CN112610608B - A kind of wide temperature range self-lubricating bearing and preparation method thereof - Google Patents
A kind of wide temperature range self-lubricating bearing and preparation method thereof Download PDFInfo
- Publication number
- CN112610608B CN112610608B CN202011346102.0A CN202011346102A CN112610608B CN 112610608 B CN112610608 B CN 112610608B CN 202011346102 A CN202011346102 A CN 202011346102A CN 112610608 B CN112610608 B CN 112610608B
- Authority
- CN
- China
- Prior art keywords
- coating
- bearing
- atomic percent
- target
- layer
- 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
- 238000002360 preparation method Methods 0.000 title claims abstract description 10
- 239000011248 coating agent Substances 0.000 claims abstract description 82
- 238000000576 coating method Methods 0.000 claims abstract description 82
- 239000002131 composite material Substances 0.000 claims abstract description 37
- 239000000758 substrate Substances 0.000 claims abstract description 9
- 239000010410 layer Substances 0.000 claims description 73
- 238000000034 method Methods 0.000 claims description 17
- 229910000831 Steel Inorganic materials 0.000 claims description 7
- 238000000151 deposition Methods 0.000 claims description 7
- 238000005516 engineering process Methods 0.000 claims description 7
- 238000012545 processing Methods 0.000 claims description 7
- 239000002356 single layer Substances 0.000 claims description 7
- 239000010959 steel Substances 0.000 claims description 7
- 239000011247 coating layer Substances 0.000 claims description 6
- 238000007733 ion plating Methods 0.000 claims description 4
- 238000001755 magnetron sputter deposition Methods 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 229910016021 MoTe2 Inorganic materials 0.000 claims 2
- 229910052735 hafnium Inorganic materials 0.000 claims 2
- 230000001050 lubricating effect Effects 0.000 abstract description 12
- 238000005461 lubrication Methods 0.000 abstract description 8
- 150000001875 compounds Chemical class 0.000 abstract description 3
- 230000000694 effects Effects 0.000 abstract description 3
- 238000005299 abrasion Methods 0.000 abstract 1
- 239000011159 matrix material Substances 0.000 description 7
- 239000000463 material Substances 0.000 description 4
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 239000000314 lubricant Substances 0.000 description 2
- 239000010687 lubricating oil Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 229910052582 BN Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- WUKWITHWXAAZEY-UHFFFAOYSA-L calcium difluoride Chemical compound [F-].[F-].[Ca+2] WUKWITHWXAAZEY-UHFFFAOYSA-L 0.000 description 1
- 229910001634 calcium fluoride Inorganic materials 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 229910021389 graphene Inorganic materials 0.000 description 1
- 238000004372 laser cladding Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/66—Special parts or details in view of lubrication
- F16C33/6696—Special parts or details in view of lubrication with solids as lubricant, e.g. dry coatings, powder
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/02—Pretreatment of the material to be coated
- C23C14/021—Cleaning or etching treatments
- C23C14/022—Cleaning or etching treatments by means of bombardment with energetic particles or radiation
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0635—Carbides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0641—Nitrides
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/24—Vacuum evaporation
- C23C14/32—Vacuum evaporation by explosion; by evaporation and subsequent ionisation of the vapours, e.g. ion-plating
- C23C14/325—Electric arc evaporation
-
- C—CHEMISTRY; METALLURGY
- C23—COATING 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
- C23C—COATING 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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/34—Sputtering
- C23C14/35—Sputtering by application of a magnetic field, e.g. magnetron sputtering
- C23C14/352—Sputtering by application of a magnetic field, e.g. magnetron sputtering using more than one target
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2202/00—Solid materials defined by their properties
- F16C2202/50—Lubricating properties
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2204/00—Metallic materials; Alloys
- F16C2204/60—Ferrous alloys, e.g. steel alloys
- F16C2204/66—High carbon steel, i.e. carbon content above 0.8 wt%, e.g. through-hardenable steel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2204/00—Metallic materials; Alloys
- F16C2204/60—Ferrous alloys, e.g. steel alloys
- F16C2204/70—Ferrous alloys, e.g. steel alloys with chromium as the next major constituent
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/30—Coating surfaces
- F16C2223/60—Coating surfaces by vapour deposition, e.g. PVD, CVD
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Physical Vapour Deposition (AREA)
- Sliding-Contact Bearings (AREA)
Abstract
Description
技术领域technical field
本发明涉及轴承制造技术领域,具体来说,涉及一种宽温域自润滑轴承及其制备方法。The invention relates to the technical field of bearing manufacturing, in particular to a wide temperature range self-lubricating bearing and a preparation method thereof.
背景技术Background technique
轴承是当代机械设备中一种重要零部件,轴承工作过程中存在较大的摩擦磨损,使用过程通常需要使用润滑剂;自润滑技术能够实现轴承无油润滑,突破润滑油或润滑脂等使用的局限性,自润滑轴承已成为绿色制造的一个研究热点。因此,开发新型的高强度、低摩擦、低磨损及长寿命的自润滑轴承对先进制造业具有重要意义!Bearings are an important part of contemporary mechanical equipment. There is a large amount of friction and wear in the working process of bearings, and lubricants are usually used during the use process; Due to limitations, self-lubricating bearings have become a research hotspot in green manufacturing. Therefore, the development of new high-strength, low-friction, low-wear and long-life self-lubricating bearings is of great significance to advanced manufacturing!
中国专利申请号201910511263.1公开了一种减摩抗磨自润滑涂层轴承及其制备方法,该轴承通过等离子体喷涂方法,在基体表面制备硬质合金层、氮化硅陶瓷层和立方氮化硼层复合润滑涂层,实现工作过程中的润滑功效。中国专利申请号201320341799.1公开了一种镶嵌式固体自润滑轴承,轴承本体侧部设有环形凹槽及储存固体润滑剂的通孔,可实现工作过程的自润滑,降低摩擦系数,延长轴承寿命。中国专利申请号CN201710547274.6公开了一种自润滑轴承及其制备方法,通过激光熔覆方法在含铬合金钢轴承基体表面制备出石墨烯/氟化钙/陶瓷自润滑涂层,从而实现轴承本身的自润滑功能。Chinese Patent Application No. 201910511263.1 discloses a friction-reducing and anti-wear self-lubricating coated bearing and a preparation method thereof. The bearing is prepared with a cemented carbide layer, a silicon nitride ceramic layer and a cubic boron nitride layer on the surface of the substrate by a plasma spraying method. Layer composite lubricating coating to achieve the lubricating effect during the working process. Chinese Patent Application No. 201320341799.1 discloses an inlaid solid self-lubricating bearing. The side of the bearing body is provided with an annular groove and a through hole for storing solid lubricant, which can realize self-lubrication in the working process, reduce the friction coefficient and prolong the bearing life. Chinese Patent Application No. CN201710547274.6 discloses a self-lubricating bearing and a preparation method thereof. A graphene/calcium fluoride/ceramic self-lubricating coating is prepared on the surface of a chromium-containing alloy steel bearing substrate by a laser cladding method, thereby realizing the bearing Its own self-lubricating function.
发明内容SUMMARY OF THE INVENTION
本发明所要解决的技术问题是:提供一种宽温域自润滑轴承及其制备方法,该轴承在宽温域及交变温度范围内具有良好的润滑功效,可实现轴承工作过程中的润滑,减小轴承磨损,提高轴承寿命。The technical problem to be solved by the present invention is: to provide a wide temperature range self-lubricating bearing and a preparation method thereof, the bearing has good lubricating effect in a wide temperature range and an alternating temperature range, and can realize the lubrication during the working process of the bearing, Reduce bearing wear and improve bearing life.
为解决上述技术问题,本发明一方面提供一种宽温域自润滑轴承,包括轴承基体、微织构和复合涂层,所述微织构设置在轴承基体的表面,所述复合涂层沉积在所述微织构的表面;所述复合涂层包括第一涂层和第二涂层,所述第一涂层和第二涂层交替叠加;所述复合涂层包括至少10层第一涂层和至少10层第二涂层。In order to solve the above technical problems, one aspect of the present invention provides a wide temperature range self-lubricating bearing, comprising a bearing matrix, a microtexture and a composite coating, the microtexture is arranged on the surface of the bearing matrix, and the composite coating is deposited. On the micro-textured surface; the composite coating comprises a first coating and a second coating, the first coating and the second coating are alternately stacked; the composite coating comprises at least 10 layers of the first coating coating and at least 10 second coats.
作为本发明实施例的进一步改进,所述第一涂层为TiVZnN层,所述第二涂层为MoTeHfC层,第一涂层和第二涂层的单层厚度均小于等于500nm。As a further improvement of the embodiment of the present invention, the first coating is a TiVZnN layer, the second coating is a MoTeHfC layer, and the single-layer thicknesses of the first coating and the second coating are both less than or equal to 500 nm.
作为本发明实施例的进一步改进,所述第一涂层中,Ti元素原子百分比为30-50%,V元素原子百分比为10-20%,Zn元素原子百分比为5-15%,N元素原子百分比为20-40%,Ti元素原子百分比、V元素原子百分比、Zn元素原子百分比和N元素原子百分比之和为100%。As a further improvement of the embodiment of the present invention, in the first coating, the atomic percentage of Ti element is 30-50 atomic%, the atomic percentage of V element is 10-20 atomic%, the atomic percentage of Zn element is 5-15 atomic%, and the atomic percentage of N element is 5-15 atomic%. The percentage is 20-40%, and the sum of the atomic percentage of Ti element, the atomic percentage of V element, the atomic percentage of Zn element and the atomic percentage of N element is 100%.
作为本发明实施例的进一步改进,所述第二涂层中,Mo元素原子百分比为30-40%,Te元素原子百分比为30-40%,Hf元素原子百分比为8-12%,C元素原子百分比为10-20%,Mo元素原子百分比、Te元素原子百分比、Hf元素原子百分比和C元素原子百分比之和为100%。As a further improvement of the embodiment of the present invention, in the second coating, the atomic percentage of Mo element is 30-40%, the atomic percentage of Te element is 30-40%, the atomic percentage of Hf element is 8-12%, and the atomic percentage of C element is 8-12%. The percentage is 10-20%, and the sum of the atomic percentage of Mo element, the atomic percentage of Te element, the atomic percentage of Hf element and the atomic percentage of C element is 100%.
作为本发明实施例的进一步改进,所述轴承基体由轴承钢制成。As a further improvement of the embodiment of the present invention, the bearing base is made of bearing steel.
另一方面,本发明实施例还提供一种制备上述宽温域自润滑轴承的制备方法,包括以下步骤:On the other hand, an embodiment of the present invention also provides a preparation method for preparing the above-mentioned wide temperature range self-lubricating bearing, comprising the following steps:
步骤1、采用激光加工技术在轴承基体的表面制备微织构,激光功率为10-50W,频率为10-20kHz,扫描速度为5-300mm/s;微织构的宽度为10-200μm,深度为5-200μm;
步骤2、采用多弧离子镀与中频磁控溅射共沉积的方法,在微织构的表面制备复合涂层,得到宽温域自润滑轴承。
作为本发明实施例的进一步改进,所述步骤2具体包括:As a further improvement of the embodiment of the present invention, the
步骤21、打开Ti靶和VZnN靶,调整工作气压为0.5-2.5Pa,偏压为100-300V,调整Ti靶电流为50-160A,VZnN靶电流调至50-100A,沉积TiVZnN层2-5min;Step 21. Turn on the Ti target and the VZnN target, adjust the working pressure to 0.5-2.5Pa, the bias voltage to 100-300V, adjust the Ti target current to 50-160A, the VZnN target current to 50-100A, and deposit the TiVZnN layer for 2-5min ;
步骤22、开启MoTe2靶、Hf靶和C靶,调整工作气压为0.5-2.0Pa,偏压为100-120V,调整MoTe2靶电流为80-120A,Hf靶电流为30-50A,C靶电流为50-80A,沉积MoTeHfC层3-8min;Step 22. Turn on the MoTe 2 target, Hf target and C target, adjust the working pressure to 0.5-2.0Pa, the bias voltage to 100-120V, adjust the MoTe 2 target current to 80-120A, the Hf target current to 30-50A, and the C target current to be 30-50A. The current is 50-80A, and the MoTeHfC layer is deposited for 3-8min;
步骤23、重复步骤21和步骤22,交替沉积TiVZnN层和MoTeHfC层,使得复合涂层总厚度为预设厚度,得到宽温域自润滑轴承。Step 23, repeating steps 21 and 22, alternately depositing TiVZnN layers and MoTeHfC layers, so that the total thickness of the composite coating is a preset thickness, and a wide temperature range self-lubricating bearing is obtained.
作为本发明实施例的进一步改进,所述预设厚度为1-10μm。As a further improvement of the embodiment of the present invention, the preset thickness is 1-10 μm.
与现有技术相比,本发明的技术方案具有以下有益效果:本发明实施例的轴承在宽温域工作范围内具有良好的自润滑作用,工作温度较低时,MoTeHfC涂层能够起到润滑作用;工作温度较高时,TiVZnN、MoTeHfC及空气中氧气会发生反应,生成具有高温润滑作用的ZnMoO4和V2O5化合物,从而能够在高温条件下起到良好的润滑作用。本发明实施例的轴承,无需润滑油和复杂的润滑系统,结构简单,使用方便;TiVZnN层和MoTeHfC层交错叠加提高了单一涂层的性能,增加了轴承适用范围。本实施例的轴承表面的微织构能够提高轴承基体与复合涂层之间的结合强度,且能够收集磨屑及高温润滑相,起到减小磨粒磨损及提供二次润滑作用,从而提高轴承寿命。本实施例轴承在宽温度范围或交变温度条件下均具有良好的润滑功效,可减小工作过程中轴承摩擦磨损,提高轴承寿命。Compared with the prior art, the technical solution of the present invention has the following beneficial effects: the bearing of the embodiment of the present invention has a good self-lubricating effect in a wide temperature range, and when the working temperature is low, the MoTeHfC coating can lubricate When the working temperature is high, TiVZnN, MoTeHfC and oxygen in the air will react to generate ZnMoO 4 and V 2 O 5 compounds with high temperature lubrication, which can play a good lubricating effect under high temperature conditions. The bearing of the embodiment of the present invention does not need lubricating oil and complex lubrication system, and has a simple structure and is convenient to use; the interlaced stacking of the TiVZnN layer and the MoTeHfC layer improves the performance of a single coating and increases the application range of the bearing. The micro-texture of the bearing surface of this embodiment can improve the bonding strength between the bearing matrix and the composite coating, and can collect wear debris and high-temperature lubricating phases, reduce abrasive wear and provide secondary lubrication, thereby improving bearing life. The bearing of this embodiment has a good lubricating effect in a wide temperature range or under alternating temperature conditions, which can reduce the friction and wear of the bearing during the working process and improve the bearing life.
附图说明Description of drawings
图1为本发明实施例的宽温域自润滑轴承的结构示意图;1 is a schematic structural diagram of a wide temperature range self-lubricating bearing according to an embodiment of the present invention;
图2为本发明实施例的宽温域自润滑轴承的剖视图。2 is a cross-sectional view of a wide temperature range self-lubricating bearing according to an embodiment of the present invention.
图中:轴承基体1、微织构2、第一涂层31、第二涂层32、内圈6、外圈7、滚珠8。In the figure:
具体实施方式Detailed ways
下面结合附图,对本发明的技术方案进行详细的说明。The technical solutions of the present invention will be described in detail below with reference to the accompanying drawings.
本发明实施例提供一种宽温域自润滑轴承,如图1和图2所示,包括含有内圈6和外圈7的轴承基体1,滚珠8位于内圈6和外圈7之间。本实施例的宽温域自润滑轴承还包括微织构和复合涂层,微织构2设在内圈6的外表面以及外圈7的内表面,复合涂层沉积在微织构2的表面。复合涂层包括第一涂层31和第二涂层32,第一涂层31和第二涂层32交替叠加。复合涂层中,第一涂层31至少有10层,第二涂层32至少有10层。The embodiment of the present invention provides a wide temperature range self-lubricating bearing, as shown in FIG. 1 and FIG. 2 , comprising a
所述第一涂层31为TiVZnN层,第二涂层32为MoTeHfC层,第一涂层31和第二涂层32的单层厚度均小于等于500nm。The
优选的,第一涂层31中,Ti元素原子百分比为30-50%,V元素原子百分比为10-20%,Zn元素原子百分比为5-15%,N元素原子百分比为20-40%,Ti元素原子百分比、V元素原子百分比、Zn元素原子百分比和N元素原子百分比之和为100%。Preferably, in the
优选的,第二涂层32中,Mo元素原子百分比为30-40%,Te元素原子百分比为30-40%,Hf元素原子百分比为8-12%,C元素原子百分比为10-20%,Mo元素原子百分比、Te元素原子百分比、Hf元素原子百分比和C元素原子百分比之和为100%。Preferably, in the
优选的,轴承基体1由轴承钢制成。Preferably, the
本发明实施例还提供一种制备上述宽温域自润滑轴承的制备方法,包括以下步骤:The embodiment of the present invention also provides a preparation method for preparing the above-mentioned wide temperature range self-lubricating bearing, comprising the following steps:
步骤1、采用激光加工技术在轴承基体1的表面制备微织构2,激光功率为10-50W,频率为10-20kHz,扫描速度为5-300mm/s;微织构2的宽度为10-200μm,深度为5-200μm;
步骤2、采用多弧离子镀与中频磁控溅射共沉积的方法,在微织构2的表面制备复合涂层,得到宽温域自润滑轴承。
本发明实施例方法,采用多弧离子镀与中频磁控溅射共沉积的方法在轴承基体的表面制备复合涂层,制备方法简单。The method of the embodiment of the present invention adopts the method of co-deposition of multi-arc ion plating and intermediate frequency magnetron sputtering to prepare the composite coating on the surface of the bearing substrate, and the preparation method is simple.
优选的,步骤2具体包括:Preferably,
步骤21、打开Zr靶和VZnN靶,调整工作气压为0.5-2.5Pa,偏压为100-300V,调整Zr靶电流为50-160A,VZnN靶电流调至50-100A,沉积TiVZnN层2-5min;Step 21. Open the Zr target and the VZnN target, adjust the working pressure to 0.5-2.5Pa, the bias voltage to 100-300V, adjust the Zr target current to 50-160A, the VZnN target current to 50-100A, and deposit the TiVZnN layer for 2-5min ;
步骤22、开启MoTe2靶、Hf靶和C靶,调整工作气压为0.5-2.0Pa,偏压为100-120V,调整MoTe2靶电流为80-120A,Hf靶电流为30-50A,C靶电流为50-80A,沉积MoTeHfC层3-8min;Step 22. Turn on the MoTe 2 target, Hf target and C target, adjust the working pressure to 0.5-2.0Pa, the bias voltage to 100-120V, adjust the MoTe 2 target current to 80-120A, the Hf target current to 30-50A, and the C target current to be 30-50A. The current is 50-80A, and the MoTeHfC layer is deposited for 3-8min;
步骤23、重复步骤21和步骤22,直至复合涂层总厚度为预设厚度,得到宽温域自润滑轴承。Step 23: Repeat steps 21 and 22 until the total thickness of the composite coating is the preset thickness, and a wide temperature range self-lubricating bearing is obtained.
优选的,预设厚度为1-10μm。Preferably, the preset thickness is 1-10 μm.
本发明实施例的轴承在宽温域工作范围内具有良好的自润滑作用,工作温度较低时,MoTeHfC涂层能够起到润滑作用;工作温度较高时,TiVZnN、MoTeHfC及空气中氧气会发生反应,生成具有高温润滑作用的ZnMoO4和V2O5化合物,从而能够在高温条件下起到良好的润滑作用。本发明实施例的轴承,无需润滑油和复杂的润滑系统,结构简单,使用方便;TiVZnN+MoTeHfC叠层涂层提高了单一涂层的性能,增加了轴承适用范围。本实施例方法制备得到的轴承基体表面的微织构能够提高轴承基体与复合涂层之间的结合强度,且能够收集磨屑及高温润滑相,起到减小磨粒磨损及提供二次润滑作用,从而提高轴承寿命。The bearing of the embodiment of the present invention has a good self-lubricating effect in a wide temperature range. When the working temperature is low, the MoTeHfC coating can play a lubricating effect; when the working temperature is high, TiVZnN, MoTeHfC and oxygen in the air will occur After the reaction, ZnMoO 4 and V 2 O 5 compounds with high temperature lubricating effect are generated, which can play a good lubricating effect under high temperature conditions. The bearing of the embodiment of the present invention does not need lubricating oil and complex lubrication system, and has a simple structure and is convenient to use; the TiVZnN+MoTeHfC laminated coating improves the performance of a single coating and increases the application range of the bearing. The micro-texture on the surface of the bearing base prepared by the method in this embodiment can improve the bonding strength between the bearing base and the composite coating, and can collect wear debris and high-temperature lubricating phases, thereby reducing abrasive wear and providing secondary lubrication function, thereby increasing bearing life.
实施例1Example 1
采用激光加工技术在轴承基体的表面制备微织构,激光功率为12W,频率为20kHz,扫描速度为10mm/s,微织构宽度为50μm,织构深度为100μm;打开Ti靶和VZnN靶,调整工作气压为0.5Pa,偏压为150V,调整Ti靶电流为50A,VZnN靶电流调至60A,沉积TiVZnN层5min;开启MoTe2靶、Hf靶和C靶,调整工作气压为0.5Pa,偏压为100V,调整MoTe2靶电流为90A,Hf靶电流为30A,C靶电流为60A,沉积MoTeHfC层8min;交替沉积TiVZnN层和MoTeHfC层,直至复合涂层总厚度为10μm,得到宽温域自润滑轴承。The microtexture was prepared on the surface of the bearing matrix by laser processing technology. The laser power was 12W, the frequency was 20kHz, the scanning speed was 10mm/s, the microtexture width was 50μm, and the texture depth was 100μm; the Ti target and VZnN target were turned on, Adjust the working pressure to 0.5Pa, the bias voltage to 150V, adjust the Ti target current to 50A, the VZnN target current to 60A, and deposit the TiVZnN layer for 5min; turn on the MoTe 2 target, Hf target and C target, adjust the working pressure to 0.5Pa, and the bias The voltage is 100V, the MoTe 2 target current is adjusted to 90A, the Hf target current is 30A, the C target current is 60A, and the MoTeHfC layer is deposited for 8min; the TiVZnN layer and the MoTeHfC layer are alternately deposited until the total thickness of the composite coating is 10μm, obtaining a wide temperature range Self-lubricating bearings.
制备得到的宽温域自润滑轴承,轴承基体的材料为GCr15轴承钢,轴承基体的表面具有微织构,微织构的表面具有复合涂层。该复合涂层包括交替叠加的10层TiVZnN层和10层MoTeHfC层,且TiVZnN层与MoTeHfC层的单个层的厚度为500nm。TiVZnN层中,Ti元素原子百分比为30%,V元素原子百分比为20%,Zn元素原子百分比为15%,N元素原子百分比为35%。MoTeHfC层中,Mo元素原子百分比为30%,Te元素原子百分比为40%,Hf元素原子百分比为10%,C元素原子百分比为20%。In the prepared wide temperature range self-lubricating bearing, the material of the bearing base is GCr15 bearing steel, the surface of the bearing base has a micro-texture, and the surface of the micro-texture has a composite coating. The composite coating includes 10 layers of TiVZnN layers and 10 layers of MoTeHfC layers that are alternately stacked, and the thickness of a single layer of the TiVZnN layer and the MoTeHfC layer is 500 nm. In the TiVZnN layer, the atomic percentage of Ti element is 30%, the atomic percentage of V element is 20%, the atomic percentage of Zn element is 15%, and the atomic percentage of N element is 35%. In the MoTeHfC layer, the atomic percentage of Mo element is 30%, the atomic percentage of Te element is 40%, the atomic percentage of Hf element is 10%, and the atomic percentage of C element is 20%.
实施例2Example 2
采用激光加工技术在轴承基体的表面制备微织构,激光功率为30W,频率为10kHz,扫描速度为300mm/s,微织构宽度为100μm,微织构深度为50μm;打开Ti靶和VZnN靶,调整工作气压为2.0Pa,偏压为300V,调整Ti靶电流为150A,VZnN靶电流调至80A,沉积TiVZnN层3min;开启MoTe2靶、Hf靶和C靶,调整工作气压为2.0Pa,偏压为120V,调整MoTe2靶电流为100A,Hf靶电流为50A,C靶电流为50A,沉积MoTeHfC层3min;交替沉积TiVZnN层和MoTeHfC层,直至复合涂层总厚度为4μm,得到宽温域自润滑轴承。The microtexture was prepared on the surface of the bearing matrix by laser processing technology. The laser power was 30W, the frequency was 10kHz, the scanning speed was 300mm/s, the width of the microtexture was 100μm, and the depth of the microtexture was 50μm; the Ti target and the VZnN target were turned on. , adjust the working pressure to 2.0Pa, the bias voltage to 300V, adjust the Ti target current to 150A, the VZnN target current to 80A, and deposit the TiVZnN layer for 3 minutes; turn on the MoTe 2 target, Hf target and C target, adjust the working pressure to 2.0Pa, The bias voltage is 120V, the MoTe 2 target current is adjusted to 100A, the Hf target current is 50A, the C target current is 50A, and the MoTeHfC layer is deposited for 3min; the TiVZnN layer and the MoTeHfC layer are alternately deposited until the total thickness of the composite coating is 4μm, and a wide temperature range is obtained. Domain self-lubricating bearings.
制备得到的宽温域自润滑轴承,轴承基体的材料为G8Cr4M04V轴承钢,轴承基体的表面具有微织构,微织构的表面具有复合涂层。该复合涂层包括交替叠加的20层TiVZnN层和20层MoTeHfC层,且TiVZnN层与MoTeHfC层的单个层的厚度为100nm。TiVZnN层中,Ti元素原子百分比为50%,V元素原子百分比为10%,Zn元素原子百分比为10%,N元素原子百分比为30%。MoTeHfC层中,Mo元素原子百分比为40%,Te元素原子百分比为40%,Hf元素原子百分比为8%,C元素原子百分比为12%。In the prepared wide temperature range self-lubricating bearing, the material of the bearing base is G8Cr4M04V bearing steel, the surface of the bearing base has a micro-texture, and the surface of the micro-texture has a composite coating. The composite coating includes 20 layers of TiVZnN layers and 20 layers of MoTeHfC layers alternately stacked, and the thickness of a single layer of the TiVZnN layer and the MoTeHfC layer is 100 nm. In the TiVZnN layer, the atomic percentage of Ti element is 50%, the atomic percentage of V element is 10%, the atomic percentage of Zn element is 10%, and the atomic percentage of N element is 30%. In the MoTeHfC layer, the atomic percentage of Mo element is 40%, the atomic percentage of Te element is 40%, the atomic percentage of Hf element is 8%, and the atomic percentage of C element is 12%.
实施例3Example 3
采用激光加工技术在轴承基体的表面制备微织构,激光功率为50W,频率为25kHz,扫描速度为100mm/s,微织构宽度为200μm,织构深度为200μm;打开Ti靶和VZnN靶,调整工作气压为0.5Pa,偏压为150V,调整Ti靶电流为50A,VZnN靶电流调至60A,沉积TiVZnN层5min;开启MoTe2靶、Hf靶和C靶,调整工作气压为0.5Pa,偏压为100V,调整MoTe2靶电流为90A,Hf靶电流为30A,C靶电流为60A,沉积MoTeHfC层8min;交替沉积TiVZnN层和MoTeHfC层,直至复合涂层总厚度为10μm,得到宽温域自润滑轴承。The microtexture was prepared on the surface of the bearing matrix by laser processing technology. The laser power was 50W, the frequency was 25kHz, the scanning speed was 100mm/s, the microtexture width was 200μm, and the texture depth was 200μm; open the Ti target and the VZnN target, Adjust the working pressure to 0.5Pa, the bias voltage to 150V, adjust the Ti target current to 50A, the VZnN target current to 60A, and deposit the TiVZnN layer for 5min; turn on the MoTe 2 target, Hf target and C target, adjust the working pressure to 0.5Pa, and the bias The voltage is 100V, the MoTe 2 target current is adjusted to 90A, the Hf target current is 30A, the C target current is 60A, and the MoTeHfC layer is deposited for 8min; the TiVZnN layer and the MoTeHfC layer are alternately deposited until the total thickness of the composite coating is 10μm, obtaining a wide temperature range Self-lubricating bearings.
制备得到的宽温域自润滑轴承,轴承基体的材料为GCr15轴承钢,轴承基体的表面具有微织构,微织构的表面具有复合涂层。该复合涂层包括交替叠加的10层TiVZnN层和10层MoTeHfC层,且TiVZnN层与MoTeHfC层的单个层的厚度为500nm。TiVZnN层中,Ti元素原子百分比为40%,V元素原子百分比为15%,Zn元素原子百分比为5%,N元素原子百分比为40%。MoTeHfC层中,Mo元素原子百分比为38%,Te元素原子百分比为30%,Hf元素原子百分比为12%,C元素原子百分比为20%。In the prepared wide temperature range self-lubricating bearing, the material of the bearing base is GCr15 bearing steel, the surface of the bearing base has a micro-texture, and the surface of the micro-texture has a composite coating. The composite coating includes 10 layers of TiVZnN layers and 10 layers of MoTeHfC layers that are alternately stacked, and the thickness of a single layer of the TiVZnN layer and the MoTeHfC layer is 500 nm. In the TiVZnN layer, the atomic percentage of Ti element is 40%, the atomic percentage of V element is 15%, the atomic percentage of Zn element is 5%, and the atomic percentage of N element is 40%. In the MoTeHfC layer, the atomic percentage of Mo is 38%, the atomic percentage of Te is 30%, the atomic percentage of Hf is 12%, and the atomic percentage of C is 20%.
实施例4Example 4
采用激光加工技术在轴承基体的表面制备微织构,激光功率为1W,频率为10kHz,扫描速度为5mm/s,微织构宽度为10μm,微织构深度为5μm;打开Ti靶和VZnN靶,调整工作气压为2.0Pa,偏压为300V,调整Ti靶电流为150A,VZnN靶电流调至80A,沉积TiVZnN层3min;开启MoTe2靶、Hf靶和C靶,调整工作气压为2.0Pa,偏压为120V,调整MoTe2靶电流为100A,Hf靶电流为50A,C靶电流为50A,沉积MoTeHfC层3min;交替沉积TiVZnN层和MoTeHfC层,直至复合涂层总厚度为4μm,得到宽温域自润滑轴承。The microtexture was prepared on the surface of the bearing matrix by laser processing technology. The laser power was 1W, the frequency was 10kHz, the scanning speed was 5mm/s, the width of the microtexture was 10μm, and the depth of the microtexture was 5μm; the Ti target and the VZnN target were turned on. , adjust the working pressure to 2.0Pa, the bias voltage to 300V, adjust the Ti target current to 150A, the VZnN target current to 80A, and deposit the TiVZnN layer for 3 minutes; turn on the MoTe 2 target, Hf target and C target, adjust the working pressure to 2.0Pa, The bias voltage is 120V, the MoTe 2 target current is adjusted to 100A, the Hf target current is 50A, the C target current is 50A, and the MoTeHfC layer is deposited for 3min; the TiVZnN layer and the MoTeHfC layer are alternately deposited until the total thickness of the composite coating is 4μm, and a wide temperature range is obtained. Domain self-lubricating bearings.
制备得到的宽温域自润滑轴承,轴承基体的材料为G8Cr4M04V轴承钢,轴承基体的表面具有微织构,微织构的表面具有复合涂层。该复合涂层包括交替叠加的20层TiVZnN层和20层MoTeHfC层,且TiVZnN层与MoTeHfC层的单个层的厚度为100nm。TiVZnN层中,Ti元素原子百分比为50%,V元素原子百分比为20%,Zn元素原子百分比为10%,N元素原子百分比为20%。MoTeHfC层中,Mo元素原子百分比为40%,Te元素原子百分比为38%,Hf元素原子百分比为12%,C元素原子百分比为10%。In the prepared wide temperature range self-lubricating bearing, the material of the bearing base is G8Cr4M04V bearing steel, the surface of the bearing base has a micro-texture, and the surface of the micro-texture has a composite coating. The composite coating includes 20 layers of TiVZnN layers and 20 layers of MoTeHfC layers alternately stacked, and the thickness of a single layer of the TiVZnN layer and the MoTeHfC layer is 100 nm. In the TiVZnN layer, the atomic percentage of Ti element is 50%, the atomic percentage of V element is 20%, the atomic percentage of Zn element is 10%, and the atomic percentage of N element is 20%. In the MoTeHfC layer, the atomic percentage of Mo is 40%, the atomic percentage of Te is 38%, the atomic percentage of Hf is 12%, and the atomic percentage of C is 10%.
以上显示和描述了本发明的基本原理、主要特征和优点。本领域的技术人员应该了解,本发明不受上述具体实施例的限制,上述具体实施例和说明书中的描述只是为了进一步说明本发明的原理,在不脱离本发明精神和范围的前提下,本发明还会有各种变化和改进,这些变化和改进都落入要求保护的本发明范围内。本发明要求保护的范围由权利要求书及其等效物界定。The foregoing has shown and described the basic principles, main features and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited by the above-mentioned specific embodiments. The above-mentioned specific embodiments and descriptions in the specification are only to further illustrate the principle of the present invention. Without departing from the spirit and scope of the present invention, this Various changes and modifications of the invention are also possible, all of which fall within the scope of the claimed invention. The claimed scope of the present invention is defined by the claims and their equivalents.
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011346102.0A CN112610608B (en) | 2020-11-26 | 2020-11-26 | A kind of wide temperature range self-lubricating bearing and preparation method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011346102.0A CN112610608B (en) | 2020-11-26 | 2020-11-26 | A kind of wide temperature range self-lubricating bearing and preparation method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN112610608A CN112610608A (en) | 2021-04-06 |
CN112610608B true CN112610608B (en) | 2022-07-15 |
Family
ID=75225301
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011346102.0A Active CN112610608B (en) | 2020-11-26 | 2020-11-26 | A kind of wide temperature range self-lubricating bearing and preparation method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN112610608B (en) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104278234A (en) * | 2013-07-02 | 2015-01-14 | 中国科学院兰州化学物理研究所 | Preparation technology for self-lubricating coating with wide temperature range of room temperature to 800 DEG C |
WO2017136971A1 (en) * | 2016-02-11 | 2017-08-17 | 广东工业大学 | (ti, al, zr)n multi-component composite coating, graded structure ultrafine hard alloy cutting tool with the composite coating, and method for manufacturing same |
CN110343991A (en) * | 2019-06-13 | 2019-10-18 | 东南大学 | A kind of antifriction antiwear self-lubricating coat in use bearing and preparation method thereof |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4812352A (en) * | 1986-08-25 | 1989-03-14 | Minnesota Mining And Manufacturing Company | Article having surface layer of uniformly oriented, crystalline, organic microstructures |
JP4711177B2 (en) * | 2005-06-14 | 2011-06-29 | 三菱マテリアル株式会社 | Surface coated cemented carbide cutting tool with excellent wear resistance due to lubricity coating layer |
CN100371496C (en) * | 2005-07-07 | 2008-02-27 | 浙江大学 | A kind of self-lubricating multi-layer composite coating and preparation method thereof |
JP2008095903A (en) * | 2006-10-13 | 2008-04-24 | Ihi Corp | Plain bearing with texture and method for estimating performance thereof |
JP5485922B2 (en) * | 2011-01-28 | 2014-05-07 | 日本精工株式会社 | Rolling device |
JP5981097B2 (en) * | 2011-05-25 | 2016-08-31 | 大同メタル工業株式会社 | Al alloy bearing and manufacturing method of Al alloy bearing |
CN103162452B (en) * | 2013-03-05 | 2015-04-15 | 日出东方太阳能股份有限公司 | Inoxidizability solar spectrum selective absorbing coating and preparation method thereof |
CN109338287B (en) * | 2018-08-15 | 2021-02-26 | 南京理工大学 | Textured Ta/Ag wide-temperature-zone self-lubricating coating and preparation method thereof |
CN111286701B (en) * | 2018-12-07 | 2022-03-15 | 中国科学院宁波材料技术与工程研究所 | A wide temperature range wear-resistant lubricating coating and its preparation method and application |
CN110016642B (en) * | 2019-05-13 | 2021-04-27 | 东南大学 | Micro-texture gradient coating cutter and preparation method thereof |
CN110318017B (en) * | 2019-06-13 | 2021-06-11 | 东南大学 | Toughening and reinforcing in-situ reaction type micro-texture self-lubricating bearing and preparation method thereof |
CN110241412B (en) * | 2019-06-13 | 2021-04-06 | 东南大学 | Laminated coating self-lubricating bearing and preparation method thereof |
-
2020
- 2020-11-26 CN CN202011346102.0A patent/CN112610608B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104278234A (en) * | 2013-07-02 | 2015-01-14 | 中国科学院兰州化学物理研究所 | Preparation technology for self-lubricating coating with wide temperature range of room temperature to 800 DEG C |
WO2017136971A1 (en) * | 2016-02-11 | 2017-08-17 | 广东工业大学 | (ti, al, zr)n multi-component composite coating, graded structure ultrafine hard alloy cutting tool with the composite coating, and method for manufacturing same |
CN110343991A (en) * | 2019-06-13 | 2019-10-18 | 东南大学 | A kind of antifriction antiwear self-lubricating coat in use bearing and preparation method thereof |
Also Published As
Publication number | Publication date |
---|---|
CN112610608A (en) | 2021-04-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN110343991B (en) | Antifriction and antiwear self-lubricating coating bearing and preparation method thereof | |
JPH0578821A (en) | Piston ring and its manufacture | |
CN107699859B (en) | Bearing shell all-metal self-lubricating antifriction coating and preparation method thereof | |
JP4359979B2 (en) | Covered sliding member | |
EP0707622A1 (en) | Thermoset polymer/solid lubricant coating system | |
CN106521493A (en) | Diamond-like carbon film of gradient structure and preparation method thereof | |
Fan et al. | Surface composition–lubrication design of Al2O3/Ni laminated composites—Part I: Tribological synergy effect of micro–dimpled texture and diamond–like carbon films in a water environment | |
JP2015059544A (en) | Combination of cylinder bore and piston ring | |
CN102825855A (en) | Ultra-thick CrSiBN composite coating on surface of base body and preparation method thereof | |
CN101665940A (en) | Method for preparing diamond-like composite coating on surface of piston ring | |
CN107460475A (en) | A kind of self-lubricating bearing and preparation method thereof | |
CN112610608B (en) | A kind of wide temperature range self-lubricating bearing and preparation method thereof | |
CN115354288B (en) | Wide-temperature-range low-friction composite coating and preparation method and application thereof | |
CN107245697B (en) | Method for enhancing wear resistance of friction pair of hydraulic system, friction pair of hydraulic system, hydraulic system | |
CN112483549A (en) | Light self-lubricating wear-resistant joint bearing and preparation method thereof | |
CN110241412A (en) | Laminated coating self-lubricating bearing and preparation method thereof | |
CN102644076A (en) | Self-adaptive lubrication coating used in wide temperature ranges and preparing method thereof | |
CN109881138A (en) | A kind of protective coating construction technology | |
CN118028936A (en) | Method for improving tribological performance of silicon carbide reinforced aluminum-based composite material | |
CN112746247A (en) | Self-lubricating gear and preparation method thereof | |
JP4374153B2 (en) | piston ring | |
CN206692735U (en) | A kind of face coat structure of automobile piston rings | |
CN105671496A (en) | MoN/TiBN nano-composite laminated coating tool and manufacturing method thereof | |
RU2613757C2 (en) | Internal combustion engine sleeve | |
JP2022511519A (en) | Manufacturing methods for bearing elements for plain bearings and plain bearings |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |