CN106533352A - Shading device for satellite solar cell array and using method thereof - Google Patents
Shading device for satellite solar cell array and using method thereof Download PDFInfo
- Publication number
- CN106533352A CN106533352A CN201610815973.XA CN201610815973A CN106533352A CN 106533352 A CN106533352 A CN 106533352A CN 201610815973 A CN201610815973 A CN 201610815973A CN 106533352 A CN106533352 A CN 106533352A
- Authority
- CN
- China
- Prior art keywords
- satellite
- cloth
- aluminized mylar
- solar cell
- electrostatic preventive
- 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
- 238000000034 method Methods 0.000 title claims abstract description 8
- 239000004744 fabric Substances 0.000 claims abstract description 49
- 229920000134 Metallised film Polymers 0.000 claims description 21
- 230000003449 preventive effect Effects 0.000 claims description 21
- 229920006267 polyester film Polymers 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 238000004891 communication Methods 0.000 abstract description 2
- 238000009434 installation Methods 0.000 abstract 1
- 210000004027 cell Anatomy 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 210000001057 smooth muscle myoblast Anatomy 0.000 description 2
- 239000008280 blood Substances 0.000 description 1
- 210000004369 blood Anatomy 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000001678 irradiating effect Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S40/00—Components or accessories in combination with PV modules, not provided for in groups H02S10/00 - H02S30/00
- H02S40/20—Optical components
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Landscapes
- Photovoltaic Devices (AREA)
Abstract
The invention provides a shading device for a satellite solar cell array and a using method thereof. The shading device comprises a piece of anti-static cloth, an aluminium-plated polyester film, and elastic cords. The anti-static cloth is a cloth sleeve; the aluminium-plated polyester film is arranged at the outer surface of the cloth sleeve; and the elastic cords are connected with the cloth sleeve. The shading device has the following beneficial effects: (1), with the aluminium-plated polyester film, light irradiation on solar cell pieces of a solar cell array can be prevented; (2), with the anti-static cloth, performances of the satellite solar cell array and other instrument equipment are not affected; and (3), the shading device has advantages of simple structure, easy installation, and high adaptability and can be applied to various satellites of remote sensing, communication, and testing and the like.
Description
Technical field
The present invention relates to satellite ground equipment, in particular it relates to Satellite vapour image shade and using method.
Background technology
Satellite vapour image is the important composition of satellite energy resource system, by the sun electricity on surface during satellite flight
Pond piece carries out energy acceptance and conversion, provides electric energy for satellite instrument equipment., after ground completes whole star assembling, the sun is electric for satellite
Pond piece is subject to light irradiation generation weak current to be powered satellite instrument equipment, directly affects the ground test of instrument and equipment
With in-orbit application.
Currently without the explanation or report that find technology similar to the present invention, domestic similar data is also not yet collected.
The content of the invention
In order to solve in prior art satellite complete assembling after before satellite launch, solar battery array by light photograph
Projection rings the problem of satellite performance, it is an object of the invention to provide a kind of Satellite vapour image shade and user
Method.
According to a kind of Satellite vapour image shade that the present invention is provided, including electrostatic preventive cloth, aluminized mylar
And elastic band；
Electrostatic preventive cloth is cloth set, and the outer surface of the cloth set is provided with aluminized mylar；Elastic band connects cloth set.
Preferably, the whole outer surface of the cloth set is covered by aluminized mylar.
Preferably, it is in cuboid when cloth set launches.
Preferably, elastic band is arranged in the surrounding of cloth set.
Preferably, cloth set includes photovoltaic panel overlay area, and the only outer surface of photovoltaic panel overlay area is covered to be provided with and aluminized
Polyester film.
The using method of a kind of above-mentioned Satellite vapour image shade provided according to the present invention, including：
Electrostatic preventive cloth is placed on outside satellite, whole satellite is located in electrostatic preventive cloth；
By the solar panel of the area covers satellite for being provided with aluminized mylar of electrostatic preventive cloth；
Elastic band is fastened, makes the region for being provided with aluminized mylar of electrostatic preventive cloth be close to cover the solar energy of satellite
Cell panel.
Compared with prior art, the present invention has following beneficial effect：
(1) aluminized mylar effectively prevents light from irradiating the solar cell piece of solar battery array.
(2) electrostatic preventive cloth is adopted, the performance of Satellite vapour image and other instrument and equipments is not affected.
(3) simple structure, be easily installed, strong adaptability, can be applicable to all kinds of satellites such as remote sensing, communication, test.
Description of the drawings
Detailed description non-limiting example made with reference to the following drawings by reading, the further feature of the present invention,
Objects and advantages will become more apparent upon：
Fig. 1 is a kind of schematic diagram of Satellite vapour image shade provided by the present invention；
Fig. 2 is a kind of application schematic diagram of Satellite vapour image shade provided by the present invention.
Specific embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill to this area
For personnel, without departing from the inventive concept of the premise, some changes and improvements can also be made.These belong to the present invention
Protection domain.
The present invention provides a kind of Satellite vapour image shade, including：Electrostatic preventive cloth, aluminized mylar and elastic
Band.The present invention solves satellite and completes after whole star general assembly too for preventing light irradiation Satellite vapour image solar cell piece
Positive cell piece is affected the problem of satellite performance by photograph, is had broad application prospects.
Fig. 1 is a kind of structural representation of Satellite vapour image shade.As shown in figure 1, Satellite vapour image
Shade includes：Electrostatic preventive cloth 1, aluminized mylar 2 and elastic band 3；The aluminized mylar 2 is pasted on antistatic
On the outside of the one of cloth 1, the elastic band 3 is arranged in 1 surrounding of electrostatic preventive cloth.
Electrostatic preventive cloth is cloth set, and the outer surface of the cloth set is provided with aluminized mylar；Elastic band connects cloth set.It is described
The whole outer surface of cloth set is covered by aluminized mylar, or cloth set includes photovoltaic panel overlay area, and only photovoltaic panel is covered
The outer surface in region is covered and is provided with aluminized mylar.Cloth set is in cuboid when launching.Elastic band is arranged in the surrounding of cloth set.
The using method of a kind of above-mentioned Satellite vapour image shade provided according to the present invention, including：
Electrostatic preventive cloth is placed on outside satellite, whole satellite is located in electrostatic preventive cloth；
By the solar panel of the area covers satellite for being provided with aluminized mylar of electrostatic preventive cloth；
Elastic band is fastened, makes the region for being provided with aluminized mylar of electrostatic preventive cloth be close to cover the solar energy of satellite
Cell panel.
Fig. 2 is a kind of application schematic diagram of Satellite vapour image shade.Satellite vapour image shade
Be pasted with aluminized mylar one faces outwardly, and another side is near solar battery array；Satellite vapour image shade is coated
In solar battery array and tighten elastic band.Compared with prior art, the present invention solves Satellite vapour image and is assembled to satellite
Affected satellite performance issue by light irradiation afterwards, simple structure, be easily assembled, strong adaptability, with being widely applied very much popularization
Value.
Above the specific embodiment of the present invention is described.It is to be appreciated that the invention is not limited in above-mentioned
Particular implementation, those skilled in the art can make a variety of changes within the scope of the claims or change, this not shadow
Ring the flesh and blood of the present invention.In the case where not conflicting, the feature in embodiments herein and embodiment can any phase
Mutually combine.
Claims (6)
1. a kind of Satellite vapour image shade, it is characterised in that including electrostatic preventive cloth, aluminized mylar and elastic
Band；
Electrostatic preventive cloth is cloth set, and the outer surface of the cloth set is provided with aluminized mylar；Elastic band connects cloth set.
2. Satellite vapour image shade according to claim 1, it is characterised in that the whole appearance of the cloth set
Face is covered by aluminized mylar.
3. Satellite vapour image shade according to claim 1, it is characterised in that in rectangular when cloth set launches
Body.
4. Satellite vapour image shade according to claim 1, it is characterised in that elastic band is arranged in cloth set
Surrounding.
5. Satellite vapour image shade according to claim 1, it is characterised in that cloth set includes photovoltaic panel covering
The outer surface in region, only photovoltaic panel overlay area is covered and is provided with aluminized mylar.
6. the using method of the Satellite vapour image shade any one of a kind of claim 1 to 5, its feature exist
In, including：
Electrostatic preventive cloth is placed on outside satellite, whole satellite is located in electrostatic preventive cloth；
By the solar panel of the area covers satellite for being provided with aluminized mylar of electrostatic preventive cloth；
Elastic band is fastened, makes the region for being provided with aluminized mylar of electrostatic preventive cloth be close to cover the solar cell of satellite
Plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610815973.XA CN106533352B (en) | 2016-09-08 | 2016-09-08 | Satellite vapour image shade and application method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610815973.XA CN106533352B (en) | 2016-09-08 | 2016-09-08 | Satellite vapour image shade and application method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106533352A true CN106533352A (en) | 2017-03-22 |
| CN106533352B CN106533352B (en) | 2018-05-01 |
Family
ID=58344299
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610815973.XA Active CN106533352B (en) | 2016-09-08 | 2016-09-08 | Satellite vapour image shade and application method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106533352B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3631735A1 (en) * | 1986-09-18 | 1988-04-07 | Messerschmitt Boelkow Blohm | MESSAGE TRANSFER DEVICE FOR SPACE VEHICLES |
| JP2000318639A (en) * | 1999-05-03 | 2000-11-21 | Hyundai Motor Co Ltd | Reinforcing structure of motor vehicle body |
| WO2014203817A1 (en) * | 2013-06-17 | 2014-12-24 | 株式会社カネカ | Solar cell module and method for producing solar cell module |
| CN204937537U (en) * | 2015-07-28 | 2016-01-06 | 上海卫星工程研究所 | A kind of device for alternative space vehicle side plate |
-
2016
- 2016-09-08 CN CN201610815973.XA patent/CN106533352B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3631735A1 (en) * | 1986-09-18 | 1988-04-07 | Messerschmitt Boelkow Blohm | MESSAGE TRANSFER DEVICE FOR SPACE VEHICLES |
| JP2000318639A (en) * | 1999-05-03 | 2000-11-21 | Hyundai Motor Co Ltd | Reinforcing structure of motor vehicle body |
| WO2014203817A1 (en) * | 2013-06-17 | 2014-12-24 | 株式会社カネカ | Solar cell module and method for producing solar cell module |
| CN204937537U (en) * | 2015-07-28 | 2016-01-06 | 上海卫星工程研究所 | A kind of device for alternative space vehicle side plate |
Non-Patent Citations (1)
| Title |
|---|
| 张国强，王锐，朱志国等: ""新型抗静电聚酯纤维的制备及其结构性能"", 《纺织学报》 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106533352B (en) | 2018-05-01 |
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