CN110501015A - A kind of sun sensor insulating mounting method applied to moonlet - Google Patents
A kind of sun sensor insulating mounting method applied to moonlet Download PDFInfo
- Publication number
- CN110501015A CN110501015A CN201910595813.2A CN201910595813A CN110501015A CN 110501015 A CN110501015 A CN 110501015A CN 201910595813 A CN201910595813 A CN 201910595813A CN 110501015 A CN110501015 A CN 110501015A
- Authority
- CN
- China
- Prior art keywords
- sun sensor
- moonlet
- sun
- insulating mounting
- solar battery
- 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.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 25
- 239000000758 substrate Substances 0.000 claims abstract description 13
- 239000004642 Polyimide Substances 0.000 claims abstract description 10
- 229920001721 polyimide Polymers 0.000 claims abstract description 10
- 238000009413 insulation Methods 0.000 claims abstract description 7
- 150000003949 imides Chemical class 0.000 claims abstract description 4
- 239000012528 membrane Substances 0.000 claims abstract description 4
- 238000009434 installation Methods 0.000 abstract description 9
- 229920003223 poly(pyromellitimide-1,4-diphenyl ether) Polymers 0.000 description 4
- 239000000463 material Substances 0.000 description 2
- 230000008447 perception Effects 0.000 description 2
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/24—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for cosmonautical navigation
-
- 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
-
- 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
Abstract
The invention discloses a kind of sun sensors applied to moonlet to be insulated method, directly sun sensor is installed on solar battery array substrate using polyimides screw, add a strata imide membrane between sun sensor and windsurfing, to realize the insulating mounting of sun sensor.Such insulating mounting method eliminates the components such as the mounting bracket of traditional sun sensor, insulating bushing, and installation method is simple and reliable, and insulation effect is good, is a kind of sun sensor insulating mounting method suitable for moonlet.
Description
Technical field
The present invention relates to spacecraft structure installation method, specially a kind of sun sensor applied to moonlet, which insulate, pacifies
Dress method.
Background technique
Sun sensor is significant components on satellite, is the fixed to day of solar battery array by the perception to sun light intensity
Corner information is provided to driving.Due to the important function and its electrically susceptible perception of sun sensor, need to use during installation and base
The installation method of plate opposing insulation.
Traditional installation method is the preset embedded part inside sun battle array substrate, and in the side of the cementing insulating bushing in embedded part edge
Method realizes the insulation of sun sensor fastener and substrate, and finally realizes the insulating mounting of sun sensor and substrate.The party
Method has complex procedures, insulating bushing cracky, and potential conducting risk is larger, and after failure of insulation, and maintenance cost is larger etc.
Disadvantage, and process is cumbersome when actually carrying out installation operation.For moonlet field, due to the limit of cost and lead time
The insulating mounting method of system, simple and reliable low cost has bigger application prospect.
Summary of the invention
For the demand, the present invention devises a kind of sun sensor insulating mounting method applied to moonlet, should
Installation method replaces the cooperation of traditional polyimides bushing and hole, is directly installed sun sensor using polyimides screw
In on solar battery array substrate, using the insulation performance of polyimide material itself, the insulation of sun sensor installation foot is realized.
Meanwhile Kapton is pasted between sun sensor and solar battery array substrate, by two measures, realize that the sun is sensitive
The insulating mounting of device.
Due to the technical solution more than using, so that the present invention has the advantage that
1. reducing the quantity and kind of the components (such as screw, insulating bushing, sun sensor bracket) of insulating mounting
Class is installed simple and reliable；
2. polyimides screw is at low cost, and there are enough stiffness and strength, reliably connecting for sun sensor can guarantee
It connects, is especially suitable for the use in moonlet field；
3. for the relatively conventional stainless steel of polyimide material and Titanium Alloy Screw, the advantage for having density low weight light,
The requirement of moonlet weight harshness can be met very well.
Detailed description of the invention
Fig. 1 is the sun sensor insulating mounting method schematic diagram applied to moonlet.
Specific implementation method
The present invention is described in detail combined with specific embodiments below.
The embodiment of the invention provides a kind of sun sensors applied to moonlet to be insulated method, and feature exists
In directly sun sensor 2 being installed on solar battery array substrate 1, and in sun sensor using polyimides screw 3
Add a strata imide membrane 4 between windsurfing, Kapton 4 is laid on 2 bottom of sun sensor, to realize the sun
The insulating mounting of sensor 2 and solar battery array substrate 1.
When this specific implementation is used, as shown in Fig. 1, include the following steps:
Step 1: first clearing up corresponding site on solar battery array substrate 1, reserves suitable space and carry out the sun
The installation of sensor 2；
Step 2: the Kapton 4 of suitable dimension is pasted on solar battery array substrate 1；
Step 3: sun sensor 2 is placed on Kapton 4, it is corresponding that hole location alignment is installed；
Step 4: sun sensor 2 is tightened fixation by polyimides screw 3, and realized by torque spanner method
Polyimides screw carries out screw-down torque monitoring, the final insulating mounting for realizing sun sensor 2.
Specific embodiments of the present invention are described above.It is to be appreciated that the invention is not limited to above-mentioned
Particular implementation method, those skilled in the art can make various deformations or amendments within the scope of the claims, this not shadow
Ring substantive content of the invention.
Claims (2)
1. a kind of sun sensor applied to moonlet is insulated method, which is characterized in that use polyimides screw
(3), directly sun sensor (2) is installed on solar battery array substrate (1), and adds one between sun sensor and windsurfing
Strata imide membrane (4), to realize the insulating mounting of sun sensor (2) Yu solar battery array substrate (1).
2. the sun sensor of moonlet as described in claim 1 is insulated method, which is characterized in that in sun sensor
(2) bottom spreads the insulation of a strata imide membrane (5) realization and solar battery array substrate (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910595813.2A CN110501015A (en) | 2019-07-03 | 2019-07-03 | A kind of sun sensor insulating mounting method applied to moonlet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910595813.2A CN110501015A (en) | 2019-07-03 | 2019-07-03 | A kind of sun sensor insulating mounting method applied to moonlet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110501015A true CN110501015A (en) | 2019-11-26 |
Family
ID=68585546
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910595813.2A Pending CN110501015A (en) | 2019-07-03 | 2019-07-03 | A kind of sun sensor insulating mounting method applied to moonlet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110501015A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000128092A (en) * | 1998-10-20 | 2000-05-09 | Mitsubishi Electric Corp | Sandwich structure for outer space cruiser |
| US6318673B1 (en) * | 1999-01-29 | 2001-11-20 | Dornier Gmbh | Structure for the thermal insulation of satellites |
| CN203133190U (en) * | 2012-12-24 | 2013-08-14 | 中国电子科技集团公司第十八研究所 | Thermoelectric refrigeration assembly aging screening automatic testing device |
| CN103616619A (en) * | 2013-11-19 | 2014-03-05 | 北京卫星环境工程研究所 | Polyimide film insulation inspection tool on SADA support |
| CN104833334A (en) * | 2015-04-16 | 2015-08-12 | 上海空间电源研究所 | Analog solar sensor |
-
2019
- 2019-07-03 CN CN201910595813.2A patent/CN110501015A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2000128092A (en) * | 1998-10-20 | 2000-05-09 | Mitsubishi Electric Corp | Sandwich structure for outer space cruiser |
| US6318673B1 (en) * | 1999-01-29 | 2001-11-20 | Dornier Gmbh | Structure for the thermal insulation of satellites |
| CN203133190U (en) * | 2012-12-24 | 2013-08-14 | 中国电子科技集团公司第十八研究所 | Thermoelectric refrigeration assembly aging screening automatic testing device |
| CN103616619A (en) * | 2013-11-19 | 2014-03-05 | 北京卫星环境工程研究所 | Polyimide film insulation inspection tool on SADA support |
| CN104833334A (en) * | 2015-04-16 | 2015-08-12 | 上海空间电源研究所 | Analog solar sensor |
Non-Patent Citations (4)
| Title |
|---|
| 于登云，等: "《航天器机构技术》", 31 January 2011, 北京：中国科学技术出版社 * |
| 吴迪，等: "基于SiP技术的单片集成数字式太阳敏感器", 《深空探测学报》 * |
| 李国欣: "《航天器电源系统技术概论 下》", 30 September 2008, 北京：中国宇航出版社 * |
| 雷营生，等: "固定工艺对多层隔热组件隔热性能的影响", 《低温工程》 * |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| SE9900103D0 (en) | Electric connection of electrochemical and photoelectrochemical cells | |
| US20050034754A1 (en) | Photovoltaic insulating glazing | |
| CN110501015A (en) | A kind of sun sensor insulating mounting method applied to moonlet | |
| CN109273660B (en) | Power battery top cover assembly, power battery and battery module | |
| WO2005004242A3 (en) | Solar cell with an electrically insulating layer under the busbar | |
| CN103440992A (en) | Aluminum electrolytic capacitor cover plate | |
| CN204333311U (en) | A kind of novel vertical connects tee connector | |
| CN201846282U (en) | Grounded system of roof photovoltaic power generation system | |
| CN215186558U (en) | Photovoltaic power generation product installation device | |
| CN203984334U (en) | Solar module ground structure | |
| CN211904436U (en) | Steam boiler surface heat detection device | |
| JP2004324233A (en) | Method of mounting solar battery module | |
| CN207399086U (en) | A kind of solar components crimp of function with ground | |
| CN207896624U (en) | A kind of cable bearer of factories and miness cable shaft | |
| CN217998647U (en) | Downpipe fixing device | |
| CN212078495U (en) | Heat-insulating decorative board with anchoring device | |
| JP2009010262A (en) | Thin film solar cell module and its manufacturing method | |
| CN205883128U (en) | Solar panel's side pressure fixing device | |
| CN105609579A (en) | Solar photovoltaic composite plate | |
| CN213772219U (en) | Resistance type sacrificial anode for yacht | |
| CN207122059U (en) | A kind of roof clamping device | |
| CN204424479U (en) | One is vertical connects tee connector | |
| CN219298642U (en) | Integrated rock board heat preservation device | |
| CN220873730U (en) | Outdoor energy storage battery heat insulation top plate and battery cabinet provided with same | |
| CN217930589U (en) | Novel intelligent thermocouple |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20191126 |
|
| RJ01 | Rejection of invention patent application after publication |