Silicon nitride-based self-lubricating composite material

A composite material, self-lubricating technology, applied in the field of materials, can solve the problems of inability to cope with high and low temperature heavy loads, failure of lubrication mechanism, corrosion of special media, etc., to enrich the lubrication mechanism, reduce the sintering temperature, and improve the effects of poor toughness

Active Publication Date: 2017-08-08
YANSHAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Today, with the rapid development of aerospace technology and space technology, most of the working parts of aerospace equipment are in extreme environments such as ultra-high and ultra-low temperature, vacuum, high speed, and corrosive media. Under such extreme conditions, conventional lubricants are very easy to evaporate, causing The lubrication mechanism fails; plastic-based solid self-lubricating composite materials are only suitable for low-speed, low-load, and low-temperature conditions; metal-based self-lubricating composite materials cannot cope with extreme conditions such as high and low temperature heavy loads, radiation, special medium corrosion, and thermal shock; therefore, It is of practical significance to study a self-lubricating composite material suitable for extreme working conditions in space as a sliding bearing material

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0020] (1) Preparation of mixed powder: 9% TiN according to volume fraction percentage 0.3 , 11% OLC, the rest is α-Si 3 N 4 The proportion of TiN with particle size ≤10μm 0.3 powder, OLC with an average particle size of 5 nm, α-Si with an average particle size of 0.3 μm 3 N 4 Add the planetary ball mill for uniform ball mixing. The mixing process is carried out in an argon atmosphere. Every 100g of mixed powder is added with 0.5ml of alcohol as a dispersant. The ball-to-material ratio is 10:1. Rotate for 30 minutes, rest for 15 minutes, rotate counterclockwise for 30 minutes, rest for 15 minutes, take this as a cycle, and cycle 4 times.

[0021] (2) Pre-compression drying: dry the mixed powder in step (1) and put it into a cylindrical mold with a diameter of 20mm, press 20MPa, hold the pressure for 10s, and then dry the pre-compressed sample in an electric blast drying oven dry 8h

[0022] (3) High-temperature and high-pressure sintering: the pre-pressed sample in step ...

Embodiment 2

[0025] (1) Preparation of mixed powder: 10% TiN according to volume fraction 0.3 , 10% OLC, the rest is α-Si 3 N 4 The proportion of TiN with particle size ≤10μm 0.3 powder, OLC with an average particle size of 5 nm, and α-Si with an average particle size of 0.4 μm 3 N 4 Add the planetary ball mill for uniform ball mixing. The mixing process is carried out in an argon atmosphere. Every 100g of mixed powder is added with 0.5ml of alcohol as a dispersant. The ball-to-material ratio is 10:1. Rotate for 30 minutes, rest for 15 minutes, rotate counterclockwise for 30 minutes, rest for 15 minutes, take this as a cycle, and cycle 4 times.

[0026] (2) Pre-pressing drying: dry the mixed powder in step (1) and put it into a cylindrical mold with a diameter of 20mm, the pressure is 30MPa, and the holding time is 10s. Then dry the pre-pressed sample in an electric blast drying oven for 8 hours

[0027] (3) High-temperature and high-pressure sintering: The pre-pressed sample in step...

Embodiment 3

[0030] (1) Preparation of mixed powder: 11% TiN according to volume fraction percentage 0.3 , 9% OLC, the rest is α-Si 3 N 4 The proportion of TiN with particle size ≤10μm 0.3 powder, OLC with an average particle size of 5 nm, α-Si with an average particle size of 0.5 μm 3 N 4 Add the planetary ball mill for uniform ball mixing. The mixing process is carried out in an argon atmosphere. Every 100g of mixed powder is added with 0.5ml of alcohol as a dispersant. The ball-to-material ratio is 10:1. Rotate for 30 minutes, rest for 15 minutes, rotate counterclockwise for 30 minutes, rest for 15 minutes, take this as a cycle, and cycle 4 times.

[0031](2) Pre-press drying: dry the mixed powder in step (1) and put it into a cylindrical mold with a diameter of 20mm, the pressure is 40MPa, and the holding time is 10s. Then the pre-pressed samples were dried in an electric blast drying oven for 8 h.

[0032] (3) High-temperature and high-pressure sintering: The pre-pressed sample ...

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Abstract

The invention discloses a silicon nitride-based self-lubricating composite material. The silicon nitride-based self-lubricating composite material is prepared from the following chemical components in percentage by volume: 8 to 12 percent of OLC (Onion-like carbon), 8 to 12 percent of TiN0.3 and the balance of alpha-Si3N4. A preparation method of the self-lubricating material comprises the following steps: putting the TiN0.3, the OLC and the alpha-Si3N4 into a planetary ball mill, wherein a ratio of grinding media to material is 10 to 1, and the rotating speed is 300 to 350r / min; clockwise rotating for 30 minutes, stopping for 15 minutes, counterclockwise rotating for 30 minutes, stopping for 15 minutes, and circulating for four cycles; filling a die with mixed powder, maintaining the pressure of 20 to 40MPa for 10s, drying for 8 hours, and then carrying out high-temperature and high-pressure sintering, wherein the pressure is 5GPa; heating to 1480 to 1520 DEG C, keeping the temperature for 14 to 16 minutes, and furnace cooling; grinding a prepared blank, and carrying out deburring treatment to obtain the Si3N4-based self-lubricating composite material. The self-lubricating composite material prepared by the preparation method disclosed by the invention has the advantages of high hardness, high thermal shock resistance, wear resistance, corrosion resistance and the like; the self-lubricating composite material also has higher toughness, and is suitable for being applied to a device material between lubrication-free interfaces at higher temperature.

Description

technical field [0001] The invention belongs to the technical field of materials, in particular to a self-lubricating composite material. Background technique [0002] Ordinary Si 3 N 4 The base material has a series of excellent properties such as high strength and high hardness, thermal shock resistance, spalling fatigue wear, wear resistance, acid and alkali corrosion resistance, but has disadvantages such as low toughness, difficult sintering, and high dry friction coefficient. In order to improve Si 3 N 4 In the case of poor toughness and difficult sintering of ceramics, Zou Bin used nano-TiN powder as the second phase additive to prepare silicon nitride-based nanocomposite ceramic cutting tools. The fracture toughness, Vickers hardness and bending strength were 9.1MPa m 1 / 2 , 15.47GPa and 1079.8MPa, and it is proposed that nano-TiN can reduce the sintering temperature, improve the sintering activity of the powder, and improve the mechanical properties and mechanica...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C04B35/584
CPCC04B35/584C04B2235/3886C04B2235/422C04B2235/5436C04B2235/5454C04B2235/96
Inventor 王明智邹芹赵玉成李晓普柯雨蛟唐虎彭冲
Owner YANSHAN UNIV
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