is provided with
There is a linking arm 74 being connected with spacecraft rotating mechanism.
In the present invention, the spacing of array connect band 200 is equal, and connect band 200 is using with strong nonmetallic of toughness
Material is made (it is makrolon in the present invention, to have the strong nonmetallic materials of toughness), wherein, thin film solar windsurfing
100 quantity is odd number.Main trachea and bronchus is respectively air bag.
As shown in figs. 7-14, another object of the present invention is to additionally provide a kind of receipts of Pneumatic-control type thin film solar windsurfing
Receive method, it is comprised the following steps that：
Step S1, winding prepares
The gas in main trachea and bronchus is extracted out first, several thin film solar windsurfings is lost tension, then
According to the distance between connect band 200 and connect band 200, calculating will often enclose winding to some cluster film solar energy sailboards 100
Girth, make every circumference length equal with the spacing of connect band 200, it is overlapping with connect band 200 to reach connect band 200, and will
Some cluster film solar energy sailboards 100 are wound into cylindrical shape；
Step S2, fold and prepare
After some cluster film solar energy sailboards 100 are wound into cylindrical shape, with a most middle cluster film solar energy sail
Centered on plate groups of volume 100, other volume groups at its both ends are close to cluster film solar energy sailboard groups of volume 100 of centre successively,
Make a thin film solar windsurfing packaging container for being made up of (in the present embodiment, exemplified by seven groups) multiple cylinders is integrally formed
101；
Step S3, store
Because spacecraft shape is usually a cylindrical structure, by the thin film solar windsurfing packaging container in step S2
101 are fitted into spacecraft storage storehouse, the surrounding of thin film solar windsurfing packaging container 101 is affixed with space flight storage storehouse inwall, so as to
Dimensional footprint is saved.
Embodiment one
As shown in Figure 1 and Figure 2, the present invention implements supply by the main tracheae 400 of gas generator 600, and gas moves quickly through master
Tracheae 400 is simultaneously entered in all bronchuses 300, and now bronchus 300 and main tracheae 400 expand under the influence of air pressure,
And certain tension is produced, due to being connected between thin film solar windsurfing 100 using connect band 200, make several film sun
Energy windsurfing 100 deploys in the presence of tension, and forms an entirety.
When lighting angle deviates thin film solar windsurfing 100, and by spacecraft to thin film solar windsurfing 100 to the left or
Adjust to the right when also can not realize that illumination is relative with thin film solar windsurfing 100, now, control is sent by control system 500
Signal is controlled to the upward exhaust solenoid valve 30a on bronchus 300 and downward exhaust solenoid valve 30b.
When light tilts from the front of thin film solar windsurfing 100 to be injected：
The upward exhaust solenoid valve 30a that the front upper place of bronchus 300 is opened by control system 500 carries out exhaust upwards (downwards
Exhaust solenoid valve 30b and the upward exhaust solenoid valve of back upper place are at closed mode), due to that when gas is discharged, can produce
A raw opposite force, the front end of whole thin film solar windsurfing 100 is promoted downwards, make whole film too by the opposite force
The front end of positive energy windsurfing 100 is less than rear height, so as to reach (as shown in figure 13) corresponding with light.
When light is injected from the back sweep of thin film solar windsurfing 100：
The downward exhaust solenoid valve 30b that the front lower place of bronchus 300 is opened by control system 500 carries out exhaust downwards (upwards
Exhaust solenoid valve 30a and the downward exhaust solenoid valve of the back lower place are at closed mode), due to that when gas is discharged, can produce
A raw opposite force, the front end of whole thin film solar windsurfing 100 is promoted, make whole film too upward by the opposite force
The front end of positive energy windsurfing 100 is higher than rear height, so as to reach (as shown in figure 14) corresponding with light.
In addition, in the use of the present invention, directly being supplied by gas generator to main tracheae, gas can pass through main gas
Pipe enters each bronchus, and now, main trachea and bronchus can expand, and drives the group exhibitions of volume 100 of thin film solar windsurfing
Open, due to being provided with connect band between thin film solar windsurfing 100, tension is produced after the expansion of main trachea and bronchus, and
Several thin film solar windsurfings 100 are made to form an entirety in the presence of tension, so as to realize the collection to solar energy.
The basic principles, principal features and advantages of the present invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, the original for simply illustrating the present invention described in above-described embodiment and specification
Reason, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these changes and improvements
It all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its equivalent circle
It is fixed.
Claims (8)
- A kind of 1. Pneumatic-control type thin film solar windsurfing, it is characterised in that：It includes some cluster film solar energy sailboards (100), often The both sides of cluster film solar energy sailboard (100) are respectively equipped with a bronchus (300), in described some cluster film solar energy sails The connection of some cluster film solar energy sailboards (100) is integral by array connect band (200) between plate (100), if described One end of dry cluster film solar energy sailboard (100) is additionally provided with a main tracheae (400), and the main tracheae (400) is thin with every group respectively The bronchus (300) of film solar windsurfing (100) both sides is connected, and UNICOM；Air inlet electromagnetic valve (401) is being additionally provided with lower section among described main tracheae (400), in some cluster film solar energy The top of the bronchus (300) of windsurfing (100) both sides is provided with several upward exhaust solenoid valves (30a), sets also set thereunder There are several downward exhaust solenoid valves (30b)；The application also includes control system 500 and gas generator 600.
- A kind of 2. Pneumatic-control type thin film solar windsurfing according to claim 1, it is characterised in that：Described control system (500) it is connected with described gas generator (600), and gas generator (600) is controlled by control system (500) in real time Air demand, described gas generator (600) is connected by pipeline with air inlet electromagnetic valve (401), right by gas generator (600) Main tracheae (400) provides source of the gas in real time；Described control system (500) is also vented electromagnetism with the downward exhaust solenoid valve (30b) on bronchus 300 and upwards respectively Valve (30a) is connected, and the air pressure in bronchus (300) is adjusted by control system (500).
- A kind of 3. Pneumatic-control type thin film solar windsurfing according to claim 1, it is characterised in that：In the main tracheae (400) Between opening position be additionally provided with an active connection being connected with spacecraft (700).
- A kind of 4. Pneumatic-control type thin film solar windsurfing according to claim 1, it is characterised in that：The array connect band (200) spacing is equal.
- A kind of 5. Pneumatic-control type thin film solar windsurfing according to claim 4, it is characterised in that：The connect band (200) is adopted The strong nonmetallic materials of apparatus flexible are made.
- A kind of 6. Pneumatic-control type thin film solar windsurfing according to claim 1, it is characterised in that：Thin film solar windsurfing (100) quantity is odd number.
- A kind of 7. Pneumatic-control type thin film solar windsurfing according to claim 1, it is characterised in that：Main tracheae (400) and branch gas It is air bag to manage (300).
- 8. a kind of accommodation method of Pneumatic-control type thin film solar windsurfing, it is comprised the following steps that：Step S1, winding preparesThe gas in main tracheae (400) and bronchus (300) is extracted out first, loses several thin film solar windsurfings (100) Tension is gone, then will be to some cluster film solar energy according to the distance between connect band (200) and connect band (200), calculating Windsurfing (100) often encloses the girth of winding, makes every circumference length equal with the spacing of connect band (200), reaches connect band (200) It is overlapping with connect band (200), and some cluster film solar energy sailboards (100) are wound into cylindrical shape；Step S2, fold and prepareAfter some cluster film solar energy sailboards (100) are wound into cylindrical shape, with a most middle cluster film solar energy sailboard (100) centered on volume group, the cluster film solar energy sailboard (100) that other volume groups at its both ends are close to centre successively is rolled up Group, make a thin film solar windsurfing packaging container (101) being made up of multiple cylinders is integrally formed；Step S3, storeBecause spacecraft shape is usually a cylindrical structure, by the thin film solar windsurfing packaging container (101) in step S2 It is fitted into spacecraft storage storehouse, thin film solar windsurfing packaging container (101) surrounding is affixed with space flight storage storehouse inwall, so as to save About dimensional footprint.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710507689.0A CN107416231B (en) | 2017-06-28 | 2017-06-28 | Pneumatic-control type thin film solar windsurfing and its accommodation method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710507689.0A CN107416231B (en) | 2017-06-28 | 2017-06-28 | Pneumatic-control type thin film solar windsurfing and its accommodation method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107416231A true CN107416231A (en) | 2017-12-01 |
| CN107416231B CN107416231B (en) | 2019-11-08 |
Family
ID=60426147
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710507689.0A Active CN107416231B (en) | 2017-06-28 | 2017-06-28 | Pneumatic-control type thin film solar windsurfing and its accommodation method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107416231B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108583913A (en) * | 2018-04-13 | 2018-09-28 | 合肥凯石投资咨询有限公司 | Towed solar powered aircraft and its take-off and landing device |
| CN108762313A (en) * | 2018-06-14 | 2018-11-06 | 合肥凯石投资咨询有限公司 | Solar energy unmanned plane towed solar cell folding electromagnetic accommodation method |
| CN109094821A (en) * | 2018-09-30 | 2018-12-28 | 哈尔滨工业大学 | A kind of flexibility solar wing elasticity boom repetition Zhan Shou mechanism |
| CN110148518A (en) * | 2019-06-18 | 2019-08-20 | 天津大学 | The magnet array and preparation method thereof in customized enhancing magnetic field |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101383568A (en) * | 2008-10-24 | 2009-03-11 | 哈尔滨工业大学 | Synchronous expansion mechanism for foldable inflating expansion solar cell paddles |
| CN102437404A (en) * | 2011-08-18 | 2012-05-02 | 哈尔滨工业大学 | Integrated structure of rigidized inflatable deployable truss type planar antenna and solar array |
| US20140326833A1 (en) * | 2010-01-21 | 2014-11-06 | Deployable Space Systems, Inc. | Directionally Controlled Elastically Deployable Roll-Out Array |
| US9156568B1 (en) * | 2012-04-16 | 2015-10-13 | Deployable Space Systems, Inc. | Elastically deployable panel structure solar arrays |
| CN105857643A (en) * | 2016-04-01 | 2016-08-17 | 上海微小卫星工程中心 | Flexible solar wing used for satellite power supply and two-degree-of-freedom storage device applied to flexible solar wing |
| CN106163965A (en) * | 2014-01-13 | 2016-11-23 | 康克斯科技公司 | Clasp and hanger system |
| US9653632B1 (en) * | 2013-03-15 | 2017-05-16 | Richard Clark Howell Beitman, Sr. | Solar power system and related methods |
-
2017
- 2017-06-28 CN CN201710507689.0A patent/CN107416231B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101383568A (en) * | 2008-10-24 | 2009-03-11 | 哈尔滨工业大学 | Synchronous expansion mechanism for foldable inflating expansion solar cell paddles |
| US20140326833A1 (en) * | 2010-01-21 | 2014-11-06 | Deployable Space Systems, Inc. | Directionally Controlled Elastically Deployable Roll-Out Array |
| CN102437404A (en) * | 2011-08-18 | 2012-05-02 | 哈尔滨工业大学 | Integrated structure of rigidized inflatable deployable truss type planar antenna and solar array |
| US9156568B1 (en) * | 2012-04-16 | 2015-10-13 | Deployable Space Systems, Inc. | Elastically deployable panel structure solar arrays |
| US9653632B1 (en) * | 2013-03-15 | 2017-05-16 | Richard Clark Howell Beitman, Sr. | Solar power system and related methods |
| CN106163965A (en) * | 2014-01-13 | 2016-11-23 | 康克斯科技公司 | Clasp and hanger system |
| CN105857643A (en) * | 2016-04-01 | 2016-08-17 | 上海微小卫星工程中心 | Flexible solar wing used for satellite power supply and two-degree-of-freedom storage device applied to flexible solar wing |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108583913A (en) * | 2018-04-13 | 2018-09-28 | 合肥凯石投资咨询有限公司 | Towed solar powered aircraft and its take-off and landing device |
| CN108583913B (en) * | 2018-04-13 | 2020-02-11 | 合肥凯石投资咨询有限公司 | Dragging type solar airplane and landing gear thereof |
| CN108762313A (en) * | 2018-06-14 | 2018-11-06 | 合肥凯石投资咨询有限公司 | Solar energy unmanned plane towed solar cell folding electromagnetic accommodation method |
| CN109094821A (en) * | 2018-09-30 | 2018-12-28 | 哈尔滨工业大学 | A kind of flexibility solar wing elasticity boom repetition Zhan Shou mechanism |
| CN110148518A (en) * | 2019-06-18 | 2019-08-20 | 天津大学 | The magnet array and preparation method thereof in customized enhancing magnetic field |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107416231B (en) | 2019-11-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107416231A (en) | Pneumatic-control type thin film solar windsurfing and its accommodation method | |
| US11001379B2 (en) | Airborne data farming | |
| US9493223B2 (en) | System, method and apparatus for widespread commercialization of hydrogen as a carbon-free alternative fuel source | |
| US8132762B2 (en) | Space based rotating film solar battery array | |
| US20200262536A1 (en) | Buoyancy aerial vehicle | |
| US20090127861A1 (en) | Fluid-dynamic renewable energy harvesting system | |
| WO2014158202A1 (en) | Active volume energy level large scale sub-sea energy fluids storage methods and apparatus for power generation and integration of renewable energy sources | |
| CN110748467A (en) | Intelligent control air suction type electric propulsion system applicable to multiple flow states | |
| CN110466729B (en) | Buoyancy pressure and mass center integrated adjusting system of soft stratospheric airship | |
| CN110374830A (en) | Storage tank is heated in heat radiation suitable for iodine working medium electric propulsion device | |
| CN102295066B (en) | Remote off-line regulation suspension-type wind energy umbrella sail device with double-air sac system | |
| CN103236804B (en) | Spherical inflatable space solar power station | |
| CN103466197A (en) | Supporting packaging structure oriented to solar sail adopting inflatable auxiliary self-rebounding supporting arm | |
| CN208149586U (en) | Dirigible | |
| WO2017061968A1 (en) | Vessel system with photovoltaic energy having collapsible and floating properties | |
| CN107940106B (en) | A kind of attitude control engine pipeline support component | |
| GB2569002A (en) | Buoyancy aerial vehicle and method of flight | |
| CN110469427B (en) | Anti-shaking method and structure for vertical recovery liquid rocket propulsion system | |
| CN105438501A (en) | Space station aqueous-based propulsion system based on hydrogen arc thruster and hydrogen oxygen engine | |
| CN108528712A (en) | A kind of jet-propelled unmanned aerial vehicle of bull | |
| US20200385098A1 (en) | System, method and apparatus for widespread commercialization of hydrogen as a carbon-free alternative fuel source | |
| CN103094591B (en) | Be applied to the efficient gas storage system of the regeneratable fuel cell of aerostatics | |
| CN108880405B (en) | Pneumatic type space sun umbrella photovoltaic power station | |
| CN105799907A (en) | Bionic telescopic airship and coordination control method thereof | |
| CN108688788A (en) | A kind of Powered Propulsion fire balloon |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |