CN205564780U - Solar cell panel for satellite - Google Patents
Solar cell panel for satellite Download PDFInfo
- Publication number
- CN205564780U CN205564780U CN201620350712.0U CN201620350712U CN205564780U CN 205564780 U CN205564780 U CN 205564780U CN 201620350712 U CN201620350712 U CN 201620350712U CN 205564780 U CN205564780 U CN 205564780U
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- CN
- China
- Prior art keywords
- satellite
- solar cell
- cell panel
- solar panel
- eva layer
- 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.)
- Expired - Fee Related
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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
- 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
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- Photovoltaic Devices (AREA)
Abstract
The utility model discloses a solar cell panel for satellite, include the alloy frame and install the frame heat preservation of alloy frame one side, just frame heat preservation side -mounting bottom heat preservation, bottom heat preservation bottom sets up galvanized iron, bottom heat preservation top installation collection distributive pipe, just collection distributive pipe top installation solar cell panel, solar cell panel top installation guard net, solar cell panel inside sets up super white toughened glass, super white toughened glass bottom sets up a EVA layer, just EVA layer bottom sets up the silicon crystal, the silicon crystal bottom sets up the 2nd EVA layer, just the 2nd EVA layer bottom installation TPT backplate. This solar cell panel for satellite accessible solar cell panel turns into the electric energy with light energy, for the satellite provides power, makes the life of satellite obtain the improvement. It can effectual protection solar cell panel at the guard net at solar cell panel top to install.
Description
Technical field
This utility model relates to space technology field, is specially a kind of satellite solar panel.
Background technology
Along with the economic and development of science and technology and mankind's yearning to space, space technology is quickly developed, its Satellite occupies highly important status at space industry again, artificial earth satellite purposes is wide, of a great variety, has deep space communication satellite, space remote sensing earth resources satellite, space weather satellite, space aeronautical satellite, space reconnaissance satellite, space broadcast satellite, space geodetic satellite, space astronomical satellite etc..Satellite plays the most important effect in social life, and human society has be unable to do without artificial earth satellite, but, current satellite is short for service life, causes the great wasting of resources.For this it is proposed that a kind of satellite solar panel.
Utility model content
The purpose of this utility model is to provide a kind of satellite solar panel, with the problem solving to propose in above-mentioned background technology.
For achieving the above object, this utility model provides following technical scheme: a kind of satellite solar panel, including alloy frame and the frame heat-insulation layer that is arranged on described alloy frame side, and described frame heat-insulation layer side install bottom heat-insulation layer；Arranging galvanized iron sheet bottom the heat-insulation layer of described bottom, collection distributive pipe is installed at heat-insulation layer top, described bottom, and solar panel is installed at described collection distributive pipe top；Catch net is installed at described solar panel top, and described solaode intralaminar part arranges ultrawhite safety glass, arranges and arrange silicon crystal bottom the first EVA layer, and described first EVA layer bottom described ultrawhite safety glass；Installation TPT backboard bottom second EVA layer, and described second EVA layer is set bottom described silicon crystal.
Preferably, seamless between described ultrawhite safety glass with described first EVA layer contact.
Preferably, it is in close contact between described silicon crystal and described second EVA layer.
Preferably, between described catch net with described alloy frame, bolt is connected.
Preferably, it is electrically connected with between several described solar panels.
Compared with prior art, the beneficial effects of the utility model are: this satellite solar panel can convert light energy into electric energy by solar panel, provide power for satellite, make be improved the service life of satellite.The catch net being arranged on solar panel top can be effectively protected solar panel; stop the space trash destruction to solar panel; meanwhile, bottom heat-insulation layer and frame heat-insulation layer, can effectively prevent that solar panel temperature difference is excessive causes solar panel to lose efficacy.
Accompanying drawing explanation
Fig. 1 is this utility model overall structure schematic diagram；
Fig. 2 is this utility model solar panel cut-away view.
In figure: 1, alloy frame, 2, bottom heat-insulation layer, 3, frame heat-insulation layer, 4, collection distributive pipe; 5, catch net, 6, galvanized iron sheet, 7, solar panel, 71, ultrawhite safety glass; 72, the first EVA layer, 73, silicon crystal, the 74, second EVA layer, 75, TPT backboard.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
Refer to Fig. 1-2, a kind of technical scheme of this utility model offer: a kind of satellite solar panel, including alloy frame 1 and the frame heat-insulation layer 3 that is arranged on frame side, alloy limit 1, heat-insulation layer 2 bottom the installation of frame heat-insulation layer 3 side, bottom heat-insulation layer, arranging galvanized iron sheet 6 bottom 2, collection distributive pipe 4 is installed at bottom heat-insulation layer 2 top, and solar panel 7 is installed at collection distributive pipe 4 top；Catch net 5 is installed at solar panel 7 top, and solar panel 7 is internal arranges ultrawhite safety glass 71, arranges and arrange silicon crystal 73 bottom the first EVA layer 72, and the first EVA layer 72 bottom ultrawhite safety glass 71；Installation TPT backboard 75 bottom second EVA layer 74, and the second EVA layer 74 is set bottom silicon crystal 73.
Seamless between ultrawhite safety glass 71 with the first EVA layer 72 contact；It is in close contact between silicon crystal 73 and the second EVA layer 74；Between catch net 5 with alloy frame 1, bolt is connected；It is electrically connected with between several solar panels 7.
This utility model is in use; first solar panel 7 is arranged on alloy frame 1 internal; by bolt, catch net 5 is arranged on alloy frame 1 side; the catch net 5 being arranged on solar panel 7 top can be effectively protected solar panel 7, stops the space trash destruction to solar panel 7.Meanwhile, bottom heat-insulation layer 2 and frame heat-insulation layer 3, can effectively prevent that solar panel 7 temperature difference is excessive causes solar panel 7 to lose efficacy.
Embodiment the most of the present utility model, for the ordinary skill in the art, being appreciated that in the case of without departing from principle of the present utility model and spirit and these embodiments can carry out multiple change, revise, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a satellite solar panel, including alloy frame (1) and the frame heat-insulation layer (3) that is arranged on described alloy frame (1) side, it is characterized in that: heat-insulation layer (2) bottom the installation of described frame heat-insulation layer (3) side, bottom, described bottom heat-insulation layer (2) arranges galvanized iron sheet (6), collection distributive pipe (4) is installed at heat-insulation layer (2) top, described bottom, and solar panel (7) is installed at described collection distributive pipe (4) top；Catch net (5) is installed at described solar panel (7) top; described solar panel (7) is internal arranges ultrawhite safety glass (71); described ultrawhite safety glass (71) bottom arranges the first EVA layer (72), and described first EVA layer (72) bottom arranges silicon crystal (73)；Described silicon crystal (73) bottom arranges the second EVA layer (74), and TPT backboard (75) is installed in described second EVA layer (74) bottom.
A kind of satellite solar panel the most according to claim 1, it is characterised in that: seamless between described ultrawhite safety glass (71) with described first EVA layer (72) contact.
A kind of satellite solar panel the most according to claim 1, it is characterised in that: it is in close contact between described silicon crystal (73) and described second EVA layer (74).
A kind of satellite solar panel the most according to claim 1, it is characterised in that: between described catch net (5) with described alloy frame (1), bolt is connected.
A kind of satellite solar panel the most according to claim 1, it is characterised in that: it is electrically connected with between several described solar panels (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620350712.0U CN205564780U (en) | 2016-04-25 | 2016-04-25 | Solar cell panel for satellite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620350712.0U CN205564780U (en) | 2016-04-25 | 2016-04-25 | Solar cell panel for satellite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205564780U true CN205564780U (en) | 2016-09-07 |
Family
ID=56807331
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620350712.0U Expired - Fee Related CN205564780U (en) | 2016-04-25 | 2016-04-25 | Solar cell panel for satellite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205564780U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116639266A (en) * | 2023-07-27 | 2023-08-25 | 航天恒星科技有限公司 | Multifunctional satellite configuration |
-
2016
- 2016-04-25 CN CN201620350712.0U patent/CN205564780U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116639266A (en) * | 2023-07-27 | 2023-08-25 | 航天恒星科技有限公司 | Multifunctional satellite configuration |
| CN116639266B (en) * | 2023-07-27 | 2023-10-13 | 航天恒星科技有限公司 | Multifunctional satellite configuration |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Kang Renlu Inventor after: Li Yuhua Inventor before: Lan Canyu |
|
| CB03 | Change of inventor or designer information | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170525 Address after: Shangyou Industrial Park North Huang Town 341200 Jiangxi city of Ganzhou province Shangyou County Patentee after: JIANGXI OURSUN NEW ENERGY CO.,LTD. Address before: 510000 unit 2414-2416, building, No. five, No. 371, Tianhe District, Guangdong, China Patentee before: GUANGDONG GAOHANG INTELLECTUAL PROPERTY OPERATION Co.,Ltd. Effective date of registration: 20170525 Address after: 510000 unit 2414-2416, building, No. five, No. 371, Tianhe District, Guangdong, China Patentee after: GUANGDONG GAOHANG INTELLECTUAL PROPERTY OPERATION Co.,Ltd. Address before: Longyan City, Fujian Province, south of the 364299 village of Shanghang County in the camp 2 Road flat grocery store Patentee before: Lan Canyu |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160907 Termination date: 20190425 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |