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Radiation-proof shading material and preparing method thereof

A shielding material and anti-radiation technology, which is applied in the field of composite materials and its preparation, can solve the problems of low mechanical properties, difficult to use the environment of spacecraft, electronic instrument protection, aging, etc., to reduce radiation damage, wide application prospects and military The effect of applying value

Inactive Publication Date: 2006-07-26
SHANGHAI JIAOTONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The process is complex and the pollution is serious. Although the prepared composite materials have a certain shielding effect on 100-2000MHz and 8-12GHz X-rays, their mechanical properties are not high, and because these materials are unstable under the action of rays, Cross-linking occurs, aging phenomenon occurs, and it is not conducive to environmental protection, so it is difficult to apply to the use environment of spacecraft and the protection of electronic instruments
Due to its special use environment, aerospace instruments require the materials used to have high mechanical properties, high temperature and low temperature resistance, and anti-aging capabilities. Therefore, the above materials are not suitable for aerospace instruments.

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0012] Weight percent of anti-radiation shielding material components: Pb 10%, Ba 1%, TiO 2 10%, TiB 2 1%, the balance is pure aluminum.

[0013] Melt pure aluminum at 750°C, add Pb 10%, Ba 1%, TiO 2 10%, TiB 2 1% anti-radiation strengthening phase, the melt is kept warm to 750°C, and formed under the conditions of cooling rate 5 degrees / second and electromagnetic frequency 7kHz. This kind of gradient composite material has a good anti-high-energy ray effect. It can shield 8.0% of γ-rays, 9.2% of X-rays, meet the standard of α and β-rays, 7% of neutron rays, and 5.7% of its density.

Embodiment 2

[0015] Weight percent of anti-radiation shielding material components: Pb 6%, Ba 3%, TiO 2 5%, TiB 2 8%, the balance is pure aluminum.

[0016] Melt pure aluminum at 850°C, add alloy elements to get LY12 alloy melt, add Pb 6%, Ba 3%, TiO 2 5%, TiB 2 8% anti-radiation strengthening phase, the melt is kept warm to 850°C, and formed under the conditions of a cooling rate of 10 degrees per second and an electromagnetic frequency of 10kHz. This kind of gradient composite material has a good anti-high-energy ray effect. It can shield 9.4% of gamma rays, 12.6% of x-rays, reach the standard for alpha and beta rays, 8.8% of neutron rays, and 4.3% of its density.

Embodiment 3

[0018] Weight percent of anti-radiation shielding material components: Pb 2%, Ba 5%, TiO 2 15%, TiB 2 10%, the balance is pure aluminum.

[0019] Melt pure aluminum at 1000°C, add Pb 2%, Ba 5%, TiO 2 15%, TiB 2 10% anti-radiation strengthening phase, the melt is kept warm to 1100°C, and formed under the conditions of cooling rate of 30 degrees per second and electromagnetic frequency of 16kHz. This kind of gradient composite material has a good anti-high-energy ray effect. It can shield 9.8% of γ-rays, 16.7% of x-rays, meet the standard of α and β-rays, 9.1% of neutron rays, and 4.8% of its density.

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PUM

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Abstract

The component percentage of the anti-radiation, shielding material is Pb 2-10%, Ba 1-5%, TiO2 5-15%, TiB2 1-10%, the rest is aluminum (Al) Under the smelting temperature, the Al is melt down. Then add the anti-radiation material of Pb, Ba, TiO2 and TiB2, the distribution of the material can be controlled by utilizing the magnetic field and controlling the cooling speed. Thus the grading structure is formed. The material is applied to protect the electrnic component of the spacecraft from outer-sphere radiation damage.

Description

technical field [0001] The invention relates to a composite material and a preparation method thereof, in particular to an anti-radiation shielding material and a preparation method thereof. Used in the field of composite material preparation. Background technique [0002] The working environment of spacecraft such as missiles, satellites, airplanes and electronic devices such as warships is full of various high-energy charged particles and electromagnetic radiation of various bands, such as high-energy protons, electrons, neutrons, ions and radio waves, microwaves, x-rays, Gamma rays, etc., will cause serious radiation damage and electromagnetic interference to electronic devices, and are an important cause of spacecraft failure and failure. For example, high-energy charged particles make semiconductor devices SiO 2 The increase of electron-hole pairs in the insulating layer leads to the threshold voltage shift of MOS transistors and the decrease of the gain of bipolar tr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G21F1/08C04B35/00
Inventor 姚利丽倪红军孙宝德王俊
Owner SHANGHAI JIAOTONG UNIV
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