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Antioxidant for aero-engine graphite material and preparation method and application method thereof

An aero-engine and anti-oxidant technology, applied in the direction of graphite, etc., can solve problems such as unfavorable film formation, mechanical wear, and fatigue wear of carbon-graphite sealing materials, and achieve the effects of improving anti-oxidation performance, increasing cross-linking degree, and inhibiting over-curing

Pending Publication Date: 2022-07-05
ZIGONG DONGXIN CARBON CO LTD +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Sodium salt and potassium salt have no anti-friction effect. If used in aviation carbon graphite system, it is not conducive to film formation, and it is easy to cause fatigue wear and mechanical wear of carbon graphite sealing materials

Method used

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  • Antioxidant for aero-engine graphite material and preparation method and application method thereof
  • Antioxidant for aero-engine graphite material and preparation method and application method thereof
  • Antioxidant for aero-engine graphite material and preparation method and application method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0041] 1) Accurately weigh 12 parts of zinc oxide, 2 parts of manganese oxide, 0.2 part of 4-hydroxybutyl, 0.1 part of -aminopropyl, 40.5 parts of phosphoric acid, 19 parts of boric acid, 0.1 part of sodium silicate, 0.1 part of trisodium phosphate by mass parts 0.1 part, 5 parts ammonium hydrogen phosphate, 21 parts water;

[0042] 2) Put the raw materials weighed in step 1) into a constant temperature liquid storage tank at 80°C, stir at a constant speed until it becomes a transparent liquid, prepare a solution with a pH value of 3, and age for 10 hours to obtain an antioxidant;

[0043] 3) Clean the surface of the carbon graphite material to be impregnated until there is no obvious powder residue, put it into a mixed solution of absolute ethanol and water (the mass ratio of sewage ethanol and water is 3:1), and ultrasonically clean it for 0.5h. It was placed in a vacuum drying oven, dried at 110°C for 10h, and set aside;

[0044]4) The carbon-graphite material treated in s...

Embodiment 2

[0052] 1) Accurately weigh 13 parts by mass of zinc oxide, 4 parts of magnesium oxide, 0.1 part of -aminopropyl group, 0.3 part of β-hydroxyethyl group, 45 parts of phosphoric acid, 13 parts of boric acid, 0.4 part of trisodium phosphate, and sodium silicate 0.2 parts, 4 parts ammonium hydrogen phosphate, 20 parts water;

[0053] 2) put the raw materials weighed in step 1) into a constant temperature liquid storage tank, stir at a constant speed until it becomes a transparent liquid, prepare a solution with a pH value of 3, and age for 10h to obtain an antioxidant;

[0054] 3) Clean the surface of the carbon-graphite material to be impregnated until there is no obvious powder residue, put it into a mixed solution of absolute ethanol and water (the mass ratio of absolute ethanol and water is 3:1), and ultrasonically clean it for 0.5h. It was placed in a vacuum drying oven, dried at 110 ° C for 10 h, and set aside;

[0055] 4) The carbon-graphite material treated in step 3) is ...

Embodiment 3

[0062] 1) Accurately weigh in parts by mass 15 parts of zinc oxide, 5 parts of alumina, 0.7 parts of β-hydroxyethyl, 0.3 parts of -aminopropyl, 50 parts of phosphoric acid, 10 parts of boric acid, 0.4 parts of sodium silicate, and aluminum silicate 0.6 parts, 2 parts ammonium hydrogen phosphate, 16 parts water

[0063] 2) put the raw materials weighed in step 1) into a constant temperature liquid storage tank, stir at a constant speed until it becomes a transparent liquid, prepare a solution with a pH value of 3, and age for 10h to obtain an antioxidant;

[0064] 3) Clean the surface of the carbon graphite material to be impregnated until there is no obvious powder residue, put it into a mixed solution of absolute ethanol and water (the mass ratio of sewage ethanol and water is 3:1), and ultrasonically clean it for 0.5h. It was placed in a vacuum drying oven, dried at 110°C for 10h, and set aside;

[0065] 4) The carbon-graphite material treated in step 3) is placed in the an...

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Abstract

The invention discloses an antioxidant for an aero-engine graphite material as well as a preparation method and an application method of the antioxidant, and the antioxidant comprises the following components in parts by weight: 13-20 parts of metal oxide; 0.1-1 part of a high-temperature curing agent; 40-50 parts of phosphoric acid; 10-20 parts of boric acid; 2-5 parts of ammonium hydrogen phosphate; 0.1-1 part of a stabilizer; and 15 to 25 parts of water. The preparation method comprises the following steps: putting the antioxidant components into a constant-temperature liquid storage tank, stirring at a constant speed until the antioxidant components are transparent liquid, preparing a solution with the pH value of 1-5, and standing and aging for 1-20 hours to obtain the antioxidant solution. The antioxidant is good in dipping effect, good in film-forming property and excellent in mechanical property, the high-temperature oxidation resistance of the carbon-graphite material can be effectively improved, it can be guaranteed that the anti-oxidation weight loss rate is smaller than 5% under the condition that the temperature is 650 DEG C * 50 h, and no obvious moisture absorption phenomenon exists.

Description

technical field [0001] The invention belongs to the technical field of carbon-graphite materials, and in particular relates to an antioxidant for aero-engine graphite materials and a preparation method and application method thereof. Background technique [0002] Carbon-graphite materials have unique self-lubricating properties due to their unique layered structure. In its layered crystal structure, carbon atoms form sp 2 A network of hexagonal graphitic layers of hybrid orbitals, which enables strong covalent bonds within the layers and weak van der Waals forces between the layers. This structure determines the low friction coefficient, corrosion resistance, low thermal expansion coefficient, good film formation and excellent processing performance of the graphite layer. [0003] However, because carbon-graphite materials are prone to oxidation failure under high temperature hot oxygen or hot air conditions (>450 °C) (the carbon-graphite sealing material does not have ...

Claims

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Application Information

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IPC IPC(8): C01B32/21
CPCC01B32/21
Inventor 郭世明刘平鄢鹏涂川俊陈赤杨剑宋延礼叶大鑫沈欣夏尚能
Owner ZIGONG DONGXIN CARBON CO LTD