CN101285136A - A kind of preparation method of porous titanium and porous titanium alloy - Google Patents
A kind of preparation method of porous titanium and porous titanium alloy Download PDFInfo
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- 239000010936 titanium Substances 0.000 title claims abstract description 47
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 title claims abstract description 37
- 229910052719 titanium Inorganic materials 0.000 title claims abstract description 35
- 229910001069 Ti alloy Inorganic materials 0.000 title claims abstract description 34
- 238000002360 preparation method Methods 0.000 title claims abstract description 15
- 239000000843 powder Substances 0.000 claims abstract description 42
- 239000000758 substrate Substances 0.000 claims abstract description 33
- 238000010438 heat treatment Methods 0.000 claims abstract description 27
- 238000000034 method Methods 0.000 claims abstract description 25
- 239000011247 coating layer Substances 0.000 claims abstract description 12
- 239000007921 spray Substances 0.000 claims abstract description 11
- 238000010288 cold spraying Methods 0.000 claims abstract description 9
- 238000005488 sandblasting Methods 0.000 claims abstract description 8
- 238000007788 roughening Methods 0.000 claims abstract description 4
- 238000005507 spraying Methods 0.000 claims description 22
- 239000011148 porous material Substances 0.000 claims description 20
- 239000002245 particle Substances 0.000 claims description 19
- 239000004576 sand Substances 0.000 claims description 10
- 238000009826 distribution Methods 0.000 abstract description 9
- 238000004519 manufacturing process Methods 0.000 abstract description 8
- 238000000576 coating method Methods 0.000 description 29
- 239000011248 coating agent Substances 0.000 description 21
- 239000007789 gas Substances 0.000 description 17
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 8
- 229910000883 Ti6Al4V Inorganic materials 0.000 description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 4
- 229910052786 argon Inorganic materials 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 238000004321 preservation Methods 0.000 description 3
- 238000005245 sintering Methods 0.000 description 3
- 238000010290 vacuum plasma spraying Methods 0.000 description 3
- 239000012620 biological material Substances 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000009718 spray deposition Methods 0.000 description 2
- 230000003746 surface roughness Effects 0.000 description 2
- 238000007751 thermal spraying Methods 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 238000006555 catalytic reaction Methods 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000004053 dental implant Substances 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 238000010285 flame spraying Methods 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000006262 metallic foam Substances 0.000 description 1
- 238000005272 metallurgy Methods 0.000 description 1
- 238000001000 micrograph Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 230000008929 regeneration Effects 0.000 description 1
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- 239000002344 surface layer Substances 0.000 description 1
- 229910000048 titanium hydride Inorganic materials 0.000 description 1
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Abstract
本发明涉及一种多孔钛与多孔钛合金的制备方法,其特征在于制备步骤如下:将Ti粉末或Ti合金粉末在烘箱中烘烤,对平板状基体表面或者棒状基体表面进行喷砂粗化预处理;采用冷喷涂方法在上述基体上喷涂步骤一中准备的Ti粉末或Ti合金粉末,将步骤三得到的涂覆层置于真空热处理炉内进行热处理。本发明的工艺简单,生产周期短,生产成本低廉的特点。利用本发明提出的方法制备的多孔钛与多孔钛合金孔隙度分布较均匀、可控性较好。本发明方法制备的多孔钛与多孔钛合金的孔隙率可在5%~50%范围变化,强度根据孔隙度不同在30~75MPa变化。该方法可控性好、生产效率高,有助于工业化应用。The invention relates to a preparation method of porous titanium and porous titanium alloy, which is characterized in that the preparation steps are as follows: baking Ti powder or Ti alloy powder in an oven, performing sandblasting roughening on the surface of a flat substrate or a rod-shaped substrate. Treatment: Spray the Ti powder or Ti alloy powder prepared in step 1 on the above substrate by cold spraying method, and place the coating layer obtained in step 3 in a vacuum heat treatment furnace for heat treatment. The invention has the characteristics of simple process, short production cycle and low production cost. The porosity distribution of the porous titanium and the porous titanium alloy prepared by the method proposed by the invention is relatively uniform and controllable. The porosity of the porous titanium and porous titanium alloy prepared by the method of the invention can vary from 5% to 50%, and the strength can vary from 30 to 75MPa according to the porosity. The method has good controllability and high production efficiency, and is conducive to industrial application.
Description
技术领域 technical field
本发明涉及一种多孔钛与多孔钛合金的制备方法,采用冷喷涂成形技术,配合真空热处理来获得所需多孔材料。主要适用于生物材料,也可用于特殊情况下的结构材料。The invention relates to a preparation method of porous titanium and porous titanium alloy, which adopts cold spray forming technology and cooperates with vacuum heat treatment to obtain the required porous material. Mainly suitable for biological materials, but also for structural materials in special cases.
背景技术 Background technique
金属泡沫或金属多孔材料是80年代后期国际上迅速发展起来的一种物理功能与结构一体化的新型工程材料。它是一种具有渗透性好、孔隙和孔径可控、形状稳定、耐高温、抗热震、能再生、可加工等特殊性能的功能材料。金属多孔材料广泛应用于航空、航天、原子能、石化、冶金、机械、医药、环保等行业的过滤、分离、消音、布气、催化、热交换等工艺中。近年来,各领域对金属多孔材料的需求大大促进了其发展。另一方面,钛与钛合金因其良好的耐腐蚀性能、高的比强度、优异的生物相容性等特点在航空航天、生物等领域得到广泛应用。在其生物应用中,多孔钛与钛合金的制备是一个需要解决的关键问题,其中还涉及多孔材料质量优劣的重要指标:孔洞尺寸和形状的均匀性。目前已有的多孔钛制备方法主要有:烧结法与热喷涂法。烧结法主要是在钛或钛合金基体上堆积钛球、短钛纤维、钛网或TiH2进行烧结(美国专利US4206516、中国专利03810032.0),但该方法制备的多孔钛与基体结合较差,钛纤维易脱落。热喷涂法主要用于制备多孔钛涂层。1971年美国专利US3605123报道了等离子喷涂TiH2制备多孔钛涂层,但所得涂层的孔隙均匀性较差。1985年美国专利US4542539用火焰喷涂制备了梯度多孔钛涂层,但涂层结合强度低,仅7MPa。日本Kobe Steel公司采用真空等离子喷涂制备出孔隙率40~60%、弹性模量4.7GPa、压缩强度85MPa的多孔钛涂层。Sulzer Calcitek公司将真空等离子喷涂制备的多孔钛涂层成功地应用于牙种植体,并于1997年获得FDA认证,进入市场。但真空等离子喷涂设备昂贵,且仍然存在孔隙均匀性和开孔连通性较差的问题。最近的研究表明[W.-Y.Li,et al.,Ti and Ti-6Al-4V coatings by cold spraying and microstructure modification by heattreatment,Advanced Engineering Materials,2007,9(5),418-423],冷喷涂可用于制备Ti与Ti合金涂层,并且所制备的涂层表现出较高的气孔率;所制备涂层热处理后,涂层与基体的结合强度得到提高。但这些初步的研究只涉及较薄涂层制备,对所制备涂层的本身性能没有表征,喷涂工艺与热处理工艺单一,缺乏系统性。Metal foam or metal porous material is a new type of engineering material that integrates physical function and structure, which developed rapidly internationally in the late 1980s. It is a functional material with special properties such as good permeability, controllable pores and pore sizes, stable shape, high temperature resistance, thermal shock resistance, regeneration, and machinability. Metal porous materials are widely used in filtration, separation, noise reduction, gas distribution, catalysis, heat exchange and other processes in aviation, aerospace, atomic energy, petrochemical, metallurgy, machinery, medicine, environmental protection and other industries. In recent years, the demand for metal porous materials in various fields has greatly promoted their development. On the other hand, titanium and titanium alloys are widely used in aerospace, biology and other fields due to their good corrosion resistance, high specific strength, and excellent biocompatibility. In its biological application, the preparation of porous titanium and titanium alloy is a key problem to be solved, which also involves an important indicator of the quality of porous materials: the uniformity of pore size and shape. At present, the existing porous titanium preparation methods mainly include: sintering method and thermal spraying method. The sintering method is mainly to pile up titanium balls, short titanium fibers, titanium mesh or TiH 2 on the titanium or titanium alloy substrate for sintering (US patent US4206516, Chinese patent 03810032.0), but the porous titanium prepared by this method is poorly bonded to the substrate. Fibers fall off easily. Thermal spraying is mainly used to prepare porous titanium coatings. In 1971, U.S. Patent US3605123 reported the preparation of porous titanium coating by plasma spraying TiH2 , but the pore uniformity of the obtained coating was poor. In 1985, the US patent US4542539 prepared a gradient porous titanium coating by flame spraying, but the bonding strength of the coating was low, only 7MPa. Japan's Kobe Steel Company used vacuum plasma spraying to prepare a porous titanium coating with a porosity of 40-60%, an elastic modulus of 4.7GPa, and a compressive strength of 85MPa. Sulzer Calcitek successfully applied the porous titanium coating prepared by vacuum plasma spraying to dental implants, and obtained FDA certification in 1997 and entered the market. However, vacuum plasma spraying equipment is expensive, and there are still problems of poor uniformity of pores and poor connectivity of openings. Recent studies have shown [W.-Y.Li, et al., Ti and Ti-6Al-4V coatings by cold spraying and microstructure modification by heattreatment, Advanced Engineering Materials, 2007, 9(5), 418-423], cold Spraying can be used to prepare Ti and Ti alloy coatings, and the prepared coatings exhibit high porosity; after heat treatment of the prepared coatings, the bonding strength between the coatings and the substrate is improved. However, these preliminary studies only involve the preparation of thinner coatings, and there is no characterization of the properties of the prepared coatings. The spraying process and heat treatment process are single and lack of system.
发明内容 Contents of the invention
要解决的技术问题technical problem to be solved
为了避免现有技术的不足之处,本发明提出一种多孔钛与多孔钛合金的制备方法,该方法制备的多孔钛与钛合金孔隙度分布较均匀、可控性较好,并且设备、工艺简单,生产周期短,生产成本低廉。In order to avoid the deficiencies of the prior art, the present invention proposes a method for preparing porous titanium and porous titanium alloy. The porosity distribution of porous titanium and titanium alloy prepared by the method is relatively uniform and controllable, and the equipment and process Simple, short production cycle and low production cost.
技术方案Technical solutions
本发明的基本思想是:首先在基体上冷喷涂成形制备钛或钛合金涂覆层,然后进行真空热处理,一是增加沉积颗粒间的结合强度,二是改善孔隙及其分布。The basic idea of the present invention is: first, cold spray forming on the substrate to prepare titanium or titanium alloy coating layer, and then conduct vacuum heat treatment, one is to increase the bonding strength between deposited particles, and the other is to improve the pores and their distribution.
一种多孔钛与多孔钛合金的制备方法,其特征在于制备步骤如下:A method for preparing porous titanium and porous titanium alloy, characterized in that the preparation steps are as follows:
步骤一:将粒度范围在5~200μm的Ti粉末或Ti合金粉末,在80~100℃的烘箱中烘烤1~4小时;Step 1: Bake Ti powder or Ti alloy powder with a particle size ranging from 5 to 200 μm in an oven at 80 to 100° C. for 1 to 4 hours;
步骤二:对平板状基体表面或者棒状基体表面进行喷砂粗化预处理;Step 2: performing sandblasting roughening pretreatment on the surface of the flat substrate or the surface of the rod substrate;
步骤三:采用冷喷涂方法在上述基体上喷涂步骤一中准备的Ti粉末或Ti合金粉末,喷涂时送粉量为:10~100g/min;涂覆层厚度为:100μm~50mm;Step 3: Spray the Ti powder or Ti alloy powder prepared in Step 1 on the above substrate by cold spraying method, the powder feeding amount during spraying is: 10-100g/min; the thickness of the coating layer is: 100μm-50mm;
步骤四:将步骤三得到的涂覆层置于真空热处理炉内进行热处理,真空室真空度要求小于10-3Pa;保温温度在600~900℃;保温时间在1~8小时。Step 4: Place the coating layer obtained in Step 3 for heat treatment in a vacuum heat treatment furnace. The vacuum degree of the vacuum chamber is required to be less than 10 -3 Pa; the holding temperature is 600-900° C.; the holding time is 1-8 hours.
基体需要剥离时,应将基体在步骤四的热处理之前进行剥离。When the substrate needs to be peeled off, the substrate should be peeled off before the heat treatment in Step 4.
所述的Ti粉末或Ti合金粉末的粉末粒度的选择原则是:当要求喷涂完成后的孔隙度小于20%~40%时选择粒度5~100μm的粉末;当要求喷涂完成后的孔隙大于40%时,选择100~200μm的粉末。The selection principle of the particle size of the Ti powder or Ti alloy powder is: when the porosity after spraying is required to be less than 20% to 40%, the powder with a particle size of 5-100 μm is selected; when the porosity after spraying is required to be greater than 40% , choose 100-200μm powder.
所述的喷砂预处理,对于钛或钛合金基体采用-24目的砂粒;对于需剥离的基体采用-100目的砂粒。In the sandblasting pretreatment, -24 mesh sand grains are used for the titanium or titanium alloy substrate; -100 mesh sand grains are used for the substrate to be stripped.
有益效果Beneficial effect
本发明的提出的多孔钛与多孔钛合金的制备方法,具有工艺简单,生产周期短,生产成本低廉的特点。利用本发明提出的方法制备的多孔钛与多孔钛合金孔隙度分布较均匀、可控性较好。本发明方法制备的多孔钛与多孔钛合金的孔隙率可在5%~50%范围变化,强度根据孔隙度不同在30~75MPa变化。该方法可控性好、生产效率高,有助于工业化应用。The preparation method of porous titanium and porous titanium alloy proposed by the present invention has the characteristics of simple process, short production cycle and low production cost. The porosity distribution of the porous titanium and the porous titanium alloy prepared by the method proposed by the invention is relatively uniform and controllable. The porosity of the porous titanium and porous titanium alloy prepared by the method of the invention can vary from 5% to 50%, and the strength can vary from 30 to 75MPa according to the porosity. The method has good controllability and high production efficiency, and is conducive to industrial application.
附图说明 Description of drawings
图1:为实施本发明所涉及的原始粉末形貌照片,其中(a)为Ti粉,粒度11-45μm,(b)为Ti粉,粒度45-160μm,(c)为Ti-6Al-4V粉,粒度11-63μm;Fig. 1: It is the photograph of the original powder appearance involved in implementing the present invention, wherein (a) is Ti powder, particle size 11-45 μ m, (b) is Ti powder, particle size 45-160 μ m, (c) is Ti-6Al-4V Powder, particle size 11-63μm;
图2:为采用图1(a)Ti粉所制备多孔材料断面光镜照片,其中(a)为喷涂态,(b)为热处理态;Figure 2: Light microscope photo of the cross-section of the porous material prepared by using the Ti powder in Figure 1(a), where (a) is the sprayed state, and (b) is the heat-treated state;
图3:为采用图1(b)Ti粉所制备多孔材料断面光镜照片,其中(a)为喷涂态,(b)为热处理态;Figure 3: Light microscope photo of the cross-section of the porous material prepared by using the Ti powder in Figure 1(b), where (a) is the sprayed state, and (b) is the heat-treated state;
图4:为采用图1(c)Ti-6Al-4V粉所制备多孔材料断面光镜照片,其中(a)为喷涂态,(b)为热处理态;Figure 4: Light microscope photo of the cross-section of the porous material prepared by using the Ti-6Al-4V powder in Figure 1(c), where (a) is the sprayed state, and (b) is the heat-treated state;
图5:为采用图1(a)Ti粉在Ti-6Al-4V基体上所制备多孔Ti涂层断面光镜照片,其中(a)为喷涂态,(b)为热处理态。Figure 5: Light micrograph of the cross-section of the porous Ti coating prepared on the Ti-6Al-4V substrate using the Ti powder shown in Figure 1(a), where (a) is sprayed and (b) is heat-treated.
具体实施方式 Detailed ways
现结合实施例对本发明作进一步描述:Now in conjunction with embodiment the present invention will be further described:
实施实例1:Implementation example 1:
选用11-45μm钛粉。基体为45mm×30mm×4mm低碳钢板,喷涂前采用-100目氧化铝细砂进行表面粗化处理。冷喷涂工作气体为压缩空气,喷枪入口处气体压力2.7MPa,气体温度500~520℃;送粉气体为氩气,压力3.0MPa;送粉率大约30g/min;喷涂距离30mm,喷枪移动速度150mm/s。涂覆层厚度约5mm。喷涂后剥离基体,然后进行真空热处理,热处理温度850℃,保温时间4小时,然后随炉冷却到室温。观察涂层断面组织,如图2所示,涂层中气孔分布较均匀。喷涂态平均孔隙率约11%,热处理态平均孔隙率约15%。热处理后,涂层中粒子间接触界面达到冶金结合,结合强度明显提高,从喷涂态的25MPa左右到热处理态的75MPa以上。Choose 11-45μm titanium powder. The substrate is a 45mm×30mm×4mm low-carbon steel plate, and the surface is roughened with -100 mesh alumina fine sand before spraying. The working gas of cold spraying is compressed air, the gas pressure at the inlet of the spray gun is 2.7MPa, and the gas temperature is 500-520°C; the powder feeding gas is argon, the pressure is 3.0MPa; the powder feeding rate is about 30g/min; the spraying distance is 30mm, and the moving speed of the spray gun is 150mm /s. The thickness of the coating layer is about 5mm. After spraying, the substrate is peeled off, and then vacuum heat treatment is carried out, the heat treatment temperature is 850°C, the heat preservation time is 4 hours, and then cooled to room temperature with the furnace. Observe the cross-sectional structure of the coating, as shown in Figure 2, the distribution of pores in the coating is relatively uniform. The average porosity of the sprayed state is about 11%, and the average porosity of the heat treatment state is about 15%. After heat treatment, the contact interface between particles in the coating achieves metallurgical bonding, and the bonding strength is significantly improved, from about 25MPa in the sprayed state to more than 75MPa in the heat treated state.
实施实例2:Implementation example 2:
选用45-160μm钛粉。基体为45mm×30mm×4mm低碳钢板,喷涂前采用-100目氧化铝细砂进行表面粗化处理。冷喷涂工作气体为压缩空气,喷枪入口处气体压力2.8MPa,气体温度约550℃;送粉气体为氩气,压力3.1Mpa;送粉率大约30g/min;喷涂距离30mm,喷枪移动速度150mm/s。涂覆层厚度约5mm。喷涂后剥离基体,然后进行真空热处理,热处理温度850℃,保温时间4小时,然后随炉冷却到室温。观察涂层断面组织,如图3所示,涂层中气孔分布较均匀。喷涂态平均孔隙率约15%,热处理态平均孔隙率约18%。热处理后,涂层中粒子间接触界面达到冶金结合,结合强度明显提高,从喷涂态的18MPa左右到热处理态的70MPa以上。Choose 45-160μm titanium powder. The substrate is a 45mm×30mm×4mm low-carbon steel plate, and the surface is roughened with -100 mesh alumina fine sand before spraying. The working gas of cold spraying is compressed air, the gas pressure at the inlet of the spray gun is 2.8MPa, and the gas temperature is about 550°C; the powder feeding gas is argon, the pressure is 3.1Mpa; the powder feeding rate is about 30g/min; the spraying distance is 30mm, and the moving speed of the spray gun is 150mm/ s. The thickness of the coating layer is about 5mm. After spraying, the substrate is peeled off, and then vacuum heat treatment is carried out, the heat treatment temperature is 850°C, the heat preservation time is 4 hours, and then cooled to room temperature with the furnace. Observe the cross-sectional structure of the coating, as shown in Figure 3, the distribution of pores in the coating is relatively uniform. The average porosity of the sprayed state is about 15%, and the average porosity of the heat treatment state is about 18%. After heat treatment, the contact interface between particles in the coating achieves metallurgical bonding, and the bonding strength is significantly improved, from about 18MPa in the sprayed state to more than 70MPa in the heat treated state.
实施实例3:Implementation example 3:
选用11-63μm的Ti-6Al-4V粉。基体为45mm×30mm×4mm低碳钢板,喷涂前采用-100目氧化铝细砂进行表面粗化处理。冷喷涂工作气体为压缩空气,喷枪入口处气体压力2.8MPa,气体温度约550℃;送粉气体为氩气,压力3.1MPa;送粉率大约30g/min;喷涂距离30mm,喷枪移动速度150mm/s。涂覆层厚度约5mm。喷涂后剥离基体,然后进行真空热处理,热处理温度850℃,保温时间4小时,然后随炉冷却到室温。观察涂层断面组织,如图4所示,涂层中气孔分布较均匀。因钛合金强度高,变形能力差,所制备涂层孔隙率更高,喷涂态平均孔隙率约28%,热处理态平均孔隙率约38%。热处理后,涂层中粒子间接触界面达到冶金结合,结合强度明显提高,从喷涂态的10MPa左右到热处理态的55MPa左右。Choose 11-63μm Ti-6Al-4V powder. The substrate is a 45mm×30mm×4mm low-carbon steel plate, and the surface is roughened with -100 mesh alumina fine sand before spraying. The working gas for cold spraying is compressed air, the gas pressure at the inlet of the spray gun is 2.8MPa, and the gas temperature is about 550°C; the powder feeding gas is argon, the pressure is 3.1MPa; the powder feeding rate is about 30g/min; the spraying distance is 30mm, and the moving speed of the spray gun is 150mm/ s. The thickness of the coating layer is about 5mm. After spraying, the substrate is peeled off, and then vacuum heat treatment is carried out, the heat treatment temperature is 850°C, the heat preservation time is 4 hours, and then cooled to room temperature with the furnace. Observe the cross-sectional structure of the coating, as shown in Figure 4, the distribution of pores in the coating is relatively uniform. Because the titanium alloy has high strength and poor deformation ability, the porosity of the prepared coating is higher, the average porosity of the sprayed state is about 28%, and the average porosity of the heat treated state is about 38%. After heat treatment, the contact interface between particles in the coating achieves metallurgical bonding, and the bonding strength is significantly improved, from about 10MPa in the sprayed state to about 55MPa in the heat treated state.
实施实例4:Implementation example 4:
选用11-45μm钛粉。基体为直径25.4mm、长度10mm的Ti-6Al-4V圆盘状试样,喷涂前采用-24目氧化铝细砂进行表面粗化处理。冷喷涂工作气体为压缩空气,喷枪入口处气体压力3.0MPa,气体温度500~520℃;送粉气体为氩气,压力3.3MPa;送粉率大约30g/min;喷涂距离30mm,喷枪移动速度150mm/s。涂覆层厚度约0.7mm。喷涂后直接进行真空热处理,热处理温度800℃,保温时间4小时,然后随炉冷却到室温。观察涂层断面组织,如图5所示,涂层表层300μm内气孔分布较均匀,且气孔率较高。涂层与基体结合良好。喷涂态平均孔隙率约7%,热处理态平均孔隙率约13%。热处理后,涂层中粒子间接触界面达到冶金结合,结合强度明显提高,从喷涂态的25MPa左右到热处理态的70MPa以上。Choose 11-45μm titanium powder. The substrate is a disc-shaped sample of Ti-6Al-4V with a diameter of 25.4mm and a length of 10mm, and the surface is roughened with -24 mesh alumina fine sand before spraying. The working gas for cold spraying is compressed air, the gas pressure at the inlet of the spray gun is 3.0MPa, and the gas temperature is 500-520°C; the powder feeding gas is argon, the pressure is 3.3MPa; the powder feeding rate is about 30g/min; the spraying distance is 30mm, and the moving speed of the spray gun is 150mm /s. The thickness of the coating layer is about 0.7mm. Vacuum heat treatment is carried out directly after spraying, the heat treatment temperature is 800 ℃, the holding time is 4 hours, and then cooled to room temperature with the furnace. Observing the section structure of the coating, as shown in Figure 5, the distribution of pores within 300 μm of the surface layer of the coating is relatively uniform, and the porosity is relatively high. The coating is well bonded to the substrate. The average porosity of the sprayed state is about 7%, and the average porosity of the heat treated state is about 13%. After heat treatment, the contact interface between particles in the coating achieves metallurgical bonding, and the bonding strength is significantly improved, from about 25MPa in the sprayed state to more than 70MPa in the heat treated state.
实施本发明方法时,粉末粒度及范围根据所要求孔隙度及孔隙尺寸等来选择,当要求孔隙度小于20%~40%,选择粒度5~100μm;当要求孔隙大于40%时,选择100~200μm的粉末进行喷涂。When implementing the inventive method, the powder particle size and scope are selected according to required porosity and pore size etc., when requiring porosity to be less than 20%~40%, select particle size 5~100 μ m; When requiring porosity greater than 40%, select 100~ 200μm powder for spraying.
基体材料种类选择,根据所需基体生物材料种类而定,以便形成多孔钛或多孔钛合金。当要求独立多孔钛或多孔钛合金材料时,需考虑制备涂覆层的剥离,选择一般工业金属材料做为基体即可,如碳钢等,在喷涂后采用机械捶击或机械加工方法剥离基体。The type of matrix material is selected according to the type of matrix biological material required, so as to form porous titanium or porous titanium alloy. When independent porous titanium or porous titanium alloy materials are required, it is necessary to consider the peeling of the prepared coating layer. Just choose general industrial metal materials as the substrate, such as carbon steel, etc., and use mechanical hammering or mechanical processing to peel off the substrate after spraying .
喷砂预处理也是根据应用需要而定,对于钛或钛合金基体,要求喷砂粗化效果好,表面粗糙度大,采用-24目砂粒;对于需剥离的基体表面,可简单喷砂处理,表面粗糙度小,采用-100目砂粒。The sandblasting pretreatment is also determined according to the application requirements. For titanium or titanium alloy substrates, it is required that the sandblasting roughening effect is good and the surface roughness is large, and -24 mesh sand particles are used; for the substrate surface that needs to be stripped, simple sandblasting treatment can be used. The surface roughness is small, using -100 mesh sand grains.
涂覆层的制备,要求喷涂时送粉量在10~100g/min。The preparation of the coating layer requires that the powder feeding amount during spraying be 10-100g/min.
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
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CN101838785A (en) * | 2010-06-01 | 2010-09-22 | 中国航空工业集团公司北京航空材料研究院 | Post weld vacuum heat treatment process of TC18 titanium alloy welding component |
CN102303117A (en) * | 2011-08-27 | 2012-01-04 | 北京科技大学 | Method for preparing porous heat exchange surface of TiAl-based intermetallic compound |
CN102443796A (en) * | 2011-12-02 | 2012-05-09 | 九江学院 | Porous Fe-Al intermetallic compound coating and preparation method thereof |
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CN101838785A (en) * | 2010-06-01 | 2010-09-22 | 中国航空工业集团公司北京航空材料研究院 | Post weld vacuum heat treatment process of TC18 titanium alloy welding component |
CN101838785B (en) * | 2010-06-01 | 2011-12-21 | 中国航空工业集团公司北京航空材料研究院 | Post weld vacuum heat treatment process of TC18 titanium alloy welding component |
CN102303117A (en) * | 2011-08-27 | 2012-01-04 | 北京科技大学 | Method for preparing porous heat exchange surface of TiAl-based intermetallic compound |
CN102443796A (en) * | 2011-12-02 | 2012-05-09 | 九江学院 | Porous Fe-Al intermetallic compound coating and preparation method thereof |
CN102443796B (en) * | 2011-12-02 | 2014-01-22 | 九江学院 | Porous Fe-Al intermetallic compound coating and its preparation method |
CN107523717A (en) * | 2016-06-21 | 2017-12-29 | 张家港市思杰五金工具有限公司 | A kind of preparation method of POROUS TITANIUM |
CN108309063A (en) * | 2017-01-17 | 2018-07-24 | 佛山市顺德区美的电热电器制造有限公司 | The preparation method of cookware, cooking apparatus and cookware |
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CN114411140A (en) * | 2022-01-19 | 2022-04-29 | 西部宝德科技股份有限公司 | Preparation method of porous titanium coating |
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