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CN110586936A - Preparation method of 3D printing low-cost high-strength titanium alloy part - Google Patents

Preparation method of 3D printing low-cost high-strength titanium alloy part Download PDF

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Publication number
CN110586936A
CN110586936A CN201910876959.4A CN201910876959A CN110586936A CN 110586936 A CN110586936 A CN 110586936A CN 201910876959 A CN201910876959 A CN 201910876959A CN 110586936 A CN110586936 A CN 110586936A
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powder
pure titanium
titanium alloy
cost high
alloy part
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杨鑫
孙朝晖
张兆洋
王犇
马文君
王婉琳
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Xian University of Technology
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Xian University of Technology
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20Direct sintering or melting
    • B22F10/28Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/14Treatment of metallic powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/36Process control of energy beam parameters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/36Process control of energy beam parameters
    • B22F10/366Scanning parameters, e.g. hatch distance or scanning strategy
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y10/00Processes of additive manufacturing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B33ADDITIVE MANUFACTURING TECHNOLOGY
    • B33YADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y40/00Auxiliary operations or equipment, e.g. for material handling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/30Process control
    • B22F10/34Process control of powder characteristics, e.g. density, oxidation or flowability
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
    • B22F12/10Auxiliary heating means
    • B22F12/13Auxiliary heating means to preheat the material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F12/00Apparatus or devices specially adapted for additive manufacturing; Auxiliary means for additive manufacturing; Combinations of additive manufacturing apparatus or devices with other processing apparatus or devices
    • B22F12/60Planarisation devices; Compression devices
    • B22F12/63Rollers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00Making metallic powder or suspensions thereof
    • B22F9/02Making metallic powder or suspensions thereof using physical processes
    • B22F9/04Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling
    • B22F2009/043Making metallic powder or suspensions thereof using physical processes starting from solid material, e.g. by crushing, grinding or milling by ball milling
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00Technologies related to metal processing
    • Y02P10/25Process efficiency

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Automation & Control Theory (AREA)
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Abstract

The invention discloses a preparation method of a 3D printing low-cost high-strength titanium alloy part, which is implemented by the following steps: step 1, firstly, modifying pure titanium powder; step 2, mixing the pure titanium powder modified in the step 1 with spherical pure titanium powder to obtain mixed powder; step 3, preparing the mixed powder obtained in the step 2 into a deposition state part by adopting a selective laser melting technology; the preparation method provided by the invention solves the problems of overhigh cost and overlow performance of raw material powder for cheap medical and automobile parts for 3D printing.

Description

一种3D打印低成本高强钛合金零部件的制备方法A preparation method of 3D printing low-cost high-strength titanium alloy parts

技术领域technical field

本发明属于3D打印技术领域,具体涉及一种3D打印低成本高强钛合金零部件的制备方法。The invention belongs to the technical field of 3D printing, and in particular relates to a method for preparing 3D printing low-cost high-strength titanium alloy parts.

背景技术Background technique

金属粉床3D打印技术所采用的原料要求纯度高、流动性好、粒径分布均匀、球形度高等。目前主要采用等离子旋转电极法、气雾化法、射频等离子体球化法生产满足3D打印用的粉末,但是生产的粉末成本昂贵,高达4000元/kg左右。高纯球形纯钛粉末可用来成形航空航天等高昂零部件,但是对于高性能的廉价零部件,使用球形粉则成本过高。氢化脱氢法制备的纯钛粉末价格在300~500元/kg左右,但是该粉末为不规则形状,流动性差,不能直接用于金属粉床3D打印,因此,针对高性能的廉价零部件,开发一种满足3D打印用的低成本高强钛合金零部件的技术尤为重要。The raw materials used in metal powder bed 3D printing technology require high purity, good fluidity, uniform particle size distribution, and high sphericity. At present, the plasma rotating electrode method, gas atomization method, and radio frequency plasma spheroidization method are mainly used to produce powders suitable for 3D printing, but the cost of the powders produced is expensive, as high as 4,000 yuan/kg. High-purity spherical pure titanium powder can be used to form expensive parts such as aerospace, but for high-performance inexpensive parts, the cost of using spherical powder is too high. The price of pure titanium powder prepared by hydrodehydrogenation is about 300-500 yuan/kg, but the powder is irregular in shape and has poor fluidity, so it cannot be directly used for metal powder bed 3D printing. Therefore, for high-performance and cheap parts, It is particularly important to develop a technology that meets the requirements of low-cost high-strength titanium alloy parts for 3D printing.

发明内容Contents of the invention

本发明的目的是提供一种3D打印低成本高强钛合金零部件的制备方法,解决了3D打印廉价零部件的原料粉末成本过高以及性能过低的问题。The purpose of the present invention is to provide a method for preparing 3D printing low-cost high-strength titanium alloy parts, which solves the problems of high cost and low performance of raw material powder for 3D printing cheap parts.

本发明所采用的技术方案是,一种3D打印低成本高强钛合金零部件的制备方法,具体按以下步骤实施:The technical solution adopted in the present invention is a method for preparing 3D printing low-cost high-strength titanium alloy parts, which is specifically implemented according to the following steps:

步骤1,首先对纯钛粉进行改性;Step 1, first modifying the pure titanium powder;

步骤2,将经步骤1改性处理后的纯钛粉与球形纯钛粉混合,得到混合粉;Step 2, mixing the pure titanium powder modified in step 1 with spherical pure titanium powder to obtain a mixed powder;

步骤3,将经步骤2得到的混合粉采用激光选区熔化技术制备具沉积态零部件;Step 3, using the mixed powder obtained in step 2 to prepare deposited parts by laser selective melting technology;

本发明的特点还在于:The present invention is also characterized in that:

其中步骤1中采用高转速球磨工艺对氢化脱氢法制备的形状不规则的纯钛粉进行改性;Wherein step 1 adopts high-speed ball milling process to modify the irregularly shaped pure titanium powder prepared by hydrodehydrogenation;

其中高转速球磨工艺具体包括:使用转速1200r/min的高速振动球磨机对氢化脱氢制备的纯钛粉末进行球磨,球料比为5:1,球磨过程中添加占总质量1.5~5%的硬脂酸;The high-speed ball milling process specifically includes: using a high-speed vibrating ball mill with a speed of 1200r/min to mill the pure titanium powder prepared by hydrogenation dehydrogenation, the ball-to-material ratio is 5:1, and adding 1.5-5% of the total mass during the ball milling process. Fatty acid;

其中步骤2中进行混合之前将经步骤1改性的纯钛粉进行筛分,筛选后纯钛粉粒径不大于53μm;Wherein, before mixing in step 2, the pure titanium powder modified in step 1 is sieved, and the particle size of the pure titanium powder after screening is not greater than 53 μm;

其中步骤2中将经步骤1改性处理后的纯钛粉和球形纯钛粉在全方位行星式球磨机中进行混合;Wherein in the step 2, the pure titanium powder and the spherical pure titanium powder after the modification treatment in the step 1 are mixed in an omnidirectional planetary ball mill;

其中球形纯钛粉和改性处理后的纯钛粉混合比例为8:2或7:3;The mixing ratio of spherical pure titanium powder and modified pure titanium powder is 8:2 or 7:3;

其中全方位行星式球磨机的运动频率为23Hz~30Hz,混合时间为1h~1.5h;Among them, the motion frequency of the omnidirectional planetary ball mill is 23Hz-30Hz, and the mixing time is 1h-1.5h;

其中全方位行星式球磨机混合结束后将混合粉放入干燥箱中进行烘干1h~1.5h,干燥箱温度为110℃~120℃;Among them, after the omnidirectional planetary ball mill is mixed, put the mixed powder into the drying box for drying for 1h~1.5h, and the temperature of the drying box is 110℃~120℃;

其中步骤3中激光选区熔化技术的工艺参数为:激光束斑尺寸为45μm~50μm,激光功率为80w~100w,扫描速度为500mm·s-1~650mm·s-1,预热温度为180℃~200℃,每层铺粉厚度为25μm;The process parameters of the laser selective melting technology in step 3 are: the laser beam spot size is 45 μm ~ 50 μm, the laser power is 80w ~ 100w, the scanning speed is 500mm·s -1 ~ 650mm·s -1 , and the preheating temperature is 180°C ~200℃, the thickness of each layer of powder coating is 25μm;

其中激光选区熔化技术工作前对激光选区熔化设备冲入氩气至设备内空气氧含量不大于0.2%~0.5%。Among them, before the laser selective melting technology works, the laser selective melting equipment is flushed with argon until the oxygen content of the air in the equipment is not more than 0.2% to 0.5%.

本发明的有益效果是:The beneficial effects of the present invention are:

传统的3D制备的钛合金零部件所需的原料的成本过高,本发明一种3D打印低成本高强钛合金零部件的制备方法的提出,从原料降低成本,并且从原料改变零部件的性能,以激光选区熔化的方法制备钛合金零部件,其硬度和强度明显高于传统制备方法;The cost of raw materials required for traditional 3D-prepared titanium alloy parts is too high. The present invention proposes a preparation method for 3D printing low-cost high-strength titanium alloy parts, which reduces the cost from raw materials and changes the performance of parts from raw materials. , the titanium alloy parts are prepared by selective laser melting, and its hardness and strength are significantly higher than those of traditional preparation methods;

附图说明Description of drawings

图1为本发明的一种3D打印低成本高强钛合金零部件的制备方法中氢化脱氢生成的纯钛粉改性前的SEM图;Fig. 1 is the SEM figure before the modification of the pure titanium powder generated by hydrogenation dehydrogenation in a kind of preparation method of 3D printing low-cost high-strength titanium alloy parts of the present invention;

图2为本发明的一种3D打印低成本高强钛合金零部件的制备方法中氢化脱氢生成的纯钛粉改性后的SEM图;Fig. 2 is the SEM diagram of the modified pure titanium powder generated by hydrogenation dehydrogenation in a kind of preparation method of 3D printing low-cost high-strength titanium alloy parts of the present invention;

图3为本发明的一种3D打印低成本高强钛合金零部件的制备方法中球形纯钛粉的SEM图;Fig. 3 is the SEM figure of spherical pure titanium powder in the preparation method of a kind of 3D printing low-cost high-strength titanium alloy part of the present invention;

图4为本发明的一种3D打印低成本高强钛合金零部件的制备方法中混合后形成的粉末的SEM图;Fig. 4 is the SEM diagram of the powder formed after mixing in a kind of preparation method of 3D printing low-cost high-strength titanium alloy parts of the present invention;

图5为本发明一种3D打印低成本高强钛合金零部件的制备方法中不同粉末配比的成形件图;Fig. 5 is a forming part diagram of different powder ratios in a preparation method of a 3D printing low-cost high-strength titanium alloy part of the present invention;

图6为本发明一种3D打印低成本高强钛合金零部件的制备方法中不同粉末配比压缩应力应变曲线图;Fig. 6 is a graph of compressive stress-strain curves of different powder ratios in a preparation method of 3D printing low-cost high-strength titanium alloy parts of the present invention;

具体实施方式Detailed ways

下面结合附图和具体实施方式对本发明进行详细说明。The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

本发明提供一种3D打印低成本高强钛合金零部件的制备方法,具体按以下步骤实施:The invention provides a method for preparing 3D printing low-cost high-strength titanium alloy parts, which is specifically implemented according to the following steps:

步骤1,采用高转速球磨工艺对氢化脱氢法制备的形状不规则的纯钛粉(如图1所示)进行改性:高转速球磨工艺具体包括使用转速1200r/min的高速振动球磨机对氢化脱氢制备的纯钛粉末进行球磨,球料比为5:1,罐和球的材质均为不锈钢,球磨过程中添加占总质量1.5~5%的硬脂酸;Step 1, using a high-speed ball milling process to modify the irregularly shaped pure titanium powder (as shown in Figure 1) prepared by the hydrodehydrogenation method: the high-speed ball milling process specifically includes using a high-speed vibrating ball mill with a speed of 1200r/min to hydrogenate The pure titanium powder prepared by dehydrogenation is ball milled, the ball to material ratio is 5:1, the material of the tank and the ball are all stainless steel, and stearic acid accounting for 1.5-5% of the total mass is added during the ball milling process;

其中高转速球磨的过程可使形状不规则粉末的同时发生形貌改性和物相改性,形貌的改性主要体现在不规则粉末的棱角钝化,部分发生破碎,粒径分布降低,外观形貌近球化;物相改性是利用球磨过程中摩擦生热产生高温,使过量的硬脂酸的分解后与纯钛粉末原位形成非化学计量的氢化钛和碳化钛,在粉末中形成弥散的第二相;Among them, the process of high-speed ball milling can make the powder with irregular shape undergo shape modification and phase modification at the same time. The modification of shape is mainly reflected in the passivation of the corners of the irregular powder, partial crushing, and the decrease of particle size distribution. Appearance and morphology are nearly spherical; phase modification is to use the frictional heat generated in the ball milling process to generate high temperature, so that the excess stearic acid is decomposed and in situ with pure titanium powder to form non-stoichiometric titanium hydride and titanium carbide, in the powder A dispersed second phase is formed in

其中硬脂酸是一种低成本的18碳链饱和脂肪酸,其分解温度在63℃,故而过量的硬脂酸在高能球磨过程中会分解为碳、氢等元素,为粉末的物相改性提供元素;Among them, stearic acid is a low-cost 18-carbon chain saturated fatty acid, and its decomposition temperature is 63°C, so the excess stearic acid will be decomposed into carbon, hydrogen and other elements during the high-energy ball milling process, which is the phase modification of the powder provide elements;

步骤2,将经步骤1改性处理后的纯钛粉(如图2所示)与球形纯钛粉混合,得到混合粉:首先将经步骤1改性的纯钛粉进行筛分,筛选后纯钛粉粒径不大于53μm,然后将改性处理后的纯钛粉和球形纯钛粉在全方位行星式球磨机中进行混合,如图3所示,球形纯钛粉的D50为100μm,不同于以往的激光选区熔化采用球形粉末的平均粒径为15μm~53μm,粒径较大的球形粉末之间的空隙增大,球形纯钛粉与改性后的钛粉混合比例为8:2或7:3,全方位行星式球磨机的运动频率为23Hz~30Hz,混合时间为1h~1.5h,混合结束后将混合粉放入干燥箱中进行烘干1h~1.5h,干燥箱温度为110℃~120℃,烘干主要是去除混合粉末吸附的水分;Step 2, mixing the pure titanium powder modified in step 1 (as shown in Figure 2) with spherical pure titanium powder to obtain a mixed powder: first, sieve the pure titanium powder modified in step 1, and after screening The particle size of pure titanium powder is not more than 53 μm, and then the modified pure titanium powder and spherical pure titanium powder are mixed in an omnidirectional planetary ball mill, as shown in Figure 3, the D 50 of spherical pure titanium powder is 100 μm, Different from the previous laser selective melting, the average particle size of the spherical powder is 15 μm to 53 μm, and the gap between the spherical powder with larger particle size increases. The mixing ratio of spherical pure titanium powder and modified titanium powder is 8:2 Or 7:3, the motion frequency of the omnidirectional planetary ball mill is 23Hz~30Hz, the mixing time is 1h~1.5h, after the mixing is completed, put the mixed powder into the drying oven for 1h~1.5h, and the temperature of the drying oven is 110 ℃~120℃, drying is mainly to remove the moisture absorbed by the mixed powder;

步骤3,将经步骤2得到的混合粉(如图4所示)采用激光选区熔化技术制备具沉积态零部件:用CONCEPT公司生产的Concept Laser MLABcusing R型激光金属增材制造加工系统对混合粉末进行打印,首先利用Solidworks软件、Pro/Engineer软件或Unigraphic软件建立三维实体模型,然后对三维立体模型利用Magics软件进行分层切片,获取在不同高度上分层的信息;然后将将经处理过的混合粉在激光增材制造机配套的手套箱中冲入氩气,待打印室内的空气氧含量降低至0.2~0.5%以下后,将混合粉装入料仓中,然后铺粉辊均匀铺粉,每层铺粉厚度为25μm,当每一层粉铺好之后,扫描系统在计算机的控制下开始按得到的分层信息打印,经激光扫描、熔化以及成形过程,不断重复扫描至成形过程,直至三维零件制造完成,其中激光选区熔化技术的工艺参数为:激光束斑尺寸为45μm~50μm,激光功率为80w~100w,扫描速度为500mm·s-1~650mm·s-1,预热温度为180℃~200℃。Step 3, use the mixed powder obtained in step 2 (as shown in Figure 4) to prepare deposited parts by laser selective melting technology: use the Concept Laser MLABcusing R-type laser metal additive manufacturing processing system produced by CONCEPT to process the mixed powder For printing, first use Solidworks software, Pro/Engineer software or Unigraphic software to establish a three-dimensional solid model, and then use Magics software to layer and slice the three-dimensional model to obtain layered information at different heights; then the processed The mixed powder is poured into the argon gas in the glove box of the laser additive manufacturing machine. After the oxygen content of the air in the printing room is reduced to below 0.2-0.5%, the mixed powder is loaded into the silo, and then the powder spreading roller is evenly spread. The thickness of each layer of powder is 25 μm. When each layer of powder is laid, the scanning system starts to print according to the obtained layered information under the control of the computer. After laser scanning, melting and forming processes, the scanning is repeated until the forming process. Until the three-dimensional parts are manufactured, the process parameters of the laser selective melting technology are: the laser beam spot size is 45 μm ~ 50 μm, the laser power is 80w ~ 100w, the scanning speed is 500mm·s -1 ~ 650mm·s -1 , the preheating temperature It is 180°C to 200°C.

从原料制备和成形过程解释本发明的一种3D打印低成本高强钛合金零部件的制备方法的优点:传统的3D打印粉末原料成本高,将低成本的氢化脱氢钛粉与硬脂酸混合后进行高能球磨,改善粉末的流动性,并且利用硬脂酸的分解,提供碳、氢等固溶元素,与纯钛粉末原位形成非化学计量的氢化钛和碳化钛第二相,球磨将改性的粉末与球形粉混合,提升打印原料的流动性和松装密度,本发明提出以激光选区熔化技术成形高性能的钛合金零部件,是利用间隙元素与钛的固溶强化以及弥散强化提升成形件的强度和硬度,明显高于传统制备方法;The advantages of the preparation method of a 3D printing low-cost high-strength titanium alloy parts of the present invention are explained from the raw material preparation and forming process: the traditional 3D printing powder raw material costs are high, and the low-cost hydrogenated dehydrogenated titanium powder is mixed with stearic acid Afterwards, high-energy ball milling is carried out to improve the fluidity of the powder, and the decomposition of stearic acid is used to provide solid solution elements such as carbon and hydrogen to form a non-stoichiometric second phase of titanium hydride and titanium carbide in situ with the pure titanium powder. Ball milling will The modified powder is mixed with the spherical powder to improve the fluidity and bulk density of the printing material. This invention proposes to use laser selective melting technology to form high-performance titanium alloy parts, which uses the solid solution strengthening and dispersion strengthening of interstitial elements and titanium. Improve the strength and hardness of formed parts, significantly higher than traditional preparation methods;

实施例1Example 1

步骤1,对氢化脱氢的纯钛粉放入转速为1200r/min高速振动球磨机进行球磨时间分别为15min、30min、45min和60min的球磨,硬脂酸的添加量为5%,改性粉末SEM形貌如图1所示,发现球磨时间为15min和30min时纯钛粉的尖锐棱角钝化,形貌近球形,超过30min后纯钛粉就会剧烈细化,出现严重的团聚现象,在球磨时间30min的纯钛粉也有轻微的团聚现象,所以对球磨时间为15min的纯钛粉性能进一步表征:球磨15min的纯钛粉最大粒径为45.2μm,最小粒径为12.1μm,平均粒径为23.2μm,球磨前的休止角为38.7°,改性后的纯钛粉休止角为34.3°,高转速短时间的球磨即可满足粉末流动性的要求,降低了原料的成本,进一步表明纯钛粉改性使用高转速的条件输入高能量,可以实现纯钛粉破碎和尖角钝化,提高改性粉末的流动性,但是球磨时间应严格控制,时间越长,球磨罐内的温度越高,达到硬脂酸分解温度63℃以上,即可通过控制硬脂酸的添加量实现对纯钛粉的物相定性调控;Step 1, put the hydrodehydrogenated pure titanium powder into a high-speed vibrating ball mill with a rotating speed of 1200r/min for ball milling with the ball milling time being 15min, 30min, 45min and 60min respectively, the addition of stearic acid is 5%, and the modified powder SEM The morphology is shown in Figure 1. It is found that the sharp edges and corners of the pure titanium powder are passivated when the ball milling time is 15min and 30min, and the morphology is nearly spherical. The pure titanium powder with a time of 30 minutes also has a slight agglomeration phenomenon, so the performance of the pure titanium powder with a ball milling time of 15 minutes is further characterized: the maximum particle size of the pure titanium powder after ball milling for 15 minutes is 45.2 μm, the minimum particle size is 12.1 μm, and the average particle size is 23.2μm, the angle of repose before ball milling is 38.7°, and the angle of repose of the modified pure titanium powder is 34.3°. Ball milling at high speed and short time can meet the requirements of powder fluidity and reduce the cost of raw materials, which further shows that pure titanium powder Powder modification uses high-speed conditions to input high energy, which can achieve pure titanium powder crushing and sharp corner passivation, and improve the fluidity of the modified powder, but the ball milling time should be strictly controlled. The longer the time, the higher the temperature in the ball milling tank , when the decomposition temperature of stearic acid is above 63°C, the qualitative control of the phase of pure titanium powder can be realized by controlling the amount of stearic acid added;

步骤2,将粒径分布为325目~100目(45μm~150μm)的球形纯钛粉末与改性的纯钛粉末按照8:2和7:3的比例混合,在全方位行星式球磨机上,以23Hz的频率运行1h混合均匀,最后在干燥箱中以120℃烘干1h,混合粉的SEM形貌如图2所示;Step 2: Mix the spherical pure titanium powder with a particle size distribution of 325 mesh to 100 mesh (45 μm to 150 μm) and the modified pure titanium powder at a ratio of 8:2 and 7:3, and in the omnidirectional planetary ball mill, Run at a frequency of 23Hz for 1h to mix evenly, and finally dry in a drying oven at 120°C for 1h. The SEM morphology of the mixed powder is shown in Figure 2;

步骤3,通过改变成形工艺参数调控激光能量密度,利用Pro/Engineer分层软件对步骤1的三维实体模型进行切片离散化处理,利用为Magics软件分层,扫描路径为Z字形网格式扫描,搭接率为50%,得到每层的截面数据,然后将各层的截面数据作为激光扫描路径导入激光选区熔化成形设备中,之后在激光选区熔化设备上设定加工参数,加工参数包括金属粉末层厚、束斑直径、搭接率、激光功率、扫描速度;金属粉末层厚为25μm;束斑直径为45μm;所述激光功率为100w;激光扫描速度为550mm/s,预热温度为200℃;Step 3, adjust the laser energy density by changing the forming process parameters, use Pro/Engineer layering software to slice and discretize the 3D solid model in step 1, use Magics software to layer, scan the path in a zigzag grid format, and build The connection rate is 50%, and the cross-sectional data of each layer are obtained, and then the cross-sectional data of each layer are imported into the laser selective melting forming equipment as the laser scanning path, and then the processing parameters are set on the laser selective melting equipment, and the processing parameters include the metal powder layer. Thickness, beam spot diameter, lap rate, laser power, scanning speed; metal powder layer thickness is 25 μm; beam spot diameter is 45 μm; the laser power is 100w; laser scanning speed is 550mm/s, and the preheating temperature is 200°C ;

将经处理过的混合粉末在激光增材制造机配套的手套箱中冲入氩气,待打印室内的空气氧含量降低至0.5%以下后,将混合粉末平铺在底板上,然后采用较大的激光光斑和较高的扫描速度对平铺在底板上的混合粉末进行预热;采用激光按照激光扫描路径对预热后的混合粉末进行选区熔化扫描,形成单层实体片层;升降台下降一层,重复所述的平铺混合粉末并进行预热的加工工艺以及对预热后的混合粉末进行选区熔化扫描形成单层实体片层的加工工艺,直至各层实体均制备完成,得到激光选区熔化成型件;最后采用压缩空气除去成型件中多余的粉末,清洗干净后烘干,得到致密零部件,如图5所示,可以看出成形件的外观为银白色,具有金属光泽,没有过烧或熔合不良现象,并且成形精度在0.3~0.5mm;Pour the processed mixed powder into argon in the glove box of the laser additive manufacturing machine. After the oxygen content in the air in the printing room is reduced to below 0.5%, spread the mixed powder on the bottom plate, and then use a larger The laser spot and high scanning speed are used to preheat the mixed powder on the bottom plate; the laser is used to perform selective melting and scanning on the preheated mixed powder according to the laser scanning path to form a single-layer solid sheet; the lifting platform descends One layer, repeating the process of flat laying the mixed powder and preheating, and performing selective melting and scanning on the preheated mixed powder to form a single-layer solid sheet, until the preparation of each layer of solids is completed, and the laser Melt the molded parts in selected areas; finally use compressed air to remove excess powder in the molded parts, clean them and dry them to obtain compact parts, as shown in Figure 5, it can be seen that the appearance of the molded parts is silvery white with metallic luster, without Overburning or poor fusion, and the forming accuracy is 0.3-0.5mm;

经检测可知,本实施例所制备的钛合金致密度最高为98.32%,不同原料配比的成形件的压缩应力应变曲线如图6所示,可以看出混粉比为8:2(线条a)时的最大抗压强度为1580MPa,混粉比为7:3(线条b)时的抗压强度为1040MPa,混粉比为8:2的强度和塑性均优于混粉比为7:3试样的塑性,8:2的比例成形件的强度和塑性提升的原因是第二相在钛基体的弥散分布得到的效果。It can be seen through testing that the highest density of the titanium alloy prepared in this embodiment is 98.32%, and the compressive stress-strain curves of formed parts with different raw material ratios are shown in Figure 6, and it can be seen that the powder mixing ratio is 8:2 (line a ) is 1580MPa, the compressive strength is 1040MPa when the powder mixing ratio is 7:3 (line b), and the strength and plasticity of the powder mixing ratio of 8:2 are better than that of 7:3 The reason for the plasticity of the specimen, the strength and plasticity of the 8:2 ratio forming part is the effect obtained by the dispersion distribution of the second phase in the titanium matrix.

实施例2Example 2

步骤1,采用1200r/min的高转速球磨工艺对氢化脱氢法制备的形状不规则的纯钛粉进行改性,球磨后的到的纯钛粉粒径不大于53μm,硬脂酸的添加量为1.5%;Step 1, using a high-speed ball milling process of 1200r/min to modify the irregularly shaped pure titanium powder prepared by the hydrodehydrogenation method, the particle size of the pure titanium powder obtained after ball milling is not greater than 53 μm, and the amount of stearic acid added 1.5%;

步骤2,将经步骤1改性处理后的纯钛粉和球形纯钛粉按照2:8在全方位行星式球磨机中进行混合,全方位行星式球磨机的运动频率为30Hz,混合时间为1.5h,结束后将混合粉放入干燥箱中进行烘干1.5h,干燥箱温度为110℃;Step 2, mix the pure titanium powder and spherical pure titanium powder modified in step 1 in the omnidirectional planetary ball mill according to the ratio of 2:8, the motion frequency of the omnidirectional planetary ball mill is 30Hz, and the mixing time is 1.5h , put the mixed powder into the drying oven for drying for 1.5h after the completion, and the temperature of the drying oven is 110°C;

步骤3,将经步骤2得到的混合粉采用激光选区熔化技术制备具沉积态零部件:用CONCEPT公司生产的Concept Laser MLAB cusing R型激光金属增材制造加工系统对混合粉末进行打印,首先利用Solidworks软件建立三维实体模型,然后对三维立体模型利用Magics软件进行分层切片,获取在不同高度上分层的信息;然后将将经处理过的混合粉在激光增材制造机配套的手套箱中冲入氩气,待打印室内的空气氧含量降低至0.2%以下后,将混合粉装入料仓中,然后铺粉辊均匀铺粉,每层铺粉厚度为25μm,当每一层粉铺好之后,扫描系统在计算机的控制下开始按得到的分层信息打印,经激光扫描、熔化以及成形过程,不断重复扫描至成形过程,直至三维零件制造完成,其中激光选区熔化技术的工艺参数为:激光束斑尺寸为50μm,激光功率为80w,扫描速度为650mm·s-1,预热温度为180℃。Step 3, use the mixed powder obtained in step 2 to prepare deposited parts by laser selective melting technology: use the Concept Laser MLAB cusing R laser metal additive manufacturing processing system produced by CONCEPT to print the mixed powder, first use Solidworks The software builds a three-dimensional solid model, and then uses the Magics software to slice the three-dimensional model layered to obtain layered information at different heights; then the processed mixed powder is punched in the glove box of the laser additive manufacturing machine. Inject argon gas, and after the oxygen content in the air in the printing room is reduced to below 0.2%, put the mixed powder into the hopper, and then spread the powder evenly with the powder spreading roller. The thickness of each layer of powder is 25 μm. When each layer of powder is laid After that, the scanning system starts to print according to the obtained layered information under the control of the computer. After laser scanning, melting and forming process, the scanning is repeated until the forming process is completed until the three-dimensional parts are manufactured. The process parameters of the laser selective melting technology are: The laser beam spot size is 50 μm, the laser power is 80w, the scanning speed is 650mm·s -1 , and the preheating temperature is 180°C.

实施例3Example 3

步骤1,采用1200r/min的高转速球磨工艺对氢化脱氢法制备的形状不规则的纯钛粉进行改性,球磨后的到的纯钛粉粒径不大于53μm,硬脂酸的添加量为3%;Step 1, using a high-speed ball milling process of 1200r/min to modify the irregularly shaped pure titanium powder prepared by the hydrodehydrogenation method, the particle size of the pure titanium powder obtained after ball milling is not greater than 53 μm, and the amount of stearic acid added 3%;

步骤2,将经步骤1改性处理后的纯钛粉和球形纯钛粉按照2:8在全方位行星式球磨机中进行混合,全方位行星式球磨机的运动频率为30Hz,混合时间为1.2h,结束后将混合粉放入干燥箱中进行烘干1.2h,干燥箱温度为115℃;Step 2, mix the pure titanium powder and spherical pure titanium powder modified in step 1 in the omnidirectional planetary ball mill according to the ratio of 2:8, the motion frequency of the omnidirectional planetary ball mill is 30Hz, and the mixing time is 1.2h , put the mixed powder into the drying oven for drying for 1.2 hours after the completion, and the temperature of the drying oven is 115°C;

步骤3,将经步骤2得到的混合粉采用激光选区熔化技术制备具沉积态零部件:用CONCEPT公司生产的Concept Laser MLAB cusing R型激光金属增材制造加工系统对混合粉末进行打印,首先利用Unigraphic软件软件建立三维实体模型,然后对三维立体模型利用Magics软件进行分层切片,获取在不同高度上分层的信息;然后将将经处理过的混合粉在激光增材制造机配套的手套箱中冲入氩气,待打印室内的空气氧含量降低至0.3%以下后,将混合粉装入料仓中,然后铺粉辊均匀铺粉,每层铺粉厚度为25μm,当每一层粉铺好之后,扫描系统在计算机的控制下开始按得到的分层信息打印,经激光扫描、熔化以及成形过程,不断重复扫描至成形过程,直至三维零件制造完成,其中激光选区熔化技术的工艺参数为:激光束斑尺寸为48μm,激光功率为90w,扫描速度为600mm·s-1,预热温度为190℃。Step 3, use the mixed powder obtained in step 2 to prepare deposited parts by laser selective melting technology: use the Concept Laser MLAB cusing R laser metal additive manufacturing processing system produced by CONCEPT to print the mixed powder, first use Unigraphic The software software builds a three-dimensional solid model, and then uses the Magics software to slice the three-dimensional model layered to obtain layered information at different heights; then put the processed mixed powder in the glove box of the laser additive manufacturing machine Rush into the argon gas, after the oxygen content in the air in the printing room is reduced to below 0.3%, put the mixed powder into the silo, and then spread the powder evenly with the powder spreading roller, the thickness of each layer of powder is 25 μm, when each layer of powder is spread After finishing, the scanning system starts to print according to the obtained layered information under the control of the computer. After laser scanning, melting and forming process, the scanning is repeated until the forming process is completed until the three-dimensional parts are manufactured. The process parameters of the laser selective melting technology are : The laser beam spot size is 48 μm, the laser power is 90w, the scanning speed is 600mm·s -1 , and the preheating temperature is 190°C.

Claims (10)

1. A preparation method of a 3D printing low-cost high-strength titanium alloy part is characterized by comprising the following steps:
step 1, firstly, modifying pure titanium powder;
step 2, mixing the pure titanium powder modified in the step 1 with spherical pure titanium powder to obtain mixed powder;
and 3, preparing the mixed powder obtained in the step 2 into a deposition state part by adopting a selective laser melting technology.
2. The method for preparing the 3D printed low-cost high-strength titanium alloy part as claimed in claim 1, wherein the pure titanium powder with irregular shape prepared by the hydrogenation and dehydrogenation method is modified by a high-speed ball milling process in step 1.
3. The preparation method of the 3D printed low-cost high-strength titanium alloy part as claimed in claim 2, wherein the high-speed ball milling process specifically comprises: and (2) carrying out ball milling on the pure titanium powder prepared by hydrogenation and dehydrogenation by using a high-speed vibration ball mill with the rotating speed of 1200r/min, wherein the ball-to-material ratio is 5:1, and stearic acid accounting for 1.5-5% of the total mass is added in the ball milling process.
4. The method for preparing the 3D printed low-cost high-strength titanium alloy part according to claim 1, wherein the pure titanium powder modified in the step 1 is sieved before mixing in the step 2, and the particle size of the sieved pure titanium powder is not more than 53 μm.
5. The method for preparing the 3D-printed low-cost high-strength titanium alloy part according to claim 1, wherein the pure titanium powder modified in the step 1 and the spherical pure titanium powder are mixed in an all-directional planetary ball mill in the step 2.
6. The preparation method of the 3D printed low-cost high-strength titanium alloy part as claimed in claim 5, wherein the mixing ratio of the spherical pure titanium powder to the modified pure titanium powder is 8: 2.
7. The preparation method of 3D printing low-cost high-strength titanium alloy parts according to claim 5, wherein the movement frequency of the all-directional planetary ball mill is 23Hz to 30Hz, and the mixing time is 1h to 1.5 h.
8. The preparation method of the 3D printed low-cost high-strength titanium alloy part as claimed in claim 5, wherein the mixed powder is placed into a drying oven for drying for 1-1.5 hours after the all-directional planetary ball mill is mixed, and the temperature of the drying oven is 110-120 ℃.
9. The method for preparing the 3D printed low-cost high-strength titanium alloy part according to claim 1, wherein the process parameters of the selective laser melting technology in the step 3 are as follows: the size of the laser beam spot is 45-50 μm, the laser power is 80-100 w, and the scanning speed is 500mm s-1~650mm·s-1The preheating temperature is 180-200 ℃, and the powder spreading thickness of each layer is 25 mu m.
10. The method for preparing a 3D printed low-cost high-strength titanium alloy part as claimed in claim 9, wherein before the selective laser melting technique is used, argon is injected into the selective laser melting equipment until the oxygen content in the equipment is not more than 0.2% -0.5%.
CN201910876959.4A 2019-09-17 2019-09-17 Preparation method of 3D printing low-cost high-strength titanium alloy part Pending CN110586936A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112077307A (en) * 2020-08-21 2020-12-15 西安理工大学 A kind of preparation method of 3D printing doped graphene high-strength titanium alloy parts
CN114226735A (en) * 2021-11-23 2022-03-25 成都先进金属材料产业技术研究院股份有限公司 Powdery titanium-based brazing filler metal and preparation method thereof

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101284308A (en) * 2007-04-12 2008-10-15 吴旭升 Low nickel austenitic stainless steel power and use thereof
KR101450661B1 (en) * 2014-04-22 2014-10-15 한국지질자원연구원 The method of preparation for ternary titanium carbonitride sintered bodies having enhanced mechanical properties and ternary titanium carbonitride sintered bodies prepared thereby
EP3103568A1 (en) * 2015-06-08 2016-12-14 The Boeing Company Additive manufacturing methods
CN107138732A (en) * 2017-06-15 2017-09-08 北京康普锡威科技有限公司 A kind of method that low cost, short route prepare 3D printing titanium valve
CN107891155A (en) * 2017-10-09 2018-04-10 南方科技大学 Process for manufacturing near-spherical titanium powder and high-performance titanium material
CN108080621A (en) * 2017-11-21 2018-05-29 北京科技大学 Cost laser selective melting titanium valve, its preparation method and titanium preparation method
CN108326282A (en) * 2018-02-02 2018-07-27 广东省材料与加工研究所 A kind of powder injection forming Ti-6Al-4V alloy feedings and preparation method thereof
CN108856701A (en) * 2017-05-08 2018-11-23 东莞华晶粉末冶金有限公司 Stainless base steel feeding and preparation method thereof, stainless base steel green body and preparation method thereof
CN109226773A (en) * 2018-08-20 2019-01-18 北京科技大学 Hollow bolted node sphere of titanium alloy and preparation method thereof

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101284308A (en) * 2007-04-12 2008-10-15 吴旭升 Low nickel austenitic stainless steel power and use thereof
KR101450661B1 (en) * 2014-04-22 2014-10-15 한국지질자원연구원 The method of preparation for ternary titanium carbonitride sintered bodies having enhanced mechanical properties and ternary titanium carbonitride sintered bodies prepared thereby
EP3103568A1 (en) * 2015-06-08 2016-12-14 The Boeing Company Additive manufacturing methods
CN108856701A (en) * 2017-05-08 2018-11-23 东莞华晶粉末冶金有限公司 Stainless base steel feeding and preparation method thereof, stainless base steel green body and preparation method thereof
CN107138732A (en) * 2017-06-15 2017-09-08 北京康普锡威科技有限公司 A kind of method that low cost, short route prepare 3D printing titanium valve
CN107891155A (en) * 2017-10-09 2018-04-10 南方科技大学 Process for manufacturing near-spherical titanium powder and high-performance titanium material
CN108080621A (en) * 2017-11-21 2018-05-29 北京科技大学 Cost laser selective melting titanium valve, its preparation method and titanium preparation method
CN108326282A (en) * 2018-02-02 2018-07-27 广东省材料与加工研究所 A kind of powder injection forming Ti-6Al-4V alloy feedings and preparation method thereof
CN109226773A (en) * 2018-08-20 2019-01-18 北京科技大学 Hollow bolted node sphere of titanium alloy and preparation method thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
范亚卓等: "熔盐电解制备骨骼3D打印用非球形高纯钛粉", 《钢铁钒钛》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112077307A (en) * 2020-08-21 2020-12-15 西安理工大学 A kind of preparation method of 3D printing doped graphene high-strength titanium alloy parts
CN114226735A (en) * 2021-11-23 2022-03-25 成都先进金属材料产业技术研究院股份有限公司 Powdery titanium-based brazing filler metal and preparation method thereof
CN114226735B (en) * 2021-11-23 2024-03-26 成都先进金属材料产业技术研究院股份有限公司 Powdery titanium-based brazing filler metal and preparation method thereof

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Application publication date: 20191220