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Anti-icing coating for low-temperature storage tank of rocket and preparation method thereof

A low-temperature storage tank and anti-icing technology, applied in the field of coatings, can solve problems such as condensation into ice, adhesion, launch accidents, and coating effects to be improved, so as to reduce adhesion, increase speed, and quickly and effectively deice Effect

Inactive Publication Date: 2021-06-08
北京九天行歌航天科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The storage tank contains low-temperature fuel (the boiling point of liquid oxygen is -182.96°C, and the boiling point of liquid hydrogen is -252.78°C). Under the induction of the low temperature of the storage tank, it is easy to cause the water vapor outside the storage tank to condense into ice and adhere to the outer wall of the storage tank. , causing a launch accident
[0003] However, the existing coating effect still needs to be improved, so based on this, the technical scheme of the present invention is proposed

Method used

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  • Anti-icing coating for low-temperature storage tank of rocket and preparation method thereof
  • Anti-icing coating for low-temperature storage tank of rocket and preparation method thereof
  • Anti-icing coating for low-temperature storage tank of rocket and preparation method thereof

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Embodiment 1

[0031] This embodiment provides a preparation method of an anti-icing coating for a low-temperature storage tank of a rocket, comprising the following steps:

[0032] (1) Add fluorine-containing polyether polyol (BHF-1000), ordinary polyether polyol (DDL-210) and chain extender into the first reactor, and raise the temperature from room temperature to 90°C, during the heating period, the reactor was evacuated to a vacuum degree of -0.09MPa, and the mixture a was obtained after completion;

[0033] (2) Add diisobutyl phthalate, titanium dioxide and anti-aging agent into the high-speed dispersant, and mix for 1 hour under the condition of 500r / min to obtain the color paste mixture; then add the color paste mixture to In a sander, grind at a rate of 1500r / min until the particle size is less than 10 μm to obtain mixture b;

[0034] (3) Add mixture a, mixture b, butyl acetate, defoamer, and leveling agent into the second reactor, mix at 500r / min for 1h, and then filter through a f...

Embodiment 2

[0040] This embodiment provides a preparation method of an anti-icing coating for a low-temperature storage tank of a rocket, comprising the following steps:

[0041] (1) Add fluorine-containing polyether polyol (BHF-1000), ordinary polyether polyol (DDL-210) and chain extender into the first reactor, and raise the temperature from room temperature to 120°C, during the heating period, the reactor was evacuated to a vacuum of -0.1MPa, and the mixture a was obtained after completion;

[0042] (2) Add diisobutyl phthalate, titanium dioxide and anti-aging agent into the high-speed dispersant, and mix for 2 hours under the condition of 2000r / min to obtain the color paste mixture; then add the color paste mixture to In a sander, grind at a rate of 1500r / min until the particle size is less than 10 μm to obtain mixture b;

[0043] (3) Add mixture a, mixture b, butyl acetate, defoamer, and leveling agent into the second reactor, mix for 1 hour under the condition of 1000r / min, and the...

Embodiment 3

[0049] This embodiment provides a preparation method of an anti-icing coating for a low-temperature storage tank of a rocket, comprising the following steps:

[0050] (1) Add fluorine-containing polyether polyol (BHF-1000), ordinary polyether polyol (DDL-210) and chain extender into the first reactor, and raise the temperature from room temperature to 105°C, during the heating period, the reactor was evacuated to a vacuum of -0.1MPa, and the mixture a was obtained after completion;

[0051](2) Add diisobutyl phthalate, titanium dioxide and anti-aging agent into the high-speed dispersant, and mix for 1.5 hours under the condition of 1200r / min to obtain the color paste mixture; then add the color paste mixture to the Put it into a grinding machine, grind at a rate of 1500r / min until the particle size is less than 10 μm, and obtain mixture b;

[0052] (3) Add mixture a, mixture b, butyl acetate, defoamer, and leveling agent into the second reactor, mix at 750r / min for 1h, and th...

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Abstract

The invention relates to an anti-icing coating for a low-temperature storage tank of a rocket and a preparation method thereof. The anti-icing coating for the low-temperature storage tank of the rocket comprises a component A and a component B; the component A is prepared from the following raw materials in parts by weight: 8 to 20 parts of fluorine-containing polyether polyol, 10 to 25 parts of common polyether polyol, 6 to 7.2 parts of diisobutyl phthalate, 33 to 34.4 parts of butyl acetate, 1 to 1.4 parts of chain extender, 0.1 to 0.3 part of defoaming agent, 0.1 to 0.3 part of flatting agent, 3 to 3.6 parts of titanium dioxide and 0.1 to 0.3 part of anti-aging agent; the component B comprises the following raw materials in parts by weight: 21 to 22.2 parts of a curing agent. A coating layer formed by the anti-icing coating can reduce condensation on the surface of a base material and has excellent hydrophobicity; the adhesion capability of ice can be reduced; according to the preparation method, technological parameters are easy to control, and large-scale output is facilitated.

Description

technical field [0001] The invention belongs to the field of coatings, and in particular relates to an anti-icing coating for low-temperature storage tanks of rockets and a preparation method thereof. Background technique [0002] Large-scale launch vehicles are generally launched at coastal launch sites close to the equator, and the surrounding environment is characterized by high temperature and high humidity. The storage tank contains low-temperature fuel (the boiling point of liquid oxygen is -182.96°C, and the boiling point of liquid hydrogen is -252.78°C). Under the induction of the low temperature of the storage tank, it is easy to cause the water vapor outside the storage tank to condense into ice and adhere to the outer wall of the storage tank. , causing a launch accident. [0003] However, the existing coating effect still needs to be improved, so based on this, the technical proposal of the present invention is proposed. Contents of the invention [0004] In ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C09D175/08C09D7/61C09D7/63C08G18/50C08G18/48B05D7/24B05D1/02
CPCC09D175/08C09D7/61C09D7/63C08G18/5015C08G18/4808B05D7/24B05D1/02C08K2003/2241
Inventor 李兴宝王志峰张应宏刘炳申尹文良胡改娟姜媛陈家恒陈博
Owner 北京九天行歌航天科技有限公司