CN112156956A - Process method for increasing hydrophilicity of metal surface of gas turbine air inlet system - Google Patents
Process method for increasing hydrophilicity of metal surface of gas turbine air inlet system Download PDFInfo
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- CN112156956A CN112156956A CN202010959799.2A CN202010959799A CN112156956A CN 112156956 A CN112156956 A CN 112156956A CN 202010959799 A CN202010959799 A CN 202010959799A CN 112156956 A CN112156956 A CN 112156956A
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- base material
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- solution
- resin
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D7/00—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
- B05D7/14—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials to metal, e.g. car bodies
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D3/00—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials
- B05D3/02—Pretreatment of surfaces to which liquids or other fluent materials are to be applied; After-treatment of applied coatings, e.g. intermediate treating of an applied coating preparatory to subsequent applications of liquids or other fluent materials by baking
- B05D3/0254—After-treatment
- B05D3/0272—After-treatment with ovens
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D5/00—Processes for applying liquids or other fluent materials to surfaces to obtain special surface effects, finishes or structures
- B05D5/04—Processes for applying liquids or other fluent materials to surfaces to obtain special surface effects, finishes or structures to obtain a surface receptive to ink or other liquid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D2502/00—Acrylic polymers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D2504/00—Epoxy polymers
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- Life Sciences & Earth Sciences (AREA)
- Engineering & Computer Science (AREA)
- Wood Science & Technology (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
Abstract
A process for increasing the hydrophilicity of a metal surface of an air intake system of a gas turbine engine, the process comprising the steps of: (1) diluting an alcohol-soluble epoxy acrylic resin material with an ethanol solution to obtain a resin solution; (2) putting the metal base material into a container filled with resin solution, completely immersing the metal base material into the solution, and taking out after immersing for 2-3 minutes; (3) standing, shaking or shaking to make the excessive solution on the metal substrate fall off, and placing in an environment with room temperature of 50 ℃ for 20-30 minutes to volatilize ethanol on the surface of the metal substrate, and observing that a layer of white resin is on the surface of the metal; (4) and then the metal base material is placed in an oven at the temperature of 150-200 ℃ for heating and curing for 2-3 hours, after the metal base material is completely dried, the metal base material is cooled and taken out, and the resin is transparent after the metal base material is completely cured, so that the hydrophilic metal base material is obtained. The invention greatly improves the hydrophilicity of the metal by coating treatment on the surface of the metal.
Description
Technical Field
The invention relates to a process method for increasing the hydrophilicity of the metal surface of an air inlet system of a gas turbine.
Background
During the working process of the marine gas turbine, a large amount of fresh air needs to be continuously sucked from the atmosphere through the air compressor and compressed, the compressed air enters the combustion chamber to be mixed with the sprayed fuel and then combusted, and high-temperature gas generated after combustion pushes turbine blades to enable the turbine to rotate at a high speed and drive the propeller to work. Because the water mist content in the air of the marine environment is high, the water in the air is evaporated after compression, salt in the air can be separated out from the water and condensed, and part of the salt is adhered to the surface of the blade to corrode the blade and destroy the surface molded line of the blade, so that the performance of the gas compressor is reduced, the power of the gas turbine is reduced, and the performance and the service life of the gas turbine are influenced. Therefore, in order to ensure the intake quality of gas turbines and the like to meet design requirements, an air intake system is arranged at the air inlet of the combustion engine as an essential important component, and the aim of the air intake system is to filter and separate moisture and other impurities in the air.
Disclosure of Invention
The present invention is directed to a process for increasing the hydrophilicity of a metal surface of an air intake system of a gas turbine, so as to solve the above problems in the background art, and the hydrophilicity of the metal is greatly increased by performing a coating process on the surface of a metal substrate, so that the probability of capturing moisture when the moisture passes through the metal surface is greatly increased, and thus, the moisture in the air is separated.
The technical scheme adopted for achieving the aim is that the technological method for increasing the hydrophilicity of the metal surface of the gas turbine air inlet system comprises the following steps:
(1) diluting an alcohol-soluble epoxy acrylic resin material with an ethanol solution to obtain a resin solution;
(2) putting the metal base material into a container filled with resin solution, completely immersing the metal base material into the solution, and taking out after immersing for 2-3 minutes;
(3) standing, shaking or shaking to make the excessive solution on the metal substrate fall off, and placing in an environment with room temperature of 50 ℃ for 20-30 minutes to volatilize ethanol on the surface of the metal substrate, and observing that a layer of white resin is on the surface of the metal;
(4) and then the metal base material is placed in an oven at the temperature of 150-200 ℃ for heating and curing for 2-3 hours, after the metal base material is completely dried, the metal base material is cooled and taken out, and the resin is transparent after the metal base material is completely cured, so that the hydrophilic metal base material is obtained.
Further, the volume ratio of the alcohol-soluble epoxy acrylic resin material in the step (1) to the ethanol solution is 4: 6 to 3: 7 to obtain a resin solution.
Advantageous effects
Compared with the prior art, the invention has the following advantages.
1. The invention obtains better hydrophilic performance than the original metal surface by coating the resin coating on the metal surface, thereby greatly improving the trapping efficiency of the moisture in the air.
2. The resin coating is a macromolecular organic matter, does not react with salt mist chemically, has better corrosion resistance than common metal and has longer service life.
Detailed Description
The present invention will be further described with reference to the following examples.
A process for increasing the hydrophilicity of a metal surface of an air intake system of a gas turbine engine, the process comprising the steps of:
(1) diluting an alcohol-soluble epoxy acrylic resin material with an ethanol solution to obtain a resin solution;
(2) putting the metal base material into a container filled with resin solution, completely immersing the metal base material into the solution, and taking out after immersing for 2-3 minutes;
(3) standing, shaking or shaking to make the excessive solution on the metal substrate fall off, and placing in an environment with room temperature of 50 ℃ for 20-30 minutes to volatilize ethanol on the surface of the metal substrate, and observing that a layer of white resin is on the surface of the metal;
(4) and then, placing the metal base material in an oven at the temperature of 150-200 ℃ for heating and curing for 2-3 hours, cooling and taking out after the metal base material is completely dried, and obtaining the hydrophilic metal base material after the resin is completely cured and transparent.
The volume ratio of the alcohol-soluble epoxy acrylic resin material in the step (1) to the ethanol solution is 4: 6 to 3: 7 to obtain a resin solution.
Example 1
A process for increasing the hydrophilicity of a metal surface of an air intake system of a gas turbine engine, the process comprising the steps of:
(1) mixing an alcohol-soluble epoxy acrylic resin material and an ethanol solution according to a volume ratio of 4: 6, diluting to obtain a resin solution;
(2) putting the metal base material into a container filled with resin solution, completely immersing the metal base material into the solution, and taking out after immersing for 2 minutes;
(3) standing, shaking or shaking to make the excessive solution on the metal substrate fall off, and placing in an environment with room temperature of 50 ℃ for 20 minutes to volatilize ethanol on the surface of the metal substrate, and observing that a layer of white resin is on the surface of the metal;
(4) and then placing the metal base material in an oven at 200 ℃ for heating and curing for 2 hours, cooling and taking out after the metal base material is completely dried, and obtaining the hydrophilic metal base material after the resin is completely cured and transparent.
Example 2
A process for increasing the hydrophilicity of a metal surface of an air intake system of a gas turbine engine, the process comprising the steps of:
(1) mixing an alcohol-soluble epoxy acrylic resin material and an ethanol solution according to a volume ratio of 3: 7, diluting to obtain a resin solution;
(2) putting the metal base material into a container filled with resin solution, completely immersing the metal base material into the solution, and taking out after immersing for 3 minutes;
(3) standing, shaking or shaking to make the excessive solution on the metal substrate fall off, and placing in an environment with room temperature of 50 ℃ for 30 minutes to volatilize ethanol on the surface of the metal substrate, and observing that a layer of white resin is on the surface of the metal;
(4) and then placing the metal base material in an oven at 150 ℃ for heating and curing for 3 hours, cooling and taking out after the metal base material is completely dried, and obtaining the hydrophilic metal base material after the resin is completely cured and transparent.
Claims (2)
1. A process for increasing the hydrophilicity of a metal surface of an air intake system of a gas turbine engine, the process comprising the steps of:
(1) diluting an alcohol-soluble epoxy acrylic resin material with an ethanol solution to obtain a resin solution;
(2) putting the metal base material into a container filled with resin solution, completely immersing the metal base material into the solution, and taking out after immersing for 2-3 minutes;
(3) standing, shaking or shaking to make the excessive solution on the metal substrate fall off, and placing in an environment with room temperature of 50 ℃ for 20-30 minutes to volatilize ethanol on the surface of the metal substrate, and observing that a layer of white resin is on the surface of the metal;
(4) and then the metal base material is placed in an oven at the temperature of 150-200 ℃ for heating and curing for 2-3 hours, after the metal base material is completely dried, the metal base material is cooled and taken out, and the resin is transparent after the metal base material is completely cured, so that the hydrophilic metal base material is obtained.
2. The process for increasing the hydrophilicity of the metal surface of the gas turbine air intake system according to claim 1, wherein the alcohol-soluble epoxy acrylic resin material and the ethanol solution in the step (1) are mixed in a volume ratio of 4: 6 to 3: 7 to obtain a resin solution.
Priority Applications (1)
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CN202010959799.2A CN112156956A (en) | 2020-09-14 | 2020-09-14 | Process method for increasing hydrophilicity of metal surface of gas turbine air inlet system |
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CN202010959799.2A CN112156956A (en) | 2020-09-14 | 2020-09-14 | Process method for increasing hydrophilicity of metal surface of gas turbine air inlet system |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20130074206A (en) * | 2011-12-26 | 2013-07-04 | 주식회사 포스코 | Method of dispersing diamond in resin solution and surface-treated steel sheet by using the resin composition |
CN104353598A (en) * | 2014-09-30 | 2015-02-18 | 广西大学 | Method for preparing transparent super-oleophobic coating on metal surface |
CN106753012A (en) * | 2016-12-29 | 2017-05-31 | 成都中节能领航科技股份有限公司 | A kind of hydrophily antifog film and preparation method thereof |
CN107987232A (en) * | 2017-11-30 | 2018-05-04 | 广东海特高新材料有限公司 | Water-soluble quantum epoxy-acrylate emulsion and its preparation method and application |
-
2020
- 2020-09-14 CN CN202010959799.2A patent/CN112156956A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20130074206A (en) * | 2011-12-26 | 2013-07-04 | 주식회사 포스코 | Method of dispersing diamond in resin solution and surface-treated steel sheet by using the resin composition |
CN104353598A (en) * | 2014-09-30 | 2015-02-18 | 广西大学 | Method for preparing transparent super-oleophobic coating on metal surface |
CN106753012A (en) * | 2016-12-29 | 2017-05-31 | 成都中节能领航科技股份有限公司 | A kind of hydrophily antifog film and preparation method thereof |
CN107987232A (en) * | 2017-11-30 | 2018-05-04 | 广东海特高新材料有限公司 | Water-soluble quantum epoxy-acrylate emulsion and its preparation method and application |
Non-Patent Citations (3)
Title |
---|
方志刚: "《舰船防腐防漏工程》", 31 December 2017, 国防工业出版社 * |
机械工程手册、电机工程手册编辑委员会: "《电机工程手册 试用本 第24篇 高压开关设备》", 30 September 1979, 机械工业出版社 * |
王霞,杨帆: "《现代建筑涂料:树脂合成与配方设计》", 30 September 2005, 上海交通大学出版社 * |
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