Multi-energy electron proton and solar radiation comprehensive environment simulation system

文档序号:1149253 发布日期:2020-09-15 浏览:29次 中文

阅读说明:本技术 多能量电子质子和太阳辐射综合环境模拟系统 (Multi-energy electron proton and solar radiation comprehensive environment simulation system ) 是由 潘阳阳 刘刚 徐骏 李艳臣 周博 杨碧琦 兰少飞 曹康丽 王惠芬 于 2020-05-19 设计创作,主要内容包括:本发明提供了一种多能量电子质子和太阳辐射综合环境模拟系统,包括电子辐射源、质子辐射源、紫外辐射源、太阳模拟器、真空容器、样品台、运动模拟器、法兰接口。样品台上的样品处在电子、质子、太阳电磁辐射、高温或低温一种或多种环境中,进行单因素试验或综合辐射试验。本发明利用电子源、质子源、紫外辐射源、太阳模拟器等装置,通过调节样品台,使样品在一次试验中其他环境条件不间断的情况下同时受到电子辐射、质子辐射、紫外辐射、太阳电磁辐射的作用,实现空间环境在地面的综合模拟,能够为今后宇航材料、器件的筛选提供地面模拟环境。(The invention provides a multi-energy electron proton and solar radiation comprehensive environment simulation system which comprises an electron radiation source, a proton radiation source, an ultraviolet radiation source, a solar simulator, a vacuum container, a sample table, a motion simulator and a flange interface. The sample on the sample table is in one or more environments of electron, proton, solar electromagnetic radiation, high temperature or low temperature, and is subjected to a single-factor test or a comprehensive radiation test. The invention utilizes the devices such as the electron source, the proton source, the ultraviolet radiation source, the solar simulator and the like, and adjusts the sample platform to ensure that the sample is simultaneously subjected to the effects of electron radiation, proton radiation, ultraviolet radiation and solar electromagnetic radiation under the condition of uninterrupted other environmental conditions in a test, thereby realizing the comprehensive simulation of the space environment on the ground and providing a ground simulation environment for screening space materials and devices in the future.)

1. A multi-energy electron proton and solar radiation comprehensive environment simulation system is characterized by comprising an electron radiation source (1), a proton radiation source (2), an ultraviolet radiation source (3), a solar simulator (4), a vacuum container (5), a sample table (6), a motion simulator (7) and a flange interface (8);

the solar simulator (4) is positioned right above the vacuum container (5), and the electron radiation source (1), the proton radiation source (2) and the ultraviolet radiation source (3) are respectively distributed on the periphery of the solar simulator (4) for one circle;

the sample table (6) is positioned in an inner cavity of the vacuum container (5), the motion simulator (7) is connected below the sample table (6), and at least one flange interface (8) is arranged on the outer surface of the vacuum container (5).

2. The multi-energy electron proton and solar radiation comprehensive environment simulation system according to claim 1, characterized in that radiation beam lines generated by the electron radiation source (1), the proton radiation source (2), the ultraviolet radiation source (3) and the solar simulator (4) are all irradiated onto the sample stage (6) from the top of the vacuum container (5).

3. The multi-energy electron proton and solar radiation comprehensive environment simulation system according to claim 1, wherein the electron radiation source (1), the proton radiation source (2) and the ultraviolet radiation source (3) are concentrically and circumferentially distributed with the solar simulator (4) as a center, and radiation beam lines generated by the electron radiation source (1), the proton radiation source (2) and the ultraviolet radiation source (3) and radiation beam lines generated by the solar simulator (4) form the same angle.

4. The multi-energy electron proton and solar radiation comprehensive environment simulation system according to claim 1, wherein said vacuum vessel (5) is of a bulb cylinder structure.

5. The multi-energy electron proton and solar radiation comprehensive environment simulation system according to claim 1, characterized in that said electron radiation source (1) comprises a plurality of electron sources, capable of covering a spectral range of 10keV-10 MeV.

6. The multi-energy electron proton and solar radiation synthetic environment simulation system according to claim 1, characterized in that the proton radiation source (2) comprises a plurality of proton sources, capable of covering a spectral range of 10keV-10 MeV.

7. The comprehensive multi-energy electron proton and solar radiation environment simulation system according to claim 1, wherein the ultraviolet radiation source (3) comprises a 10-200nm far ultraviolet radiation source and a 200-400nm near ultraviolet radiation source.

8. The integrated multi-energy electron proton and solar radiation environment simulation system according to claim 1, wherein the solar simulator (4) simulates solar electromagnetic radiation of different emittance, wavelength range 200-.

9. The comprehensive environment simulation system for multi-energy electron proton and solar radiation according to claim 1, wherein the sample stage (6) is a movable sample stage, and is driven by a motion simulator (7) to rotate and move, and performs motion with 6 degrees of freedom.

10. A multi-energy electron proton and solar radiation comprehensive environment simulation system is characterized by comprising an electron radiation source (1), a proton radiation source (2), an ultraviolet radiation source (3), a solar simulator (4), a vacuum container (5), a sample table (6), a motion simulator (7) and a flange interface (8);

the solar simulator (4) is positioned right above the vacuum container (5), and the electron radiation source (1), the proton radiation source (2) and the ultraviolet radiation source (3) are respectively distributed on the periphery of the solar simulator (4) for one circle;

the sample table (6) is positioned in an inner cavity of the vacuum container (5), the motion simulator (7) is connected below the sample table (6), and the outer surface of the vacuum container (5) is provided with at least one flange interface (8);

radiation beam lines generated by the electron radiation source (1), the proton radiation source (2), the ultraviolet radiation source (3) and the solar simulator (4) are irradiated onto the sample table (6) from the top of the vacuum container (5);

the electron radiation source (1), the proton radiation source (2) and the ultraviolet radiation source (3) are concentrically and circumferentially distributed by taking the solar simulator (4) as a center, and radiation beam lines generated by the electron radiation source (1), the proton radiation source (2) and the ultraviolet radiation source (3) and radiation beam lines generated by the solar simulator (4) form the same angle;

the vacuum container (5) is of a ball cylinder structure;

the electron radiation source (1) comprises a plurality of electron sources capable of covering a spectral range of 10keV to 10 MeV;

the proton radiation source (2) comprises a plurality of proton sources capable of covering a spectral range of 10keV to 10 MeV;

the ultraviolet radiation source (3) comprises a 10-200nm far ultraviolet radiation source and a 200-400nm near ultraviolet radiation source;

the solar simulator (4) simulates solar electromagnetic radiation with different radiation degrees, and the wavelength range is 200-2500 nm;

the sample stage (6) is a movable sample stage, and is driven by a motion simulator (7) to rotate and move so as to move with 6 degrees of freedom.

Technical Field

The invention relates to the technical field of ground simulation of a space comprehensive environment, in particular to a multi-energy electron proton and solar radiation comprehensive environment simulation system, and particularly relates to a multi-energy electron proton and solar radiation comprehensive environment simulation system constructed by a certain technical means.

Background

The spatial radiation particle components are mainly electrons, protons and a small number of heavy ions, with energies ranging from 1keV to several hundred MeV, and even up to several GeV, the higher the energy the smaller its flux. Because the energy range of the space charged particles is wide, and the energy distribution and flux of the particles can be dynamically changed along with factors such as the sun, geomagnetic activity and the like, the real space radiation environment cannot be completely simulated in the ground simulated space radiation environment.

Generally, low-energy particle radiation (below 1 MeV) only affects the change of the surface of a substance, and the particle radiation with energy of 1-10MeV can cause the change of the internal structure of the substance, so that the research on the damage mechanism and law in the substance is necessary. The range depth of the proton radiation above 10MeV is increased along with the increase of the energy, and a more remarkable ionization effect is generated on the track or the ionization effect is generated due to recoil particles in the material, so that a single event effect occurs.

Patent document CN202403923U discloses a space environment radiation simulation device, which comprises an electron accelerator main body, an electron gun, a first accelerating tube, a beam stop, a scanning magnet and an irradiation chamber, which are connected in sequence, wherein an irradiation platform is installed in the irradiation chamber, and a first molecular pump is also installed on the irradiation chamber. The irradiation platform is arranged in an irradiation chamber close to vacuum for testing, the beam output of the electron accelerator can be changed in a large range, and comprehensive state simulation and accurate parameter measurement can be realized.

Disclosure of Invention

Aiming at the defects in the prior art, the invention aims to provide a comprehensive environment simulation system for multi-energy electron protons and solar radiation.

The invention provides a multi-energy electron proton and solar radiation comprehensive environment simulation system which comprises an electron radiation source, a proton radiation source, an ultraviolet radiation source, a solar simulator, a vacuum container, a sample table, a motion simulator and a flange interface, wherein the electron radiation source is arranged on the vacuum container;

the solar simulator is positioned right above the vacuum container, and the electron radiation source, the proton radiation source and the ultraviolet radiation source are respectively distributed on the periphery of the solar simulator for one circle;

the sample platform is located in the inner cavity of the vacuum container, the motion simulator is connected below the sample platform, and at least one flange interface is arranged on the outer surface of the vacuum container.

Preferably, the electron radiation source, the proton radiation source, the ultraviolet radiation source and the radiation beam line generated by the solar simulator are irradiated onto the sample table from the top of the vacuum container.

Preferably, the electron radiation source, the proton radiation source and the ultraviolet radiation source are concentrically and circumferentially distributed around the solar simulator, and radiation beam lines generated by the electron radiation source, the proton radiation source and the ultraviolet radiation source and radiation beam lines generated by the solar simulator form the same angle.

Preferably, the vacuum container is of a ball cylinder structure.

Preferably, the electron radiation source comprises a plurality of electron sources capable of covering a spectral range of 10keV to 10 MeV.

Preferably, the source of proton radiation comprises a plurality of proton sources capable of covering a spectral range of 10keV to 10 MeV.

Preferably, the ultraviolet radiation source comprises a 10-200nm far ultraviolet radiation source and a 200-400nm near ultraviolet radiation source.

Preferably, the solar simulator simulates solar electromagnetic radiation of different emittance, in the wavelength range of 200 and 2500 nm.

Preferably, the sample stage is a movable sample stage, and is driven by the motion simulator to rotate and move, so as to perform motion with 6 degrees of freedom.

Compared with the prior art, the invention has the following beneficial effects:

1. the invention utilizes the devices such as the electron source, the proton source, the ultraviolet radiation source, the solar simulator and the like, and adjusts the sample platform to ensure that the sample is simultaneously subjected to the effects of electron radiation, proton radiation, ultraviolet radiation and solar electromagnetic radiation under the condition of uninterrupted other environmental conditions in a test, thereby realizing the comprehensive simulation of the space environment on the ground and providing a ground simulation environment for screening space materials and devices in the future.

2. The invention considers the equivalence of the radiation effect of the substance as a basic starting point to simulate the radiation of ions and electrons below 10MeV, and can further develop the comprehensive radiation effect and mechanism research of materials, devices and system modules, including the total dose effect, the displacement effect, the charge and discharge effect and the synergistic effect thereof.

Drawings

Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:

FIG. 1 is a schematic diagram of a multi-energy electron proton and solar radiation integrated environment simulation system of the present invention;

FIG. 2 is a schematic view of a radiation source arrangement of the integrated environmental simulation system of the present invention;

FIG. 3 is a schematic diagram of an integrated environment simulation architecture of the present invention.

The figures show that:

Figure BDA0002498771000000031

Detailed Description

The present invention will be described in detail with reference to specific examples. The following examples will assist those skilled in the art in further understanding the invention, but are not intended to limit the invention in any way. It should be noted that it would be obvious to those skilled in the art that various changes and modifications can be made without departing from the spirit of the invention. All falling within the scope of the present invention.

In the description of the present application, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience in describing the present application and simplifying the description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present application.

The invention takes the equivalence of the radiation effect of the substance as a basic starting point to carry out simulation, mainly simulates the radiation of ions and electrons below 10MeV, and can develop the comprehensive radiation effect and mechanism research of materials, devices and system modules, including the total dose effect, the displacement effect, the charge and discharge effect and the synergistic effect thereof. Because the energy spectrum of the space charged particle radiation is continuous, in order to realize the full-spectrum simulation below 10MeV, the radiation source is divided into 3 energy levels, the energy of the particles can be adjusted within a certain range, and the research on the particle radiation effect of different energy spectrums of materials/devices is realized.

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