[go: up one dir, main page]

CN104550949A - Method for rapidly forming Ti-6Al-4V three-dimensional metal parts by electron beams - Google Patents

Method for rapidly forming Ti-6Al-4V three-dimensional metal parts by electron beams Download PDF

Info

Publication number
CN104550949A
CN104550949A CN201310517339.4A CN201310517339A CN104550949A CN 104550949 A CN104550949 A CN 104550949A CN 201310517339 A CN201310517339 A CN 201310517339A CN 104550949 A CN104550949 A CN 104550949A
Authority
CN
China
Prior art keywords
electron beam
dimensional metal
metal part
forming
heat treatment
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.)
Pending
Application number
CN201310517339.4A
Other languages
Chinese (zh)
Inventor
李述军
侯文韬
王哲
郝玉琳
杨锐
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Institute of Metal Research of CAS
Original Assignee
Institute of Metal Research of CAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Institute of Metal Research of CAS filed Critical Institute of Metal Research of CAS
Priority to CN201310517339.4A priority Critical patent/CN104550949A/en
Publication of CN104550949A publication Critical patent/CN104550949A/en
Pending legal-status Critical Current

Links

Landscapes

  • Powder Metallurgy (AREA)
  • Welding Or Cutting Using Electron Beams (AREA)

Abstract

本发明涉及电子束加工技术领域,具体为一种电子束快速成形Ti-6Al-4V三维金属零件的方法,该方法适用于各种复杂结构Ti-6Al-4V金属零件的快速成形制备。首先,制备Ti-6Al-4V三维金属零件;然后,对制备的三维零件在800℃~1000℃进行热等静压处理;最后,对钛合金部件在700℃~1000℃进行退火处理和400℃~600℃进行时效处理。通过以上工艺过程,可以获得抗拉强度高于900MPa,延伸率高于10%,疲劳强度高于500MPa,冲击韧性高于30J/cm2的优异综合力学性能的Ti-6Al-4V复杂结构三维零件,可在航天、医疗等领域获得广泛应用。The invention relates to the technical field of electron beam processing, in particular to a method for rapid forming of Ti-6Al-4V three-dimensional metal parts by electron beams, and the method is suitable for the rapid forming preparation of Ti-6Al-4V metal parts with various complex structures. First, Ti-6Al-4V three-dimensional metal parts are prepared; then, the prepared three-dimensional parts are subjected to hot isostatic pressing at 800°C to 1000°C; finally, the titanium alloy parts are annealed at 700°C to 1000°C and 400°C ~600℃ for aging treatment. Through the above process, the Ti-6Al-4V complex structure three-dimensional parts with excellent comprehensive mechanical properties such as tensile strength higher than 900MPa, elongation higher than 10%, fatigue strength higher than 500MPa, and impact toughness higher than 30J/ cm2 can be obtained. , can be widely used in aerospace, medical and other fields.

Description

一种电子束快速成形Ti-6Al-4V三维金属零件的方法A Method for Electron Beam Rapid Forming of Ti-6Al-4V Three-dimensional Metal Parts

技术领域:Technical field:

本发明涉及电子束加工技术领域,具体为一种电子束快速成形Ti-6Al-4V高性能三维金属零件的方法,该方法适用于各种复杂结构Ti-6Al-4V金属零件的快速成形制备。The invention relates to the technical field of electron beam processing, in particular to a method for rapid forming of Ti-6Al-4V high-performance three-dimensional metal parts by electron beams, and the method is suitable for the rapid forming preparation of Ti-6Al-4V metal parts with various complex structures.

背景技术:Background technique:

电子束熔化逐层成型技术(Additive Fabrication via Electron Eeam Melting,AM-EBM)是近年快速发展的先进制造技术之一。EBM技术以电子束为能量源,通过对零件的三维数字模型分层切片处理,使其离散成一系列二维数据文件,然后按照每一层的文件信息通过计算机系统控制电子束移动将金属粉末逐层熔融堆积,最终得到与设计文件完全一致的样件。该技术集中体现了计算机辅助设计、数控、电子束加工、新材料开发等多学科、多技术的综合应用,能够快速制备精度高、结构复杂的金属部件,具有高精度、高效率和高性能等优点,在航空航天、医疗、化工等领域有着广泛的应用,受到了各国学者和研究人员的密切关注。Additive Fabrication via Electron Eeam Melting (AM-EBM) is one of the advanced manufacturing technologies that have developed rapidly in recent years. EBM technology uses the electron beam as the energy source, through the layered slice processing of the three-dimensional digital model of the part, it is discretized into a series of two-dimensional data files, and then according to the file information of each layer, the computer system controls the movement of the electron beam to move the metal powder one by one The layers are fused and accumulated, and finally a sample that is completely consistent with the design file is obtained. This technology embodies the comprehensive application of computer-aided design, numerical control, electron beam processing, new material development and other multi-disciplinary and multi-technical applications. It can quickly prepare metal parts with high precision and complex structure, and has high precision, high efficiency and high performance. It has a wide range of applications in aerospace, medical, chemical and other fields, and has received close attention from scholars and researchers from all over the world.

与另一种快速成形技术-激光快速成形技术相比,EBM技术制备的金属零件残余内应力低,成形效率高,在生产大尺寸三维金属零件方面具有明显的优势。但是EBM技术生产的零件性能与EBM工艺参数密切相关,对于不同的金属需要相对应的工艺参数进行生产制备。在EBM法制造样品过程中,输入能量、电子束扫描速度等制备工艺参数以及样品尺寸、堆积方向等均会影响各分层面的融化及凝固速率,进而影响样品的组织及性能。Compared with another rapid prototyping technology-laser rapid prototyping technology, the metal parts prepared by EBM technology have low residual internal stress and high forming efficiency, which has obvious advantages in the production of large-scale three-dimensional metal parts. However, the performance of parts produced by EBM technology is closely related to EBM process parameters, and different metals require corresponding process parameters for production and preparation. In the process of manufacturing samples by EBM method, the input energy, electron beam scanning speed and other preparation process parameters, as well as sample size and stacking direction, etc. will affect the melting and solidification rate of each layer, and then affect the structure and performance of the sample.

钛合金由于具有比强度高、弹性模量低、抗腐蚀性优异和良好的生物相容性等优点,在医疗和航空航天领域具有广泛的应用。在医疗和航空航天领域的实际应用中,常需要一些具有复杂内部结构的金属零件。对钛合金来说,采用常规加工方法加工这些部件具有很大难度,并且成本很高。而采用EBM法进行这些金属零件的加工制备具有明显的优势,能够实现这些零件的工业规模高效快速制备。目前各国学者已针对上述因素对EBM法Ti-6Al-4V合金制品的组织及性能影响开展了研究(Nikolas H,Timothy Q.Mater Sci Eng A,2013;573:271;Nikolas H,Timothy Q.Mater Sci Eng A,2013;573:264;Murr L E,Esquivel E V,Quinones S A,Gaytan S M,Lopez M I,Martinez E Y,Medina F,Hernandez D H,Martinez E,Martinez J L,Stafford S W,Brown D K,Hoppe T,Meyers W,Lindhe U,Wicker R B.Materials Characterization,2009;60:96)。但这些研究只局限于工艺参数对Ti-6Al-4V合金拉伸性能的影响,缺乏对疲劳性能、冲击性能及缺口敏感性能的影响。此外,EBM产品的后处理(热等静压和热处理)对其力学性能的应先还没有人涉及。Due to the advantages of high specific strength, low elastic modulus, excellent corrosion resistance, and good biocompatibility, titanium alloys are widely used in medical and aerospace fields. In practical applications in the medical and aerospace fields, some metal parts with complex internal structures are often required. Machining these components using conventional machining methods is difficult and expensive for titanium alloys. The use of the EBM method for the processing and preparation of these metal parts has obvious advantages, and it can realize the efficient and rapid preparation of these parts on an industrial scale. At present, scholars from various countries have carried out research on the influence of the above factors on the structure and properties of EBM Ti-6Al-4V alloy products (Nikolas H, Timothy Q. Mater Sci Eng A, 2013; 573: 271; Nikolas H, Timothy Q. Mater Sci Eng A,2013;573:264; Murr L E, Esquivel E V, Quinones S A, Gaytan S M, Lopez M I, Martinez E Y, Medina F, Hernandez D H, Martinez E, Martinez J L, Stafford S W, Brown D K, Hoppe T, Meyers W, Lindhe U, Wicker R B. Materials Characterization, 2009;60:96). However, these studies are only limited to the influence of process parameters on the tensile properties of Ti-6Al-4V alloy, and lack of influence on fatigue properties, impact properties and notch sensitivity properties. In addition, the effects of post-processing (hot isostatic pressing and heat treatment) on EBM products on their mechanical properties have not been addressed.

因此,需要研究电子束输入能量、样品尺寸等工艺参数、热等静压及热处理等后处理技术对EBM法制备的Ti-6Al-4V合金力学性能的影响,获得高效制备优异力学性能Ti-6Al-4V三维金属零件的电子束快速成形方法,更好的服务于医疗、航天等领域。Therefore, it is necessary to study the influence of process parameters such as electron beam input energy, sample size, and post-treatment technologies such as hot isostatic pressing and heat treatment on the mechanical properties of Ti-6Al-4V alloy prepared by EBM method, so as to obtain efficient preparation of Ti-6Al with excellent mechanical properties. - The electron beam rapid prototyping method of 4V three-dimensional metal parts can better serve the medical, aerospace and other fields.

发明内容:Invention content:

本发明的目的是提供一种电子束快速成形Ti-6Al-4V三维金属零件的方法,解决目前高效快速制备复杂结构Ti-6Al-4V三维金属零件的难题。The purpose of the present invention is to provide a method for rapid forming of Ti-6Al-4V three-dimensional metal parts by electron beams, which solves the current problem of efficient and rapid preparation of complex structure Ti-6Al-4V three-dimensional metal parts.

本发明的技术方案:Technical scheme of the present invention:

一种电子束快速成形Ti-6Al-4V三维金属零件的方法,具体步骤如下:A method for electron beam rapid forming of Ti-6Al-4V three-dimensional metal parts, the specific steps are as follows:

(1)Ti-6Al-4V三维金属零件制备,以Ti-6Al-4V粉末为原材料,采用电子束熔融金属成型技术制备Ti-6Al-4V块三维金属零件;(1) Preparation of Ti-6Al-4V three-dimensional metal parts, using Ti-6Al-4V powder as raw material, using electron beam molten metal forming technology to prepare Ti-6Al-4V block three-dimensional metal parts;

(2)Ti-6Al-4V三维金属零件热等静压处理,对Ti-6Al-4V三维金属零件在800℃~1000℃进行热等静压处理;(2) Hot isostatic pressing treatment of Ti-6Al-4V three-dimensional metal parts, hot isostatic pressing treatment of Ti-6Al-4V three-dimensional metal parts at 800 ° C ~ 1000 ° C;

(3)Ti-6Al-4V三维金属零件热处理,对Ti-6Al-4V三维金属零件在700℃~1000℃进行退火处理和400℃~600℃进行时效处理,最终获得优异力学性能的Ti-6Al-4V三维金属零件。(3) Heat treatment of Ti-6Al-4V three-dimensional metal parts, annealing treatment of Ti-6Al-4V three-dimensional metal parts at 700 ° C ~ 1000 ° C and aging treatment at 400 ° C ~ 600 ° C, and finally obtain Ti-6Al with excellent mechanical properties -4V 3D metal parts.

所述步骤(1)中,首先在基板表面均匀铺一层Ti-6Al-4V金属粉末,然后用电子束在真空室内将所述金属粉末逐层熔化、沉积,通过控制电子束熔化工艺参数、堆积成形参数,直至整个三维零件制造完成。In the step (1), a layer of Ti-6Al-4V metal powder is evenly spread on the surface of the substrate, and then the metal powder is melted and deposited layer by layer in a vacuum chamber with an electron beam. By controlling the electron beam melting process parameters, Build up the forming parameters until the entire 3D part is manufactured.

所述步骤(1)中,Ti-6Al-4V粉末为球形,直径为30μm~150μm。In the step (1), the Ti-6Al-4V powder is spherical with a diameter of 30 μm to 150 μm.

所述步骤(1)中,电子束熔融金属成型技术的工艺参数范围为,电子束电流为5~30mA,扫描速度为1000~20000mm/s。In the step (1), the range of process parameters of the electron beam molten metal forming technology is that the electron beam current is 5-30 mA, and the scanning speed is 1000-20000 mm/s.

为保证三维零件整体组织及力学性能均匀,零件初始成形高度应控制在距基板10mm~30mm。为保证三维零件整体组织及力学性能均匀,尽可能使堆积方向垂直于基板方向。为保证三维零件整体组织及力学性能均匀,零件壁厚应大于2mm。In order to ensure that the overall structure and mechanical properties of the three-dimensional parts are uniform, the initial forming height of the parts should be controlled at 10 mm to 30 mm from the substrate. In order to ensure that the overall structure and mechanical properties of the three-dimensional parts are uniform, the stacking direction should be perpendicular to the direction of the substrate as much as possible. In order to ensure that the overall structure and mechanical properties of the three-dimensional parts are uniform, the wall thickness of the parts should be greater than 2mm.

所述步骤(2)中,Ti-6Al-4V热等静压的具体参数为:热等静压加热温度为800℃~1000℃,保温时间为1~3h,所加压力为100~200MPa,冷却方式为炉冷。In the step (2), the specific parameters of the hot isostatic pressing of Ti-6Al-4V are: the heating temperature of the hot isostatic pressing is 800°C-1000°C, the holding time is 1-3h, and the applied pressure is 100-200MPa, The cooling method is furnace cooling.

所述步骤(3)中,Ti-6Al-4V三维金属零件热处理采用两相区二步热处理,具体步骤为:In the step (3), the heat treatment of the Ti-6Al-4V three-dimensional metal parts adopts two-step heat treatment in the two-phase zone, and the specific steps are:

(1)两相区退火处理;(1) Two-phase zone annealing treatment;

(2)两相区时效处理。(2) Aging treatment in the two-phase zone.

所述两相区退火处理所用设备为真空热处理炉,热处理温度为700℃~1000℃,保温时间为1~3h,冷却速度为1~3℃/min;The equipment used for the two-phase zone annealing treatment is a vacuum heat treatment furnace, the heat treatment temperature is 700°C-1000°C, the holding time is 1-3h, and the cooling rate is 1-3°C/min;

所述两相区时效处理所用设备为真空热处理炉,热处理温度为400℃~600℃,保温时间为1~3h,冷却速度为8~15℃/min。The equipment used for the aging treatment in the two-phase zone is a vacuum heat treatment furnace, the heat treatment temperature is 400°C-600°C, the holding time is 1-3h, and the cooling rate is 8-15°C/min.

本发明中,电子束熔融金属成型技术(Electron Beam Melting)简称EBM技术,是近年来一种新兴的先进金属快速成型制造技术,其原理是将零件的三维实体模型数据导入EBM设备,然后在EBM设备的工作舱内平铺一层微细金属粉末薄层,利用高能电子束经偏转聚焦后,在焦点所产生的高密度能量使被扫描到的金属粉末层在局部微小区域产生高温,导致金属微粒熔融,电子束连续扫描将使一个个微小的金属熔池相互融合并凝固,连接形成线状和面状金属层。In the present invention, Electron Beam Melting technology (Electron Beam Melting) is referred to as EBM technology, which is an emerging advanced metal rapid prototyping manufacturing technology in recent years. Its principle is to import the three-dimensional solid model data of parts into EBM equipment, and then A thin layer of fine metal powder is laid flat in the working chamber of the equipment. After the high-energy electron beam is deflected and focused, the high-density energy generated at the focus makes the scanned metal powder layer generate high temperature in a small local area, resulting in metal particles Melting, the continuous scanning of the electron beam will make the tiny molten metal pools fuse and solidify, and connect to form linear and planar metal layers.

本发明中,采用的电子束熔融金属成型设备为常规技术,如:泛亚特科技有限公司生产的Arcam A1电子束熔炼EBM系统(Electron Beam Melting),其工艺参数范围为:电子束电流为5~30mA,扫描速度为1000~20000mm/s。该系统直接从CAD到成品制造完成的全自动化系统,是复杂结构钛合金三维零件批量生产工具,通过金属粉末在高能电子束的轰击下,一层一层的生长,每层的形状都通过三维CAD控制,利用电子束熔炼系统,可以达到高的熔炼能力和生产率。In the present invention, the electron beam melting metal forming equipment that adopts is conventional technology, as: the Arcam A1 electron beam melting EBM system (Electron Beam Melting) that Fan Yate Technology Co., Ltd. produces, and its process parameter scope is: electron beam current is 5 ~30mA, scanning speed is 1000~20000mm/s. The system is a fully automated system directly from CAD to finished product manufacturing. It is a mass production tool for three-dimensional titanium alloy parts with complex structures. Under the bombardment of high-energy electron beams, metal powder grows layer by layer, and the shape of each layer is determined by three-dimensional CAD control, using electron beam melting system, can achieve high melting capacity and productivity.

本发明方法制备的Ti-6Al-4V三维金属零件拉伸强度高于900MPa,延伸率高于10%,疲劳强度高于500MPa,抗冲击性能高于30J/cm2,其综合力学性能明显高于铸件和锻件。The tensile strength of the Ti-6Al-4V three-dimensional metal part prepared by the method of the present invention is higher than 900MPa, the elongation is higher than 10%, the fatigue strength is higher than 500MPa, the impact resistance is higher than 30J/cm 2 , and its comprehensive mechanical properties are obviously higher than Castings and forgings.

本发明的有益效果:Beneficial effects of the present invention:

1、本发明采用电子束熔融金属成型技术制备高性能Ti-6Al-4V三维金属零件,产品的外形、内部结构完全可控,可根据实际需求进行个体化、复杂结构三维金属零件的制备;其制备工艺简单,成本明显低于机械加工等其他制备手段,生产效率高,适合工业规模生产。1. The present invention adopts electron beam molten metal forming technology to prepare high-performance Ti-6Al-4V three-dimensional metal parts. The shape and internal structure of the product are completely controllable, and the preparation of individualized and complex three-dimensional metal parts can be carried out according to actual needs; The preparation process is simple, the cost is obviously lower than other preparation means such as mechanical processing, the production efficiency is high, and it is suitable for industrial scale production.

2、本发明通过控制电子束熔融金属成型方法制备Ti-6Al-4V三维金属零件工艺过程中的工艺参数优化、后期热等静压和热处理等环节,能够获得具有优异综合力学性能的复杂结构Ti-6Al-4V三维金属零件,在医疗、航空航天领域具有非常广阔的应用前景。2. The present invention can obtain the complex structure Ti with excellent comprehensive mechanical properties by controlling the process parameters optimization, hot isostatic pressing and heat treatment in the process of preparing Ti-6Al-4V three-dimensional metal parts by the electron beam melting metal forming method. -6Al-4V three-dimensional metal parts have very broad application prospects in the fields of medical treatment and aerospace.

3、本发明通过对Ti-6Al-4V三维金属零件在800℃~1000℃进行热等静压处理,400℃~1000℃之间进行退火和时效两步热处理,获得拉伸强度高于900MPa,延伸率高于10%,疲劳强度高于500MPa,抗冲击性能高于30J/cm2,通过热等静压和热处理工艺控制EBM法Ti-6Al-4V三维金属零件的力学性能,从而获得具有优异力学性能的大尺寸复杂结构钛合金三维构件。3. In the present invention, the Ti-6Al-4V three-dimensional metal parts are subjected to hot isostatic pressing at 800°C to 1000°C, and two-step heat treatment of annealing and aging at 400°C to 1000°C to obtain a tensile strength higher than 900MPa. The elongation rate is higher than 10%, the fatigue strength is higher than 500MPa, and the impact resistance is higher than 30J/cm 2 . The mechanical properties of the EBM method Ti-6Al-4V three-dimensional metal parts are controlled by hot isostatic pressing and heat treatment processes, so as to obtain excellent Mechanical properties of large-scale and complex-structured titanium alloy three-dimensional components.

总之,本发明方法工艺简单,成本低,成形零件精度高,适用于工业大规模生产。本发明通过电子束工艺参数、热等静压工艺以及热处理工艺控制Ti-6Al-4V成形材料的力学性能,从而获得具有优异力学性能的Ti-6Al-4V复杂结构三维零件,可在航天、医疗等领域获得广泛应用。In a word, the method of the invention has simple process, low cost, high precision of formed parts, and is suitable for large-scale industrial production. The invention controls the mechanical properties of the Ti-6Al-4V forming material through electron beam process parameters, hot isostatic pressing process and heat treatment process, so as to obtain Ti-6Al-4V complex structure three-dimensional parts with excellent mechanical properties, which can be used in aerospace, medical and other fields have been widely used.

附图说明:Description of drawings:

图1(a)为人体头颅骨CAD模型;Figure 1(a) is the CAD model of the human skull;

图1(b)为Ti-6Al-4V人体头颅骨模拟件;Figure 1(b) is a Ti-6Al-4V human skull simulation piece;

图2为Ti-6Al-4V合金粉末形貌;Fig. 2 is the morphology of Ti-6Al-4V alloy powder;

图3(a)国际象棋棋子CAD模型;Figure 3 (a) CAD model of chess pieces;

图3(b)为Ti-6Al-4V国际象棋棋子;Figure 3(b) is a Ti-6Al-4V chess piece;

图4(a)为髋臼杯CAD模型;Figure 4(a) is the CAD model of the acetabular cup;

图4(b)为Ti-6Al-4V髋臼杯;Figure 4(b) is the Ti-6Al-4V acetabular cup;

图5(a)为CAD空心球模型;Figure 5(a) is a CAD hollow sphere model;

图5(b)为Ti-6Al-4V空心球。Figure 5(b) shows Ti-6Al-4V hollow spheres.

具体实施方式:Detailed ways:

本发明中,首先采用CAD软件进行模型设计,然后将设计好的图形文件导入Magics软件进行图形纠错和优化,以保证电子束熔融金属成型过程的顺利进行;将优化处理后的图形文件转换成abf格式文件导入电子束熔融金属成型设备的计算机控制系统,以Ti-6Al-4V粉末为原材料利用电子束熔融金属成型设备制备Ti-6Al-4V三维金属零件。In the present invention, at first adopt CAD software to carry out model design, import the graphic file that designs then into Magics software and carry out graphic error correction and optimization, to guarantee the smooth progress of electron beam molten metal forming process; The abf format file is imported into the computer control system of the electron beam melting metal forming equipment, and the Ti-6Al-4V three-dimensional metal parts are prepared by using the electron beam melting metal forming equipment with Ti-6Al-4V powder as the raw material.

下面结合附图和实施例对本发明进一步详细说明。The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.

实施例1Example 1

如图1(a)所示,利用CAD软件设计人体头颅骨模型模型,壁厚为3mm。以Ti-6Al-4V合金粉末(图2,粉末直径为50~80μm)为原料,采用Arcam A1型电子束熔融设备制备Ti-6Al-4V人体头颅骨模型,电子束扫描速度为10000mm/s,电子束电流为18mA,制备的Ti-6Al-4V人体头颅骨模型如图1(b)所示。As shown in Figure 1(a), the human skull model is designed using CAD software, and the wall thickness is 3 mm. Using Ti-6Al-4V alloy powder (Fig. 2, the powder diameter is 50-80 μm) as raw material, the Ti-6Al-4V human skull model was prepared by Arcam A1 electron beam melting equipment, and the electron beam scanning speed was 10000 mm/s. The electron beam current is 18mA, and the prepared Ti-6Al-4V human skull model is shown in Figure 1(b).

本实施例中,对制备的Ti-6Al-4V人体头颅骨模型进行热等静压处理,工艺为:温度为920℃,压力为120MPa,保温时间为3h。In this example, the prepared Ti-6Al-4V human skull model is subjected to hot isostatic pressing, the process is as follows: the temperature is 920° C., the pressure is 120 MPa, and the holding time is 3 hours.

本实施例中,对制备的Ti-6Al-4V人体头颅骨在两相区进行二步热处理:In this embodiment, the prepared Ti-6Al-4V human skull is subjected to two-step heat treatment in the two-phase region:

(1)两相区退火处理利用真空热处理炉,对制备的Ti-6Al-4V人体头颅骨在800℃保温1h,以1℃/min的速度冷却到室温。(1) Two-phase zone annealing treatment Using a vacuum heat treatment furnace, the prepared Ti-6Al-4V human skull was kept at 800 °C for 1 h, and cooled to room temperature at a rate of 1 °C/min.

(2)两相区时效处理利用真空热处理炉,热处理温度为500℃保温3h,以10℃/min的速度冷却到室温。(2) The aging treatment in the two-phase zone uses a vacuum heat treatment furnace. The heat treatment temperature is 500 ° C for 3 hours, and the temperature is cooled to room temperature at a rate of 10 ° C / min.

本实施例中,Ti-6Al-4V人体头颅骨模型抗拉强度、延伸率、疲劳强度、冲击韧性及缺口敏感性相关参数如下:该钛合金材料抗拉强度为1000MPa,屈服强度为900MPa,延伸率为11%,疲劳强度为530MPa,冲击韧性为32J/cm2。本实施例中Ti-6Al-4V人体头颅骨模型的抗拉强度、延伸率、疲劳强度、冲击韧性及缺口敏感性明显优于文献中报道的锻态及铸态Ti-6Al-4V合金。In this embodiment, the relevant parameters of the tensile strength, elongation, fatigue strength, impact toughness and notch sensitivity of the Ti-6Al-4V human skull model are as follows: the tensile strength of the titanium alloy material is 1000MPa, the yield strength is 900MPa, and the elongation The rate is 11%, the fatigue strength is 530MPa, and the impact toughness is 32J/cm 2 . The tensile strength, elongation, fatigue strength, impact toughness and notch sensitivity of the Ti-6Al-4V human skull model in this example are significantly better than the wrought and cast Ti-6Al-4V alloys reported in the literature.

实施例2Example 2

如图3(a)所示,利用CAD软件设计国际象棋棋子模型,棋子最薄壁厚为4mm。以Ti-6Al-4V合金粉末为原料(图2,粉末直径为50~80μm),采用ArcamA1型电子束熔融设备制备Ti-6Al-4V国际象棋棋子,电子束扫描速度为13000m/s,电子束电流为20mA,堆积方向垂直于基板方向。制备的Ti-6Al-4V国际象棋棋子如图3(b)所示。As shown in Figure 3(a), the chess piece model is designed using CAD software, and the thinnest wall thickness of the chess piece is 4mm. Using Ti-6Al-4V alloy powder as raw material (Fig. 2, the powder diameter is 50-80 μm), the Ti-6Al-4V chess piece was prepared by ArcamA1 electron beam melting equipment, the electron beam scanning speed was 13000m/s, and the electron beam The current is 20mA, and the stacking direction is perpendicular to the substrate direction. The prepared Ti-6Al-4V chess piece is shown in Fig. 3(b).

本实施例中,对制备的Ti-6Al-4V人体头颅骨模型进行热等静压处理,工艺为:温度为950℃,压力为100MPa,保温时间为2h。In this embodiment, the prepared Ti-6Al-4V human skull model is subjected to hot isostatic pressing, the process is as follows: the temperature is 950° C., the pressure is 100 MPa, and the holding time is 2 hours.

本实施例中,对制备的Ti-6Al-4V国际象棋棋子在两相区进行二步热处理:In this embodiment, the prepared Ti-6Al-4V chess pieces are subjected to two-step heat treatment in the two-phase region:

(1)两相区退火处理利用真空热处理炉,对制备的Ti-6Al-4V国际象棋棋子在900℃保温1.5h,以2℃/min的速度冷却到室温。(1) Two-phase zone annealing treatment Using a vacuum heat treatment furnace, the prepared Ti-6Al-4V chess pieces were kept at 900°C for 1.5h, and cooled to room temperature at a rate of 2°C/min.

(2)两相区时效处理利用真空热处理炉,热处理温度为600℃,保温时间1h,以15℃/min的速度冷却到室温。(2) The aging treatment in the two-phase zone uses a vacuum heat treatment furnace with a heat treatment temperature of 600°C, a holding time of 1h, and cooling to room temperature at a rate of 15°C/min.

本实施例中,Ti-6Al-4V国际象棋棋子抗拉强度、延伸率、疲劳强度、冲击韧性及缺口敏感性相关参数如下:该钛合金构件抗拉强度为980MPa,屈服强度为880MPa,延伸率为15%,疲劳强度为550MPa,冲击韧性为33J/cm2。本实施例中Ti-6Al-4V国际象棋棋子的抗拉强度、延伸率、疲劳强度、冲击韧性及缺口敏感性明显优于文献中报道的锻态及铸态Ti-6Al-4V合金。In this embodiment, the relevant parameters of the tensile strength, elongation, fatigue strength, impact toughness and notch sensitivity of Ti-6Al-4V chess pieces are as follows: the tensile strength of the titanium alloy component is 980MPa, the yield strength is 880MPa, and the elongation 15%, the fatigue strength is 550MPa, and the impact toughness is 33J/cm 2 . The tensile strength, elongation, fatigue strength, impact toughness and notch sensitivity of the Ti-6Al-4V chess pieces in this example are significantly better than the forged and cast Ti-6Al-4V alloys reported in the literature.

实施例3Example 3

如图4(a)所示,利用CAD软件设计髋臼杯模型,髋臼杯表面带有2mm厚的多孔结构,髋臼杯最薄处为2mm。以Ti-6Al-4V合金粉末为原料(图2,粉末直径为50~80μm),采用Arcam A1型电子束熔融设备制备Ti-6Al-4V髋臼杯,电子束扫描速度为12500mm/s,电子束电流为25mA,堆积方向为垂直基板方向。制备的Ti-6Al-4V髋臼杯如图4(b)所示。As shown in Figure 4(a), the acetabular cup model was designed using CAD software. The surface of the acetabular cup has a porous structure with a thickness of 2 mm, and the thinnest part of the acetabular cup is 2 mm. Using Ti-6Al-4V alloy powder as raw material (Fig. 2, the powder diameter is 50-80 μm), the Ti-6Al-4V acetabular cup was prepared by Arcam A1 electron beam melting equipment, and the scanning speed of the electron beam was 12500 mm/s. The beam current is 25mA, and the stacking direction is vertical to the substrate. The prepared Ti-6Al-4V acetabular cup is shown in Fig. 4(b).

本实施例中,对制备的Ti-6Al-4V髋臼杯进行热等静压处理,工艺为:温度为940℃,压力为110MPa,保温时间为2.5h。In this example, the prepared Ti-6Al-4V acetabular cup is subjected to hot isostatic pressing, the process is as follows: the temperature is 940° C., the pressure is 110 MPa, and the holding time is 2.5 hours.

本实施例中,对制备的Ti-6Al-4V髋臼杯在两相区进行二步热处理:In this example, the prepared Ti-6Al-4V acetabular cup is subjected to two-step heat treatment in the two-phase region:

(1)两相区退火处理利用真空热处理炉,对制备的Ti-6Al-4V髋臼杯在700℃保温3h,以1℃/min的速度冷却到室温。(1) Two-phase zone annealing treatment Using a vacuum heat treatment furnace, the prepared Ti-6Al-4V acetabular cup was kept at 700°C for 3 hours, and cooled to room temperature at a rate of 1°C/min.

(2)两相区时效处理利用真空热处理炉,热处理温度为550℃,保温时间3h,以8℃/min的速度冷却到室温。(2) The aging treatment in the two-phase zone uses a vacuum heat treatment furnace with a heat treatment temperature of 550°C, a holding time of 3h, and cooling to room temperature at a rate of 8°C/min.

本实施例中,Ti-6Al-4V髋臼杯抗拉强度、延伸率、疲劳强度、冲击韧性及缺口敏感性相关参数如下:该钛合金构件抗拉强度为1180MPa,屈服强度为1100MPa,延伸率为10%,疲劳强度为568MPa,冲击韧性为31J/cm2。本实施例中Ti-6Al-4V髋臼杯的抗拉强度、延伸率、疲劳强度、冲击韧性及缺口敏感性明显优于文献中报道的锻态及铸态Ti-6Al-4V合金。In this embodiment, the relevant parameters of the tensile strength, elongation, fatigue strength, impact toughness and notch sensitivity of the Ti-6Al-4V acetabular cup are as follows: the tensile strength of the titanium alloy member is 1180MPa, the yield strength is 1100MPa, and the elongation 10%, the fatigue strength is 568MPa, and the impact toughness is 31J/cm 2 . The tensile strength, elongation, fatigue strength, impact toughness and notch sensitivity of the Ti-6Al-4V acetabular cup in this example are significantly better than the forged and cast Ti-6Al-4V alloys reported in the literature.

实施例4Example 4

如图5(a)所示,利用CAD软件设计空心球体,空心球壁厚为3mm,且一半为多孔结构。以Ti-6Al-4V合金粉末为原料(图2,粉末直径为50~80μm),采用Arcam A1型电子束熔融设备Ti-6Al-4V空心球体,电子束扫描速度为15000mm/s,电子束电流为24mA,堆积方向为垂直于基板方向。制备的Ti-6Al-4V空心球体如图5(b)所示。As shown in Figure 5(a), the hollow sphere is designed using CAD software. The wall thickness of the hollow sphere is 3 mm, and half of the hollow sphere is a porous structure. Using Ti-6Al-4V alloy powder as raw material (Fig. 2, the powder diameter is 50-80 μm), using Arcam A1 electron beam melting equipment Ti-6Al-4V hollow sphere, the electron beam scanning speed is 15000mm/s, the electron beam current It is 24mA, and the stacking direction is perpendicular to the substrate direction. The prepared Ti-6Al-4V hollow spheres are shown in Fig. 5(b).

本实施例中,对制备的Ti-6Al-4V空心球体进行热等静压处理,工艺为:温度为920℃,压力为120MPa,保温时间为2.5h。In this embodiment, the prepared Ti-6Al-4V hollow spheres are subjected to hot isostatic pressing treatment, the process is as follows: the temperature is 920° C., the pressure is 120 MPa, and the holding time is 2.5 hours.

本实施例中,对制备的Ti-6Al-4V空心球体在两相区进行二步热处理:In this example, the prepared Ti-6Al-4V hollow spheres are subjected to two-step heat treatment in the two-phase region:

(1)两相区退火处理利用真空热处理炉,对制备的空心球体在750℃保温1h,以3℃/min的速度冷却到室温。(1) Two-phase zone annealing treatment Using a vacuum heat treatment furnace, the prepared hollow spheres were kept at 750°C for 1 hour, and cooled to room temperature at a rate of 3°C/min.

(2)两相区时效处理利用真空热处理炉,热处理温度为450℃,保温时间2.5h,以9℃/min的速度冷却到室温。(2) The aging treatment in the two-phase zone uses a vacuum heat treatment furnace with a heat treatment temperature of 450°C, a holding time of 2.5h, and cooling to room temperature at a rate of 9°C/min.

本实施例中,Ti-6Al-4V空心球体抗拉强度、延伸率、疲劳强度、冲击韧性及缺口敏感性相关参数如下:该空心球体抗拉强度为1050MPa,屈服强度为950MPa,延伸率为11%,疲劳强度为550MPa,冲击韧性为33J/cm2。本实施例中Ti-6Al-4V空心球体的抗拉强度、延伸率、疲劳强度、冲击韧性及缺口敏感性明显优于文献中报道的锻态及铸态Ti-6Al-4V合金。In this embodiment, the relevant parameters of the tensile strength, elongation, fatigue strength, impact toughness and notch sensitivity of the Ti-6Al-4V hollow sphere are as follows: the tensile strength of the hollow sphere is 1050MPa, the yield strength is 950MPa, and the elongation is 11 %, the fatigue strength is 550MPa, and the impact toughness is 33J/cm 2 . The tensile strength, elongation, fatigue strength, impact toughness and notch sensitivity of the Ti-6Al-4V hollow spheres in this example are significantly better than the forged and cast Ti-6Al-4V alloys reported in the literature.

实施例结果表明,采用该方法可制备具有复杂结构Ti-6Al-4V三维构件,工艺简单,成本低,适合工业规模大批量生产,获得的Ti-6Al-4V三维构件具有高抗拉强度、高韧性、高疲劳性能、高抗冲击能力,在医疗及航空航天领域具有非常广阔的应用前景。The results of the examples show that the method can be used to prepare Ti-6Al-4V three-dimensional components with complex structures, the process is simple, the cost is low, and it is suitable for mass production on an industrial scale. The obtained Ti-6Al-4V three-dimensional components have high tensile strength, high Toughness, high fatigue performance, high impact resistance, has very broad application prospects in the medical and aerospace fields.

Claims (10)

1. a method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part, it is characterized in that, concrete steps are as follows:
(1) Ti-6Al-4V 3-dimensional metal part preparation, with Ti-6Al-4V powder for raw material, adopts electron beam melting rapid metallic prototyping technique to prepare Ti-6Al-4V block 3-dimensional metal part;
(2) Ti-6Al-4V 3-dimensional metal part hip treatment, carries out hip treatment to Ti-6Al-4V 3-dimensional metal part at 800 DEG C ~ 1000 DEG C;
(3) Ti-6Al-4V 3-dimensional metal part heat treatment, to Ti-6Al-4V 3-dimensional metal part 700 DEG C ~ 1000 DEG C carry out annealing in process and 400 DEG C ~ 600 DEG C carry out Ageing Treatment, the final Ti-6Al-4V 3-dimensional metal part obtaining excellent mechanical performance.
2. according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 1, it is characterized in that, in described step (1), first at substrate surface uniform spreading one deck Ti-6Al-4V metal dust, then with electron beam, described metal dust is successively melted, deposits in vacuum chamber, by controlling electron-beam melting technological parameter, stack shaping parameter, until whole 3 d part manufacture completes.
3., according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 1, it is characterized in that, in described step (1), Ti-6Al-4V powder is spherical, and diameter is 30 μm ~ 150 μm.
4. according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 1, it is characterized in that, in described step (1), the process parameters range of electron beam melting rapid metallic prototyping technique is, electron beam current is 5 ~ 30mA, and sweep speed is 1000 ~ 20000mm/s.
5. according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 2, it is characterized in that, for ensureing 3 d part global tissue and mechanical property evenly, part initial formation height should control at distance substrate 10mm ~ 30mm.
6. according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 2, it is characterized in that, for ensureing 3 d part global tissue and mechanical property evenly, making stacked direction perpendicular to orientation substrate as far as possible.
7. according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 2, it is characterized in that, for ensureing 3 d part global tissue and mechanical property evenly, part wall thickness should be greater than 2mm.
8. according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 1, it is characterized in that, in described step (2), the design parameter of Ti-6Al-4V high temperature insostatic pressing (HIP) is: high temperature insostatic pressing (HIP) heating-up temperature is 800 DEG C ~ 1000 DEG C, temperature retention time is 1 ~ 3h, institute's plus-pressure is 100 ~ 200MPa, and the type of cooling is that stove is cold.
9. according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 1, it is characterized in that, in described step (3), the heat treatment of Ti-6Al-4V 3-dimensional metal part adopts the heat treatment of two-phase section two step, and concrete steps are:
(1) two-phase section annealing in process;
(2) two-phase section Ageing Treatment.
10., according to the method for electron beam Quick-forming Ti-6Al-4V 3-dimensional metal part according to claim 9, it is characterized in that:
Described two-phase section annealing in process device therefor is vacuum heat treatment furnace, and heat treatment temperature is 700 DEG C ~ 1000 DEG C, and temperature retention time is 1 ~ 3h, and cooling velocity is 1 ~ 3 DEG C/min;
Described two-phase section Ageing Treatment device therefor is vacuum heat treatment furnace, and heat treatment temperature is 400 DEG C ~ 600 DEG C, and temperature retention time is 1 ~ 3h, and cooling velocity is 8 ~ 15 DEG C/min.
CN201310517339.4A 2013-10-24 2013-10-24 Method for rapidly forming Ti-6Al-4V three-dimensional metal parts by electron beams Pending CN104550949A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310517339.4A CN104550949A (en) 2013-10-24 2013-10-24 Method for rapidly forming Ti-6Al-4V three-dimensional metal parts by electron beams

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310517339.4A CN104550949A (en) 2013-10-24 2013-10-24 Method for rapidly forming Ti-6Al-4V three-dimensional metal parts by electron beams

Publications (1)

Publication Number Publication Date
CN104550949A true CN104550949A (en) 2015-04-29

Family

ID=53068607

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310517339.4A Pending CN104550949A (en) 2013-10-24 2013-10-24 Method for rapidly forming Ti-6Al-4V three-dimensional metal parts by electron beams

Country Status (1)

Country Link
CN (1) CN104550949A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105562694A (en) * 2015-12-31 2016-05-11 中国钢研科技集团有限公司 Hot isostatic pressing three-control method suitable for additive manufacturing parts
CN105834431A (en) * 2016-04-11 2016-08-10 西安欧中材料科技有限公司 Preparation method of high-uniformity Ti-6Al-4V alloy powder metallurgic block
CN106312060A (en) * 2015-06-29 2017-01-11 中国科学院金属研究所 Preparation method for high-performance low-modulus medical titanium alloy three-dimensional metal part
CN107234240A (en) * 2017-06-29 2017-10-10 西安欧中材料科技有限公司 A kind of electron beam powdering of use SS PREP Ti6Al4V spherical powders increases the manufacture method of material
CN107695350A (en) * 2017-09-28 2018-02-16 西北有色金属研究院 The method that TiAl alloy component is prepared based on electron beam 3D printing technique
CN109261963A (en) * 2018-10-30 2019-01-25 西安理工大学 A kind of fine grain TC4 alloy increasing material manufacturing method
CN112427652A (en) * 2020-11-02 2021-03-02 中国航空制造技术研究院 Titanium alloy structural part and preparation method thereof
CN113941715A (en) * 2021-09-15 2022-01-18 武汉理工大学 A kind of metal lattice structure material processing method and its application
CN113996812A (en) * 2021-10-15 2022-02-01 中国航发北京航空材料研究院 A heat treatment method for improving fatigue properties of laser selective melting of α-β titanium alloys

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0349766A (en) * 1989-07-18 1991-03-04 Kawasaki Steel Corp Production of porous body having excellent osteoaffinity
CN1486371A (en) * 2000-12-20 2004-03-31 株式会社丰田中央研究所 Titanium alloy with high elastic deformation ability and its manufacturing method
CN1743482A (en) * 2004-09-02 2006-03-08 盖恩斯马特有限公司 High strength low cost titanium and method for making same
CN101128609A (en) * 2005-02-25 2008-02-20 沃尔德马连接两合公司 Method for casting titanium alloy
EP2060343A1 (en) * 2006-08-28 2009-05-20 Panasonic Electric Works Co., Ltd Metal powder for metal photofabrication and method of metal photofabrication using the same
CN102459670A (en) * 2009-06-29 2012-05-16 博格华纳公司 Fatigue resistant cast titanium alloy articles
CN102764888A (en) * 2012-06-07 2012-11-07 中国人民解放军第四军医大学 Compound porous beta-TCP (tertiary calcium phosphate) titanium alloy human astragal support bar and preparation method thereof
CN102776412A (en) * 2012-07-13 2012-11-14 中国科学院金属研究所 Moderate-strength high-tenacity titanium alloy wire for electron beam fuse stack rapid manufacturing member
CN102994804A (en) * 2012-12-03 2013-03-27 中国科学院金属研究所 Method for preparing high fatigue property porous Ti-6Al-4V bulk material
CN103008657A (en) * 2013-01-13 2013-04-03 北京科技大学 Method for preparing oxide dispersion strengthened alloy by rapid forming

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0349766A (en) * 1989-07-18 1991-03-04 Kawasaki Steel Corp Production of porous body having excellent osteoaffinity
CN1486371A (en) * 2000-12-20 2004-03-31 株式会社丰田中央研究所 Titanium alloy with high elastic deformation ability and its manufacturing method
CN1743482A (en) * 2004-09-02 2006-03-08 盖恩斯马特有限公司 High strength low cost titanium and method for making same
CN101128609A (en) * 2005-02-25 2008-02-20 沃尔德马连接两合公司 Method for casting titanium alloy
EP2060343A1 (en) * 2006-08-28 2009-05-20 Panasonic Electric Works Co., Ltd Metal powder for metal photofabrication and method of metal photofabrication using the same
CN102459670A (en) * 2009-06-29 2012-05-16 博格华纳公司 Fatigue resistant cast titanium alloy articles
CN102764888A (en) * 2012-06-07 2012-11-07 中国人民解放军第四军医大学 Compound porous beta-TCP (tertiary calcium phosphate) titanium alloy human astragal support bar and preparation method thereof
CN102776412A (en) * 2012-07-13 2012-11-14 中国科学院金属研究所 Moderate-strength high-tenacity titanium alloy wire for electron beam fuse stack rapid manufacturing member
CN102994804A (en) * 2012-12-03 2013-03-27 中国科学院金属研究所 Method for preparing high fatigue property porous Ti-6Al-4V bulk material
CN103008657A (en) * 2013-01-13 2013-04-03 北京科技大学 Method for preparing oxide dispersion strengthened alloy by rapid forming

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
S.S. AL-BERMANI ET AL: "The Origin of Microstructural Diversity, Texture, and Mechanical Properties in Electron Beam Melted Ti-6Al-4V", 《METALLURGICAL AND MATERIALS TRANSACTIONS A》 *

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106312060A (en) * 2015-06-29 2017-01-11 中国科学院金属研究所 Preparation method for high-performance low-modulus medical titanium alloy three-dimensional metal part
CN106312060B (en) * 2015-06-29 2019-02-26 中国科学院金属研究所 A kind of preparation method of high-performance low-modulus medical titanium alloy three-dimensional metal parts
CN105562694A (en) * 2015-12-31 2016-05-11 中国钢研科技集团有限公司 Hot isostatic pressing three-control method suitable for additive manufacturing parts
CN105562694B (en) * 2015-12-31 2018-12-21 中国钢研科技集团有限公司 A kind of three prosecutor method of hot isostatic pressing suitable for increasing material manufacturing components
CN105834431A (en) * 2016-04-11 2016-08-10 西安欧中材料科技有限公司 Preparation method of high-uniformity Ti-6Al-4V alloy powder metallurgic block
CN107234240A (en) * 2017-06-29 2017-10-10 西安欧中材料科技有限公司 A kind of electron beam powdering of use SS PREP Ti6Al4V spherical powders increases the manufacture method of material
CN107695350A (en) * 2017-09-28 2018-02-16 西北有色金属研究院 The method that TiAl alloy component is prepared based on electron beam 3D printing technique
CN107695350B (en) * 2017-09-28 2019-08-30 西北有色金属研究院 Method for preparing TiAl alloy components based on electron beam 3D printing technology
CN109261963A (en) * 2018-10-30 2019-01-25 西安理工大学 A kind of fine grain TC4 alloy increasing material manufacturing method
CN112427652A (en) * 2020-11-02 2021-03-02 中国航空制造技术研究院 Titanium alloy structural part and preparation method thereof
CN113941715A (en) * 2021-09-15 2022-01-18 武汉理工大学 A kind of metal lattice structure material processing method and its application
CN113996812A (en) * 2021-10-15 2022-02-01 中国航发北京航空材料研究院 A heat treatment method for improving fatigue properties of laser selective melting of α-β titanium alloys

Similar Documents

Publication Publication Date Title
CN104550949A (en) Method for rapidly forming Ti-6Al-4V three-dimensional metal parts by electron beams
CN106312060B (en) A kind of preparation method of high-performance low-modulus medical titanium alloy three-dimensional metal parts
CN105499566B (en) A kind of method for realizing electron beam selective melting increasing material manufacturing metallic element situ heat treatment
CN107971491B (en) A method for eliminating microcracks in parts of nickel-based superalloy parts manufactured by electron beam selective melting additive manufacturing
Wang et al. Study on the designing rules and processability of porous structure based on selective laser melting (SLM)
CN102941343B (en) Quick manufacturing method of titanium-aluminum alloy composite part
CN104084584B (en) For the Laser Scanning of high temperature alloy structural member rapid shaping
RU2566117C2 (en) Production of 3d body
CN102335742B (en) A preparation method of biomedical porous titanium-molybdenum alloy implant with complex shape
CN108393492A (en) A method of shaping complexity NiTi alloy components using increasing material manufacturing
CN104646669A (en) Biomedical porous pure-titanium implant material and preparation method thereof
CN108339984B (en) Method for growing complex structure on surface of cast-forged piece based on wire 3D printing
CN102994804B (en) A kind of method preparing high fatigue property porous Ti-6Al-4V block materials
Mosallanejad et al. Additive manufacturing of titanium alloys: processability, properties, and applications
CN106148749B (en) One kind has both high intensity and the gradient porous Ti-6Al-4V block materials of high-selenium corn energy and preparation method thereof
CN102501006A (en) Method for manufacturing shape memory alloy-aluminum metal matrix composite material through ultrasonic welding
Abdulrahman et al. Laser metal deposition of titanium aluminide composites: A review
CN114653967B (en) A method for additive manufacturing of metallic glass lattice structure composite parts
CN105256160B (en) A kind of 3D printing method of ceramic base nickel alloy composite
CN107855522A (en) A kind of laser gain material manufacture method of porous micro-channel structure
CN105728722A (en) 3D printing method of ceramic titanium alloy composite biological implanting product
KR102546408B1 (en) Manufacturing method for Ti-6Al-4V alloy multilayer shaped structure and Ti-6Al-4V alloy multilayer shaped structure thereof
CN115106540A (en) Tantalum-tungsten alloy product and preparation method thereof
Wang et al. Research on the redesign of precision tools and their manufacturing process based on selective laser melting (SLM)
Kiel-Jamrozik et al. The heat treatment influence on the structure and mechanical properties of Ti6Al4V alloy manufactured by SLM technology

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20150429