Non-Newtonian fuselage deicing and anti-icing fluid and preparation method thereof

A non-Newtonian, anti-icing fluid technology, applied in chemical instruments and methods, other chemical processes, etc., can solve the problem that there is no deicing and anti-icing fluid viscosity and low temperature shear rheology, can not effectively reduce the ice on the surface of the object. Adhesion performance, only meeting the time requirements and other issues, to achieve the effects of excellent shear recovery ability, prolonged liquid freezing failure, and long anti-icing time

Active Publication Date: 2013-04-24
成都民航六维航化有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the formulas of the above-mentioned patents, since each formula is a conventional choice, and no targeted ingredients are added, it cannot effectively reduce the adhesion of ice on the surface of the object, and does not make the deicing and anti-icing fluid have a good performance. The behavior of viscosity and low temperature shear rheology also has a very limited role in improving the anti-icing time, and only meets the time requirements of type II fluids

Method used

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  • Non-Newtonian fuselage deicing and anti-icing fluid and preparation method thereof
  • Non-Newtonian fuselage deicing and anti-icing fluid and preparation method thereof
  • Non-Newtonian fuselage deicing and anti-icing fluid and preparation method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0045] A non-Newtonian airframe deicing and anti-icing fluid is characterized in that it comprises the following components by mass and deionized water:

[0046] 40 ～ 50 parts of freezing point depressants;

[0047] 0.05 ～ 0.6 parts of rheology modifier;

[0048] 0.01 ～ 0.15 parts of anti-icing compound;

[0049] 0.01 ～ 1.5 parts of pH regulator;

[0050] 0.01 ～ 1.5 parts of corrosion inhibitor;

[0051] 0.01 ～ 0.25 parts of dyeing agent;

[0052] 40 ～ 50 parts of deionized water;

[0053] The rheology modifier is a modified carboxylic acid polymer in the form of loose powder, and the rheology modifier consists of 70 parts by mass. ～ 80 parts of at least one unsaturated carboxylic acid, and at least one double-branched structure monomer in the range of 0.5 to 12.5 parts by mass, are obtained by polymerizing in a mixed solvent;

[0054] The unsaturated carboxylic acid comprises acrylic acid, methacrylic acid, α-cyanoacrylic acid, crotonic acid, crotonic acid or ita...

Embodiment 2

[0067] A non-Newtonian airframe deicing and anti-icing fluid is characterized in that it comprises the following components by mass and deionized water:

[0068] 50-60 parts of freezing point depressants;

[0069] 0.6-1.2 parts of rheology modifier;

[0070] 0.15-0.3 parts of anti-icing compound;

[0071] 1.5-3 parts of PH regulator;

[0072] 1.5-3 parts of corrosion inhibitor;

[0073] 0.25 to 0.5 parts of dyeing agent;

[0074] 50-60 parts of deionized water;

[0075] The rheology modifier is a hydrophobically modified carboxylic acid polymer in the form of loose powder, and the rheology modifier is composed of at least one unsaturated carboxylic acid in 80-90 parts by mass, and the range of parts by mass is It is obtained by polymerizing 12.5-25 parts of at least one double-branched monomer in a mixed solvent.

[0076] The unsaturated carboxylic acid is acrylic acid or methacrylic acid.

[0077] The mixed solvent is water and toluene, cyclohexane or ethyl acetate.

...

Embodiment 3

[0089] Examples of rheology modifiers:

[0090]

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Abstract

The invention relates to a deicing and anti-icing fluid, particularly a non-Newtonian fuselage deicing and anti-icing fluid and a preparation method thereof. The non-Newtonian fuselage deicing and anti-icing fluid can reduce adhesion of ice on the object surface to eliminate and prevent icing on the aircraft fuselage surface, and has superlong anti-icing retention time. The non-Newtonian fuselage deicing and anti-icing fluid comprises the following components in parts by mass: 40-60 parts of freezing-point depressant, 0.05-1.2 parts of rheologic modifier, 0.01-0.3 part of anti-icing compounding agent, 0.01-3 parts of pH regulator, 0.01-3 parts of corrosion inhibitor, 0.01-0.5 part of staining agent and 40-60 parts of deionized water. The invention is based on the low-temperature rheologic research, especially aims at the low-temperature operating environment and characteristics of the deicing and anti-icing fluid, and determines the distribution and arrangement of the main chain and branch chain of the rheologic modifier as well as the preparation and acquisition method of the low-temperature conformation. By combining the anti-icing compounding agent, corrosion inhibitor and other assistants in the formula, the prepared deicing and anti-icing fluid has the characteristics of excellent shearing restorability, excellent ice adhesion inhibition capacity at 0 to -20 DEG C, and long anti-icing time.

Description

technical field [0001] The invention relates to a liquid for deicing and anti-icing. Specifically, it relates to a non-Newtonian airframe deicing and anti-icing fluid capable of reducing ice adhesion on the surface of objects, eliminating and preventing ice formation on the surface of an aircraft fuselage, and having super long anti-icing holding time and a preparation method thereof. Background technique [0002] In icy weather conditions, the surface of an aircraft staying on the ground can easily form pollutants such as ice, snow, and frost. These pollutants will not only increase the weight and resistance of the aircraft, but also cause the flight attitude of the aircraft to take off to be difficult to control, and in severe cases, cause air crashes. The most effective way to prevent ground aircraft from icing is to use aircraft deicing and anti-icing fluids. The deicing and anti-icing fluid melts the pollutants such as ice, snow and frost that have accumulated on the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C09K3/18C08F290/06C08F220/06
Inventor 梅拥军韦勇强周洪王航钟祖勤孙传鹏祝军谢麟
Owner 成都民航六维航化有限责任公司
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