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A kind of coating system for aircraft

A technology for aircraft and coatings, which is applied in the direction of anti-corrosion coatings, epoxy resin coatings, coatings, etc. It can solve the problems of poor surface gloss retention rate and color durability, easy chalking, and harsh coating quality, so as to ensure delivery Joint density and flexibility, improved weather resistance, weight reduction effect

Active Publication Date: 2017-03-08
CHINA NAT OFFSHORE OIL CORP +3
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although the performance of aerospace coatings formed by conventional coating systems can basically meet the needs of various types of aircraft, there are still the following problems: ①Because both the primer coating and the top coating contain a large amount of pigments and fillers with high density, conventional coatings The aircraft coating formed by the system is heavy, which increases the weight of the aircraft and thus increases the fuel consumption of the aircraft; ②In order to obtain a high-gloss and smooth surface for each coating, the drying process of the coating must be slowed down, and it takes about 5 ~7 hours, therefore, the construction interval is long, and at the same time, due to the thick dry film thickness of the surface layer, it must go through two constructions to reach the specified thickness, so the overall coating efficiency is low; ③Due to the gloss of the final aircraft coating The degree and color presentation are directly related to the coating effect of the surface coating. Therefore, once defects such as orange peel, sagging, pinholes, and sandy surfaces appear on the surface, the glossiness of the final aircraft coating will be greatly reduced. At the same time, the accuracy of its color rendering will also be affected. Therefore, there are strict requirements on the quality of the coating; ④Since the surface layer is in direct contact with the atmospheric environment, it is easily pulverized due to long-term erosion by ultraviolet light, oxygen in the air and rainwater , loss of gloss, while the surface gloss retention rate and color durability of conventional coating systems are relatively poor

Method used

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  • A kind of coating system for aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] Embodiment 1 prepares the component A1 of anticorrosion coloring primer

[0033] The components of the anti-corrosion coloring primer of the aviation vehicle coating system of the present invention A1 and their mass percentages are as follows: hydrogenated epoxy resin 15%~30%, modified resin 2%~10%, coloring pigment 10%-20%, environment-friendly anti-corrosion pigment 10%-20%, filler 5-15%, auxiliary agent 0.5%-1%, and the balance is composed of solvent.

[0034] (1) Preparation of raw materials

[0035] Prepare raw materials according to the ratio in Table 1.

[0036] The components and their mass percentages of Example 1 component A1 are as follows: 17.0% hydrogenated epoxy resin, 5.0% modified resin, 18.5% colored pigment, 15.5% environmentally friendly anti-corrosion pigment, 8.5% filler, auxiliary agent 0.9%, the solvent is 34.6% composition. The specific formula is shown in Table 1.

[0037] Table 1

[0038]

[0039]

[0040]Note: ST-3000 is hydrogenate...

Embodiment 2

[0043] Embodiment 2 prepares the component B1 of anticorrosion coloring primer

[0044] The components of the component B1 of the anti-corrosion coloring primer of the aircraft coating system of the present invention and their mass percentages are as follows: 3% to 15% of liquid epoxy resin, 5% of polyamines with primary amine groups ~25%, the balance is solvent.

[0045] (1) Preparation of raw materials

[0046] Prepare the raw materials according to the ratio in Table 2.

[0047] Example 2 The components and mass percentages of component B1 are as follows: 8.1% liquid epoxy resin, 22.6% polyamine with primary amine groups, and 69.3% solvent. The specific formula is shown in Table 2.

[0048] Table 2

[0049]

[0050]

[0051] (2) Preparation method

[0052] In the reaction kettle, add the polyamine and solvent with primary amino groups prepared in step (1) according to the formula amount in Table 2, and heat up to 60°C while stirring, then start to add the formula ...

Embodiment 3

[0053] Embodiment 3 prepares component A2

[0054] Each component of the component A2 of the weather-resistant transparent surface coating of the coating system for aircraft of the present invention and its mass percentage are as follows: polyol resin 50% ~ 80%, auxiliary agent 1% ~ 4%, the balance is solvent ;

[0055] (1) Preparation of raw materials

[0056] Prepare the raw materials according to the ratio in Table 3.

[0057] The components and their mass percentages of Example 3 component A2 are as follows: 71.4% polyol resin, 2.1% additives, and 26.5% solvent. The specific formula is shown in Table 3.

[0058] table 3

[0059]

[0060] Note: PE-6 is a polyester polyol resin (solid content: 70wt%, hydroxyl content: 6.0wt%) produced by CNOOC Changzhou Environmental Protection Coatings Co., Ltd.; TINUVIN 1130 is a benzotriazole UV absorber produced by BASF TINUVIN 292 is a hindered amine (HAL) UV light stabilizer produced by BASF; EFKA-3777 is a modified polyacrylate...

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Abstract

The invention relates to a coating system for an aerial aircraft. The coating system consists of an anti-corrosion coloring bottom coating and a weather-resistant transparent surface course coating matched in use, wherein the bottom coating consists of a component A1 and a component B1 in a mass ratio of (4-6): 1 and the surface course coating consists of a component A2 and a component B2 in a mass ratio of (1-4): 1; the component A1 comprises 15-30% of hydrogenated terpinene-maleic ester type epoxy resin, 2-10% of modified resin, 10-20% of coloring pigments, 10-20% of an environment-friendly anti-corrosion pigment, 5-15% of filler, 0.5-1% of auxiliaries and the balance of a solvent; the component B1 comprises 3-15% of liquid epoxy resin, 5-25% of polyamine with a primary amine and the balance of a solvent; the component A2 comprises 50-80% of polyhydric alcohol resin, 1-4% of auxiliaries and the balance of a solvent; and the component B2 comprises 60-90% of aliphatic polyisocyanate and the balance of a solvent. The coating system is light, good in comprehensive performance and time-saving in construction.

Description

technical field [0001] The invention relates to a paint system for aircraft, in particular to a paint system for aircraft with longer color and lighter weight. Background technique [0002] At present, conventional paint systems for aerospace vehicles are composed of anti-corrosion primers and colored top coats. Usually, the dry film thickness of the bottom layer formed by the primer paint ranges from about 15 to 25 μm, and the dry film thickness of the surface layer formed by the top coat paint ranges from about 50 to 80 μm. Although the performance of aerospace coatings formed by conventional coating systems can basically meet the needs of various types of aircraft, there are still the following problems: ①Because both the primer coating and the top coating contain a large amount of pigments and fillers with high density, conventional coatings The aircraft coating formed by the system is heavy, which increases the weight of the aircraft and thus increases the fuel consump...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C09D163/00C09D5/08C09D7/12
CPCC08K3/04C08K3/22C08K3/32C08K3/34C08K5/1515C08K13/02C08K2003/2241C08K2003/321C08K2003/327C09D5/08C09D7/61C09D163/00
Inventor 周如东王李军陆文明赵宝华朱亚君李文凯王留方
Owner CHINA NAT OFFSHORE OIL CORP
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