CN112542526A - Solar cell array combination device for aerostat and installation method - Google Patents
Solar cell array combination device for aerostat and installation method Download PDFInfo
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- CN112542526A CN112542526A CN202011434493.1A CN202011434493A CN112542526A CN 112542526 A CN112542526 A CN 112542526A CN 202011434493 A CN202011434493 A CN 202011434493A CN 112542526 A CN112542526 A CN 112542526A
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- aerostat
- bottom plate
- fixing piece
- plate fixing
- battery
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- 238000009434 installation Methods 0.000 title claims abstract description 9
- 238000000034 method Methods 0.000 title claims abstract description 9
- 239000002775 capsule Substances 0.000 claims abstract description 32
- 238000009413 insulation Methods 0.000 claims abstract description 28
- 239000004744 fabric Substances 0.000 claims description 7
- 238000007789 sealing Methods 0.000 claims description 6
- 239000000853 adhesive Substances 0.000 claims description 4
- 230000001070 adhesive effect Effects 0.000 claims description 4
- 239000000835 fiber Substances 0.000 claims description 4
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004593 Epoxy Substances 0.000 claims description 3
- 239000004698 Polyethylene Substances 0.000 claims description 3
- 229920005830 Polyurethane Foam Polymers 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 229920001971 elastomer Polymers 0.000 claims description 3
- 239000006260 foam Substances 0.000 claims description 3
- 239000003365 glass fiber Substances 0.000 claims description 3
- 229910001095 light aluminium alloy Inorganic materials 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- -1 polyethylene Polymers 0.000 claims description 3
- 229920000573 polyethylene Polymers 0.000 claims description 3
- 239000011496 polyurethane foam Substances 0.000 claims description 3
- 239000011347 resin Substances 0.000 claims description 3
- 229920005989 resin Polymers 0.000 claims description 3
- 239000002131 composite material Substances 0.000 claims description 2
- 230000002035 prolonged effect Effects 0.000 abstract description 3
- 230000003139 buffering effect Effects 0.000 abstract 1
- 239000000463 material Substances 0.000 description 7
- 239000004677 Nylon Substances 0.000 description 3
- 238000004146 energy storage Methods 0.000 description 3
- 229920001778 nylon Polymers 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009941 weaving Methods 0.000 description 2
- 229910001218 Gallium arsenide Inorganic materials 0.000 description 1
- 229910021417 amorphous silicon Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910021421 monocrystalline silicon Inorganic materials 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000002194 synthesizing effect Effects 0.000 description 1
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/042—PV modules or arrays of single PV cells
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/042—PV modules or arrays of single PV cells
- H01L31/048—Encapsulation of modules
-
- 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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- Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Power Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention discloses a solar cell array combination device for an aerostat and an installation method thereof, wherein the solar cell array combination device comprises a plurality of binding belts and a cell sub-array which are fixed on an aerostat capsule body, wherein the cell sub-array is connected and fixed on the aerostat capsule body through the binding belts; the battery subarray comprises a bottom plate fixing piece, a battery piece group and a heat insulation block, wherein the periphery of the bottom plate fixing piece is connected with a binding belt, a plurality of battery piece groups are fixed on the upper surface of the bottom plate fixing piece, a plurality of heat insulation blocks are fixed on the lower surface of the bottom plate fixing piece, and the bottom surface of each heat insulation block is attached to the pocket body of the aerostat. The battery array combination device has the advantages that the battery array combination device can protect the battery piece set from being damaged by strain caused by the shaking of the air floater capsule body, and the service life of the battery piece set is prolonged; the potential safety hazard caused by the reduction of the mechanical property of the aerostat capsule body can be prevented; meanwhile, the heat insulation blocks also protect the bag body of the aerostat from being abraded by the bottom plate fixing piece, so that the aerostat has a certain buffering effect and improves the safety factor of the aerostat.
Description
Technical Field
The invention relates to the technical field of aerostat manufacturing, in particular to a solar cell array combination device for an aerostat and an installation method.
Background
The ultra-high altitude large aerostat cannot be controlled by a mooring method, needs to be provided with better energy and power systems, and ensures long-endurance operation in a parking stage, and the energy system adopts a circulating power supply mode of a solar battery array and an energy storage battery to be the best scheme under the condition: when the aerostat flies in the sky in the daytime, the solar cell array provides power energy and charges the energy storage battery at the same time; the energy storage battery provides power at night.
Because the aerostatics utricule is flexible structure, solar cell has great degree of difficulty in laying on its surface. Although the flexible amorphous silicon solar cell can meet the laying requirement, the efficiency of the cell is low, the energy requirement of the aerostat cannot be met, and the cost of the flexible gallium arsenide cell is high. Therefore, monocrystalline silicon batteries are mainly adopted for laying, and the cost is acceptable and the efficiency is higher. For example, chinese utility model patent publication No. CN209258366U discloses a quick laying device of aerostat solar cell, including be fixed in the turn-ups on the aerostat covering and with solar cell with the zip fastener that the turn-ups is connected. The zipper is respectively connected to the flanging on the aerostat skin and the side edge of the solar cell packaged in a modularized mode in advance, so that the solar panel can be laid quickly. However, the solar cell itself is fragile and easily damaged, and therefore cannot be directly laid on the surface of the aerostat capsule. In addition, the temperature of the solar cell is high in the daytime, if the solar cell is directly contacted with the surface of the capsule body, the surface temperature of the capsule body material is possibly too high, various mechanical properties of the capsule body material are seriously reduced under the high-temperature condition, and the mechanical properties of the capsule body material are lower than the index requirements of the capsule body material, so that potential safety hazards are caused.
Disclosure of Invention
The invention aims to solve the technical problem of how to prevent the solar cell from being damaged and improve the safety coefficient of the aerostat.
In order to solve the technical problems, the invention provides the following technical scheme:
a solar cell array combination device for an aerostat comprises a plurality of binding belts and a cell sub-array which are fixed on an aerostat bag body, wherein the cell sub-array is connected and fixed on the aerostat bag body through the binding belts;
the battery subarray comprises a bottom plate fixing piece, a battery piece group and a heat insulation block, wherein the periphery of the bottom plate fixing piece is connected with a binding belt, a plurality of battery piece groups are fixed on the upper surface of the bottom plate fixing piece, a plurality of heat insulation blocks are fixed on the lower surface of the bottom plate fixing piece, and the bottom surface of each heat insulation block is attached to the pocket body of the aerostat.
Preferably, a plurality of first connecting holes are formed in the binding belt side by side, second connecting holes corresponding to the positions and the number of the first connecting holes are formed in the periphery of the bottom plate fixing piece, and the bottom plate fixing piece sequentially penetrates through the first connecting holes and the second connecting holes through binding ropes to be connected with the binding belt.
Preferably, the binding band is integrated with the aerostat capsule in a high-frequency heat sealing mode.
Preferably, a plurality of lugs are arranged on the periphery of the battery piece group, and the lugs are fixed on the bottom plate fixing piece through screws.
Preferably, the heat insulation blocks are uniformly arranged at intervals and fixed on the lower surface of the bottom plate fixing piece.
Preferably, the bottom plate fixing piece is epoxy glass fiber cloth, carbon fiber resin cloth or a light aluminum alloy plate.
Preferably, the material of the heat insulation block is polyurethane foam, polyethylene foam sponge or aviation sponge rubber.
Preferably, the edge of the bottom surface of the bottom plate fixing piece and the aerostat bag body are sealed through an adhesive buckle belt.
Preferably, the aerostat fixing piece further comprises a hanging strip, wherein the hanging strip is made of a strong fiber rope through weaving, one end of the hanging strip is fixed on the aerostat base, and the other end of the hanging strip is attached to the aerostat bag body in a high-frequency heat sealing mode or a bonding mode and is connected with the bottom plate fixing piece.
Preferably, the invention also provides an installation method of the solar cell array combination device for the aerostat, which comprises the following steps:
step 1: fixing a plurality of binding belts on the aerostat capsule body according to the designed positions;
step 2: fixing the battery piece group on the upper surface of the bottom plate fixing piece, and fixing the heat insulation block on the lower surface of the bottom plate fixing piece to form a battery subarray;
and step 3: and connecting the periphery of a bottom plate fixing piece in the battery subarray with the binding belt to complete the installation of the battery subarray on the aerostat capsule.
Compared with the prior art, the invention has the beneficial effects that:
1. by fixing the cell group and the bottom plate fixing piece, the cell group can be protected from strain damage caused by the shaking of the aerostat capsule, and the service life of the cell group is prolonged; meanwhile, the thermal insulation block is used for preventing the direct contact between the battery subarray and the aerostat capsule, so that the situation that the temperature of the aerostat capsule is increased due to overhigh temperature of the solar battery during working in the daytime, and the potential safety hazard is caused due to the fact that the mechanical property of the aerostat capsule is reduced is prevented; meanwhile, the heat insulation block also protects the bag body of the aerostat from being abraded by the bottom plate fixing piece, and vibration caused by strong wind or movement is reduced in the buffer of the heat insulation block when the aerostat is high in altitude, so that the aerostat has a certain buffer effect, and the safety coefficient of the aerostat is improved.
2. Through the ligature rope with the bottom plate stationary blade with the ligature area be connected, this kind of connected mode not only intensity is high, the good reliability, and the probability of damage aerostatics utricule 3 is little, improves aerostatics factor of safety.
3. Through the setting of bonding hasp area and suspender, all be in order to improve the stability of bottom plate stationary blade, and then improve the stability of this battery battle array composite set.
Drawings
Fig. 1 is a schematic structural diagram of a solar cell array assembly for an aerostat according to an embodiment of the present invention;
FIG. 2 is a cross-sectional view A-A of FIG. 1;
FIG. 3 is a partial schematic view of an embodiment of the present invention;
FIG. 4 is a schematic structural diagram of a battery sub-array according to an embodiment of the present invention;
fig. 5 is a rear view of a battery sub-array in accordance with an embodiment of the present invention.
Detailed Description
In order to facilitate the understanding of the technical solutions of the present invention for those skilled in the art, the technical solutions of the present invention will be further described with reference to the drawings attached to the specification.
In this application, unless expressly stated or limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can include, for example, fixed connections, removable connections, or integral parts; the connection can be mechanical connection, electrical connection or communication; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present application can be understood by those of ordinary skill in the art as appropriate.
The terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present application, "a plurality" means two or more unless specifically limited otherwise.
Referring to fig. 1 to 5, the embodiment discloses a solar cell array combination device for an aerostat, which comprises a plurality of binding bands 1 fixed on an aerostat capsule 3 and a cell sub-array 2, wherein the cell sub-array 2 is fixed on the aerostat capsule 3 by being connected with the binding bands 2.
In the embodiment, the binding belt 1 is made of a main airbag heat seal cloth material, and the binding belt 1 and the aerostat airbag 3 are thermally integrated into a whole in a high-frequency heat seal mode; a plurality of first connecting holes 11 are opened side by side in the bandage 1, the hole interval of first connecting hole 11 is not more than 10 cm.
The battery subarray 2 comprises a bottom plate fixing sheet 21, a battery sheet group 22 and a heat insulation block 23, wherein in the embodiment, the bottom plate fixing sheet 21 is made of epoxy glass fiber cloth, carbon fiber resin cloth or a light aluminum alloy plate. The second connecting hole 211 that corresponds with 11 positions in first connecting hole and quantity is seted up to bottom plate stationary blade 21 periphery, bottom plate stationary blade 21 through the ligature rope 4 run through first connecting hole 11 and second connecting hole 211 in proper order with ligature area 1 is connected, this kind of connected mode not only intensity is high, the good reliability, and the probability that damages aerostatics utricule 3 is little, improves aerostatics factor of safety.
Further, the binding rope 4 is a woven fiber rope with a protective sleeve.
The periphery of the battery pack 22 is provided with a plurality of lugs 221, the lugs 221 are fixed on the bottom plate fixing piece 21 through screws, so that the battery pack 22 and the bottom plate fixing piece 21 are fixed, the battery pack 22 can be protected from strain damage caused by shaking of the aerostat capsule 3, and the service life of the battery pack 22 is prolonged.
The heat insulation blocks 23 are uniformly arranged and fixed on the lower surface of the bottom plate fixing piece 21 at intervals, the bottom surface of the heat insulation block 23 is attached to the aerostat bag body 3, and blank positions are reserved in the range of 10cm from the peripheral edge of the lower surface of the bottom plate fixing piece 21; in the embodiment, the material of the heat insulation block 23 is polyurethane foam, polyethylene foam sponge or aviation sponge rubber, and the size of the heat insulation block is 40mm × 20mm × 20 mm; specifically, the thermal insulation blocks 23 are used for preventing the direct contact between the battery subarray 2 and the aerostat capsule 3, so that potential safety hazards caused by the fact that the aerostat capsule 3 is lowered in mechanical property due to the fact that the aerostat capsule 3 is raised in temperature when the solar battery works in the daytime are prevented; meanwhile, the heat insulation block 23 also protects the aerostat capsule 3 from being abraded by the bottom plate fixing piece 21, and vibration caused by strong wind or movement at high altitude is reduced in the buffer of the heat insulation block 23, so that a certain buffer effect is achieved, and the safety coefficient of the aerostat is improved.
Furthermore, the blank position left in the range of 10cm from the peripheral edge of the lower surface of the bottom plate fixing piece 21 and the aerostat bag body 3 are sealed by an adhesive fastener tape (not shown), so that the stability of the bottom plate fixing piece 21 is further improved, and the stability of the battery array combination device is further improved.
Furthermore, the bonding buckle belt is a nylon buckle belt with double-sided adhesive, one surface of the nylon buckle belt is bonded on the aerostat capsule body 3, and the other surface of the nylon buckle belt is bonded on the edge of the bottom plate fixing piece 21.
Further, the battery array combination device further comprises a hanging strip (not shown in the figure), wherein the hanging strip is made by weaving a strong fiber rope, one end of the hanging strip is fixed on the aerostat base, and the other end of the hanging strip is attached to the aerostat capsule body 3 in a high-frequency heat sealing mode or a bonding mode and is connected with the bottom plate fixing piece 21, so that the stability of the bottom plate fixing piece 21 is improved, and the stability of the battery array combination device is improved.
The embodiment also discloses an installation method of the solar cell array combination device for the aerostat, which comprises the following steps:
step 1: and (3) thermally synthesizing a plurality of binding belts 1 and the aerostat airbag body 3 into a whole and fixing the same on the aerostat airbag body 3 in a high-frequency heat seal mode according to the designed positions.
Step 2: the lug 221 is fixed on the upper surface of the bottom plate fixing piece 21 through screws, so that the battery piece group 22 and the bottom plate fixing piece 21 are fixed, and meanwhile, the heat insulation blocks 23 are uniformly arranged and fixed on the lower surface of the bottom plate fixing piece 21 at intervals, and finally, the battery subarray 2 is formed.
And step 3: run through first connecting hole 11 and second connecting hole 211 in proper order through ligature rope 4 will bottom plate stationary blade 21 with ligature area 1 is connected, and simultaneously, the thermal-insulated piece 23 bottom surface is the laminating on aerostatics utricule 3, accomplishes the fixed connection of battery subarray 2 and aerostatics utricule 3 at last.
And 4, step 4: and the bonding buckle belt is used for sealing the space between the blank position reserved in the range of 10cm on the peripheral edge of the lower surface of the bottom plate fixing piece 21 and the aerostat capsule body 3, one end of the hanging strip is fixed on the aerostat base, the other end of the hanging strip is attached to the aerostat capsule body 3 in a high-frequency heat sealing mode or bonding mode and is connected with the bottom plate fixing piece 21, and finally, the installation of the battery array combination device on the aerostat capsule body 3 is completed.
It should be noted here that step 1 and step 2 can be performed simultaneously.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein, and any reference signs in the claims are not intended to be construed as limiting the claim concerned.
The above-mentioned embodiments only represent embodiments of the present invention, and the protection scope of the present invention is not limited to the above-mentioned embodiments, and it will be apparent to those skilled in the art that several variations and modifications can be made without departing from the concept of the present invention, and these embodiments are all within the protection scope of the present invention.
Claims (10)
1. The utility model provides a solar cell battle array composite set for aerostatics which characterized in that: the battery subarray is connected with the binding belts and fixed on the aerostat capsule;
the battery subarray comprises a bottom plate fixing piece, a battery piece group and a heat insulation block, wherein the periphery of the bottom plate fixing piece is connected with a binding belt, a plurality of battery piece groups are fixed on the upper surface of the bottom plate fixing piece, a plurality of heat insulation blocks are fixed on the lower surface of the bottom plate fixing piece, and the bottom surface of each heat insulation block is attached to the pocket body of the aerostat.
2. The solar cell array assembly of claim 1, wherein: a plurality of first connecting holes have been seted up side by side to the ligature area, the second connecting hole that corresponds with first connecting hole position and quantity is seted up to bottom plate stationary blade periphery, the bottom plate stationary blade pass through first connecting hole and second connecting hole in proper order through the ligature rope with the ligature area is connected.
3. The solar cell array assembly of claim 1, wherein: the binding belt is integrated with the aerostat airbag in a high-frequency heat seal mode.
4. The solar cell array assembly of claim 1, wherein: the battery piece group is provided with a plurality of lugs at the periphery, and the lugs are fixed on the bottom plate fixing piece through screws.
5. The solar cell array assembly of claim 1, wherein: the heat insulation blocks are uniformly arranged at intervals and fixed on the lower surface of the bottom plate fixing piece.
6. The solar cell array assembly of claim 1, wherein: the bottom plate fixing piece is made of epoxy glass fiber cloth, carbon fiber resin cloth or a light aluminum alloy plate.
7. The solar cell array assembly of claim 1, wherein: the heat insulation block is made of polyurethane foam, polyethylene foam sponge or aviation sponge rubber.
8. The solar cell array assembly of claim 1, wherein: and the edge of the bottom surface of the bottom plate fixing piece and the aerostat bag body are sealed through the adhesive fastener belt.
9. The solar cell array assembly of claim 1, wherein: the hanging strip is woven by a strong fiber rope, one end of the hanging strip is fixed on the aerostat base, and the other end of the hanging strip is attached to the aerostat bag body in a high-frequency heat sealing mode or a bonding mode and is connected with the bottom plate fixing piece.
10. The method for mounting a solar cell array assembly for an aerostat according to any one of claims 1 to 9, wherein: the method comprises the following steps:
step 1: fixing a plurality of binding belts on the aerostat capsule body according to the designed positions;
step 2: fixing the battery piece group on the upper surface of the bottom plate fixing piece, and fixing the heat insulation block on the lower surface of the bottom plate fixing piece to form a battery subarray;
and step 3: and connecting the periphery of a bottom plate fixing piece in the battery subarray with the binding belt to complete the installation of the battery subarray on the aerostat capsule.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011434493.1A CN112542526A (en) | 2020-12-10 | 2020-12-10 | Solar cell array combination device for aerostat and installation method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011434493.1A CN112542526A (en) | 2020-12-10 | 2020-12-10 | Solar cell array combination device for aerostat and installation method |
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| Publication Number | Publication Date |
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| CN112542526A true CN112542526A (en) | 2021-03-23 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202011434493.1A Pending CN112542526A (en) | 2020-12-10 | 2020-12-10 | Solar cell array combination device for aerostat and installation method |
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201188929Y (en) * | 2008-05-13 | 2009-02-04 | 东南大学 | Belt shaped binding fastening |
| CN102897330A (en) * | 2012-10-22 | 2013-01-30 | 湖南航天机电设备与特种材料研究所 | Method for reliably connecting flexible thin-film solar cell and airship envelop |
| CN103280472A (en) * | 2013-05-28 | 2013-09-04 | 北京航空航天大学 | Flexible netlike solar battery array for stratospheric aerostat |
| CN205203335U (en) * | 2015-12-17 | 2016-05-04 | 东莞前沿技术研究院 | A fixed connector and aerostatics for aerostatics |
| CN106129156A (en) * | 2016-02-29 | 2016-11-16 | 上海交通大学 | Flexible floating pocket is laid the method and device of monocrystaline silicon solar cell |
| CN208922739U (en) * | 2018-10-29 | 2019-05-31 | 李昊天 | A kind of shockproof heat radiation protection device of hard disc of computer |
| CN209258366U (en) * | 2018-12-08 | 2019-08-16 | 丹阳昊天飞行器技术有限公司 | A kind of quick laying apparatus of aerostatics solar battery |
| CN111284674A (en) * | 2018-12-08 | 2020-06-16 | 丹阳昊天飞行器技术有限公司 | Quick laying device of aerostatics solar cell |
-
2020
- 2020-12-10 CN CN202011434493.1A patent/CN112542526A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201188929Y (en) * | 2008-05-13 | 2009-02-04 | 东南大学 | Belt shaped binding fastening |
| CN102897330A (en) * | 2012-10-22 | 2013-01-30 | 湖南航天机电设备与特种材料研究所 | Method for reliably connecting flexible thin-film solar cell and airship envelop |
| CN103280472A (en) * | 2013-05-28 | 2013-09-04 | 北京航空航天大学 | Flexible netlike solar battery array for stratospheric aerostat |
| CN205203335U (en) * | 2015-12-17 | 2016-05-04 | 东莞前沿技术研究院 | A fixed connector and aerostatics for aerostatics |
| CN106129156A (en) * | 2016-02-29 | 2016-11-16 | 上海交通大学 | Flexible floating pocket is laid the method and device of monocrystaline silicon solar cell |
| CN208922739U (en) * | 2018-10-29 | 2019-05-31 | 李昊天 | A kind of shockproof heat radiation protection device of hard disc of computer |
| CN209258366U (en) * | 2018-12-08 | 2019-08-16 | 丹阳昊天飞行器技术有限公司 | A kind of quick laying apparatus of aerostatics solar battery |
| CN111284674A (en) * | 2018-12-08 | 2020-06-16 | 丹阳昊天飞行器技术有限公司 | Quick laying device of aerostatics solar cell |
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