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CN111139475A - Preparation of self-lubricating coating suitable for middle-low temperature air bearing journal - Google Patents

Preparation of self-lubricating coating suitable for middle-low temperature air bearing journal Download PDF

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Publication number
CN111139475A
CN111139475A CN201910602877.0A CN201910602877A CN111139475A CN 111139475 A CN111139475 A CN 111139475A CN 201910602877 A CN201910602877 A CN 201910602877A CN 111139475 A CN111139475 A CN 111139475A
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China
Prior art keywords
coating
powder
self
ball
particle size
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Pending
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CN201910602877.0A
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Chinese (zh)
Inventor
丁春华
李�浩
付冬梅
刘艳
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Yancheng Baisheng Machinery Co ltd
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Yancheng Baisheng Machinery Co ltd
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Priority to CN201910602877.0A priority Critical patent/CN111139475A/en
Publication of CN111139475A publication Critical patent/CN111139475A/en
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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C26/00Coating not provided for in groups C23C2/00 - C23C24/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/06Bearings not otherwise provided for with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention discloses a preparation method of a self-lubricating coating suitable for a middle-low temperature (room temperature-450 ℃) air bearing journal. Firstly, Cr is mixed according to the weight ratio2O3: 5% -20%, graphite powder: 15% -20%, CaF2: 1% -5% of nano MoS2: 1 to 3 percent of NiCr alloy powder (80/20) and the balance. And ball milling the mixture by adopting a ball milling process to obtain mixed powder with uniformly distributed components. The powder is prepared into slurry to be coated on the surface of a shaft neck, after the coating is dried, the density of the coating is improved by adopting a cold isostatic pressing method, induction sintering is carried out for 1-2 hours in vacuum or nitrogen protective atmosphere, and a high-temperature-resistant self-lubricating coating with fine and uniform microstructure is obtained after sintering. The friction and wear performance of the self-lubricating coating prepared by the invention at room temperature of 450 ℃ is obviously superior to that of the existing self-lubricating coating.

Description

Preparation of self-lubricating coating suitable for middle-low temperature air bearing journal
Technical Field
The invention belongs to the field of medium and low temperature friction and wear materials, and particularly relates to a preparation method of a medium and low temperature (room temperature-450 ℃) self-lubricating coating.
Background
At present, the elastic foil aerodynamic bearing has been successfully applied to high-speed rotating machines, such as air refrigerators, auxiliary energy units, various small turbo compressors and aviation machines, that is, the foil aerodynamic bearing has been well applied to both civil and military fields. One of the key technologies in foil aerodynamic bearing technology is start-stop lubrication. During normal high speed operation, the bearing is supported on a thin film of air generated by itself and therefore does not wear, but at start-up and shut-down of the shaft the foils rub against the journal, inevitably resulting in wear. The air bearing has failed when the foil wears more than 25% of its thickness and when the shaft wears more than 0.025 m. High-temperature oxidation resistance, high-temperature corrosion resistance and basic mechanical strength
Therefore, such bearings often require the use of self-lubricating coatings, such as those provided on the journal. In order to improve the frictional wear performance and the mechanical property of the coating, how to realize the coating with low porosity and greatly improved medium and low temperature lubricating property of the coating is the key of the problem.
Disclosure of Invention
In view of the above, the invention aims to provide a preparation method of a self-lubricating coating with high medium-low temperature lubricating performance.
In order to achieve the purpose, the preparation method adopted by the invention comprises the following steps: firstly, NiCr with the purity of more than 99.0 percent and the particle size of 30-200 mu m, graphite powder and Cr are mixed2O3、CaF2、MoS2Powder of Cr2O3: 5% -20%, graphite powder: 15% -20%, CaF2: 1% -5% of nano MoS2: 1% -3%, the rest is NiCr. Ball-milling the mixture for 3-5 hours by a high-energy ball mill under the conditions that the ball-material ratio is 8-10: 1 and the rotating speed is 800-1200rps and under the protection of nitrogen, so that the powder is uniformly mixed, and the composite powder with the particle size of less than 20 mu m is ball-milled. Adding polyvinyl alcohol (1.5-3.0 wt%) as binder into the above composite powder, and mixing with alcohol (75 wt% of alcohol and 25 wt% of water) at a weight ratio of 8-10: 1Slurry, coating the prepared slurry on the surface of the shaft neck to form a coating, and then drying the coating at the temperature of 100-120 ℃, wherein the drying time is 0.5-1.0 hour. Then, the coating of the shaft neck is processed for 5 to 10 minutes by a cold isostatic pressing method under the condition of 50 to 70 Mpa. Finally, sintering the coating subjected to cold isostatic pressing for 1-2 hours at the temperature of 900-1100 ℃ under the vacuum condition or the protection of nitrogen.
The invention adopts graphite powder as a lubricating phase, the graphite powder has good self-lubricating property at room temperature of 450 ℃ below zero and very low cost, the granularity of the powder after high-energy ball milling is less than 20 mu m, and the active energy of the surface of the powder is higher and the sintering property is better. Moreover, the self-lubricating alexandrite ink powder and CaF can be prepared under certain ball milling conditions2Particle size of less than 5 μm, nano MoS2The particle size is only 50-100nm, so that the lubricating phase of the coating prepared by sintering is fine and is uniformly distributed.
Detailed Description
Example 1: firstly, NiCr with the purity of more than 99.0 percent and the particle size of 30-200um, graphite powder and Cr are mixed2O3、CaF2、MoS2Powder of Cr2O3: 10%, graphite powder: 20% of CaF2: 1% of nano MoS2: 1.5 percent and the balance of NiCr. And (3) mixing the mixture by a high-energy ball mill at a ball-to-material ratio of 10: 1, ball milling for 3 hours under the conditions that the diameter of a GCr15 steel ball is 5mm and the rotating speed is 1200rpm and under the protection of nitrogen, uniformly mixing the powder, and carrying out ball milling on the powder to obtain composite powder with the particle size of less than 10 mu m, wherein Cr is2O3、CaF2Has a particle size of less than 5 μm and a nano MoS2The particle size is 50-100 nm. Adding polyvinyl alcohol with the total weight of 3 percent into the composite powder as a binder, mixing the mixture with alcohol (the components are 75 percent of alcohol content and 25 percent of water) according to the weight ratio of 8: 1, stirring the mixture to prepare slurry, coating the prepared slurry on the surface of a shaft neck to form a coating, and then drying the coating for 0.5 hour at the temperature of 100 ℃. Processing the shaft neck coating for 10 minutes under the condition of 50Mpa by adopting a cold isostatic pressing method; finally sintering the cold isostatic pressed coating at 900 ℃ for 3 hours under the vacuum condition or under the protection of nitrogenIt is just needed.
Example 2: firstly, NiCr with the purity of more than 99.0 percent and the particle size of 30-200um, graphite powder and Cr are mixed2O3、CaF2、MoS2Powder of Cr2O3: 15%, graphite powder: 15% of CaF2: 3% of nano MoS2: 2 percent, and the balance of NiCr. Ball-milling the mixture for 2 hours by using a high-energy ball mill under the conditions that the ball-material ratio is 9: 1, the diameter of a GCr15 steel ball is 5mm, the rotating speed is 900rpm and under the protection of inert gas, uniformly mixing the powder, and ball-milling the powder into composite powder with the particle size of less than 15 mu m, wherein Cr is contained in the composite powder2O3、CaF2Has a particle size of less than 5 μm and a nano MoS2The particle size is 50-100 nm. Adding polyvinyl alcohol accounting for 3 percent of the total weight into the composite powder as a binder, mixing the powder with alcohol (the components are 75 percent of alcohol content and 25 percent of water) according to the weight ratio of 10: 1, stirring the mixture to prepare slurry, coating the prepared slurry on the surface of a shaft neck to form a coating, and then drying the coating for 1.0 hour at the temperature of 120 ℃. Treating the shaft neck coating for 7 minutes under the condition of 60Mpa by adopting a cold isostatic pressing method; and finally sintering the cold isostatic pressed coating for 2 hours at 1000 ℃ under the vacuum condition or the protection of nitrogen.
Example 3: firstly, NiCr and Cr with the purity of more than 99.0 percent and the particle size of 30-200um are mixed2O3、CaF2、Ag、MoS2Powder of Cr2O3: 20%, graphite powder: 17% of CaF2: 2% of nano MoS2: 3 percent, and the balance of NiCr. Ball-milling the mixture for 3 hours by using a high-energy ball mill under the conditions that the ball-material ratio is 8: 1 and the rotating speed is 800rpm and protecting with inert gas to uniformly mix the powder, and ball-milling the powder into composite powder with the particle size of less than 10 mu m, wherein Cr is2O3、CaF2Has a particle size of less than 5 μm and a nano MoS2The particle size is 50-100 nm. Adding polyvinyl alcohol accounting for 3 percent of the weight of the composite powder into the composite powder as a binder, mixing the mixture with water or alcohol according to the weight ratio of 9: 1, stirring the mixture to prepare slurry, coating the prepared slurry on the surface of a shaft neck to form a coating, and then heating the coating at 110 DEG CThe coating was dried for 45 minutes under the conditions of (1). And (3) treating the journal coating for 5 minutes under the condition of 70Mpa by adopting a cold isostatic pressing method, and finally sintering the cold isostatic pressed coating for 1 hour at 1050 ℃ under the vacuum condition or under the protection of nitrogen.
The composite powder is sintered, and Cr in the coating2O3Graphite powder, CaF2Nano MoS with particle less than 5 micron2The particle size is 50-100nm and these components are uniformly distributed in the matrix NiCr alloy. Tests show that the coating of the invention is suitable for medium and low temperature, wherein the Cr is2O3(5% -20%), graphite powder (15% -20%), CaF2(1% -5%) and nano MoS2The weight ratio of (1-3%) and the balance of NiCr is proper, and the performance of the obtained lubricating coating in the formula range is superior to that of the existing PS304 coating. Test data show that the abrasion loss is reduced by 25 percent compared with the existing PS304 coating at room temperature of 450 ℃, the strength is improved by 30 percent, and the microhardness is improved by 40 percent, which has great significance for prolonging the service life of the foil bearing and reducing the maintenance cost.

Claims (1)

1. A preparation method suitable for a medium-low temperature self-lubricating coating is characterized by comprising the following steps:
1) firstly, a mixture with a purity of more than 99.0% and a particle size of 30-200 μm: NiCr, Cr2O3Graphite powder, CaF2And nano MoS with purity of more than 99.0 percent2Powder, according to: cr (chromium) component2O3: 5% -20%, graphite powder: 15% -20%, CaF2: 1% -5% of nano MoS2: 1% -3%, the balance of NiCr by weight to form a mixture, wherein the nano MoS2The particle size is 50-100 nm;
2) ball-milling the mixture for 3-5 hours by a high-energy ball mill under the conditions of ball-material ratio of 8-10: 1, rotation speed of 800-1200rps and nitrogen protection to uniformly mix the powder, and ball-milling the powder to form composite powder with the particle size of less than 20 mu m, wherein after ball-milling: graphite powder and Cr2O3、CaF2Has a particle size of less than 5 μm;
3) adding water-soluble micron-sized powdery polyvinyl alcohol which is 1.5-3.0% of the total weight of the composite powder as a binder, mixing the mixture with alcohol with the concentration of 75% according to the weight ratio of the composite powder to the alcohol of 8-10: 1, stirring to prepare slurry, coating the prepared slurry on the surface of a shaft neck to form a coating, and drying the coating at the temperature of 100-120 ℃ for 0.5-1.0 hour; at the moment, the alcohol and the water in the coating are completely volatilized;
4) treating the journal coating for 5-10 minutes under the condition of 50-70Mpa by adopting a cold isostatic pressing method, and finally sintering the journal coating treated by the cold isostatic pressing method for 1-2 hours at the temperature of 900-1100 ℃ under the vacuum condition or the nitrogen protection atmosphere; wherein, in the sintering process, the melting point of the polyvinyl alcohol is only 230 ℃, and in the sintering process of 900-1100 ℃, the polyvinyl alcohol in the coating is completely volatilized.
CN201910602877.0A 2019-07-04 2019-07-04 Preparation of self-lubricating coating suitable for middle-low temperature air bearing journal Pending CN111139475A (en)

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Citations (8)

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Publication number Priority date Publication date Assignee Title
US5866518A (en) * 1997-01-16 1999-02-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Self-lubricating composite containing chromium oxide
CN1613981A (en) * 2004-09-13 2005-05-11 西安交通大学 Paillon air bearing high-temperature resistant nanometer composite lubricating coating and preparation thereof
CN1727420A (en) * 2005-07-11 2006-02-01 西安交通大学 Method for preparing self-lubricating coat in use for high temperature
CN102041466A (en) * 2010-07-30 2011-05-04 中国科学院金属研究所 High-performance high temperature solid self-lubricating coating and preparation method thereof
US8753417B1 (en) * 2010-03-18 2014-06-17 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration High temperature solid lubricant coating for high temperature wear applications
CN105986147A (en) * 2016-07-26 2016-10-05 中国科学院兰州化学物理研究所 Nickel base self-lubricating composite material with wide temperature range and preparation method of composite material
CN106086526A (en) * 2016-07-26 2016-11-09 中国科学院兰州化学物理研究所 A kind of high temperature resistant wide temperature range self-lubricating composite and preparation method thereof
CN108441734A (en) * 2018-03-16 2018-08-24 南京航空航天大学 A kind of WC NEW TYPE OF COMPOSITEs lubricant coating and preparation method thereof

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5866518A (en) * 1997-01-16 1999-02-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Self-lubricating composite containing chromium oxide
CN1613981A (en) * 2004-09-13 2005-05-11 西安交通大学 Paillon air bearing high-temperature resistant nanometer composite lubricating coating and preparation thereof
CN1727420A (en) * 2005-07-11 2006-02-01 西安交通大学 Method for preparing self-lubricating coat in use for high temperature
US8753417B1 (en) * 2010-03-18 2014-06-17 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration High temperature solid lubricant coating for high temperature wear applications
CN102041466A (en) * 2010-07-30 2011-05-04 中国科学院金属研究所 High-performance high temperature solid self-lubricating coating and preparation method thereof
CN105986147A (en) * 2016-07-26 2016-10-05 中国科学院兰州化学物理研究所 Nickel base self-lubricating composite material with wide temperature range and preparation method of composite material
CN106086526A (en) * 2016-07-26 2016-11-09 中国科学院兰州化学物理研究所 A kind of high temperature resistant wide temperature range self-lubricating composite and preparation method thereof
CN108441734A (en) * 2018-03-16 2018-08-24 南京航空航天大学 A kind of WC NEW TYPE OF COMPOSITEs lubricant coating and preparation method thereof

Non-Patent Citations (1)

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Title
丁春华等: "耐高温自润滑材料PM304的磨损性能", 《稀有金属材料与工程》 *

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Application publication date: 20200512