CN113253361A - Testing device for extreme low-temperature physical properties of lunar soil water ice - Google Patents
Testing device for extreme low-temperature physical properties of lunar soil water ice Download PDFInfo
- Publication number
- CN113253361A CN113253361A CN202110410705.0A CN202110410705A CN113253361A CN 113253361 A CN113253361 A CN 113253361A CN 202110410705 A CN202110410705 A CN 202110410705A CN 113253361 A CN113253361 A CN 113253361A
- Authority
- CN
- China
- Prior art keywords
- vacuum
- low temperature
- water ice
- temperature
- experimental chamber
- 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
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 31
- 238000012360 testing method Methods 0.000 title claims abstract description 22
- 230000000704 physical effect Effects 0.000 title claims abstract description 19
- 239000002689 soil Substances 0.000 title claims abstract description 18
- 238000005057 refrigeration Methods 0.000 claims abstract description 6
- 238000010438 heat treatment Methods 0.000 claims description 10
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 8
- 229910052802 copper Inorganic materials 0.000 claims description 8
- 239000010949 copper Substances 0.000 claims description 8
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims description 3
- 229910052737 gold Inorganic materials 0.000 claims description 3
- 239000010931 gold Substances 0.000 claims description 3
- 239000003973 paint Substances 0.000 claims description 3
- 238000005259 measurement Methods 0.000 claims description 2
- 238000007747 plating Methods 0.000 claims description 2
- 238000001514 detection method Methods 0.000 abstract description 4
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 abstract description 3
- 238000002474 experimental method Methods 0.000 description 34
- NMFHJNAPXOMSRX-PUPDPRJKSA-N [(1r)-3-(3,4-dimethoxyphenyl)-1-[3-(2-morpholin-4-ylethoxy)phenyl]propyl] (2s)-1-[(2s)-2-(3,4,5-trimethoxyphenyl)butanoyl]piperidine-2-carboxylate Chemical compound C([C@@H](OC(=O)[C@@H]1CCCCN1C(=O)[C@@H](CC)C=1C=C(OC)C(OC)=C(OC)C=1)C=1C=C(OCCN2CCOCC2)C=CC=1)CC1=CC=C(OC)C(OC)=C1 NMFHJNAPXOMSRX-PUPDPRJKSA-N 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000008014 freezing Effects 0.000 description 2
- 238000007710 freezing Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012795 verification Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01V—GEOPHYSICS; GRAVITATIONAL MEASUREMENTS; DETECTING MASSES OR OBJECTS; TAGS
- G01V13/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices covered by groups G01V1/00 – G01V11/00
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Life Sciences & Earth Sciences (AREA)
- General Physics & Mathematics (AREA)
- Geophysics (AREA)
- Investigating Or Analyzing Materials Using Thermal Means (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
本发明提出一种月壤水冰极端低温物性测试装置，该测试装置包括制冷系统、真空系统和真空低温实验舱，真空低温实验舱位于真空系统内部，制冷系统与真空低温实验舱连接；真空低温实验舱的导冷样品台放置在实验舱舱体中，所述导冷样品台与多级冷头相连，密封样本盒和温控加热片放置在导冷样品台上，温控加热片上设置有被测传感器，密封样本盒被分为若干个独立单元，每个独立单元中放置水冰样本和被测传感器；解决现有技术没有能实现月球极端低温真空环境的实验装置的技术问题。本发明能够模拟如此苛刻的月球环境，是国内第一次对水冰探测的传感器件进行测试，填补了国内对于水冰探测的空白，对于我国追赶国际太空探索水平有着重大意义。
The invention provides a test device for the extreme low temperature physical properties of lunar soil water ice. The test device includes a refrigeration system, a vacuum system and a vacuum low temperature experimental chamber. The vacuum low temperature experimental chamber is located inside the vacuum system, and the refrigeration system is connected with the vacuum low temperature experimental chamber; The cooling-conducting sample stage of the experimental cabin is placed in the experimental cabin, and the cooling-conducting sample stage is connected with the multi-stage cold head. The tested sensor, the sealed sample box is divided into several independent units, and the water ice sample and the tested sensor are placed in each independent unit; it solves the technical problem that the existing technology does not have an experimental device that can realize the extreme low temperature vacuum environment of the moon. The invention can simulate such harsh lunar environment, is the first time in China to test the sensor device for water ice detection, fills the blank of water ice detection in China, and has great significance for my country to catch up with the international space exploration level.
Description
Technical Field
The invention relates to a testing device for extreme low-temperature physical properties of lunar soil water ice, and belongs to the technical field of lunar soil testing devices.
Background
The exploration of the moon water ice is bound to face extreme environments such as vacuum and extremely low temperature, and in order to guarantee the performance of the sensor used for the exploration, the performance of the sensor under the extreme environments needs to be verified on the ground by a performance verification device, and the performance of the sensor under different conditions needs to be verified. However, because the required extreme environment is too harsh, no experimental device capable of realizing such an extremely low-temperature vacuum environment exists at present.
Disclosure of Invention
The invention provides a testing device for extreme low-temperature physical properties of lunar soil water ice, aiming at solving the technical problem that no experimental device capable of realizing an extreme low-temperature vacuum environment of a moon exists in the prior art.
The invention provides a testing device for extreme low-temperature physical properties of lunar soil water ice, which comprises a refrigerating system, a vacuum system and a vacuum low-temperature experiment chamber, wherein the vacuum low-temperature experiment chamber is positioned in the vacuum system, and the refrigerating system is connected with the vacuum low-temperature experiment chamber and used for refrigerating the vacuum low-temperature experiment chamber;
the refrigeration system mainly comprises a low-temperature refrigerator and a multi-stage cold head, wherein the low-temperature refrigerator is connected with the vacuum low-temperature experiment chamber through the multi-stage cold head;
the vacuum low-temperature experiment cabin comprises an experiment cabin body, a cold guide sample table, a sealed sample box and a temperature control heating sheet, wherein the cold guide sample table is placed in the experiment cabin body, the cold guide sample table is connected with a multi-stage cold head, the sealed sample box and the temperature control heating sheet are placed on the cold guide sample table, a sensor to be tested is arranged on the temperature control heating sheet, the sealed sample box is divided into a plurality of independent units, and a water ice sample and a sensor to be tested are placed in each independent unit;
the vacuum system comprises a vacuum cover and a cold screen, wherein the cold screen is arranged in the vacuum cover, an experiment cabin body is arranged in the cold screen, and a sensor measuring interface is arranged on the vacuum cover.
Preferably, a base is connected below the vacuum cover through a vacuum cover flange.
Preferably, the outer surfaces of the cold screen and the vacuum low-temperature experiment cabin are subjected to gold plating treatment, and the inner surfaces of the cold screen and the vacuum low-temperature experiment cabin are coated with heat sink black paint.
Preferably, the multistage cold head cools down step by step, finally transmits extreme low temperature to the vacuum low temperature experiment cabin.
Preferably, a cold conducting copper block is arranged below the cold conducting sample table and connected with the multistage cold head.
The testing device for extreme low-temperature physical properties of the lunar soil water ice has the beneficial effects that:
1. the sealed sample box comprises five layers of independent units, so that position decoupling and distribution decoupling are facilitated.
2. The invention can simulate the harsh lunar environment, is a first time of testing the sensing device for water ice detection in China, fills the blank of water ice detection in China, and has great significance for pursuing the international space exploration level in China.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this application, illustrate embodiments of the invention and, together with the description, serve to explain the invention and not to limit the invention.
In the drawings:
FIG. 1 is a schematic diagram of an internal structure of a testing device for extreme low-temperature physical properties of lunar soil water ice according to the present invention;
FIG. 2 is a schematic diagram of an external structure of a testing device for extreme low-temperature physical properties of lunar soil water ice according to the present invention;
wherein, 1-cold shielding; 2-an experiment cabin body; 3-sealing the sample box; 4-a sensor measurement interface; 5-a base; 6-a cryogenic refrigerator; 7-multi-stage cold head; 8-vacuum hood flange; 9-cold conducting copper blocks; 10-temperature control heating sheet; 11-a sensor under test; 12-vacuum hood.
Detailed Description
The following detailed description of embodiments of the invention is provided in conjunction with the appended drawings:
the first embodiment is as follows: the present embodiment is explained with reference to fig. 1-2. The testing device for extreme low-temperature physical properties of lunar soil water ice in the embodiment comprises a refrigerating system, a vacuum system and a vacuum low-temperature experiment chamber, wherein the vacuum low-temperature experiment chamber is positioned in the vacuum system, the refrigerating system is connected with the vacuum low-temperature experiment chamber and used for refrigerating the vacuum low-temperature experiment chamber, and a thermal control system is positioned outside the vacuum low-temperature experiment chamber;
the refrigerating system mainly comprises a low-temperature refrigerator 6 and a multi-stage cold head 7, wherein the low-temperature refrigerator 6 is connected with the vacuum low-temperature experiment chamber through the multi-stage cold head 7;
the vacuum low-temperature experiment chamber comprises an experiment chamber body, a cold guide sample table, a sealed sample box 3 and a temperature control heating sheet 10, wherein the cold guide sample table is placed in the experiment chamber body, the cold guide sample table is connected with a multistage cold head 7, the sealed sample box 3 and the temperature control heating sheet 10 are placed on the cold guide sample table, a sensor 11 to be tested is arranged on the temperature control heating sheet 10, the sealed sample box 3 is divided into a plurality of independent units, and a water ice sample and the sensor 11 to be tested are placed in each independent unit;
the vacuum system comprises a vacuum cover 12 and a cold screen 1, wherein the cold screen 1 is arranged in the vacuum cover 12, an experimental cabin body is arranged in the cold screen 1, and a sensor measuring interface is arranged on the vacuum cover 12.
A base 5 is connected below the vacuum cover 12 through a vacuum cover flange 8.
The measured sensor 11 can be replaced by different sensors according to different experiments.
The multistage cold head 7 cools down step by step, and finally extremely low temperature is transmitted to the vacuum low temperature experiment cabin.
And a cold guide copper block 4 is arranged below the cold guide sample table, and the cold guide copper block 4 is connected with a multistage cold head 7.
The outer surfaces of the cold screen 1 and the vacuum low-temperature experiment chamber are plated with gold to reduce heat leakage, the inner surfaces of the cold screen 1 are coated with heat sink black paint, and the cold screen 1 is used for keeping vacuum and low temperature.
Wherein, the inside of the upper vacuum hood 2 is a cold shield 1, and the inner side of the cold shield 1 is an experiment chamber 10. The inner and outer layer mechanisms are adopted to simulate an extremely low temperature environment as much as possible, wherein the thermodynamic temperature in the cold shield 1 can reach 40K, and the thermodynamic temperature in the hot vacuum chamber can reach 50K. The junction of vacuum cup 2 is provided with the sealing ring, and the effect of vacuum cup 2 and sealing ring is for keeping the condition of vacuum, and vacuum cup 2 links to each other with the molecular pump, can be with the air in the extraction vacuum cup 2 when the experiment begins, and vacuum cup 2 inside can reach certain vacuum degree when the guarantee experiment.
The sample and the detected sensing device required by the experiment are placed on the cold guide sample table, the cold guide sample table is characterized in that the cold guide sample table is connected with a cold guide copper block 9, the cold guide copper block 9 is connected with a multistage cold head 7, in order to ensure the working efficiency, each device is tightly attached to the cold guide sample table, and meanwhile, the instrument is connected with the experimental device through a sensor measurer interface 4, so that the temperature of each cabin can be monitored in real time.
In order to verify the performance of the measured sensor 11, two types of experiments need to be completed, namely the experiment for directly verifying the tolerance of the sensor in a vacuum, low-temperature and anhydrous environment, and the experiment for verifying the tolerance of an instrument in lunar soil with different water contents.
In order to verify the performance of the sensor 11 under different conditions, a sample library is established, lunar soil water ice samples with different water contents and mean values of compactness are configured, low-temperature freezing treatment is performed, then a calibrated sensor device is used for performing comprehensive physical property test, and the water contents, the freezing temperature and the compactness are continuously changed for performing the test, so that the mapping relation between the temperature, the water contents, the compactness and the comprehensive physical property can be obtained.
The sealed sample box 3 is divided into five independent units, and a water ice sample with known comprehensive physical properties and a calibrated sensing device are placed on each layer so as to carry out position decoupling and distribution decoupling. The tested sensor 11 is kept in full contact with the water ice sample during the experiment, and the performance of the sensing device in the extreme environment can be judged whether to meet the index or not by comparing and analyzing the measured data and the known physical property parameters of the sample after the experiment is finished.
The above-mentioned embodiments further explain the objects, technical solutions and advantages of the present invention in detail. It should be understood that the above-mentioned embodiments are only examples of the present invention, and are not intended to limit the present invention, and that the reasonable combination of the features described in the above-mentioned embodiments can be made, and any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (5)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110410705.0A CN113253361B (en) | 2021-04-14 | 2021-04-14 | A device for testing the physical properties of lunar soil and water ice at extremely low temperatures |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110410705.0A CN113253361B (en) | 2021-04-14 | 2021-04-14 | A device for testing the physical properties of lunar soil and water ice at extremely low temperatures |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN113253361A true CN113253361A (en) | 2021-08-13 |
| CN113253361B CN113253361B (en) | 2024-04-26 |
Family
ID=77220957
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110410705.0A Active CN113253361B (en) | 2021-04-14 | 2021-04-14 | A device for testing the physical properties of lunar soil and water ice at extremely low temperatures |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113253361B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113624063A (en) * | 2021-08-17 | 2021-11-09 | 中国科学院合肥物质科学研究院 | A kind of manufacturing method of low temperature helium chamber with large heat exchange and low flow resistance |
| CN113920804A (en) * | 2021-09-26 | 2022-01-11 | 哈尔滨工业大学 | A large-scale multi-factor space irradiation environment integrated simulation device and simulation method |
| CN115343326A (en) * | 2022-07-01 | 2022-11-15 | 哈尔滨工业大学 | Device and method for measuring thermal characteristics of low-temperature vacuum ice-containing soil simulant |
| CN115876971A (en) * | 2022-12-30 | 2023-03-31 | 中国科学院地质与地球物理研究所 | A method for online calibration of water ice sample analyzer in vacuum low temperature environment |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201298003Y (en) * | 2008-11-18 | 2009-08-26 | 西安航空发动机（集团）有限公司 | Low-temperature device for fatigue crack test |
| CN102156304A (en) * | 2010-12-30 | 2011-08-17 | 中国航天科技集团公司第五研究院第五一○研究所 | Small-sized comprehensive simulation system of lunar environment |
| CN102854056A (en) * | 2012-09-18 | 2013-01-02 | 中国科学院理化技术研究所 | Material low-temperature mechanical property testing device with refrigerating machine as cold source |
| CN205826401U (en) * | 2016-07-20 | 2016-12-21 | 兰州大学 | The multi-environment equipment of superconductor Mechanics Performance Testing after the match |
| CN206132495U (en) * | 2016-07-20 | 2017-04-26 | 兰州大学 | Superconducting material power under extremely low alternating temperature environment thermal coupling loading system |
| CN107941261A (en) * | 2017-12-05 | 2018-04-20 | 中国科学院高能物理研究所 | A kind of sensor device low-temperature test platform |
| CN109799421A (en) * | 2019-03-12 | 2019-05-24 | 北京卫星环境工程研究所 | The combined environment test of aerospace optical connector studies system |
| CN110440912A (en) * | 2019-08-19 | 2019-11-12 | 中国电子科技集团公司第四十一研究所 | A kind of use for laboratory low temperature radiometer |
| CN110631741A (en) * | 2019-09-18 | 2019-12-31 | 兰州大学 | An automatic and batch calibration system for fiber grating temperature sensors under ultra-low temperature and large temperature changes |
-
2021
- 2021-04-14 CN CN202110410705.0A patent/CN113253361B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201298003Y (en) * | 2008-11-18 | 2009-08-26 | 西安航空发动机（集团）有限公司 | Low-temperature device for fatigue crack test |
| CN102156304A (en) * | 2010-12-30 | 2011-08-17 | 中国航天科技集团公司第五研究院第五一○研究所 | Small-sized comprehensive simulation system of lunar environment |
| CN102854056A (en) * | 2012-09-18 | 2013-01-02 | 中国科学院理化技术研究所 | Material low-temperature mechanical property testing device with refrigerating machine as cold source |
| CN205826401U (en) * | 2016-07-20 | 2016-12-21 | 兰州大学 | The multi-environment equipment of superconductor Mechanics Performance Testing after the match |
| CN206132495U (en) * | 2016-07-20 | 2017-04-26 | 兰州大学 | Superconducting material power under extremely low alternating temperature environment thermal coupling loading system |
| CN107941261A (en) * | 2017-12-05 | 2018-04-20 | 中国科学院高能物理研究所 | A kind of sensor device low-temperature test platform |
| CN109799421A (en) * | 2019-03-12 | 2019-05-24 | 北京卫星环境工程研究所 | The combined environment test of aerospace optical connector studies system |
| CN110440912A (en) * | 2019-08-19 | 2019-11-12 | 中国电子科技集团公司第四十一研究所 | A kind of use for laboratory low temperature radiometer |
| CN110631741A (en) * | 2019-09-18 | 2019-12-31 | 兰州大学 | An automatic and batch calibration system for fiber grating temperature sensors under ultra-low temperature and large temperature changes |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113624063A (en) * | 2021-08-17 | 2021-11-09 | 中国科学院合肥物质科学研究院 | A kind of manufacturing method of low temperature helium chamber with large heat exchange and low flow resistance |
| CN113920804A (en) * | 2021-09-26 | 2022-01-11 | 哈尔滨工业大学 | A large-scale multi-factor space irradiation environment integrated simulation device and simulation method |
| CN115343326A (en) * | 2022-07-01 | 2022-11-15 | 哈尔滨工业大学 | Device and method for measuring thermal characteristics of low-temperature vacuum ice-containing soil simulant |
| CN115343326B (en) * | 2022-07-01 | 2025-05-30 | 哈尔滨工业大学 | A device and method for measuring thermal properties of low-temperature vacuum ice-containing star soil simulant |
| CN115876971A (en) * | 2022-12-30 | 2023-03-31 | 中国科学院地质与地球物理研究所 | A method for online calibration of water ice sample analyzer in vacuum low temperature environment |
Also Published As
| Publication number | Publication date |
|---|---|
| CN113253361B (en) | 2024-04-26 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN113253361A (en) | Testing device for extreme low-temperature physical properties of lunar soil water ice | |
| CN110082046A (en) | A valve low temperature leak detection system and leak detection method | |
| CN105044147B (en) | A kind of nearly phase change zone thermal conductivity of frozen soils measure apparatus and method | |
| CN109799421B (en) | Comprehensive environment experiment research system of aerospace optical cable connector | |
| CN104569046A (en) | Ultra-high temperature heat-insulating property testing device and method | |
| CN103925759A (en) | Wide-temperature-range control thermostat for thermophysical property | |
| CN104215749A (en) | Realization method of combined temperature gradient in frozen earth | |
| CN111175341A (en) | Optical test system and test method for low-temperature linear expansion coefficient of material | |
| CN109738701A (en) | A conductivity measurement device and method | |
| CN207717368U (en) | Rotating device for combustor exit parameter measurement | |
| CN206096193U (en) | A environment case for electronic components electrical property in situ test | |
| CN100439817C (en) | Electron optical device for direct cooling of long-wave infrared detection devices by pulse tube refrigerator | |
| CN101750227A (en) | Operational capacity test device of low-temperature pressure gloves | |
| CN100334425C (en) | Method for measuring deformation at lous temp of focal plane probe and special Dewar | |
| CN206684009U (en) | A kind of infrared acquisition high-low-temperature environmental testing case | |
| CN112611552B (en) | Aeroengine high temperature high altitude ventilation valve test device | |
| CN111413099B (en) | Verification device for measuring method of inner wall temperature of engine heat-receiving parts | |
| CN110749115B (en) | Multifunctional low-temperature vortex coil precooling heat exchanger | |
| CN209802606U (en) | Valve low-temperature leakage detection system | |
| CN209069460U (en) | A kind of temperature sensor testing device | |
| CN103941437A (en) | Experimental facility used for high-low temperature optical evaluation | |
| CN105319024B (en) | Air separation cooling box leakage point tuning on-line method | |
| CN103115743B (en) | Can test spring at the device of wide low-temperature space elastic performance | |
| CN211204483U (en) | Multifunctional low-temperature vortex coil precooling heat exchanger | |
| CN116183400A (en) | Small adjustable low-temperature environment generation cabin for high strain rate test and use method thereof |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |