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High-temperature sealing gum capable of being used at 700 DEG C and application method of high-temperature sealing gum

A technology of high-temperature sealing and application method, applied in the direction of adhesives, non-polymer adhesive additives, adhesive additives, etc., can solve the problems of hidden dangers and shadows in transportation, and achieve good application conditions, convenient construction and reliable quality. Effect

Inactive Publication Date: 2020-02-14
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In an aero-engine, there are always gaps between the joint surfaces of its parts. In order to ensure the normal operation of the engine and maintain the normal operating pressure and safety of the system, the joint surfaces must be aligned and sealed to prevent oil leakage, air leakage, water leakage, etc. The sealant is mainly used in parts where the sealing gap is very small, such as the joint surface between the rear mounting edge of the casing and the inner mounting edge of the guide (including the adjusting ring), the joint surface of the inner ring of the guide and the cyclone, and the oil leakage valve (housing, Gaskets, valves) thermocouples, nozzles, pressure sensors and other components; imported sealants are used in the prior art, and imported materials take time to order, produce, and customs, and will be affected to varying degrees by temperature differences; Moreover, the colloid is a fluid, and there are hidden dangers in the transportation process.

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0038] A high-temperature sealant that can be used at 700°C, weigh 57g of sealant, 11.5g of alumina, 17g of titanium dioxide, 6g of iron oxide, and 8.5g of distilled water for use;

[0039] After calcining the alumina at 900°C±20°C for 3 hours, sieve it through a 500-mesh standard sieve, and keep the part under the sieve for later use;

[0040] After calcining titanium dioxide at 300°C±10°C for 3 hours, sieve it through a 300-mesh standard sieve, and keep the under-sieve part for later use;

[0041] Put 57g of sealant in a clean container;

[0042] Mix 11.5g of alumina and 17g of titanium dioxide together, grind them evenly in a mortar, then add 11.5g of alumina, stir evenly to become a viscous colloid;

[0043] Add 6g of iron oxide to 8.5g of distilled water and stir evenly, add the filtrate filtered through a 250-mesh screen into the viscous colloid, stir evenly, and shake it through a medical oscillator for 12min to become a red high-temperature sealant.

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PUM

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Abstract

The invention discloses high-temperature sealing gum capable of being used at 700 DEG C. The high-temperature sealing gum is prepared from the components in percentage by mass: 50%-65% of a sealant, 8%-15% of aluminum oxide, 14%-20% of titanium dioxide, 4%-8% of ferric oxide, and 6%-11% of distilled water. The invention further discloses an application method of the high-temperature sealing gum capable of being used at 700 DEG C. The high-temperature sealing gum has good heat resistance, sealing property and corrosivity and is suitable for sealing of corresponding high-temperature parts of aircraft engines.

Description

technical field [0001] The invention relates to the field of mechanical processing, in particular to a high-temperature sealant that can be used at 700°C and an application method thereof. Background technique [0002] In an aero-engine, there are always gaps between the joint surfaces of its parts. In order to ensure the normal operation of the engine and maintain the normal operating pressure and safety of the system, the joint surfaces must be aligned and sealed to prevent oil leakage, air leakage, water leakage, etc. The sealant is mainly used in parts where the sealing gap is very small, such as the joint surface between the rear mounting edge of the casing and the inner mounting edge of the guide (including the adjusting ring), the joint surface of the inner ring of the guide and the cyclone, and the oil leakage valve (housing, Gaskets, valves) thermocouples, nozzles, pressure sensors and other components; imported sealants are used in the prior art, and imported mater...

Claims

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Application Information

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IPC IPC(8): C09J11/04C09J201/00
CPCC08K2003/2227C08K2003/2241C08K2003/2272C09J11/04C09J201/00C08K3/22
Inventor 王杰徐琪刘翔王景峰南辉
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION