CN114858689B - A space comprehensive environment in-situ and semi-situ testing shielding device and its testing shielding method - Google Patents
A space comprehensive environment in-situ and semi-situ testing shielding device and its testing shielding method Download PDFInfo
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- CN114858689B CN114858689B CN202210275812.1A CN202210275812A CN114858689B CN 114858689 B CN114858689 B CN 114858689B CN 202210275812 A CN202210275812 A CN 202210275812A CN 114858689 B CN114858689 B CN 114858689B
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- 238000012360 testing method Methods 0.000 title claims abstract description 200
- 238000011065 in-situ storage Methods 0.000 title claims abstract description 122
- 238000000034 method Methods 0.000 title claims abstract description 20
- 239000000523 sample Substances 0.000 claims abstract description 56
- 230000005855 radiation Effects 0.000 claims abstract description 27
- 239000002245 particle Substances 0.000 claims abstract description 19
- 238000004458 analytical method Methods 0.000 claims description 4
- 230000003287 optical effect Effects 0.000 claims description 4
- 238000001069 Raman spectroscopy Methods 0.000 claims description 3
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims description 3
- 239000011449 brick Substances 0.000 claims description 3
- 238000004891 communication Methods 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 claims description 3
- 238000011056 performance test Methods 0.000 claims description 3
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- 239000010959 steel Substances 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims 1
- 230000007613 environmental effect Effects 0.000 abstract description 4
- 238000004088 simulation Methods 0.000 abstract description 4
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- 238000005457 optimization Methods 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
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- G—PHYSICS
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- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N17/00—Investigating resistance of materials to the weather, to corrosion, or to light
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D21/00—Measuring or testing not otherwise provided for
- G01D21/02—Measuring two or more variables by means not covered by a single other subclass
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N17/00—Investigating resistance of materials to the weather, to corrosion, or to light
- G01N17/004—Investigating resistance of materials to the weather, to corrosion, or to light to light
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Abstract
本发明是一种空间综合环境原位和半原位测试屏蔽装置及其测试屏蔽方法。本发明涉及空间环境模拟与测试技术领域，所述装置包括：测试设备、驱动机构和远程控制系统，所述驱动机构上搭载测试设备，所述远程控制系统控制驱动机构；所述测试设备包括测试设备主机、测试设备探头和测试设备穿舱线缆，测试设备穿舱线缆连接测试设备主机和测试设备探头；测试设备主机位于综合舱容器内，测试设备主机外围设有辐射防护结构；本发明面向地面模拟的真空、高低温、太阳辐照、紫外辐照、带电粒子辐照等空间极端环境因素，可在试验中对样品进行原位、半原位测试。
The invention is a space comprehensive environment in-situ and semi-situ testing shielding device and a testing shielding method thereof. The invention relates to the technical field of space environment simulation and testing. The device includes: testing equipment, a driving mechanism and a remote control system. The driving mechanism is equipped with testing equipment, and the remote control system controls the driving mechanism; the testing equipment includes a testing device. The equipment host, the test equipment probe and the test equipment cabin cable, the test equipment cabin cable connects the test equipment host and the test equipment probe; the test equipment host is located in the integrated cabin container, and a radiation protection structure is provided around the test equipment host; the present invention For the extreme environmental factors in space such as vacuum, high and low temperatures, solar radiation, ultraviolet radiation, and charged particle radiation that are simulated on the ground, in-situ and semi-situ tests can be performed on samples during the test.
Description
Technical Field
The invention relates to the technical field of space environment simulation and test, in particular to a space comprehensive environment in-situ and semi-in-situ test shielding device and a test shielding method thereof.
Background
In order to timely and accurately grasp the evolution rule of the material, the device and the system component module in the extreme comprehensive environment such as vacuum, high and low temperature, irradiation (sun, ultraviolet, charged particles and the like), the test analysis can be carried out in a position, an environment state unchanged (in situ) and a position changeable (semi-in-situ) mode. Moreover, the test on the aspect is mainly remained in a laboratory state, and instruments and equipment work in a conventional environment and cannot meet the in-situ/semi-in-situ test requirement.
Disclosure of Invention
The invention is vacuum, high and low temperature, solar radiation, ultraviolet radiation, charged particle radiation and other space extreme environmental factors facing ground simulation, and can perform in-situ and semi-in-situ test on samples in the test, so the invention provides a space comprehensive environment in-situ and semi-in-situ test shielding device and a test shielding method thereof, and the invention provides the following technical scheme:
a spatially integrated environmental in-situ and semi-in-situ test shielding apparatus, the apparatus comprising: the test device comprises test equipment, a driving mechanism and a remote control system, wherein the test equipment is carried on the driving mechanism, and the remote control system controls the driving mechanism;
the test equipment comprises a test equipment host, a test equipment probe and a test equipment cabin penetrating cable, wherein the test equipment cabin penetrating cable is connected with the test equipment host and the test equipment probe; the testing equipment host is positioned in the comprehensive cabin container, and the periphery of the testing equipment host is provided with a radiation protection structure;
the driving mechanism comprises an in-situ test equipment driving mechanism and a semi-in-situ test equipment driving mechanism; the in-situ test equipment driving mechanism is integrated on the sample table, and the semi-in-situ test equipment driving mechanism is installed in the in-situ auxiliary cabin.
Preferably, the device further comprises a test equipment driving mechanism cabin penetrating cable, wherein the test equipment driving mechanism cabin penetrating cable comprises an in-situ test equipment driving mechanism cabin penetrating cable and a semi-in-situ test equipment driving mechanism cabin penetrating cable;
the driving mechanism and the remote control system are connected by an in-situ test equipment driving mechanism cabin penetrating cable and a semi-in-situ test equipment driving mechanism cabin penetrating cable for transmission communication.
Preferably, the test equipment probes include probes of in situ test equipment and probes of semi-in situ test equipment;
the in-situ test equipment is used for tolerating particle irradiation and comprises a discharge pulse tester, and an electrical property test is carried out in the irradiation process;
the probe of the semi-in-situ test equipment is used for intolerance or weak particle irradiation tolerance, including a Raman spectrometer, a fluorescence spectrometer and an optical performance tester, and needs to be tested in an irradiation intermittent stage.
Preferably, the radiation protection structure is provided with a radiation protection door for test and equipment maintenance personnel to enter and exit.
Preferably, the in-situ test equipment driving mechanism comprises a folding assembly, a Y-direction moving assembly and an X/Z-direction moving assembly, drives the in-situ test equipment probe to move in X, Y, Z directions, has multi-point test capability, and can be folded and folded after the test is finished.
Preferably, the driving mechanism of the semi-in-situ testing equipment comprises a primary extending component, a secondary extending component and a rotating component, wherein the primary extending component is a large-stroke rough adjusting mechanism, the secondary extending component is a short-stroke fine adjusting mechanism, the number of probes can be carried on the rotating component to be not less than 3, and when a specified performance test is carried out, the probes are rotated to positions corresponding to a sample testing surface.
Preferably, the radiation protection structure comprises a framework and a shielding layer, wherein the framework adopts a steel frame structure, and the shielding layer is built by adopting an aluminum plate and a lead brick.
A space comprehensive environment in-situ and semi-in-situ test shielding method comprises the following steps:
step 1: clamping a sample to be tested on a sample table, mounting an in-situ test equipment probe on an in-situ test equipment driving mechanism, and mounting a semi-in-situ test equipment probe on a semi-in-situ test equipment driving mechanism;
step 2: a tester enters the radiation protection structure to start a test equipment host and set parameters so that the tester can acquire signals through a test equipment cabin penetrating cable; after preparation is completed, closing the cabin door to start a test;
step 3: after the test is finished, the tester enters the radiation protection structure again, and test data are exported through the test equipment host machine for subsequent processing and analysis.
Preferably, during the test, the particle irradiation dose rate in the in situ secondary chamber is typically much lower than that of the primary chamber and the temperature is near room temperature.
Preferably, the in-situ test works stably in vacuum 10-3Pa magnitude, high and low temperature 100K-473K, solar irradiation 0.5-2 solar constants, ultraviolet irradiation 0-3.5 vacuum ultraviolet constants and charged particle irradiation environment 1.2MeV electron irradiation sources.
The invention has the following beneficial effects:
the in-situ/semi-in-situ test system has an optical and electrical test function; the in-situ test system can stably and reliably work in vacuum (10-3 Pa level), high and low temperature (100K-473K), solar irradiation (0.5-2 solar constants), ultraviolet irradiation (0-3.5 vacuum ultraviolet constants), charged particle irradiation environment (1.2 MeV electron irradiation source: electron highest energy is not less than 1.2MeV, highest current intensity is not less than 10mA@1.0MeV,200keV electron irradiation source: electron highest energy is not less than 200keV, highest current intensity is not less than 50mA@200keV, proton irradiation source: terminal voltage is 0.1-2 MV, proton beam intensity is not less than 100 mu A@ total proton energy range); the test equipment driving mechanism has the capability of simultaneously carrying a plurality of probes. The tested sample is arranged on a sample table, and is subjected to space extreme environment assessment such as simulated vacuum, high and low temperature, solar irradiation, ultraviolet irradiation, charged particle irradiation and the like in the comprehensive cabin container, and in-situ/semi-in-situ test is carried out by a test system in the test process.
The invention provides a space comprehensive irradiation environment in-situ/semi-in-situ test method, which is oriented to space extreme environment factors such as vacuum, high and low temperature, solar irradiation, ultraviolet irradiation, charged particle irradiation and the like of ground simulation, can test samples in-situ and semi-in-situ during test,
drawings
FIG. 1 is a schematic diagram of the composition of an in situ/semi-in situ test system for a spatially integrated irradiation environment;
FIG. 2 is a schematic diagram of the drive mechanism of an in situ test equipment mounted on a sample stage;
FIG. 3 is a schematic diagram of the drive mechanism of the semi-in-situ test equipment mounted in the in-situ sub-bay;
fig. 4 instrument shielding diagram.
Detailed Description
The present invention will be described in detail with reference to specific examples.
First embodiment:
according to the embodiments shown in fig. 1 to 4, the specific optimization technical scheme adopted by the present invention to solve the above technical problems is as follows: the invention relates to a space comprehensive environment in-situ and semi-in-situ test shielding device and a test shielding method thereof.
A spatially integrated environmental in-situ and semi-in-situ test shielding apparatus, the apparatus comprising: test equipment, a driving mechanism and a remote control system 10, wherein the driving mechanism is provided with the test equipment, and the remote control system controls the driving mechanism;
the test equipment comprises a test equipment host machine 2, a test equipment probe 3 and a test equipment cabin penetrating cable 4, wherein the test equipment cabin penetrating cable 4 is connected with the test equipment host machine 2 and the test equipment probe 3; the testing equipment host machine 2 is positioned in the comprehensive cabin container, and the periphery of the testing equipment host machine 2 is provided with a radiation protection structure 7;
the driving mechanism comprises an in-situ test equipment driving mechanism 5 and a semi-in-situ test equipment driving mechanism 6; the in-situ test equipment driving mechanism 5 is integrated on the sample platform 1-1, and the semi-in-situ test equipment driving mechanism 6 is arranged in the in-situ auxiliary cabin 1-2.
The device also comprises a test equipment driving mechanism cabin penetrating cable, wherein the test equipment driving mechanism cabin penetrating cable comprises an in-situ test equipment driving mechanism cabin penetrating cable 8 and a semi-in-situ test equipment driving mechanism cabin penetrating cable 9;
the driving mechanism and the remote control system are connected by an in-situ test equipment driving mechanism cabin penetrating cable 8 and a semi-in-situ test equipment driving mechanism cabin penetrating cable 9 for transmission communication.
The tested sample is arranged on a sample table 1-1, and is subjected to space extreme environment examination such as simulated vacuum, high and low temperature, solar irradiation, ultraviolet irradiation, charged particle irradiation and the like in a comprehensive cabin container 1, and in-situ/semi-in-situ test is carried out by a test system in the test process.
The test equipment probe 3 comprises a probe 3-1 of in-situ test equipment and a probe 3-2 of semi-in-situ test equipment;
the in-situ test equipment is used for tolerating particle irradiation and comprises a discharge pulse tester, and an electrical property test is carried out in the irradiation process;
the probe of the semi-in-situ test equipment is used for intolerance or weak particle irradiation tolerance, including a Raman spectrometer, a fluorescence spectrometer and an optical performance tester, and needs to be tested in an irradiation intermittent stage.
The radiation protection structure 7 is provided with a radiation protection door for test and equipment maintenance personnel to enter and exit.
The in-situ test equipment driving mechanism 5 comprises a folding assembly 5-1, a Y-direction moving assembly 5-2 and an X/Z-direction moving assembly 5-3, can drive the in-situ test equipment probe to move in X, Y, Z directions, has multi-point test capability, can be folded and retracted after the test is finished, and reduces the occupied space.
The semi-in-situ test equipment driving mechanism 6 comprises a primary extending component 6-1, a secondary extending component 6-2 and a rotating component 6-3, wherein the primary extending component is a large-stroke rough adjusting mechanism, a probe (3-2) can be driven to rapidly extend out of the in-situ auxiliary cabin, the secondary extending component is a short-stroke fine adjusting mechanism and is used for finely adjusting the distance between the probe and a sample, the number of probes can be carried on the rotating component to be not less than 3, and when a specified performance test is carried out, the probe is rotated to a position corresponding to a test surface of the sample.
The radiation protection structure 7 comprises a framework 7-1 and a shielding layer 7-2, wherein the framework adopts a steel frame structure, and the shielding layer is formed by building an aluminum plate and a lead brick.
A space comprehensive environment in-situ and semi-in-situ test shielding method comprises the following steps:
step 1: clamping a sample to be tested on a sample table, mounting an in-situ test equipment probe on an in-situ test equipment driving mechanism, and mounting a semi-in-situ test equipment probe on a semi-in-situ test equipment driving mechanism;
step 2: a tester enters the radiation protection structure to start a test equipment host and set parameters so that the tester can acquire signals through a test equipment cabin penetrating cable; after preparation is completed, closing the cabin door to start a test;
step 3: after the test is finished, the tester enters the radiation protection structure again, and test data are exported through the test equipment host machine for subsequent processing and analysis.
During the test, the particle irradiation dose rate in the in-situ auxiliary cabin is usually much lower than that of the main cabin, and the temperature is close to room temperature.
The in-situ test is carried out under the conditions of vacuum of 10-3Pa magnitude, high and low temperature of 100K-473K, solar irradiation of 0.5-2 solar constants, ultraviolet irradiation of 0-3.5 vacuum ultraviolet constants and charged particle irradiation environment of 1.2MeV electron irradiation sources.
The above-mentioned embodiments are only preferred embodiments of a space integrated environment in-situ and semi-in-situ test shielding device and a test shielding method thereof, and the protection scope of a space integrated environment in-situ and semi-in-situ test shielding device and a test shielding method thereof is not limited to the above-mentioned embodiments, and all technical solutions under the concept belong to the protection scope of the invention. It should be noted that modifications and variations can be made by those skilled in the art without departing from the principles of the present invention, which is also considered to be within the scope of the present invention.
Claims (7)
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| CN115639237A (en) * | 2022-09-26 | 2023-01-24 | 西安空间无线电技术研究所 | A method for in-situ monitoring of surface bonding fault profiles in irradiated discharges |
| CN116399789A (en) * | 2023-02-13 | 2023-07-07 | 哈尔滨工业大学 | Multi-degree-of-freedom in-situ testing mechanism with foldable sample table in vacuum irradiation cabin |
| CN119124347A (en) * | 2024-09-06 | 2024-12-13 | 哈尔滨工业大学 | An in-situ detection device and method for spatial uniformity of solar radiation energy |
| CN119619597A (en) * | 2024-12-04 | 2025-03-14 | 哈尔滨工业大学 | Potential measurement equipment and detection method for multi-irradiation source coupled activation of simulated lunar dust |
Citations (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101813650A (en) * | 2010-02-05 | 2010-08-25 | 北京航空航天大学 | Radiometer for performance in-situ test of thermal control coat |
| CN105836165A (en) * | 2016-05-05 | 2016-08-10 | 哈尔滨工业大学 | Space environment ground-based simulation plasma generating device and plasma generating method achieved through device |
| CN205958489U (en) * | 2016-08-23 | 2017-02-15 | 中国科学院化学研究所 | Half normal position XPS sample transfer device |
| CN206725477U (en) * | 2017-01-18 | 2017-12-08 | 中国科学院化学研究所 | A kind of sample transfer device of half in situ X-ray diffraction XPS Analysis instrument |
| CN108415281A (en) * | 2018-03-16 | 2018-08-17 | 深圳中广核沃尔辐照技术有限公司 | A kind of irradiation safety interlock control system |
| CN108872051A (en) * | 2018-07-10 | 2018-11-23 | 中国船舶重工集团公司第七二五研究所 | A kind of atmospheric corrosion test device and method of synchronously simulating natural environment |
| CN109580884A (en) * | 2018-12-18 | 2019-04-05 | 哈尔滨工业大学 | The multifactor environmental grounds simulation in space and in-situ study test cabin device |
| CN110320389A (en) * | 2019-08-02 | 2019-10-11 | 中国科学院苏州纳米技术与纳米仿生研究所 | A kind of original position property test system and sample mounting procedure |
| CN110672655A (en) * | 2019-11-06 | 2020-01-10 | 上海卫星装备研究所 | In-situ detection system and method for thermal radiation performance |
| CN211148047U (en) * | 2019-10-17 | 2020-07-31 | 天津大学 | A device for in-situ thermal cycling and ultraviolet irradiation simultaneous experiments |
| CN113063732A (en) * | 2021-03-24 | 2021-07-02 | 北京卫星环境工程研究所 | Solar absorption ratio in-situ detection device and method in vacuum low-temperature environment |
| CN113443178A (en) * | 2021-07-06 | 2021-09-28 | 哈尔滨工业大学 | Vacuum container system for simulating lunar surface comprehensive environment |
| CN113607728A (en) * | 2021-07-06 | 2021-11-05 | 哈尔滨工业大学 | Optical system in-situ measuring mechanism integrating multi-degree-of-freedom linear motion |
| CN113636115A (en) * | 2021-07-30 | 2021-11-12 | 哈尔滨工业大学 | Solar system multi-factor comprehensive environment simulation device |
| CN114018792A (en) * | 2021-10-28 | 2022-02-08 | 中国科学院上海硅酸盐研究所 | Space environment multi-factor collaborative test device and test method |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8181511B2 (en) * | 2008-07-18 | 2012-05-22 | Meier Robert R | Method and system of imaging electrons in the near earth space environment |
| CN111948065B (en) * | 2020-09-04 | 2024-04-30 | 北京理工大学 | High Wen Zaiwei loading CT test system based on laboratory X-ray source and method thereof |
-
2022
- 2022-03-21 CN CN202210275812.1A patent/CN114858689B/en active Active
Patent Citations (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101813650A (en) * | 2010-02-05 | 2010-08-25 | 北京航空航天大学 | Radiometer for performance in-situ test of thermal control coat |
| CN105836165A (en) * | 2016-05-05 | 2016-08-10 | 哈尔滨工业大学 | Space environment ground-based simulation plasma generating device and plasma generating method achieved through device |
| CN205958489U (en) * | 2016-08-23 | 2017-02-15 | 中国科学院化学研究所 | Half normal position XPS sample transfer device |
| CN206725477U (en) * | 2017-01-18 | 2017-12-08 | 中国科学院化学研究所 | A kind of sample transfer device of half in situ X-ray diffraction XPS Analysis instrument |
| CN108415281A (en) * | 2018-03-16 | 2018-08-17 | 深圳中广核沃尔辐照技术有限公司 | A kind of irradiation safety interlock control system |
| CN108872051A (en) * | 2018-07-10 | 2018-11-23 | 中国船舶重工集团公司第七二五研究所 | A kind of atmospheric corrosion test device and method of synchronously simulating natural environment |
| CN109580884A (en) * | 2018-12-18 | 2019-04-05 | 哈尔滨工业大学 | The multifactor environmental grounds simulation in space and in-situ study test cabin device |
| CN110320389A (en) * | 2019-08-02 | 2019-10-11 | 中国科学院苏州纳米技术与纳米仿生研究所 | A kind of original position property test system and sample mounting procedure |
| CN211148047U (en) * | 2019-10-17 | 2020-07-31 | 天津大学 | A device for in-situ thermal cycling and ultraviolet irradiation simultaneous experiments |
| CN110672655A (en) * | 2019-11-06 | 2020-01-10 | 上海卫星装备研究所 | In-situ detection system and method for thermal radiation performance |
| CN113063732A (en) * | 2021-03-24 | 2021-07-02 | 北京卫星环境工程研究所 | Solar absorption ratio in-situ detection device and method in vacuum low-temperature environment |
| CN113443178A (en) * | 2021-07-06 | 2021-09-28 | 哈尔滨工业大学 | Vacuum container system for simulating lunar surface comprehensive environment |
| CN113607728A (en) * | 2021-07-06 | 2021-11-05 | 哈尔滨工业大学 | Optical system in-situ measuring mechanism integrating multi-degree-of-freedom linear motion |
| CN113636115A (en) * | 2021-07-30 | 2021-11-12 | 哈尔滨工业大学 | Solar system multi-factor comprehensive environment simulation device |
| CN114018792A (en) * | 2021-10-28 | 2022-02-08 | 中国科学院上海硅酸盐研究所 | Space environment multi-factor collaborative test device and test method |
Non-Patent Citations (3)
| Title |
|---|
| PI纤维在空间带电粒子辐照下的力学性能损伤;琚丹丹等;装备环境工程;第17卷(第3期);第1-7页 * |
| Preparation and Characterization of MOS Capacitors for in Situ Measurement during Radiation Damagestudies;Ibarra, ML等;International Congress of Science and Technology of Metallurgy and Materials (SAM CONAMET);第9卷;第319-325页 * |
| 微观分系统实验设备数据采集与状态监测;沈志雄;中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑(第03期);C031-661 * |
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