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Polyethylene composite material mixed with carbon nano tube and nanometer tantalum and used for space charged particle radiation protection and preparation method and application thereof

A carbon nanotube and charged particle technology is applied to a polyethylene composite material doped with carbon nanotubes and nanotantalum for space charged particle radiation protection and its preparation and application fields. Poor stability, restricting the scope of use, etc., to solve the effects of large weight, improved thermal stability, and improved proton protection efficiency

Active Publication Date: 2013-05-08
HARBIN INST OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention is to solve the radiation protection material prepared by the existing radiation protection material method. The density of the aluminum protection layer is large and the weight used is large. When polyethylene material is used as the radiation protection material, there is a problem due to its low poor, seriously restricting the scope of its use, and provide a polyethylene composite material doped with carbon nanotubes and nano-tantalum for space charged particle radiation protection and its preparation method and application

Method used

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  • Polyethylene composite material mixed with carbon nano tube and nanometer tantalum and used for space charged particle radiation protection and preparation method and application thereof
  • Polyethylene composite material mixed with carbon nano tube and nanometer tantalum and used for space charged particle radiation protection and preparation method and application thereof
  • Polyethylene composite material mixed with carbon nano tube and nanometer tantalum and used for space charged particle radiation protection and preparation method and application thereof

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specific Embodiment approach 1

[0025] Specific embodiment 1: This embodiment is a polyethylene composite material doped with carbon nanotubes and nano-tantalum for space charged particle radiation protection, which is composed of 1 part to 100 parts of polyethylene resin, 1 part to 100 parts by weight, and 1 part to 100 parts by weight. It is prepared by 10 parts of carbon nanotubes, 5-50 parts of nano-tantalum and 0.5-20 parts of coupling agent.

[0026] Carbon nanotubes are added to the polyethylene composite material doped with carbon nanotubes and nano tantalum for space charged particle radiation protection in this embodiment, which can better prevent polyethylene cracking and improve the proton protection effect of the material. At the same time, tantalum is added to the polyethylene composite material. Due to the high density of tantalum, when electrons are incident on the material, they are prone to large scattering, which increases the energy loss of electrons in the material and improves the electr...

specific Embodiment approach 2

[0028] Specific embodiment two: the difference between this embodiment and specific embodiment one is: the composite material is composed of 20-95 parts of polyethylene resin, 4-6 parts of carbon nanotubes, 5 parts by weight It is prepared by 1-40 parts of nano-tantalum and 1-15 parts of coupling agent. Others are the same as in the first embodiment.

specific Embodiment approach 3

[0029] Embodiment 3: The difference between this embodiment and Embodiment 1 or 2 is that the density of the polyethylene resin is 0.900 g / cm 3 ~0.980g / cm 3 . Others are the same as in the first or second embodiment.

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Abstract

The invention discloses polyethylene composite material mixed with a carbon nano tube and nanometer tantalum and used for space charged particle radiation protection, a preparation method and application of the polyethylene composite material mixed with the carbon nano tube and the nanometer tantalum and used for the space charged particle radiation protection, and relates to the field of composite materials used for the space charged particle radiation protection and a preparation of the composite materials used for the space charged particle radiation protection. The problems that in radiation protection materials prepared and obtained by an existing radiation protection material method, an aluminum protection layer is large in density, and therefore using weight is large, polyethylene is adopted as the radiation protection materials, heat stability of the polyethylene is poor, and using range of the polyethylene is limited are solved. The polyethylene composite material mixed with the carbon nano tube and the nanometer tantalum and used for the space charged particle radiation protection is prepared by polyethylene resin, the carbon nano tube, the nanometer tantalum and coupling reagents. The preparation method comprises a first step of mixing the carbon nano tube, the nanometer tantalum and the coupling reagents to obtain a modified carbon nano tube and modified nanometer tantalum, and a second step of carrying out hot-pressing after mixing the modified carbon nano tube, the modified nanometer tantalum and the polyethylene resin. The material is used for defending space protons and electron radiation. The polyethylene composite material mixed with the carbon nano tube and the nanometer tantalum and used for the space charged particle radiation protection, the preparation method and the application of the polyethylene composite material mixed with the carbon nano tube and the nanometer tantalum and used for the space charged particle radiation protection are suitable for the field of the radiation protection.

Description

technical field [0001] The present invention relates to the field of composite materials for space charged particle radiation protection and their preparation methods and applications. Background technique [0002] For the design of spacecraft, space charged particle radiation protection materials have always been an important research topic, and the traditional radiation protection materials are mainly aluminum. In order to achieve the anti-radiation effect, the thickness of the aluminum protective layer must be increased, thereby increasing the weight of the spacecraft. The issue of lightweight spacecraft has always been a hot issue for designers. Studies have shown that hydrogen-containing light elements are more effective than heavy elements in resisting radiation damage, that is to say, the radiation protection efficiency increases with the decrease of atomic number. In theory, liquid hydrogen has the best protection efficiency, but it is not feasible in practical appl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G21F1/02G21F1/10
Inventor 李兴冀芮二明何世禹杨剑群
Owner HARBIN INST OF TECH
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