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Formula and preparation method of missile box shell material

A box shell and missile technology, which is applied in the field of formulation and preparation of missile box shell materials, can solve the problems of laborious handling of personnel, inability to adapt to humid environments, inability to adapt to high temperature fire environments, etc., and achieves light weight, effortless transportation, The effect of excellent high temperature resistance

Inactive Publication Date: 2021-05-28
四川威琦尔智能科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, most of the existing missile boxes use wooden packaging boxes with separate upper and lower boxes. Ordinary wooden packaging boxes are heavy, labor-intensive to carry, and the outer wall is prone to damage or permanent deformation. It cannot adapt to high-temperature fire environments, nor can it adapt to humid environments. , it is difficult to avoid damage to the missile in various environments, which seriously affects the combat performance of the missile

Method used

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  • Formula and preparation method of missile box shell material
  • Formula and preparation method of missile box shell material

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0025] In this embodiment, a formula and preparation method of a missile case shell material is composed of the following raw materials in parts by weight: 15 parts of nano-zirconia, 25 parts of resin, 10 parts of aramid fiber, 15 parts of flame retardant, silane coupling 12 parts of joint agent, 10 parts of toughening agent, 8 parts of antioxidant.

[0026] Heating the polyphenylene sulfide resin to a molten state at high temperature, adding nano-zirconia, triphenyl phosphate, magnesium hydroxide, zinc borate, silane coupling agent, nitrile rubber, 2,6-tertiary butyl-4-methyl Stir the phenol and diester thiodipropionate evenly; then add the aramid fiber and stir evenly; finally put it into a mold and let it stand, and dry it to shape.

Embodiment 2

[0028] In this embodiment, a formula and preparation method of a missile case shell material is composed of the following raw materials in parts by weight: 20 parts of nano-zirconia, 15 parts of resin, 15 parts of aramid fiber, 10 parts of flame retardant, silane coupling 18 parts of joint agent, 5 parts of toughening agent, 12 parts of antioxidant.

[0029] Heating the polysulfone resin at high temperature into a molten state, adding nano zirconia, antimony trioxide, silane coupling agent, ABS, 2,6-tertiary butyl-4-methylphenol and diphenylamine to stir evenly; then adding aromatic Stir the fiber evenly; finally put it in the mold and let it dry to form.

Embodiment 3

[0031] In this embodiment, a formula and preparation method of a missile case shell material is composed of the following raw materials in parts by weight: 17 parts of nano-zirconia, 20 parts of resin, 12 parts of aramid fiber, 13 parts of flame retardant, silane coupling 15 parts of joint agent, 8 parts of toughening agent, 10 parts of antioxidant.

[0032] Heat the polyether ketone resin to a molten state at high temperature, add nano-zirconia, antimony trioxide, magnesium hydroxide, silane coupling agent, EVA, diphenylamine and diester thiodipropionate to stir evenly; then add aramid fiber Stir evenly; finally put it into the mold and let it stand, dry and shape.

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Abstract

The invention relates to the technical field of missile box manufacturing, and discloses a formula of a missile box shell material. The formula is prepared from the following raw materials in parts by weight: 15-20 parts of nano zirconium oxide, 15-25 parts of resin, 10-15 parts of aramid fiber, 10-15 parts of a flame retardant, 12-18 parts of a silane coupling agent, 5-10 parts of a toughening agent and 8-12 parts of an antioxidant. The invention discloses a preparation method of the missile box shell material. The preparation method comprises the following steps: (1) heating resin at a high temperature to enable the resin to be in a molten state, adding nano zirconium oxide, a flame retardant, a silane coupling agent, a flexibilizer and an antioxidant, and uniformly stirring; (2) adding aramid fibers into the uniformly stirred mixture in the step (1), and uniformly stirring; and (3) putting the uniformly stirred mixture in the step (2) into a mold, standing, airing and molding. Through the proportion of the raw materials and the corresponding preparation method, the manufactured material has excellent high temperature resistance, fire resistance and pressure resistance, can protect missiles from being damaged by the environment, and is light in mass and labor-saving to carry.

Description

technical field [0001] The invention relates to the technical field of missile case production, in particular to a formulation and preparation method of a missile case shell material. Background technique [0002] The missile box is a box used for loading and transporting missiles, and is a direct carrier and protective tool in the storage and transportation of airborne missiles. The missile box is generally divided into an outer shell and an inner carrier, and the outer shell protects the entire inner carrier and the missile placed on the inner carrier. [0003] At present, most of the existing missile boxes use wooden packaging boxes with separate upper and lower boxes. Ordinary wooden packaging boxes are heavy, labor-intensive to carry, and the outer wall is prone to damage or permanent deformation. It cannot adapt to high-temperature fire environments, nor can it adapt to humid environments. , it is difficult to avoid damage to missiles in various environments, which se...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C08L81/02C08L81/06C08L77/10C08L9/02C08L55/02C08L71/10C08L23/08C08L79/04C08K13/02C08K3/22C08K5/523C08K3/38C08K5/13C08K5/18
CPCC08L81/02C08L81/06C08L77/10C08L71/10C08L79/04C08K2003/2244C08K2201/011C08K2003/2224C08K2003/387C08L2201/08C08L2201/02C08L2205/03C08L2205/16C08L9/02C08K13/02C08K3/22C08K5/523C08K3/38C08K5/13C08L55/02C08K3/2279C08K5/18C08L23/0853
Inventor 李荣璋
Owner 四川威琦尔智能科技有限公司