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A kind of sealing coating for protecting the surface of integral fuel tank of aircraft

A technology for integral fuel tank and sealing coatings, applied in anti-corrosion coatings, epoxy resin coatings, anti-fouling/underwater coatings, etc., can solve the problems that the molecular structure of the sealant is easily eroded by microorganisms, easy to breed mold, and affects the sealing effect, etc. , to achieve the effect of improving extensive adhesion, good anti-mildew and anti-corrosion performance, and fast surface drying speed

Active Publication Date: 2022-02-08
BAIMTEC MATERIAL CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Polysulfide sealants currently mainly include polysulfide sealants, modified polysulfide sealants and polythioether sealants. Such sealants are prone to mold growth under hot and humid conditions, and due to the growth and spread of mold, the sealant The internal molecular structure is easily eroded by microorganisms, resulting in degradation and deterioration, which seriously affects the sealing effect

Method used

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  • A kind of sealing coating for protecting the surface of integral fuel tank of aircraft
  • A kind of sealing coating for protecting the surface of integral fuel tank of aircraft
  • A kind of sealing coating for protecting the surface of integral fuel tank of aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0039] According to the ratio of parts by mass, add 16 parts of hydrogenated carboxylated nitrile rubber, 2.5 parts of fumed silica, 2 parts of epoxy-terminated liquid polysulfide rubber, 4 parts of novolac epoxy resin, and 0.3 parts of iron oxide red to the double rollers in sequence Mix with an open mill, crush evenly after mixing, then add the crushed rubber into the stirring tank, add 74.2 parts of mixed solvent, 0.3 parts of A-Link 599 silane coupling agent, bis-(3- (triethoxysilane) propyl)-disulfide silane coupling agent 0.7 parts, stirred at a stirring speed of 60 rpm for 4 hours until the glue was uniform and then discharged.

Embodiment 2

[0041] According to the ratio of parts by mass, add 10 parts of hydrogenated carboxylated nitrile rubber, 4 parts of fumed silica, 4 parts of epoxy-terminated liquid polysulfide rubber, 1 part of novolac epoxy resin, and 0.5 parts of neodymium oxide into the double-roller opener in sequence. Mixing in the mill, crushing after uniform mixing, and then adding the crushed rubber into the stirring tank, then adding 80.4 parts of mixed solvent, 0.1 part of A-Link 599 silane coupling agent, at 60 rpm Stir at a stirring speed for 4 hours until the glue is uniform and ready to be discharged.

Embodiment 3

[0043] According to the ratio of parts by mass, 10 parts of hydrogenated carboxylated nitrile rubber, 4 parts of fumed silica, 5 parts of epoxy-terminated liquid polysulfide rubber, 1 part of novolac epoxy resin, and 0.5 part of erbium oxide are added to the double-roller opening in sequence. Mixing in the mixer, crushing after uniform mixing, then adding the crushed rubber material into the stirring tank, adding 79 parts of mixed solvent, 0.5 part of A-Link 599 silane coupling agent, at 60 rpm Stir at a stirring speed for 5 hours until the glue is uniform and ready to be discharged.

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Abstract

The invention belongs to the technical field of sealing coatings, and relates to a sealing coating for protecting the surface of an aircraft integral fuel tank. Its main components are hydrogenated carboxylated nitrile rubber, fumed silica, phenolic epoxy resin, tackifier, pigment, coupling agent and mixed solvent. The surface protection and sealing coating of the overall fuel tank of the aircraft proposed by the present invention has extensive adhesion to polysulfide sealants and the base material of the fuel tank and has excellent oil and temperature resistance, so as to protect the overall fuel tank of the aircraft in harsh environments such as humidity, heat, and salt spray. The lower seal is safe and achieves the effect of anti-mildew and anti-corrosion.

Description

technical field [0001] The invention belongs to the technical field of sealing coating preparation, and relates to a sealing coating for protecting the surface of an aircraft integral fuel tank. Background technique [0002] Integral fuel tanks are widely used by various types of aircraft because they can make full use of the space and provide a larger fuel capacity. Anodized aluminum alloy, titanium alloy, galvanized carbon steel, etc. are the main metal materials that constitute the overall fuel tank parts of the aircraft. For the anti-corrosion of such materials, the anti-corrosion primer is usually used to directly cover the metal parts of the fuel tank before forming. Apply protective sealant paint on the surface of the fuel tank after assembly. [0003] Polysulfide sealant is the main non-metallic material of the overall fuel tank of the aircraft. It is mainly used as the sealing material for the bonding surface of the fuel tank, fillet and screws. It is an important ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C09D115/00C09D163/04C09D181/04C09D5/14C09D5/08C09D7/20C09D7/61C09D7/63C09D7/65
CPCC09D115/00C09D5/14C09D5/08C09D7/20C09D7/61C09D7/70C09D7/63C09D7/65C08L2201/08C08L2205/03C08K2003/2272C08K2003/221C08L63/04C08L81/04C08K13/04C08K7/26C08K5/548C08K5/372C08K3/22C08K3/042
Inventor 鲍传磊孙超刘刚秦蓬波吴松华
Owner BAIMTEC MATERIAL CO LTD