CN1586770A - High temperature self compensatiojn lubrication wear resistance material and its preparing method - Google Patents
High temperature self compensatiojn lubrication wear resistance material and its preparing method Download PDFInfo
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- CN1586770A CN1586770A CN 200410060662 CN200410060662A CN1586770A CN 1586770 A CN1586770 A CN 1586770A CN 200410060662 CN200410060662 CN 200410060662 CN 200410060662 A CN200410060662 A CN 200410060662A CN 1586770 A CN1586770 A CN 1586770A
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Abstract
The high temperature self-compensating lubricating wear resistant material includes substrate and solid lubricating particle compounded to the substrate. The substrate is mixed alloy, ceramic and RE element sintered body with sweat gland type structural micropores. The sweat gland type structural micropore has diameter of 0.05-8 micron and consists of internal micropore and penetrating micropore to the surface of the substrate, and the solid lubricating particle is compounded into the sweat gland type structural micropore. The present invention ensures the formation of wear resistant hard phase in the substrate material, and the composite material has its lubricant inside the substrate driven by the friction heat to diffuse toward the friction surface via the sweat gland micropores to realize the self compensating lubrication of the wear resistant material at high temperature.
Description
Technical field
The present invention relates to self-lubricating abrasion-proof material and preparation method thereof, self compensation lubricating and wear-resisting material that particularly uses under the hot environment and preparation method thereof.
Background technology
The design concept of traditional high temperature self-lubricating abrasion-proof material is: kollag is added in as the mixing constituent element forms self-lubricating composite in the high-abrasive material.Because lubricated phase and hard mutual restriction mutually in the material; When increasing lubricant component when improving the lubricity of material, the lubricated mechanical performance and hard wearability mutually that has reduced material mutually; Thereby restricted the performance of element function separately in the material.
In addition, because the porous in the metal sinter adopts infusion process that lubricant impregnation is prepared into the self-lubricating part in metal sinter, be widely used in the engineering field.Yet the micropore in the metal current sintered body is random clearance type micropore, and sintered body can only absorb lubricant (oil) by inhaling the rainbow effect; Therefore, impregnated lubricant can only be a liquid medium; And the high-temperature volatile of liquid medium makes it can't satisfy the thermal extremes job requirement.
Along with the development and the application of clean fuel in hot machine of ceramics processing, the part under the thermal extremes operating mode is learned demands for higher performance to material friction; Therefore, the high temperature self compensation lubricating and wear-resisting material that how to adopt new theory to prepare under the extreme operating condition is a urgent problem in the engineering.
Summary of the invention
Technical problem to be solved by this invention is: provide a kind of and can carry out lubricated high-abrasive material of self compensation and preparation method thereof under worst hot case.
The present invention solves the problems of the technologies described above the technical scheme that is adopted:
High temperature self compensation lubricating and wear-resisting material, it comprises matrix and the kollag particle body that is compounded on the matrix, matrix is alloy, pottery, the rare earth element mixed sintering body with sweat gland type structural micropore; The sweat gland type structural micro-pore diameter is 0.05-8 μ m, and it is made up of micropore in the body and perforation micropore, and micropore connects by connecting micropore and matrix surface in the body, and the bluk recombination of kollag particle is in the sweat gland type structural micropore.
Prepare the method for above-mentioned high temperature self compensation lubricating and wear-resisting material, its preparation methods steps is:
(1) gets by each ingredients weight parts proportioning: alloy powder 40-60 part, titanium carbide powder 25-40 part, yttrium oxide powder 1-2 part, pore creating material powder 4-13 part;
(2) will stir after above-mentioned each component mixing, and the preparation of colding pressing is shaped;
(3) place 1250-1450 ℃ of sintering temperature to make matrix;
(4) cooling;
(5) by vacuum impregnation kollag is flooded in the matrix, make high temperature self compensation lubricating and wear-resisting material by double sintering then.
The operation principle of high temperature self compensation lubricating and wear-resisting material of the present invention is: its matrix is the alloy with sweat gland type structural micropore, pottery, rare earth element mixed sintering body, it can be advanced the bluk recombination of self-lubricating solid particle in the sintered body by infusion process, because matrix and the kollag particle body that is compounded in the matrix sweat gland type micropore have different heat expansion coefficient, make the solid lubrication element that is compounded in the wear-resisting sintered body of sweat gland type under high temperature friction heat-field of force drives, by the sweat gland micropore in the wear-resisting sintered body from interior course diffusion into the surface and enrichment, and at surface formation adsorbed lubricating film, thereby realize the lubricated and wear-resisting functions of its high temperature self compensation.
In the inventive method, sintering after matrix adopting ceramic powders, alloy powder, rare earth element powder and the pore creating material powder is sintered into sweat gland type structural under vacuum; And with the carrier of this matrix sintered body as solid lubrication particle body, by vacuum impregnation solid lubrication particle body is flooded in this sintered body, prepare high-abrasive material of the present invention by double sintering then.Because the interpolation of kollag is behind wear-resisting sintered body sintering among the present invention, advance in the matrix by vacuum impregnation and double sintering are compound, therefore, matrix does not contain kollag component in owing to material mixture ratio in the first time during high temperature sintering and obtains the high abrasion sintered body; Kollag is low with combining more than matrix itself of basal body interface as separate component, therefore be easy in the high temperature friction process to separate out and be enriched in the lubrication friction surface, thereby solved the high-temperature self-lubrication problem of wear-resisting sintered body by the sweat gland type micropore of sintered body.
The inventive method and existing high temperature self-lubricating abrasion-proof material preparation method's the main distinction is: the conventional high-temperature self-lubricating abrasion-proof material is based on and mixes first component method design, be about to the solid lubrication element and be blended in the wear-resisting powder by material component, after sintered body is repressed at high temperature sintering form.The inventive method then is based on the thermal diffusion lubrication principle design of sweat gland type structural, promptly in wear-resisting sintered body matrix preparation process, do not contain the solid lubrication element, and be prepared into the sweat gland type microcellular structure, the solid lubrication element is compounded in the sweat gland type micropore by vacuum impregnation and double sintering, and self-lubricating abrasion-proof material is formed by wear-resisting sintered body of sweat gland type and lubricated particle bluk recombination.
The inventive method is prepared into the sweat gland type microcellular structure with high-abrasive material, and with solid lubrication additive with in the compound sweat gland type micropore that advances this matrix of the form secondary of particulate daughter, make it overcome traditional mixed first legal system and be equipped with the existing solid lubrication additive of self-lubricating abrasion-proof material defective to the damage of material matrix performance in high-temperature sintering process, guaranteed the formation of the wear-resisting hard phase of matrix material; Because the lubricant that this composite can utilize frictional heat to drive in the matrix spreads to friction surface by the sweat gland micropore, therefore, can realize the high temperature self compensation lubricating function of high-abrasive material.
Description of drawings
Fig. 1 is the sweat gland type microcellular structure ideal model figure of high-abrasive material of the present invention
Fig. 2 is the sweat gland type microcellular structure longitudinal section shape appearance figure among the high-abrasive material embodiment of the present invention
Fig. 3 is the sweat gland type microcellular structure cross section shape appearance figure among the high-abrasive material embodiment of the present invention
Fig. 4-10 is the structural representation of the different shape member made with high-abrasive material of the present invention
The specific embodiment
High-abrasive material of the present invention as shown in Figure 1, 2, 3, it comprises matrix and the kollag particle body that is compounded on the matrix, matrix is alloy, pottery, the rare earth element mixed sintering body with sweat gland type structural micropore, the sweat gland type structural micropore is made up of micropore in the body 2 and perforation micropore 1, micropore 2 connects with matrix surface by connecting micropore 1 in the body, and the micro-pore diameter of this sweat gland type structural sintered body is 0.05-8 μ m.The bluk recombination of kollag particle is in the sweat gland type structural micropore.Matrix contains alloy, titanium carbide (ceramic material), yittrium oxide (rare earth element material), and the weight portion proportioning of each component is: alloy 40-60 part, titanium carbide 25-40 part, yittrium oxide 1-2 part.Alloy is the high speed steel or stainless steel.The total pore size volume rate of matrix (annotate: the pore volume rate is the volume of matrix material mesopore and the ratio of matrix material volume) is 20-30%, and the pore volume rate that wherein connects micropore 1 is 10-20%.
Its preparation methods steps is:
(1) gets by each ingredients weight parts proportioning: alloy powder 40-60 part, titanium carbide powder 25-40 part, yttrium oxide powder 1-2 part, calcium carbonate 2-8 part, titantium hydride 4-8 part; (each powder size is: the 200-325 order)
(2) will stir after above-mentioned each component mixing, and through 3-6KN/cm
2The preparation of colding pressing is shaped;
(3) place and made matrix in 1250-1450 ℃ of sintering temperature 1-2 hour;
(4) cooling;
(5) by vacuum (vacuum (0.7-8) * 10
2Pa) dipping floods solid lubrication particle body in the matrix, makes high temperature self compensation lubricating and wear-resisting material by double sintering (at 600-800 ℃ of following sintering 1-2 hour) then.
The weight that each component of matrix is concrete (unit: gram) can be:
| High-speed steel | Stainless steel | Titanium carbide | Yittrium oxide | Calcium carbonate | Titantium hydride | |
| Scheme 1 | ??400 | ??250 | ??20 | ??20 | ??80 | |
| Scheme 2 | ??600 | ??250 | ??10 | ??80 | ??80 | |
| Scheme 3 | ??600 | ??400 | ??20 | ??20 | ??40 | |
| Scheme 4 | ??400 | ??300 | ??10 | ??50 | ??50 | |
| Scheme 5 | ??500 | ??300 | ??20 | ??50 | ??40 |
After each component was mixed, can cold pressing was prepared into the matrix of the different shape shown in Fig. 4-10.
When sintering, burning volatilization temperature by two kinds of pore creating material titantium hydrides and calcium carbonate is poor, make its burning volatilization under 500-600 ℃ and 900-1000 ℃ of temperature respectively, twice pore-creating, make that to have diameter in the sintered body be 0.05-8 μ m, the total pore size volume rate is 20-30%, and the pore volume rate that wherein connects micropore is the sweat gland type microcellular structure of 10-20%, and makes the structure of sweat gland type micropore fixed, is shaped.
Solid lubrication particle body is the ultramicron mixture (the weight portion proportioning is generally: soft metal 40-50 part, molybdenum bisuphide 20-30 part, fluoride 20-30 part) of soft metal, disulphide and fluoride, the granularity of solid lubrication particle body: 1000-1200 order; This solid lubrication particle body immerses in the wear-resisting sintered body of sweat gland type under vacuum, and through 600-800 ℃ double sintering and be compounded in the wear-resisting sintered body.Because the solid lubrication element is in the high temperature friction process, diffuse to friction surface owing to frictional heat-stress field effect by the sweat gland type micropore in the sintered body, amounts of lubrication at friction surface depends on sweat gland type porosity in the wear-resisting sintered body, therefore, solid lubrication particle body burden in the wear-resisting sintered body and porosity have been controlled the lubricated self compensation speed of material in the high temperature friction process.
Because the micropore of this invention sintered body is the sweat gland type microcellular structure by forming after the secondary pore-creating, therefore, when guaranteeing that micropore can satisfy ultra micron daughter immersion, make sintered body have high obdurability, the microhardness in this sintered body can reach HV800-1000; In 800 ℃ working environment, the rate of depreciation of this self-lubricating abrasion-proof material is (2-8) * 10
-6Mm
3/ N.m, coefficient of friction are 0.20-0.35.
Claims (6)
1, a kind of high temperature self compensation lubricating and wear-resisting material is characterized in that: it comprises matrix and the kollag particle body that is compounded on the matrix, and matrix is alloy, pottery, the rare earth element mixed sintering body with sweat gland type structural micropore; The sweat gland type structural micro-pore diameter is 0.05-8 μ m, and it is made up of micropore in the body (2) and perforation micropore (1), and micropore (2) is by connecting micropore (1) and matrix surface perforation in the body, and the bluk recombination of kollag particle is in the sweat gland type structural micropore.
2, high-abrasive material as claimed in claim 1 is characterized in that: ceramic material is a titanium carbide, and the rare earth element material is a yittrium oxide, and the weight portion proportioning of each component of matrix is: alloy 40-60 part, titanium carbide 25-40 part, yittrium oxide 1-2 part.
3, high-abrasive material as claimed in claim 2 is characterized in that: alloy is the high speed steel or stainless steel.
4, high-abrasive material as claimed in claim 1 is characterized in that: the total pore size volume rate in the matrix is 20-30%, and wherein, the pore volume rate that connects micropore (1) is 10-20%.
5, the method for preparation high-abrasive material as claimed in claim 1, it is characterized in that: its preparation methods steps is:
(1) gets by each ingredients weight parts proportioning: alloy powder 40-60 part, titanium carbide powder 25-40 part, yttrium oxide powder 1-2 part, pore creating material powder 4-13 part;
(2) will stir after above-mentioned each component mixing, and the preparation of colding pressing is shaped;
(3) place 1250-1450 ℃ of sintering temperature to make matrix;
(4) cooling;
(5) by vacuum impregnation kollag is flooded in the matrix, make high temperature self compensation lubricating and wear-resisting material by double sintering then.
6, the method for preparation high-abrasive material as claimed in claim 5, it is characterized in that: the pore creating material powder comprises calcium carbonate powder and titanium hydride powders, its weight portion proportioning is: calcium carbonate 2-8 part, titantium hydride 4-8 part.
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| CN 200410060662 CN1275727C (en) | 2004-07-30 | 2004-07-30 | High temperature self compensatiojn lubrication wear resistance material and its preparing method |
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| CN 200410060662 CN1275727C (en) | 2004-07-30 | 2004-07-30 | High temperature self compensatiojn lubrication wear resistance material and its preparing method |
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| CN1586770A true CN1586770A (en) | 2005-03-02 |
| CN1275727C CN1275727C (en) | 2006-09-20 |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102560176A (en) * | 2011-12-29 | 2012-07-11 | 东南大学 | Method for preparing porous metal through gum dipping and sintering |
| CN104969425A (en) * | 2012-12-18 | 2015-10-07 | 滑动环及设备制造有限公司 | Self-lubricating slip ring |
| CN105543521A (en) * | 2015-12-30 | 2016-05-04 | 武汉理工大学 | Ag-Sn-Cu/metal ceramic composite high-temperature lubricating layer material and preparation method thereof |
| CN107520446A (en) * | 2017-08-24 | 2017-12-29 | 武汉理工大学 | High-temperature imitated is born from lubrication hot forming dies materials and preparation method thereof |
| CN109351975A (en) * | 2018-10-31 | 2019-02-19 | 北京工商大学 | A kind of the micropore stainless steel base and its preparation process of physical gaseous phase deposition coating |
| CN111755085A (en) * | 2020-06-23 | 2020-10-09 | 西安科技大学 | High-temperature self-compensation wear-resistant material, design method and preparation method |
| CN114559043A (en) * | 2022-02-22 | 2022-05-31 | 武汉理工大学 | Self-lubricating composite material and preparation process thereof |
-
2004
- 2004-07-30 CN CN 200410060662 patent/CN1275727C/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102560176A (en) * | 2011-12-29 | 2012-07-11 | 东南大学 | Method for preparing porous metal through gum dipping and sintering |
| CN104969425A (en) * | 2012-12-18 | 2015-10-07 | 滑动环及设备制造有限公司 | Self-lubricating slip ring |
| CN105543521A (en) * | 2015-12-30 | 2016-05-04 | 武汉理工大学 | Ag-Sn-Cu/metal ceramic composite high-temperature lubricating layer material and preparation method thereof |
| CN107520446A (en) * | 2017-08-24 | 2017-12-29 | 武汉理工大学 | High-temperature imitated is born from lubrication hot forming dies materials and preparation method thereof |
| CN109351975A (en) * | 2018-10-31 | 2019-02-19 | 北京工商大学 | A kind of the micropore stainless steel base and its preparation process of physical gaseous phase deposition coating |
| CN111755085A (en) * | 2020-06-23 | 2020-10-09 | 西安科技大学 | High-temperature self-compensation wear-resistant material, design method and preparation method |
| CN111755085B (en) * | 2020-06-23 | 2024-02-09 | 西安科技大学 | High-temperature self-compensating wear-resistant material, design method and preparation method |
| CN114559043A (en) * | 2022-02-22 | 2022-05-31 | 武汉理工大学 | Self-lubricating composite material and preparation process thereof |
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|---|---|
| CN1275727C (en) | 2006-09-20 |
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Granted publication date: 20060920 Termination date: 20130730 |