CN100404174C - A preparation method for rapidly manufacturing functionally graded materials - Google Patents
A preparation method for rapidly manufacturing functionally graded materials Download PDFInfo
- Publication number
- CN100404174C CN100404174C CNB2006100182908A CN200610018290A CN100404174C CN 100404174 C CN100404174 C CN 100404174C CN B2006100182908 A CNB2006100182908 A CN B2006100182908A CN 200610018290 A CN200610018290 A CN 200610018290A CN 100404174 C CN100404174 C CN 100404174C
- Authority
- CN
- China
- Prior art keywords
- layer
- powder
- fgms
- materials
- laser
- 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.)
- Expired - Fee Related
Links
Classifications
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P10/00—Technologies related to metal processing
- Y02P10/25—Process efficiency
Landscapes
- Powder Metallurgy (AREA)
Abstract
本发明公开了一种快速制造功能梯度材料的制备方法,该方法根据所制功能梯度材料性能的要求,将原料组分按梯度比例进行级分配料;根据各层级分配料中组分比例,确定每一层的激光加工工艺参数;将上述配制好的各层粉末进行预热并且保温处理;然后通过送粉装置平铺在工作平台上,层层扫描,实现功能梯度材料的制造。采用本发明直接制造FGMs具有生产率高、工艺简单、制造成本低、取材广泛、致密度高和机械性能好等优点。例如:用SLM快速成形技术制造含有TiC/Ni3Al/Ni成分的FGMs时,不需要脱粘、高温后处理和烧结等工艺,生产周期相当于采用SLS方法的1/3-1/5,致密度可以达到99%,制造的FGMs具有抗高温氧化和腐蚀性能。The invention discloses a preparation method for rapidly manufacturing functional gradient materials. According to the performance requirements of the prepared functional gradient materials, the method divides the raw material components according to the gradient ratio; The laser processing parameters of each layer; preheat and heat-preserve the prepared powder of each layer above; then spread it on the working platform through the powder feeding device, and scan layer by layer to realize the manufacture of functionally graded materials. The direct production of FGMs by the present invention has the advantages of high productivity, simple process, low manufacturing cost, wide selection of materials, high density, good mechanical properties and the like. For example: when using SLM rapid prototyping technology to manufacture FGMs containing TiC/Ni3Al/Ni components, debonding, high temperature post-treatment and sintering processes are not required, and the production cycle is equivalent to 1/3-1/5 of the SLS method, and the density It can reach 99%, and the manufactured FGMs are resistant to high temperature oxidation and corrosion.
Description
技术领域 technical field
本发明属于先进快速制造领域,具体涉及一种快速制造功能梯度材料(Functionally Gradient Materials,简称FGMs)的制备方法。The invention belongs to the field of advanced rapid manufacturing, in particular to a method for rapidly manufacturing functionally gradient materials (Functionally Gradient Materials, referred to as FGMs).
背景技术 Background technique
FGMs是一种新型功能梯度材料,它要求材料的组元或内部结构沿某一特定方向呈规律性分布,从而使材料某种性能沿此方向产生连续或梯度变化。FGMs应用领域由单一的航空航天到核能源、电子材料、光学工程、化学工程和生物医学等领域,并且不断延伸。FGMs的传统制造方法有:粉末冶金法、电镀法、自蔓延燃烧高温合成法、等离子喷涂法、电沉积法、离心铸造法等。例如,粉末冶金法是将10μm~100μm粒径的粉末(金属、陶瓷)充分混合,按组分梯度分层填充或连续成分控制填充,压实后烧结制备FGMs,该方法应控制原料的粉末尺寸和粉末填充排列的精度,但是生产率低和难于精确控制材料成分及内部结构是其最大不足。采用电镀法制造FGMs即通常所说的直流电镀,通过电解的方法在固体表面获得金属(合金)沉积层的一种电化学过程,电镀的目的在于改变固体材料表面特性,电镀可以使材料改善外观,提高耐腐蚀性能,抗耐磨性,还可使材料表面具有磁、电、光、热等表面特性,但是这种方法只能制备FGMs涂层,生产率也较低。自蔓延燃烧高温合成法是利用参与合成反应的粉末混合物烧结时放出的大量热量,使反应持续进行,反应后的产物便是新材料,但是这种方法仅仅适用于发生高放热反应的体系。等离子喷涂法是将原材料粉末送入等离子射流中,在熔融状态下喷涂在衬底上形成覆膜,通过连续调整原料粉末的喷涂比例和输送条件来控制覆膜的成分和组织来制备FGMs,但是这种方法制造工艺复杂,而且难于精确控制材料成分及内部结构。由上可知:一般能够直接制造出FGMs零件的方法仅限于粉末冶金法,其他方法大都停留在制备FGMs涂层上,涂层的厚度都比较小,而且,这些传统制备方法不仅工艺复杂、制备条件高、生产效率低和难于精确控制材料成分及内部结构,因而导致材料容易产生缺陷,并且,一种制备方法往往只适用于某一特定的材料体系,应用范围比较狭窄,如自蔓延燃烧高温合成法只适用于发生高放热反应的体系,而离心铸造法只能够生产轴对称的FGMs等。FGMs is a new type of functionally graded material, which requires the components or internal structure of the material to be regularly distributed along a certain direction, so that a certain property of the material can produce continuous or gradient changes along this direction. The application fields of FGMs range from a single aerospace to nuclear energy, electronic materials, optical engineering, chemical engineering and biomedicine, and continue to expand. The traditional manufacturing methods of FGMs include: powder metallurgy, electroplating, self-propagating combustion high-temperature synthesis, plasma spraying, electrodeposition, centrifugal casting, etc. For example, the powder metallurgy method is to fully mix powders (metals, ceramics) with a particle size of 10 μm to 100 μm, fill them in layers according to the composition gradient or continuous composition control filling, and sinter to prepare FGMs after compaction. This method should control the powder size of the raw materials And the accuracy of powder filling arrangement, but the low productivity and the difficulty of precisely controlling the material composition and internal structure are its biggest shortcomings. Electroplating is used to manufacture FGMs, which is commonly referred to as DC electroplating. It is an electrochemical process in which a metal (alloy) deposition layer is obtained on a solid surface by electrolysis. The purpose of electroplating is to change the surface characteristics of solid materials. Electroplating can improve the appearance of materials , improve corrosion resistance, wear resistance, and make the surface of the material have magnetic, electrical, optical, thermal and other surface properties, but this method can only prepare FGMs coatings, and the productivity is also low. The self-propagating combustion high-temperature synthesis method uses the large amount of heat released during the sintering of the powder mixture participating in the synthesis reaction to continue the reaction, and the product after the reaction is a new material, but this method is only suitable for systems with high exothermic reactions. The plasma spraying method is to feed the raw material powder into the plasma jet and spray it on the substrate to form a coating in a molten state. The FGMs are prepared by continuously adjusting the spraying ratio and conveying conditions of the raw material powder to control the composition and organization of the coating, but The manufacturing process of this method is complicated, and it is difficult to precisely control the material composition and internal structure. It can be seen from the above that the methods that can directly manufacture FGMs parts are generally limited to the powder metallurgy method, and most of the other methods stay on the preparation of FGMs coatings, and the thickness of the coatings is relatively small. Moreover, these traditional preparation methods are not only complicated in process and difficult in preparation conditions. High, low production efficiency and difficult to precisely control the material composition and internal structure, thus causing the material to be prone to defects. Moreover, a preparation method is often only applicable to a specific material system, and the application range is relatively narrow, such as self-propagating combustion high-temperature synthesis The method is only suitable for systems with high exothermic reactions, and the centrifugal casting method can only produce axisymmetric FGMs, etc.
由上可知:采用上述传统制造方法制造FGMs大大地阻碍了FGMs的大规模生产和应用,为此,出现了几种基于快速成形技术的FGMs制造技术,克服了传统制造方法所存在的一些缺陷,但是更多的是通过间接方法得到。例如:制造FGMs的常用快速成形技术主要有:三维打印(Three Dimensionalprinting,3DP)、熔融沉积制造(Fusing Deposition Manufacturing,FDM)、选择性激光烧结(Selective Laser Sintering,SLS)。采用3DP方法制造FGMs是在喷料中加入梯度成分颗粒料浆,逐层喷射到CAD选区成形并且控制其达到区域梯度成分要求,从而制造三维FGMs。FDM是采用丝状热塑性材料熔融后逐层沉积在选区成形的方法,目前由于采用了向热塑性材料中添加金属或陶瓷颗粒的新技术,该方法可以直接成形金属和陶瓷功能梯度原型件。在国外,Sandia国家实验室的LENS(Laser Engineered NetShaping)系统、美国密西根大学的DMD系统和斯坦福大学的SDM(ShapingDeposition Manufacturing)系统等均采用三维激光熔覆(ThreeDimensional Laser Cladding,3DLC)技术直接制造FGMs。美国的奥斯汀大学采用SLS方法,利用液相烧结的方法制造FGMs,由于其可以控制结构和孔隙率,比较适合制造生物相容材料和化学催化剂等FGMs。SLS的制造优势在于不需支撑,不受结构和形状复杂的限制,但其致密度低和强度不足是一大缺陷。在国内,哈尔滨工业大学利用叠层成型系统(LOM)和自蔓延(SHS)相结合的方法制造TiC/Ni的FGMs,其中LOM用作材料成形,SHS用于材料形坯烧结致密化,但是制作工艺繁琐而难于控制。It can be seen from the above that the use of the above-mentioned traditional manufacturing methods to manufacture FGMs has greatly hindered the large-scale production and application of FGMs. For this reason, several FGMs manufacturing technologies based on rapid prototyping technology have emerged, which overcome some of the defects in the traditional manufacturing methods. But more are obtained through indirect methods. For example, the commonly used rapid prototyping technologies for manufacturing FGMs mainly include three-dimensional printing (Three Dimensional printing, 3DP), fused deposition manufacturing (Fusing Deposition Manufacturing, FDM), and selective laser sintering (Selective Laser Sintering, SLS). Using the 3DP method to manufacture FGMs is to add gradient composition particle slurry to the spray material, spray it to the CAD selection area layer by layer and control it to meet the requirements of the regional gradient composition, so as to manufacture three-dimensional FGMs. FDM is a method in which filamentous thermoplastic materials are melted and deposited layer by layer in selected areas. At present, due to the new technology of adding metal or ceramic particles to thermoplastic materials, this method can directly form metal and ceramic functional gradient prototypes. In foreign countries, the LENS (Laser Engineered NetShaping) system of Sandia National Laboratory, the DMD system of the University of Michigan and the SDM (Shaping Deposition Manufacturing) system of Stanford University are all directly manufactured by three-dimensional laser cladding (ThreeDimensional Laser Cladding, 3DLC) technology. FGMs. The University of Austin in the United States adopts the SLS method to manufacture FGMs by liquid phase sintering. Because it can control the structure and porosity, it is more suitable for the manufacture of FGMs such as biocompatible materials and chemical catalysts. The manufacturing advantage of SLS is that it does not require support and is not limited by complex structures and shapes, but its low density and insufficient strength are major defects. In China, Harbin Institute of Technology uses a combination of laminated molding system (LOM) and self-propagating (SHS) to manufacture TiC/Ni FGMs, in which LOM is used for material forming, and SHS is used for sintering and densification of material blanks. The process is cumbersome and difficult to control.
实践证明,采用现有的快速成形技术制造FGMs是可行的,但是存在诸多缺点,例如:需要脱粘和高温后处理烧结,同时要考虑材料中不同相的烧结速率,很难避免收缩和变形,致密度低和机械性能差等等。Practice has proved that it is feasible to fabricate FGMs with existing rapid prototyping techniques, but there are many disadvantages, such as: debonding and high-temperature post-treatment sintering are required, while considering the sintering rates of different phases in the material, it is difficult to avoid shrinkage and deformation, Low density and poor mechanical properties, etc.
发明内容 Contents of the invention
本发明的目的在于克服上述诸多不足,提供一种快速制造功能梯度材料的制备方法,采用本发明直接制造的FGMs具有收缩和变形小、致密度高、生产周期短和机械性能好的特点。The purpose of the present invention is to overcome the above-mentioned shortcomings and provide a preparation method for rapidly manufacturing functionally graded materials. The FGMs directly produced by the present invention have the characteristics of small shrinkage and deformation, high density, short production cycle and good mechanical properties.
本发明提供的一种快速制造功能梯度材料的制备方法,其步骤为:A kind of preparation method of fast manufacturing functional gradient material provided by the present invention, its steps are:
(1)采用三维造型软件设计出FGMs的CAD模型,然后由切片软件处理后保存为STL文件,将STL文件的数据信息输送到选择性激光熔化快速成形设备;(1) Design the CAD model of FGMs by using 3D modeling software, and then save it as an STL file after being processed by the slicing software, and transfer the data information of the STL file to the selective laser melting rapid prototyping equipment;
(2)按照所制FGMs对性能的要求,根据上述CAD模型进行级分配料,确定各层的组分比例,并确定每一层粉末的激光加工工艺参数;(2) According to the performance requirements of the prepared FGMs, carry out graded distribution according to the above CAD model, determine the component ratio of each layer, and determine the laser processing parameters of each layer of powder;
(3)将上述配制好的各层粉末进行预热保温处理,以降低熔化的每层以及成形件的残余应力;(3) Carry out preheating and heat preservation treatment to each layer of powder prepared above, to reduce the residual stress of each layer of melting and formed parts;
(4)送粉机构将第一层级分配料平铺在工作平台上,层厚为0.1mm~0.3mm;(4) The powder feeding mechanism spreads the first-level distribution material on the working platform, with a layer thickness of 0.1mm to 0.3mm;
(5)在保护气体环境下,激光器按照步骤(2)确定的该层的激光加工工艺参数对粉末扫描,熔化激光作用区的粉末材料,使粉末熔化区域温度控制在液相线以上30-100℃内,其扫描间距为0.1-0.3mm;(5) Under the protective gas environment, the laser scans the powder according to the laser processing parameters of the layer determined in step (2), and melts the powder material in the laser action area, so that the temperature of the powder melting area is controlled at 30-100°C above the liquidus line Within ℃, the scanning distance is 0.1-0.3mm;
(6)送粉机构按照相同的层厚将下一层级分配料平铺在工作平台上;(6) The powder feeding mechanism spreads the next level of distribution material on the working platform according to the same layer thickness;
(7)重复上述步骤(5)-(6),对粉末进行层层扫描,直至任务完成。(7) Repeat the above steps (5)-(6) to scan the powder layer by layer until the task is completed.
因为FGMs的成分一般由两种组元构成,而且在成形时要随CAD模型中厚度的变化及时改变成分以满足梯度性能要求,根据缓和热应力的设计原则,通过具有FGMs信息的有限元软件分析确定每层的组分比例,由计算机控制混粉机构进行每层粉末材料成分的配制,由计算机控制送粉机构来输送与CAD模型中不同位置对应的成分粉末,然后通过光纤激光器熔化每层粉末,层层叠加,从而完成FGMs的制造。在加工过程中不需要脱粘、高温后处理和烧结等工艺。采用本发明直接制造FGMs具有生产率高、工艺简单、制造成本低、取材广泛、致密度高和机械性能好等优点。例如:用SLM快速成形技术制造含有TiC/Ni3Al/Ni成分的FGMs时,不需要脱粘、高温后处理和烧结等工艺,生产周期相当于采用SLS方法的1/3-1/5,致密度可以达到99%,制造的FGMs具有抗高温氧化和腐蚀性能。Because the composition of FGMs is generally composed of two components, and the composition should be changed in time with the change of thickness in the CAD model during forming to meet the gradient performance requirements, according to the design principle of relieving thermal stress, through the analysis of finite element software with FGMs information Determine the component ratio of each layer, the powder mixing mechanism is controlled by the computer to prepare the powder material composition of each layer, the powder feeding mechanism is controlled by the computer to deliver the component powder corresponding to different positions in the CAD model, and then the powder of each layer is melted by the fiber laser , layer by layer to complete the fabrication of FGMs. No debonding, high-temperature post-treatment and sintering processes are required during processing. The direct production of FGMs by the present invention has the advantages of high productivity, simple process, low manufacturing cost, wide selection of materials, high density, good mechanical properties and the like. For example: when using SLM rapid prototyping technology to manufacture FGMs containing TiC/Ni3Al/Ni components, debonding, high temperature post-treatment and sintering processes are not required, and the production cycle is equivalent to 1/3-1/5 of the SLS method, and the density It can reach 99%, and the manufactured FGMs are resistant to high temperature oxidation and corrosion.
具体实施方式 Detailed ways
(1)用Pro/Engineer、Unigraphic等三维造型软件设计出FGMs的CAD模型,然后由切片软件处理后保存为STL文件,将STL文件的数据信息输送到选择性激光熔化快速成形设备(即SLM设备);(1) Use Pro/Engineer, Unigraphic and other three-dimensional modeling software to design the CAD model of FGMs, and then save it as an STL file after being processed by the slicing software, and send the data information of the STL file to the selective laser melting rapid prototyping equipment (ie SLM equipment );
(2)按照所制FGMs对性能的要求,根据上述CAD模型进行级分配料,确定各层的组分比例;并确定每一层粉末的激光加工工艺参数,包括激光功率、扫描速度、层厚和扫描间距。激光加工工艺参数的确定原则为:根据该层成分的熔点,来确定激光功率、扫描速度、层厚和扫描间距,使激光作用区的粉末熔化,为减少液面的表面张力,激光作用区的温度应在混合粉末的液相线以上30-100℃区域内。(2) According to the performance requirements of the prepared FGMs, carry out graded distribution according to the above CAD model, determine the component ratio of each layer; and determine the laser processing parameters of each layer of powder, including laser power, scanning speed, layer thickness and scanning distance. The principle of determining the parameters of laser processing is: according to the melting point of the layer composition, the laser power, scanning speed, layer thickness and scanning distance are determined to melt the powder in the laser action area. In order to reduce the surface tension of the liquid surface, the laser action area The temperature should be in the region of 30-100°C above the liquidus of the mixed powder.
例如:以TiCN、WC、Co和Ni为原料制得表面为硬质高耐磨TiCN-Ni相,内部为高强韧性WC-Co相的梯度金属陶瓷切削刀具,其Co成分在芯部沿断面呈梯度5%体积变化,可使材料表面产生大于0.45Gpa的残余压缩应力,从而表面得以强化而内部得以韧化,避免了切削时由于热应力而造成表面层热裂。For example: TiCN, WC, Co and Ni are used as raw materials to prepare a gradient cermet cutting tool with a hard and wear-resistant TiCN-Ni phase on the surface and a high-strength and toughness WC-Co phase inside. Gradient 5% volume change can cause residual compressive stress greater than 0.45Gpa on the surface of the material, so that the surface can be strengthened and the interior can be toughened, avoiding thermal cracking of the surface layer caused by thermal stress during cutting.
(3)将上述配制好的各层粉末进行预热保温处理,以降低熔化的每层以及成形件的残余应力。(3) Preheat and heat-preserve the powders of each layer prepared above to reduce the residual stress of each layer melted and the formed part.
(4)送粉机构将第一层级分配料平铺在工作平台上,层厚为0.1mm~0.3mm;(4) The powder feeding mechanism spreads the first-level distribution material on the working platform, with a layer thickness of 0.1mm to 0.3mm;
(5)在氩气或者氢气保护气体环境下,激光器按照步骤(2)确定的该层的激光加工工艺参数对粉末扫描,熔化激光作用区的粉末材料,使粉末熔化区域温度控制在液相线以上30-100℃内,其扫描间距为0.1-0.3mm。(5) In the argon or hydrogen protective gas environment, the laser scans the powder according to the laser processing parameters of the layer determined in step (2), and melts the powder material in the laser action area, so that the temperature of the powder melting area is controlled at the liquidus line Above 30-100°C, the scanning distance is 0.1-0.3mm.
(6)送粉机构按照相同的层厚将下一层级分配料平铺在工作平台上;(6) The powder feeding mechanism spreads the next level of distribution material on the working platform according to the same layer thickness;
(7)重复上述步骤(5)-(6),对粉末进行层层扫描,直至任务完成。这样最终实现FGMs的制造,工件制造完成后缓慢冷却即可。(7) Repeat the above steps (5)-(6) to scan the powder layer by layer until the task is completed. In this way, the fabrication of FGMs is finally realized, and the workpiece can be cooled slowly after fabrication.
上述采取的材料主要为TiC/Ni3Al/Ni和Ti/ZrO2等。The materials adopted above are mainly TiC/Ni3Al/Ni and Ti/ZrO 2 and so on.
实施例1:Example 1:
通过SLM方法制造20mm厚含有TiC粉末(5μm)、Ni3Al粉末和Ni粉末(5~6μm)组分的FGMs,目的是制造耐高温和能够经受大幅度温差反复热冲击的FGMs。根据上面性能要求,FGMs的组成设计规则为:一侧表面为厚1mm的Ni,另一侧表面为厚1mm的TiC,中间层Ni3Al粉末含量按照(x/d)p体积函数关系逐层递增,TiC粉末逐层递减。其中x是梯度层的位置坐标,d是各梯度层的总厚度,在此为20mm,p是组成分布指数,在此取值范围为1.5~1.8。The 20mm thick FGMs containing TiC powder (5μm), Ni3Al powder and Ni powder (5-6μm) components were manufactured by SLM method, the purpose is to manufacture FGMs that are resistant to high temperature and can withstand repeated thermal shocks with large temperature differences. According to the above performance requirements, the composition design rules of FGMs are as follows: one side surface is Ni with a thickness of 1mm, and the other side surface is TiC with a thickness of 1mm. The TiC powder decreases layer by layer. Where x is the position coordinate of the gradient layer, d is the total thickness of each gradient layer, which is 20 mm here, and p is the composition distribution index, and the value range here is 1.5-1.8.
本工艺首先用Pro/Engineer、Unigraphic等三维造型软件设计出FGMs的实体造型,然后由切片软件处理后保存为STL文件,将STL文件的数据信息输送到SLM的快速成形系统中,根据所制FGMs对组分和性能的要求,通过粉末成分随加工位置变化的函数(x/d)p进行系列配料,然后在氩气气氛保护下预热到1250℃,保温8h,由计算机控制送粉机构将配料平铺在工作平台上,每层的最小厚度为0.1mm,采用的TiC粉粒5μm左右,Ni3Al粉末和Ni粉末粒径5μm~6μm左右;最后采用光纤激光器、扫描速度(200mm/s-500mm/s)、扫描层厚(0.1mm-0.3mm)和扫描间距(0.1mm--0.2mm),熔化扫描层粉末材料,层层叠加,实现TiC、Ni3Al和Ni的FGMs的制造,工件制造完成后缓慢冷却至室温。经过测试:接近TiC侧的残余应力变化范围为-200Mpa-200Mpa,制造的FGMs耐高温和能够经受大幅度温差热冲击。This process first uses Pro/Engineer, Unigraphic and other three-dimensional modeling software to design the solid shape of FGMs, and then it is processed by slicing software and saved as an STL file, and the data information of the STL file is sent to the rapid prototyping system of SLM. For the requirements of components and properties, a series of batching is carried out through the function (x/d) p of the powder composition changing with the processing position, and then preheated to 1250°C under the protection of an argon atmosphere, and kept for 8 hours, and the powder feeding mechanism is controlled by a computer. The ingredients are spread on the working platform, the minimum thickness of each layer is 0.1mm, the TiC powder used is about 5μm, the particle size of Ni3Al powder and Ni powder is about 5μm~6μm; finally, the fiber laser is used, and the scanning speed (200mm/s-500mm /s), scanning layer thickness (0.1mm-0.3mm) and scanning distance (0.1mm--0.2mm), melting the scanning layer powder material, layer by layer stacking, to realize the manufacture of FGMs of TiC, Ni3Al and Ni, and the workpiece is manufactured Then slowly cool to room temperature. After testing: the range of residual stress close to the TiC side is -200Mpa-200Mpa, and the manufactured FGMs are resistant to high temperature and can withstand large temperature difference thermal shock.
实施例2:Example 2:
通过SLM方法制造16mm厚Ti/ZrO2的FGMs,首先用Pro/Engineer、Unigraphic等三维造型软件设计出FGMs的实体造型,然后由切片软件处理后保存为STL文件,将STL文件的数据信息输送到SLM的快速成形系统中,根据所制FGMs对组分和性能的要求,通过具有FGMs信息的CAD/CAM软件分析粉末成分随加工位置变化的函数关系,如按Ti/ZrO2体积之比10%的梯度增加进行系列配料,然后在氩气气氛保护下预热到1100℃,保温8h,由计算机控制送粉机构按照上述FGMs所需的加料量与加工位置之间的函数关系将配料平铺在工作平台上,每层的最小厚度为0.1mm,采用的W粉和Cu粉粒径均为0.5μM左右;最后采用光纤激光器、扫描速度(200mm/s-500mm/s)、扫描层厚(0.1mm-0.3mm)和扫描间距(0.1mm-0.2mm),熔化扫描层粉末材料,层层叠加,实现Ti/ZrO2的FGMs的制造,工件制造完成后缓慢冷却至室温。经过试验计算分析,纯Ti和ZrO2两侧的均受压应力,分别为-10Mpa和-60Mpa左右,中间大部分处在张应力状态,这样的应力状态有利于提高材料的强度特性,具有较好的热应力缓和特性。The FGMs of 16mm thick Ti/ ZrO2 are manufactured by the SLM method. Firstly, the solid shape of the FGMs is designed with 3D modeling software such as Pro/Engineer and Unigraphic, and then processed by the slicing software and saved as an STL file. The data information of the STL file is sent to In the rapid prototyping system of SLM, according to the composition and performance requirements of the prepared FGMs, the functional relationship of the powder composition with the change of the processing position is analyzed through the CAD/CAM software with FGMs information, such as the volume ratio of Ti/ZrO 2 is 10% The gradient increases for a series of batching, and then preheated to 1100°C under the protection of argon atmosphere, and kept for 8 hours. The powder feeding mechanism is controlled by the computer according to the functional relationship between the feeding amount required by the above FGMs and the processing position. On the working platform, the minimum thickness of each layer is 0.1mm, and the particle size of W powder and Cu powder used is about 0.5μM; finally, fiber laser is used, scanning speed (200mm/s-500mm/s), scanning layer thickness (0.1 mm-0.3mm) and scanning distance (0.1mm-0.2mm), the powder material of the scanning layer is melted and stacked layer by layer to realize the manufacture of FGMs of Ti/ ZrO2 , and the workpiece is slowly cooled to room temperature after the workpiece is manufactured. Through experimental calculation and analysis, both sides of pure Ti and ZrO 2 are subjected to compressive stress, which are about -10Mpa and -60Mpa respectively, and most of the middle is in a state of tensile stress. Such a stress state is conducive to improving the strength characteristics of the material and has a relatively Good thermal stress relief properties.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2006100182908A CN100404174C (en) | 2006-01-24 | 2006-01-24 | A preparation method for rapidly manufacturing functionally graded materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2006100182908A CN100404174C (en) | 2006-01-24 | 2006-01-24 | A preparation method for rapidly manufacturing functionally graded materials |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1803348A CN1803348A (en) | 2006-07-19 |
| CN100404174C true CN100404174C (en) | 2008-07-23 |
Family
ID=36865569
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2006100182908A Expired - Fee Related CN100404174C (en) | 2006-01-24 | 2006-01-24 | A preparation method for rapidly manufacturing functionally graded materials |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100404174C (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2839905A1 (en) * | 2013-08-22 | 2015-02-25 | Astrium GmbH | Manufacturing of components from parts made from different materials, particularly of space transportation components such as combustion chambers for thrusters |
Families Citing this family (35)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101899592B (en) * | 2010-08-03 | 2011-08-24 | 华中科技大学 | Method for synthesizing arbitrarily shaped NiTi shape memory alloy in situ |
| CN101985176A (en) * | 2010-11-19 | 2011-03-16 | 浙江工业大学 | Preheating temperature controllable method for preparing heterogeneous material components based on SLS prototyping |
| US20130101728A1 (en) * | 2011-10-21 | 2013-04-25 | John J. Keremes | Additive manufacturing in situ stress relief |
| CH705750A1 (en) * | 2011-10-31 | 2013-05-15 | Alstom Technology Ltd | A process for the production of components or portions, which consist of a high-temperature superalloy. |
| CH705662A1 (en) * | 2011-11-04 | 2013-05-15 | Alstom Technology Ltd | Process for producing articles of a solidified by gamma-prime nickel-base superalloy excretion by selective laser melting (SLM). |
| US20140099476A1 (en) * | 2012-10-08 | 2014-04-10 | Ramesh Subramanian | Additive manufacture of turbine component with multiple materials |
| CN102941343B (en) * | 2012-11-16 | 2014-12-24 | 西北有色金属研究院 | Quick manufacturing method of titanium-aluminum alloy composite part |
| FR2998496B1 (en) * | 2012-11-27 | 2021-01-29 | Association Pour La Rech Et Le Developpement De Methodes Et Processus Industriels Armines | ADDITIVE MANUFACTURING PROCESS OF A PART BY SELECTIVE FUSION OR SELECTIVE SINTING OF BEDS OF POWDER WITH COMPACITY OPTIMIZED BY A HIGH ENERGY BEAM |
| CN103231055B (en) * | 2013-05-13 | 2014-10-22 | 柳岸敏 | Differential laser three-dimensional (3D) metal piece printing method |
| CN103240414B (en) * | 2013-05-27 | 2015-03-18 | 黑龙江科技大学 | Parameter selecting method for manufacturing metal parts by selective laser melting technology and substrate samples |
| CN103317590B (en) * | 2013-06-26 | 2015-10-28 | 大连理工大学 | A kind of laser 3D prints the method for ceramic function gradient structure part |
| CN103611939A (en) * | 2013-11-28 | 2014-03-05 | 宁波金鹏高强度紧固件有限公司 | Method for manufacturing abrasion-resistant fastening piece through 3D printing technology |
| CN104715091B (en) * | 2013-12-16 | 2018-05-22 | 华中科技大学 | A kind of method for quickly forming and manufacturing of aluminium alloy periodic lattice porous structure |
| RU2558019C1 (en) * | 2014-03-12 | 2015-07-27 | Российская Федерация в лице Министерства промышленности и торговли РФ (МИНПРОМТОРГ РОССИИ) | Production of arc welding plasma torch |
| CN104923783A (en) * | 2014-03-19 | 2015-09-23 | 上海航天设备制造总厂 | Method forming high-melting-point high temperature alloy part via multi-laser head multi-laser beam path scanning |
| CN103952697A (en) * | 2014-05-04 | 2014-07-30 | 丹阳聚辰光电科技有限公司 | Laser-cladding tungsten-copper composite material and preparation method thereof |
| JP2017524579A (en) * | 2014-05-04 | 2017-08-31 | エオプレックス・リミテッドEoplex Limited | Multi-material 3D printer |
| CN104338931B (en) * | 2014-10-09 | 2015-06-17 | 湖南华曙高科技有限责任公司 | Method and device for preparing functionally graded structural component |
| CN105256160B (en) * | 2015-10-29 | 2018-02-16 | 广东省材料与加工研究所 | A kind of 3D printing method of ceramic base nickel alloy composite |
| CN105458260B (en) * | 2015-12-28 | 2019-06-25 | 天津清研智束科技有限公司 | Additive manufacturing device and method |
| CN105695982B (en) * | 2016-01-25 | 2018-08-14 | 西安交通大学 | A kind of method of increasing material manufacturing copper tungsten functionally graded material electrical contact |
| CN105772723B (en) * | 2016-04-18 | 2020-05-15 | 西安智熔金属打印系统有限公司 | Rapid forming system and method for gradient material structure |
| US10426976B1 (en) | 2016-06-22 | 2019-10-01 | The University Of Toledo | Nitinol organ positioner to prevent damage to healthy tissue during radiation oncology treatments |
| CN106735204A (en) * | 2016-12-07 | 2017-05-31 | 中北大学 | A kind of selective laser melting self- propagating manufacturing process |
| CN106623924B (en) * | 2016-12-07 | 2018-12-11 | 中北大学 | A method of the powder metallurgy forming functionally graded material melted based on precinct laser |
| CN106682299B (en) * | 2016-12-22 | 2020-03-31 | 西安交通大学 | Design and manufacturing method for sand mold regional variable strength by selective laser sintering |
| CN108273999A (en) * | 2018-03-08 | 2018-07-13 | 上海材料研究所 | A kind of metal material high throughput preparation method based on 3D printing technique |
| CN108580903B (en) * | 2018-05-24 | 2019-10-25 | 华中科技大学 | A lightweight metal-based lattice thermal insulation-bearing structure and its forming method |
| CN109249022B (en) * | 2018-09-21 | 2020-01-03 | 华中科技大学 | Double-gradient metal porous material and preparation method thereof |
| CN109277699A (en) * | 2018-09-28 | 2019-01-29 | 浙江浙能技术研究院有限公司 | A kind of increasing material manufacturing method of heterogenous steel pipe connector |
| CN109513925B (en) * | 2018-12-03 | 2021-05-25 | 航天特种材料及工艺技术研究所 | Thin-wall large-temperature-gradient structural component and laser direct deposition preparation method thereof |
| CN113727958A (en) * | 2019-02-11 | 2021-11-30 | 霍洛公司 | Method and system for three-dimensional printing |
| CN110453104B (en) * | 2019-09-05 | 2020-07-17 | 中国航空制造技术研究院 | Titanium-based SiC-Ti mixed gradient material and preparation method thereof |
| JP7272989B2 (en) * | 2020-03-31 | 2023-05-12 | 三菱重工業株式会社 | Method for manufacturing gas turbine combustor and burner parts |
| CN112059175B (en) * | 2020-08-12 | 2023-04-25 | 西安理工大学 | A preparation method of WC reinforced WCu double gradient structure composite material |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6526327B2 (en) * | 1998-01-12 | 2003-02-25 | University Of Central Florida | One-step rapid manufacturing of metal and composite parts |
| CN1415451A (en) * | 2001-11-02 | 2003-05-07 | 西北工业大学 | Method for high speed preparing and forming the gradient material by use of laser |
| CN1631582A (en) * | 2004-12-15 | 2005-06-29 | 华中科技大学 | Rapid forming system for direct manufacturing metal parts |
-
2006
- 2006-01-24 CN CNB2006100182908A patent/CN100404174C/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6526327B2 (en) * | 1998-01-12 | 2003-02-25 | University Of Central Florida | One-step rapid manufacturing of metal and composite parts |
| CN1415451A (en) * | 2001-11-02 | 2003-05-07 | 西北工业大学 | Method for high speed preparing and forming the gradient material by use of laser |
| CN1631582A (en) * | 2004-12-15 | 2005-06-29 | 华中科技大学 | Rapid forming system for direct manufacturing metal parts |
Non-Patent Citations (6)
| Title |
|---|
| 激光选区烧结成形机的粉末预热研究. 李湘生,史玉升,黄树槐.机械工程学报,第38卷第3期. 2002 |
| 激光选区烧结成形机的粉末预热研究. 李湘生,史玉升,黄树槐.机械工程学报,第38卷第3期. 2002 * |
| 直接金属粉末激光烧结成形机制的研究. 顾冬冬,沈以赴,潘琰峰,胥橙庭.材料工程,第5期. 2004 |
| 直接金属粉末激光烧结成形机制的研究. 顾冬冬,沈以赴,潘琰峰,胥橙庭.材料工程,第5期. 2004 * |
| 选择性激光烧结技术的发展现状. 潘琰峰,沈以赴,顾冬冬,胥橙庭.工具技术,第38卷第6期. 2004 |
| 选择性激光烧结技术的发展现状. 潘琰峰,沈以赴,顾冬冬,胥橙庭.工具技术,第38卷第6期. 2004 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2839905A1 (en) * | 2013-08-22 | 2015-02-25 | Astrium GmbH | Manufacturing of components from parts made from different materials, particularly of space transportation components such as combustion chambers for thrusters |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1803348A (en) | 2006-07-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100404174C (en) | A preparation method for rapidly manufacturing functionally graded materials | |
| Lewis et al. | Practical considerations and capabilities for laser assisted direct metal deposition | |
| Zhang et al. | Fundamental study on plasma deposition manufacturing | |
| Kumar | Selective laser sintering: a qualitative and objective approach | |
| Gu | Laser additive manufacturing of high-performance materials | |
| CN101780544A (en) | Method for forming refractory metal parts by using laser | |
| CN103949639B (en) | The method that a kind of selective laser smelting technology prepares Nb-Si based ultra-high temperature alloy | |
| Yap et al. | Review of selective laser melting: Materials and applications | |
| CN105945281B (en) | The deposition forming machining manufacture of part and mold | |
| EP3546091A1 (en) | Combined additive manufacturing method applicable to parts and molds | |
| CN109396434B (en) | A method for preparing titanium alloy parts based on selective laser melting technology | |
| Saha et al. | Additive manufacturing of ceramics and cermets: present status and future perspectives | |
| Jamaludin et al. | A review on the fabrication techniques of functionally graded ceramic-metallic materials in advanced composites | |
| CN103949646B (en) | A kind of preparation method of Nb-Si based ultra-high temperature alloy turbine blade | |
| CN108728695A (en) | Multiphase nano ceramic particle hybrid reinforced nickel-based alloy and laser forming method thereof | |
| CN104745887A (en) | Nano ceramic particle reinforced nickel-based superalloy composite material and laser 3D printing forming method thereof | |
| CN104388849A (en) | Quick molding method of metal-matrix composite part | |
| CN102773479A (en) | Near-net-shape forming method of refractory metal part | |
| WO2015185001A1 (en) | Incremental manufacturing method for part or mold | |
| WO2016013494A1 (en) | Alloy powder used in fused deposition modeling, and production method of said alloy powder | |
| Shen et al. | Large-scale NiFe2O4-based cermets prepared by composite extrusion modelling: from high-qualified composite feedstock to dense sintered microstructure | |
| Suwanpreecha et al. | A review on material extrusion additive manufacturing of metal and how it compares with metal injection moulding. Metals 2022; 12: 429 | |
| CN105798294A (en) | Rapid part prototyping method for refractory materials | |
| Karar et al. | An analysis on the advanced research in additive manufacturing | |
| US20220001447A1 (en) | Method for modifying the dimensions of a cast iron pump part |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20080723 |