CN101736279B - Hypersonic flame spraying process for self-lubricating wear-resistant coating - Google Patents
Hypersonic flame spraying process for self-lubricating wear-resistant coating Download PDFInfo
- Publication number
- CN101736279B CN101736279B CN200810228565XA CN200810228565A CN101736279B CN 101736279 B CN101736279 B CN 101736279B CN 200810228565X A CN200810228565X A CN 200810228565XA CN 200810228565 A CN200810228565 A CN 200810228565A CN 101736279 B CN101736279 B CN 101736279B
- Authority
- CN
- China
- Prior art keywords
- coating
- self
- resistant coating
- spraying process
- sprayed
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Abstract
The invention relates to a hypersonic flame spraying process for a self-lubricating wear-resistant coating, which comprises the following steps of: preparing a workpiece to be sprayed, removing oil stain with acetone, then carrying out white alundum blowing treatment, and finally carrying out hypersonic flame spraying, wherein the surface of the workpiece to be sprayed after being blown needs to be uniform, rough and free of metallic luster; and after blowing and roughening, spraying a coating of which the thickness is 300-400mum on the workpiece to be sprayed. The process comprises the following concrete conditions that: the spraying distance is 340-360mm, the powder feeding rate is 30-40g/min, the oxygen flow is 1750-1800l/h, the oxygen pressure is 131+/-10 psi, the kerosene flow is 5.3-5.5 g/hr, and the kerosene pressure is 113+/-15 psi. The invention has the advantages that by using hypersonic flame to spray chromium carbide/nickel-chromium powder containing fluoride, a high-temperature self-lubricating wear-resistant coating which is suitable for brush type sealing can be obtained; and the high-temperature self-lubricating wear-resistant coating is in a laminated structure and has excellent mechanical properties, low porosity and compact structure.
Description
Technical field
The present invention relates to the high-velocity spray technical field, a kind of hypersonic flame spraying process for self-lubricating wear-resistant coating is provided especially.
Background technology
The packing technique of streaming system is the important channel of improving motor performance in the mover.On mover, be designed with the many places tightness system, between the stator and rotor such as bearing, pneumatic plant, turbine, between pneumatic plant and turbine blade and internal cooling channel etc.The gross leak rate of traditional labyrinth gas seals constantly descends motor performance, and specific fuel oil consumption constantly increases, and brush seal is a kind of new type sealing device that can significantly reduce the gas leakage of aircraft engine secondary stream.Can adapt to the transient state radial deformation or the eccentric movement of rotor, and increase leakage rate indistinctively.In addition, the brush silk of brush sealing forms flexible the contact with rotor spindle damping is provided, and can improve the vibration performance of rotor-support-foundation system, be continue to use for many years comb tooth sealing the most simply, practicality, the most effective regeneration product.
Constant basically for guaranteeing that brush is sealed in lifetime internal leakage characteristic, brush seal brush silk when initialization be shrink-fit with the runway surface, brush silk and cause the brush seal degradation with the surperficial contact friction of runway, even the structural integrity of breakseal.In order to improve sealing property, be covered with the wear-resistant coating that contains self-lubricating material in the runway surfaces coated, time sealing brush scratches axle journal to prevent work, can reduce the frictional dissipation of sealing bristle simultaneously.Chromium carbide/nickel chromium triangle material has excellent high temperature oxidation resistance and hot hardness, often is used to the coating that bonding strength and wear-resisting resistance are had relatively high expectations.But in the Working environment of reality,, friction pair has been produced more serious frictional wear because it has higher hardness.
Summary of the invention
The objective of the invention is provides a kind of hypersonic flame spraying process for self-lubricating wear-resistant coating in order to reach the requirement of brush type sealed track to bonding strength and wear-resisting resistance.
The invention provides a kind of hypersonic flame spraying process for self-lubricating wear-resistant coating; It is characterized in that: the concrete spraying process of described hypersonic flame spraying process for self-lubricating wear-resistant coating does; Prepare to be sprayed; Treat spray piece and degrease, carry out the white fused alumina blast then and handle, carry out HVAF at last with acetone;
Wherein: answered even roughness, no metalluster by the surface behind the blast for to be sprayed, after the blast alligatoring, coating thickness is the coating of 300~400 μ m on to be sprayed; The HVAF processing parameter is specially: spray distance 340~360mm; Powder feeding rate 30~40 gram/minute, 1750~1800 liters/hour of oxygen flows, 131 ± 10 pounds/square inch of oxygen pressures; Kerosene oil flow 5.3~5.5 gallons per hours, 113 ± 15 pounds/square inch of kerosene pressure.
Described dusty spray is provided by Beijing Non-Fervoous Metal Inst., and concrete composition and quality percentage composition are following: Cr
3C
2Account for 53~57%, NiCr accounts for 34~37%, CaF
2, BaF
2Be surplus; The performance requriements of the nickel chromium triangle/chromium carbide powder of fluoride is following: flowability<110s/50g, granularity is in-200~+ 270 order≤5.0% ,-270~+ 325 order≤25.0% ,-325>=70.0% scope.
Described to be sprayed body material adopts iron and steel or superalloy.
The anchoring strength of coating scope is 43MPa~47.6Mpa.
Described HVAF characteristics are 2900~3100 ℃ of flame velocity 1500m/s~2000m/s, temperature.
HVAF is a kind of HVOF technology, and the characteristics so that its flame velocity is high, temperature is low are particularly conducive to the spray coating metal ceramic coating.High velocity of particle helps obtaining high coating compactness and good binding intensity; And low flame temperature can effectively suppress or reduce the decomposition of hard in spraying process such as carbide, makes the coating of preparation keep the weave construction of the original excellent abrasive resistance of sintering metal.HVOF spray coating metal ceramic coating, especially WC-Co, Cr
3C
2-NiCr metal-ceramic coating can make part life prolong 2~10 times with performances such as its superior wear-resistant material wearing and tearing, erosive wear, skimming wears, obtains widespread use at industrial circle.
Chromium carbide/nickel chromium triangle material has excellent high temperature oxidation resistance and hot hardness, often is used to the coating that bonding strength and wear-resisting resistance are had relatively high expectations.But in the Working environment of reality,, friction pair has been produced more serious frictional wear because it has higher hardness.In coating, add lubricants such as Calcium Fluoride (Fluorspan) and barium fluoride, can reduce the frictional coefficient of coating, improve wear resistance.
Adopt the microstructure of Leica metallography microscope sem observation supersonic spray coating chromium carbide/nickel chromium triangle coating.In the supersonic spray coating process, high velocity of particle can form the little dense coating of porosity after making powder and matrix collision, is interlaced between coating and the coating and piles up.
The bonding strength test of adopting homemade universal hydraulic testing machine to test to carry out high-temperature self-lubricating coating, the bonding strength test is carried out with reference to GBT8642-88 " mensuration of metal thermal spraying layer bonding strength ".
The anchoring strength of coating scope that records is 43MPa~47.6MPa.
The hardness of coating is the very important mechanical performance index of coating, is related to multiple functions such as abrasion property, intensity and coating work-ing life.
Macrohardness adopts HR15N, in the bonding strength test piece, makes an experiment, and on whole coat side, on average takes get its arithmetical av at 10, and microhardness detects carries out on metallographic specimen, loads the 300g metering.The test detected result is: the HR15N value is between 86~90, and HV0.3 is between 631~661.
Oxygen flow is 1750~1800SCFH, and kerosene oil flow is that 5.3~5.5gph scope is the optimal processing parameter scope, and coating structure is even compact relatively, and porosity is low, and mechanical property is qualified.
Advantage of the present invention:
Use the chromium carbide/nickel chromium triangle powder of HVAF fluoride, can obtain to be applicable to the brush high-temperature self-lubrication wear-resistant coating of obturaging.The high-temperature self-lubrication wear-resistant coating has the good mechanical performance, and coating is a laminate structure, and porosity is low, compact structure.
Description of drawings
Below in conjunction with accompanying drawing and embodiment the present invention is done further detailed explanation:
Fig. 1 is the microstructure view of HVAF self-lubricating coat in use.
Embodiment
Embodiment 1
Present embodiment provides a kind of hypersonic flame spraying process for self-lubricating wear-resistant coating; It is characterized in that: the concrete spraying process of described hypersonic flame spraying process for self-lubricating wear-resistant coating does; Prepare to be sprayed; Treat spray piece and degrease, carry out the white fused alumina blast then and handle, carry out HVAF at last with acetone;
Wherein: to be sprayed, no metalluster even by the surface behind the blast, after the blast alligatoring, coating thickness is the coating of 300 μ m on to be sprayed; The HVAF processing parameter is specially: spray distance 340mm; Powder feeding rate 30 gram/minute, 1750 liters/hour of oxygen flows, 121 pounds/square inch of oxygen pressures; Kerosene oil flow 5.3 gallons per hours, 98 pounds/square inch of kerosene pressure.
Described dusty spray is provided by Beijing Non-Fervoous Metal Inst., and concrete composition and quality percentage composition are following: Cr
3C
2Account for 53~57%, NiCr accounts for 34~37%, CaF
2, BaF
2Be surplus; The performance requriements of the nickel chromium triangle/chromium carbide powder of fluoride is following: flowability<110s/50g, granularity is in-200~+ 270 order≤5.0% ,-270~+ 325 order≤25.0% ,-325>=70.0% scope.
Described to be sprayed body material adopts iron and steel or superalloy.
The anchoring strength of coating scope is 43MPa.
Described HVAF processing parameter also comprises, 2900 ℃ of flame velocity 1500m/s, temperature.
HVAF is a kind of HVOF technology, and the characteristics so that its flame velocity is high, temperature is low are particularly conducive to the spray coating metal ceramic coating.High velocity of particle helps obtaining high coating compactness and good binding intensity; And low flame temperature can effectively suppress or reduce the decomposition of hard in spraying process such as carbide, makes the coating of preparation keep the weave construction of the original excellent abrasive resistance of sintering metal.HVOF spray coating metal ceramic coating, especially WC-Co, Cr
3C
2-NiCr metal-ceramic coating can make part life prolong 2~10 times with performances such as its superior wear-resistant material wearing and tearing, erosive wear, skimming wears, obtains widespread use at industrial circle.
Chromium carbide/nickel chromium triangle material has excellent high temperature oxidation resistance and hot hardness, often is used to the coating that bonding strength and wear-resisting resistance are had relatively high expectations.But in the Working environment of reality,, friction pair has been produced more serious frictional wear because it has higher hardness.In coating, add lubricants such as Calcium Fluoride (Fluorspan) and barium fluoride, can reduce the frictional coefficient of coating, improve wear resistance.
Adopt the microstructure of Leica metallography microscope sem observation supersonic spray coating chromium carbide/nickel chromium triangle coating.In the supersonic spray coating process, high velocity of particle can form the little dense coating of porosity after making powder and matrix collision, is interlaced between coating and the coating and piles up.
The bonding strength test of adopting homemade universal hydraulic testing machine to test to carry out high-temperature self-lubricating coating, the bonding strength test is carried out with reference to GBT8642-88 " mensuration of metal thermal spraying layer bonding strength ".
The anchoring strength of coating scope that records is 43MPa.
The hardness of coating is the very important mechanical performance index of coating, is related to multiple functions such as abrasion property, intensity and coating work-ing life.
Macrohardness adopts HR15N, in the bonding strength test piece, makes an experiment, and on whole coat side, on average takes get its arithmetical av at 10, and microhardness detects carries out on metallographic specimen, loads the 300g metering.The test detected result is: the HR15N value is about 86, and HV0.3 is about 631.
Embodiment 2
Present embodiment provides a kind of hypersonic flame spraying process for self-lubricating wear-resistant coating; It is characterized in that: the concrete spraying process of described hypersonic flame spraying process for self-lubricating wear-resistant coating does; Prepare to be sprayed; Treat spray piece and degrease, carry out the white fused alumina blast then and handle, carry out HVAF at last with acetone;
Wherein: to be sprayed, no metalluster even by the surface behind the blast, after the blast alligatoring, coating thickness is the coating of 350 μ m on to be sprayed; The HVAF processing parameter is specially: spray distance 350mm; Powder feeding rate 35 gram/minute, 1775 liters/hour of oxygen flows, 131 pounds/square inch of oxygen pressures; Kerosene oil flow 5.4 gallons per hours, 113 pounds/square inch of kerosene pressure.
Described dusty spray is provided by Beijing Non-Fervoous Metal Inst., and concrete composition and quality percentage composition are following: Cr
3C
2Account for 53~57%, NiCr accounts for 34~37%, CaF
2, BaF
2Be surplus; The performance requriements of the nickel chromium triangle/chromium carbide powder of fluoride is following: flowability<110s/50g, granularity is in-200~+ 270 order≤5.0% ,-270~+ 325 order≤25.0% ,-325>=70.0% scope.
Described to be sprayed body material can adopt iron and steel or superalloy.
Described to be sprayed body material adopts 1Cr11Ni2W2MoVN.
The anchoring strength of coating scope is 45Mpa.
Described HVAF processing parameter also comprises, 3000 ℃ of flame velocity 1750m/s, temperature.
HVAF is a kind of HVOF technology, and the characteristics so that its flame velocity is high, temperature is low are particularly conducive to the spray coating metal ceramic coating.High velocity of particle helps obtaining high coating compactness and good binding intensity; And low flame temperature can effectively suppress or reduce the decomposition of hard in spraying process such as carbide, makes the coating of preparation keep the weave construction of the original excellent abrasive resistance of sintering metal.HVOF spray coating metal ceramic coating, especially WC-Co, Cr
3C
2-NiCr metal-ceramic coating can make part life prolong 2~10 times with performances such as its superior wear-resistant material wearing and tearing, erosive wear, skimming wears, obtains widespread use at industrial circle.
Chromium carbide/nickel chromium triangle material has excellent high temperature oxidation resistance and hot hardness, often is used to the coating that bonding strength and wear-resisting resistance are had relatively high expectations.But in the Working environment of reality,, friction pair has been produced more serious frictional wear because it has higher hardness.In coating, add lubricants such as Calcium Fluoride (Fluorspan) and barium fluoride, can reduce the frictional coefficient of coating, improve wear resistance.
Adopt the microstructure of Leica metallography microscope sem observation supersonic spray coating chromium carbide/nickel chromium triangle coating.In the supersonic spray coating process, high velocity of particle can form the little dense coating of porosity after making powder and matrix collision, is interlaced between coating and the coating and piles up.
The bonding strength test of adopting homemade universal hydraulic testing machine to test to carry out high-temperature self-lubricating coating, the bonding strength test is carried out with reference to GBT8642-88 " mensuration of metal thermal spraying layer bonding strength ".The anchoring strength of coating scope that records is 43MPa~47.6MPa.
The hardness of coating is the very important mechanical performance index of coating, is related to multiple functions such as abrasion property, intensity and coating work-ing life.
Macrohardness adopts HR15N, in the bonding strength test piece, makes an experiment, and on whole coat side, on average takes get its arithmetical av at 10, and microhardness detects carries out on metallographic specimen, loads the 300g metering.The test detected result is: the HR15N value is between 86~90, and HV0.3 is between 631~661.
Embodiment 3
Present embodiment provides a kind of hypersonic flame spraying process for self-lubricating wear-resistant coating; It is characterized in that: the concrete spraying process of described hypersonic flame spraying process for self-lubricating wear-resistant coating does; Prepare to be sprayed; Treat spray piece and degrease, carry out the white fused alumina blast then and handle, carry out HVAF at last with acetone;
Wherein: to be sprayed, no metalluster even by the surface behind the blast, after the blast alligatoring, coating thickness is the coating of 400 μ m on to be sprayed; The HVAF processing parameter is specially: spray distance 360mm; Powder feeding rate 40 gram/minute, 1800 liters/hour of oxygen flows, 141 pounds/square inch of oxygen pressures; Kerosene oil flow 5.5 gallons per hours, 128 pounds/square inch of kerosene pressure.
Described dusty spray is provided by Beijing Non-Fervoous Metal Inst., and concrete composition and quality percentage composition are following: Cr
3C
2Account for 53~57%, NiCr accounts for 34~37%, CaF
2, BaF
2Be surplus; The performance requriements of the nickel chromium triangle/chromium carbide powder of fluoride is following: flowability<110s/50g, granularity is in-200~+ 270 order≤5.0% ,-270~+ 325 order≤25.0% ,-325>=70.0% scope.
Described to be sprayed body material can adopt iron and steel or superalloy.
The anchoring strength of coating scope is 47.6Mpa.
Described HVAF processing parameter also comprises, 3100 ℃ of flame velocity 2000m/s, temperature.
HVAF is a kind of HVOF technology, and the characteristics so that its flame velocity is high, temperature is low are particularly conducive to the spray coating metal ceramic coating.High velocity of particle helps obtaining high coating compactness and good binding intensity; And low flame temperature can effectively suppress or reduce the decomposition of hard in spraying process such as carbide, makes the coating of preparation keep the weave construction of the original excellent abrasive resistance of sintering metal.HVOF spray coating metal ceramic coating, especially WC-Co, Cr
3C
2-NiCr metal-ceramic coating can make part life prolong 2~10 times with performances such as its superior wear-resistant material wearing and tearing, erosive wear, skimming wears, obtains widespread use at industrial circle.
Chromium carbide/nickel chromium triangle material has excellent high temperature oxidation resistance and hot hardness, often is used to the coating that bonding strength and wear-resisting resistance are had relatively high expectations.But in the Working environment of reality,, friction pair has been produced more serious frictional wear because it has higher hardness.In coating, add lubricants such as Calcium Fluoride (Fluorspan) and barium fluoride, can reduce the frictional coefficient of coating, improve wear resistance.
Adopt the microstructure of Leica metallography microscope sem observation supersonic spray coating chromium carbide/nickel chromium triangle coating.In the supersonic spray coating process, high velocity of particle can form the little dense coating of porosity after making powder and matrix collision, is interlaced between coating and the coating and piles up.
The bonding strength test of adopting homemade universal hydraulic testing machine to test to carry out high-temperature self-lubricating coating, the bonding strength test is carried out with reference to GBT8642-88 " mensuration of metal thermal spraying layer bonding strength ".The anchoring strength of coating scope that records is 43MPa~47.6MPa.
The hardness of coating is the very important mechanical performance index of coating, is related to multiple functions such as abrasion property, intensity and coating work-ing life.
Macrohardness adopts HR15N, in the bonding strength test piece, makes an experiment, and on whole coat side, on average takes get its arithmetical av at 10, and microhardness detects carries out on metallographic specimen, loads the 300g metering.The test detected result is: the HR15N value is between 86~90, and HV0.3 is between 631~661.
Claims (5)
1. hypersonic flame spraying process for self-lubricating wear-resistant coating; It is characterized in that: the concrete spraying process of described hypersonic flame spraying process for self-lubricating wear-resistant coating does; Prepare to be sprayed; Treat spray piece and degrease, carry out the white fused alumina blast then and handle, carry out HVAF at last with acetone; Wherein: answered even roughness, no metalluster by the surface behind the blast for to be sprayed, after the blast alligatoring, coating thickness is the coating of 300~400 μ m on to be sprayed; The HVAF processing parameter is specially: spray distance 340~360mm; Powder feeding rate 30~40 gram/minute, 1750~1800 liters/hour of oxygen flows, 131 ± 10 pounds/square inch of oxygen pressures; Kerosene oil flow 5.3~5.5 gallons per hours, 113 ± 15 pounds/square inch of kerosene pressure.
2. according to the said hypersonic flame spraying process for self-lubricating wear-resistant coating of claim 1, it is characterized in that: concrete composition of described dusty spray and quality percentage composition are following:
Cr
3C
2Account for 53~57%, NiCr accounts for 34~37%, CaF
2, BaF
2Be surplus;
The performance requriements of the nickel chromium triangle/chromium carbide powder of fluoride is following: mobile<110s/50g, granularity is in-200~+ 270 order≤5.0% ,-270~+ 325 order≤25.0% ,-325>=70.0% scope.
3. according to the described hypersonic flame spraying process for self-lubricating wear-resistant coating of claim 1, it is characterized in that: described to be sprayed body material adopts iron and steel or superalloy.
4. according to the described hypersonic flame spraying process for self-lubricating wear-resistant coating of claim 1, it is characterized in that: the anchoring strength of coating scope is 43MPa~47.6Mpa.
5. according to the described hypersonic flame spraying process for self-lubricating wear-resistant coating of claim 1, it is characterized in that: described HVAF characteristics are 2900~3100 ℃ of flame velocity 1500m/s~2000m/s, temperature.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200810228565XA CN101736279B (en) | 2008-11-05 | 2008-11-05 | Hypersonic flame spraying process for self-lubricating wear-resistant coating |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200810228565XA CN101736279B (en) | 2008-11-05 | 2008-11-05 | Hypersonic flame spraying process for self-lubricating wear-resistant coating |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101736279A CN101736279A (en) | 2010-06-16 |
CN101736279B true CN101736279B (en) | 2012-07-18 |
Family
ID=42460305
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN200810228565XA Active CN101736279B (en) | 2008-11-05 | 2008-11-05 | Hypersonic flame spraying process for self-lubricating wear-resistant coating |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101736279B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103047292A (en) * | 2012-12-17 | 2013-04-17 | 吴江市金平华纺织有限公司 | Wear resistant bearing for textile machine |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104512077A (en) * | 2013-09-28 | 2015-04-15 | 江苏锋华车辆科技有限公司 | Car-roof coating |
CN104513944B (en) * | 2014-05-04 | 2018-07-24 | 水利部产品质量标准研究所 | A kind of rare earth mixing with nano composite ceramic coat and its preparation process |
CN104451516A (en) * | 2014-10-30 | 2015-03-25 | 安徽鼎恒再制造产业技术研究院有限公司 | WC-SiC nano-coating and preparation method thereof |
CN105039896A (en) * | 2015-06-24 | 2015-11-11 | 西安航空动力股份有限公司 | Aircraft engine brushing type sealing coating layer and coating method |
CN107541694B (en) * | 2016-06-23 | 2019-04-02 | 安易斯密封(宁波)有限公司 | A kind of preparation method of rotary packing ring surface lubrication wear-resisting coating |
CN106399909A (en) * | 2016-11-18 | 2017-02-15 | 无锡明盛纺织机械有限公司 | Preparation method of gradient composite wear-resisting coating |
CN106399913A (en) * | 2016-11-18 | 2017-02-15 | 无锡明盛纺织机械有限公司 | Preparation method for gradient composite abrasion-resistant coating |
CN106399911A (en) * | 2016-11-18 | 2017-02-15 | 无锡明盛纺织机械有限公司 | Preparation method for gradient composite abrasion-resistant coating |
CN109402708B (en) * | 2018-10-17 | 2020-04-24 | 中国兵器工业第五九研究所 | Preparation method of aluminum and aluminum alloy wear-resistant self-lubricating coating |
CN111334740A (en) * | 2018-12-19 | 2020-06-26 | 辽宁省轻工科学研究院有限公司 | High-temperature wear-resistant self-lubricating coating and preparation method thereof |
CN109868443B (en) * | 2019-03-12 | 2020-12-22 | 唐山学院 | Nickel-based aluminum oxide high-temperature self-lubricating wear-resistant coating and preparation method thereof |
CN110318907A (en) * | 2019-07-22 | 2019-10-11 | 西安方霖动力科技有限公司 | Rotary engine end cover structure, spray processes and application |
CN111057986A (en) * | 2019-12-31 | 2020-04-24 | 广东省新材料研究所 | Self-lubricating coating for wide temperature range, workpiece and preparation method of self-lubricating coating |
CN112323007A (en) * | 2020-10-06 | 2021-02-05 | 湖北超卓航空科技股份有限公司 | Supersonic flame spraying self-lubricating wear-resistant coating process |
CN112281151A (en) * | 2020-10-30 | 2021-01-29 | 遵义市欣茂汇机电有限公司 | Low-temperature supersonic spraying device and method for wear-resistant coating |
CN112283741A (en) * | 2020-10-30 | 2021-01-29 | 陕西能源赵石畔煤电有限公司 | Device for preventing corrosion of water cooled wall of high-sulfur coal million units boiler |
CN113073283A (en) * | 2021-03-26 | 2021-07-06 | 陕西科技大学 | Nickel-chromium/chromium carbide metal ceramic composite coating and preparation method thereof |
CN117305748B (en) * | 2023-11-28 | 2024-02-23 | 北矿新材科技有限公司 | High-temperature self-lubricating abradable seal coating and preparation method thereof |
Citations (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998014629A1 (en) * | 1996-10-02 | 1998-04-09 | Neles Controls Oy | Wear resisting parts for process valves |
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 |
US6129991A (en) * | 1994-10-28 | 2000-10-10 | Howmet Research Corporation | Aluminide/MCrAlY coating system for superalloys |
CN1342525A (en) * | 2001-08-31 | 2002-04-03 | 中国人民解放军第二炮兵工程学院 | Multifunctional supersonic flame spraying method and its intelligent control system |
US6652991B1 (en) * | 2002-10-09 | 2003-11-25 | The Governors Of The University Of Alberta | Ductile NiAl intermetallic compositions |
JP2005015874A (en) * | 2003-06-27 | 2005-01-20 | Daido Castings:Kk | Self-lubricity composite powder and method for manufacturing the same |
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 |
CN1649689A (en) * | 2002-03-01 | 2005-08-03 | 普莱克斯S.T.技术有限公司 | Corrosion resistant powder and coating |
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 |
CN1760409A (en) * | 2004-10-15 | 2006-04-19 | 福吉米株式会社 | Thermal spraying powder, thermal spraying method and method for forming thermal spray coating |
CN1938442A (en) * | 2004-03-25 | 2007-03-28 | 都美工业株式会社 | Metallic glass laminate, process for producing the same and application thereof |
EP1798302A1 (en) * | 2004-08-23 | 2007-06-20 | Kabushiki Kaisha Toshiba | Method and equipment for repairing rotor |
CN101031668A (en) * | 2004-09-29 | 2007-09-05 | 达纳公司 | Bearing materials and method for the production thereof |
CN101096308A (en) * | 2007-05-29 | 2008-01-02 | 武汉理工大学 | Seawater erosion abrasion and biologic defiling resistant composite ceramic powder for hot spraying and preparation therefor |
CN101157129A (en) * | 2007-11-21 | 2008-04-09 | 北京矿冶研究总院 | Preparation method of silver-doped nickel-chromium carbide-based high-temperature self-lubricating coating material |
CN101210499A (en) * | 2006-12-28 | 2008-07-02 | 沈阳黎明航空发动机(集团)有限责任公司 | Zirconium oxide heat barrier coating and spraying technique used for gas turbine guide vane |
CN101274366A (en) * | 2007-03-27 | 2008-10-01 | 福吉米株式会社 | Thermal spraying powder, thermal spray coating, and hearth roll |
CN101294558A (en) * | 2007-04-25 | 2008-10-29 | 株式会社丰田自动织机 | Compressor swash plate and method of manufacturing the same |
-
2008
- 2008-11-05 CN CN200810228565XA patent/CN101736279B/en active Active
Patent Citations (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6129991A (en) * | 1994-10-28 | 2000-10-10 | Howmet Research Corporation | Aluminide/MCrAlY coating system for superalloys |
WO1998014629A1 (en) * | 1996-10-02 | 1998-04-09 | Neles Controls Oy | Wear resisting parts for process valves |
US6203895B1 (en) * | 1996-10-02 | 2001-03-20 | Neles Controls Oy | Wear resisting parts for process valves |
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 |
CN1342525A (en) * | 2001-08-31 | 2002-04-03 | 中国人民解放军第二炮兵工程学院 | Multifunctional supersonic flame spraying method and its intelligent control system |
CN1649689A (en) * | 2002-03-01 | 2005-08-03 | 普莱克斯S.T.技术有限公司 | Corrosion resistant powder and coating |
US6652991B1 (en) * | 2002-10-09 | 2003-11-25 | The Governors Of The University Of Alberta | Ductile NiAl intermetallic compositions |
JP2005015874A (en) * | 2003-06-27 | 2005-01-20 | Daido Castings:Kk | Self-lubricity composite powder and method for manufacturing the same |
CN1938442A (en) * | 2004-03-25 | 2007-03-28 | 都美工业株式会社 | Metallic glass laminate, process for producing the same and application thereof |
EP1798302A1 (en) * | 2004-08-23 | 2007-06-20 | Kabushiki Kaisha Toshiba | Method and equipment for repairing rotor |
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 |
CN101031668A (en) * | 2004-09-29 | 2007-09-05 | 达纳公司 | Bearing materials and method for the production thereof |
CN1760409A (en) * | 2004-10-15 | 2006-04-19 | 福吉米株式会社 | Thermal spraying powder, thermal spraying method and method for forming thermal spray coating |
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 |
CN101210499A (en) * | 2006-12-28 | 2008-07-02 | 沈阳黎明航空发动机(集团)有限责任公司 | Zirconium oxide heat barrier coating and spraying technique used for gas turbine guide vane |
CN101274366A (en) * | 2007-03-27 | 2008-10-01 | 福吉米株式会社 | Thermal spraying powder, thermal spray coating, and hearth roll |
CN101294558A (en) * | 2007-04-25 | 2008-10-29 | 株式会社丰田自动织机 | Compressor swash plate and method of manufacturing the same |
CN101096308A (en) * | 2007-05-29 | 2008-01-02 | 武汉理工大学 | Seawater erosion abrasion and biologic defiling resistant composite ceramic powder for hot spraying and preparation therefor |
CN101157129A (en) * | 2007-11-21 | 2008-04-09 | 北京矿冶研究总院 | Preparation method of silver-doped nickel-chromium carbide-based high-temperature self-lubricating coating material |
Non-Patent Citations (1)
Title |
---|
王玮等.二硫化钼含量对自润滑涂层组织及性能的影响.《中国表面工程》.2006,第19卷(第02期), * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103047292A (en) * | 2012-12-17 | 2013-04-17 | 吴江市金平华纺织有限公司 | Wear resistant bearing for textile machine |
Also Published As
Publication number | Publication date |
---|---|
CN101736279A (en) | 2010-06-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101736279B (en) | Hypersonic flame spraying process for self-lubricating wear-resistant coating | |
Ramesh et al. | Solid particle erosion of HVOF sprayed WC-Co/NiCrFeSiB coatings | |
Zhang et al. | Role of Mo on tribological properties of atmospheric plasma-sprayed Mo-NiCrBSi composite coatings under dry and oil-lubricated conditions | |
EP1852520B1 (en) | Wear-resistant coating | |
Gao et al. | Simultaneous increase of friction coefficient and wear resistance through HVOF sprayed WC-(nano WC-Co) | |
CN107541694B (en) | A kind of preparation method of rotary packing ring surface lubrication wear-resisting coating | |
Ouyang et al. | Effects of different additives on microstructure and high-temperature tribological properties of plasma-sprayed Cr2O3 ceramic coatings | |
US20170204920A1 (en) | Bi-layer iron coating of lightweight metallic substrate | |
CN105177489A (en) | Method for enhancing corrosion and wear resistance of metal member surface | |
Barbezat | The state of the art of the internal plasma spraying on cylinder bore in AlSi cast alloys | |
CN106637035A (en) | Wear-resistant coating on valve plate of EB furnace equipment gate valve, and spraying technology thereof | |
Mahade et al. | Influence of processing conditions on the microstructure and sliding wear of a promising Fe-based coating deposited by HVAF | |
CN108486565A (en) | A kind of low pressure cold spraying copper radical self-lubricating coating and preparation method thereof | |
Tian et al. | Frictional wear performance under oil-lubricated conditions and wear resistance mechanism of high-velocity arc-sprayed FeNiCrAl coating | |
Kumar et al. | Thermally sprayed alumina and ceria-doped-alumina coatings on AZ91 Mg alloy | |
Priyan et al. | Influence of HVOF parameters on the wear resistance of Cr3C2-NiCr coating | |
Singh et al. | Performance of HVOF sprayed NiCr and Stellite-6 coatings under pin on disc wear testing | |
CN107130204A (en) | A kind of wear-resistant coating cylinder jacket and its preparation technology | |
Wang et al. | Wear resistance of a Cr 3 C 2-NiCr detonation spray coating | |
Özorak et al. | Wear and microstructural properties of coatings on Weldox 700 steel | |
Rukhande et al. | Tribological behaviour of thermally sprayed coatings: A review | |
Kumar et al. | Tribological analysis of increasing percentage of CrC content in composite coating by atmospheric plasma spray technique | |
Hwang et al. | Tribological behavior of plasma spray coatings for marine diesel engine piston ring and cylinder liner | |
CN112524116A (en) | Hydraulic piston rod, surface composite functional coating thereof and preparation method | |
Tyagi et al. | Effect of Temperature on Mo–C Blend Composite Coating for Piston Ring Applications |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CP01 | Change in the name or title of a patent holder |
Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City |
|
CP01 | Change in the name or title of a patent holder |