CN105478762A - A Laser Forming Method for Cr3C2-FeCr Composite Components - Google Patents

A Laser Forming Method for Cr3C2-FeCr Composite Components Download PDF

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CN105478762A
CN105478762A CN201510895530.1A CN201510895530A CN105478762A CN 105478762 A CN105478762 A CN 105478762A CN 201510895530 A CN201510895530 A CN 201510895530A CN 105478762 A CN105478762 A CN 105478762A
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娄德元
廖加劲
熊厚
徐显金
翟中生
P·贝内特
刘顿
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Hubei 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
    • 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
    • B22F12/40Radiation means
    • B22F12/41Radiation means characterised by the type, e.g. laser or electron beam
    • B22F1/0003
    • 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
    • B22F10/25Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS]
    • 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
    • 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
    • B22F12/50Means for feeding of material, e.g. heads
    • B22F12/52Hoppers
    • 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
    • B22F12/50Means for feeding of material, e.g. heads
    • B22F12/53Nozzles
    • 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
    • B22F12/50Means for feeding of material, e.g. heads
    • B22F12/55Two or more means for feeding material
    • 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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Abstract

The invention relates to a laser forming method of a Cr3C2-FeCr composite component. Raw material powder selected in the laser forming method comprises, by weight percent, 4.23-6.31% of graphite, 39.82-47.25% of Cr, 3.26-5.16% of Mo, 0.59-0.71% of rare earth oxide and the balance Fe. Raw materials are in the form of powder, and the particle size of metal Fe powder, metal Cr powder, metal Mo powder and graphite powder is 50-200 microns. Quantitative conveying of powder formed through lasers is finished through a multi-hopper conveying system, four-pipe coaxial and discontinuous powder sprayers are adopted for laser forming, an inner and outer gradient layering structure of the Cr3C2-FeCr component can be achieved by controlling the powder conveying system and a laser head, and the fracture toughness of the Cr3C2-FeCr component can reach more than 70% of Fe base alloy.

Description

一种Cr3C2-FeCr复合材料构件的激光成形方法A Laser Forming Method for Cr3C2-FeCr Composite Components

技术领域 technical field

本发明属于激光成形领域,涉及一种Cr3C2-FeCr复合材料构件的激光成形方法。 The invention belongs to the field of laser forming, and relates to a laser forming method for a Cr 3 C 2 -FeCr composite material component.

背景技术 Background technique

Cr的碳化物类型主要有M3C2,M3C,M7C3和M23C6等类型,热力学稳定性较好的是Cr3C2、Cr7C3和Cr23C6,Cr3C2和Cr7C3常用做金属基复合材料(MMC)的增强相。其中Cr3C2在高温条件下依然能保持相当高的硬度,还具有很强的耐蚀性和耐磨性。Cr3C2-FeCr具有良好的高温耐磨性能,在中温环境下,可以代替昂贵的镍基、钴基合金及其复合材料。 The carbide types of Cr mainly include M 3 C 2 , M 3 C, M 7 C 3 and M 23 C 6 and other types, and the ones with better thermodynamic stability are Cr 3 C 2 , Cr 7 C 3 and Cr 23 C 6 , Cr 3 C 2 and Cr 7 C 3 are commonly used as reinforcing phases of metal matrix composites (MMC). Among them, Cr 3 C 2 can still maintain a relatively high hardness under high temperature conditions, and also has strong corrosion resistance and wear resistance. Cr 3 C 2 -FeCr has good high-temperature wear resistance, and can replace expensive nickel-based, cobalt-based alloys and their composite materials in medium-temperature environments.

MMC的制备技术依据增强颗粒的加入方式的不同,可分为原位自生和强制加入两种。外加Cr3C2颗粒的激光加工复合材料,会导致材料中Cr3C2分解,并重新生成Cr7C3等碳化物,成为Cr3C2复合材料激光加工的难点之一。原位自生技术借助合金设计,在基体金属内原位反应成核,生成一种或几种热力学稳定的增强相,这种方法避免了外加增强体的分解、节约能源、资源并能够减少排放,材料的增强体表面无污染,制品性能优良。但其工艺过程要求严格、较难掌握、且增强相的成分和体积分数不易控制。 The preparation technology of MMC can be divided into in-situ self-generation and forced addition according to the different ways of adding reinforcing particles. Adding Cr 3 C 2 particles to laser processing composite materials will cause Cr 3 C 2 in the material to decompose and regenerate carbides such as Cr 7 C 3 , which becomes one of the difficulties in laser processing of Cr 3 C 2 composite materials. The in-situ self-generation technology uses alloy design to react and nucleate in situ in the matrix metal to generate one or several thermodynamically stable reinforcement phases. This method avoids the decomposition of the external reinforcement, saves energy, resources and can reduce emissions. The reinforcement surface of the material is pollution-free, and the product performance is excellent. However, the process has strict requirements, is difficult to master, and the composition and volume fraction of the reinforcing phase are not easy to control.

激光成形工艺利用小体积累积成形的方法,可以在宏观控制增强相的均匀分布,为送粉激光原位成形颗粒增强MMC提供可能。金属粉与石墨粉的堆积密度相差较大,在激光成形过程中,容易因为粉体密度相差较大而造成分层,在成形部件中造成增强相的分布不均,而且会改变增强相的设计成分,大幅降低Cr3C2-FeCr复合材料部件的性能。因此本发明采用在线连续送粉激光原位复合成形的方法,制备Cr3C2-FeCr复合材料部件,使成形部件的增强相连续可控。 The laser forming process uses the method of small-volume cumulative forming, which can control the uniform distribution of the reinforcing phase at a macroscopic level, and provides the possibility for powder-fed laser in-situ forming particle-reinforced MMC. The bulk density difference between metal powder and graphite powder is large. During the laser forming process, it is easy to cause stratification due to the large difference in powder density, which will cause uneven distribution of the reinforcement phase in the formed part, and will change the design of the reinforcement phase. composition, greatly reducing the performance of Cr 3 C 2 -FeCr composite parts. Therefore, the present invention adopts the online continuous powder feeding laser in-situ compound forming method to prepare Cr 3 C 2 -FeCr composite material parts, so that the reinforced phase of the formed parts is continuous and controllable.

发明内容 Contents of the invention

本发明所要解决的技术问题是提供一种增强相分布可控的Cr3C2-FeCr复合材料构件的激光成形方法。本发明方法从原位合成路线和激光成形工艺着手,提供一种新的Cr3C2-FeCr复合材料结构件的激光成形方法,能够使增强相在复合材料中均匀分布,实现性能优良的Cr3C2-FeCr复合材料部件的激光成形。 The technical problem to be solved by the present invention is to provide a laser forming method of a Cr 3 C 2 -FeCr composite material component with controllable reinforcement phase distribution. The method of the present invention starts from the in-situ synthesis route and the laser forming process, and provides a new laser forming method for Cr 3 C 2 -FeCr composite material structural parts, which can make the reinforcing phase uniformly distributed in the composite material, and realize Cr with excellent performance. Laser forming of 3 C 2 -FeCr composite parts.

本发明方法主要包括以下步骤: The inventive method mainly comprises the following steps:

(1)原料配方与预处理 (1) Raw material formula and pretreatment

原料配方为:石墨4.23~6.31wt.%,Cr39.82~47.25wt.%,Mo3.26~5.16%,稀土氧化物0.59~0.71wt.%,Fe余量;原料采用粉体形式,金属Fe、Cr、Mo粉和石墨粉的颗粒尺寸50~200微米;将金属Cr粉和稀土氧化物粉末球磨0.5~5小时; The raw material formula is: graphite 4.23~6.31wt.%, Cr39.82~47.25wt.%, Mo3.26~5.16%, rare earth oxide 0.59~0.71wt.%, Fe balance; raw materials are in powder form, metal Fe The particle size of Cr, Mo powder and graphite powder is 50~200 microns; the metal Cr powder and rare earth oxide powder are ball milled for 0.5~5 hours;

(2)送粉与混料 (2) Powder feeding and mixing

采用多料斗螺旋送粉混合系统,所述多料斗螺旋送粉混合系统由四个送粉器分别通过送粉管与一个共同的激光头连接组成,将Cr和稀土氧化物的混合粉末放入第1个料斗中,Fe粉置于第2料斗中,Mo粉置于第3料斗中,石墨粉置于第4个料斗中,4个送粉器同时送粉,并通过调整螺杆转速控制粉体的比例; The multi-hopper spiral powder feeding mixing system is adopted, and the multi-hopper screw powder feeding mixing system is composed of four powder feeders respectively connected to a common laser head through powder feeding pipes, and the mixed powder of Cr and rare earth oxide is put into the first In one hopper, Fe powder is placed in the second hopper, Mo powder is placed in the third hopper, graphite powder is placed in the fourth hopper, four powder feeders feed powder at the same time, and the powder is controlled by adjusting the screw speed proportion;

(3)激光成形 (3) Laser forming

所述激光头采用4管同轴不连续喷嘴,对熔池环抱送粉,使熔池各成分均匀分布;对设计部件的数字图形分层切片,建立激光扫描路径,成形过程中,调节螺杆转速,使得局部生成的增强相Cr3C2在构件中的比例成梯度连续变化,即构件外层为Cr3C2-FeCr复合材料,内层为金属基体材料,并最终使用的原料符合步骤(1)的比例要求。 The laser head uses 4 coaxial discontinuous nozzles to feed powder around the molten pool, so that the components of the molten pool are evenly distributed; the digital graphics of the designed parts are layered and sliced, and the laser scanning path is established. During the forming process, the screw speed is adjusted. , so that the proportion of the locally generated reinforcing phase Cr 3 C 2 in the component changes continuously in a gradient, that is, the outer layer of the component is Cr 3 C 2 -FeCr composite material, the inner layer is a metal matrix material, and the final raw materials used meet the steps ( 1) Proportional requirements.

步骤(3)中采用光纤/CO2激光器。光纤/CO2激光的输出功率100~3000W,光斑直径0.2~4mm,搭接率10~80%,激光头Ar气流量0.2~13L/min,送粉器Ar气流量0.2~12L/min,激光头扫描速度3~125mm/s。 A fiber/ CO2 laser is employed in step (3). Fiber/CO 2 laser output power 100~3000W, spot diameter 0.2~4mm, overlap rate 10~80%, laser head Ar gas flow 0.2~13L/min, powder feeder Ar gas flow 0.2~12L/min, laser Head scanning speed 3~125mm/s.

本发明所用的多料斗螺旋送粉混合系统由四个送粉器分别通过送粉管与一个激光头连接组成,如图1所示。所述送粉器由料斗、螺杆和流化器组成,所述螺杆由直流步进电机推动。 The multi-hopper screw powder feeding mixing system used in the present invention is composed of four powder feeders respectively connected to a laser head through powder feeding pipes, as shown in Figure 1 . The powder feeder is composed of a hopper, a screw and a fluidizer, and the screw is driven by a DC stepping motor.

Cr3C2-FeCr复合材料的性能取决于Cr3C2的含量、尺寸和均匀分布。本发明以多料斗螺旋送粉混料系统即时送粉,并利用同轴不连续激光头成形出Cr3C2-FeCr复合材料部件,实现增强相的分布控制,消除复合材料中Cr3C2不均匀分布的情况,实现Cr3C2含量可调的Cr3C2-FeCr复合材料结构件的激光成形。 The properties of Cr 3 C 2 -FeCr composites depend on the content, size and uniform distribution of Cr 3 C 2 . The invention uses a multi-hopper screw powder feeding and mixing system to feed powder immediately, and uses a coaxial discontinuous laser head to form Cr 3 C 2 -FeCr composite material parts, realizes the distribution control of the reinforcement phase, and eliminates Cr 3 C 2 in the composite material In the case of uneven distribution, laser forming of Cr 3 C 2 -FeCr composite structural parts with adjustable Cr 3 C 2 content is realized.

本发明方法同时将构件表层和内层进行分别成形,控制送粉成分,实现内外分层结构的金属基复合材料部件的激光制造,使部件内部具有金属材料的韧性,表层具有耐磨、抗高温氧化的功能,且部件整体断裂韧度为同类金属部件的70%以上。 The method of the present invention separately forms the surface layer and the inner layer of the component at the same time, controls the powder feeding composition, and realizes the laser manufacturing of the metal matrix composite material parts of the inner and outer layered structures, so that the inside of the part has the toughness of the metal material, and the surface layer has wear resistance and high temperature resistance. Oxidation function, and the overall fracture toughness of the part is more than 70% of that of similar metal parts.

附图说明 Description of drawings

图1多料斗螺旋送粉混合系统结构示意图。 Figure 1 Schematic diagram of the structure of the multi-hopper screw powder feeding mixing system.

具体实施方式 detailed description

结合实施例对本发明做进一步描述。 The present invention will be further described in conjunction with embodiments.

实施例一 Embodiment one

一种Cr3C2-FeCr复合材料冶金退火炉辊激光成形方法,包括以下流程: A Cr 3 C 2 -FeCr composite material metallurgical annealing furnace roll laser forming method, comprising the following process:

(1)原料采用粉体形式,金属Fe、Cr、Mo粉和石墨粉的颗粒尺寸50~200微米以上;原料成分为:石墨4.23wt.%,Cr43.37wt.%,Mo3.26%,稀土氧化物0.59wt.%,Fe48.55wt.%;将Cr粉、稀土氧化物球磨混合2小时。 (1) The raw material is in the form of powder, the particle size of metal Fe, Cr, Mo powder and graphite powder is 50-200 microns or more; the raw material composition is: graphite 4.23wt.%, Cr43.37wt.%, Mo3.26%, rare earth Oxide 0.59wt.%, Fe48.55wt.%; ball mill and mix Cr powder and rare earth oxide for 2 hours.

(2)采用多料斗螺旋送粉混合系统进行送粉和即时混合,将Cr和稀土氧化物的混合粉末放入第1个料斗中,Fe粉置于第2料斗中,Mo粉置于第3料斗中,石墨粉置于第4个料斗中;4个送粉器同时送粉,并通过螺杆转速调整Cr3C2在粉体反应产物中的含量。 (2) Use a multi-hopper screw powder feeding mixing system for powder feeding and instant mixing. Put the mixed powder of Cr and rare earth oxides into the first hopper, Fe powder in the second hopper, and Mo powder in the third In the hopper, graphite powder is placed in the fourth hopper; 4 powder feeders feed powder at the same time, and the content of Cr 3 C 2 in the powder reaction product is adjusted by the screw speed.

(3)激光成形 (3) Laser forming

激光成形的激光头采用4管同轴不连续喷嘴,对熔池环抱送粉以使得激光熔池的成分得以均匀分布;将待加工的部件的数字图形分层切片,并建立激光扫描路径,然后控制送粉成分,利用数控机床进行激光成形,实现部件内外分层结构的激光成形,形成外层为耐磨的Cr3C2-FeCr复合材料,内部基体为金属基体的特殊结构件。激光加工使用光纤激光器,其输出功率550W,光斑直径0.35mm,搭接率38%,激光头Ar气流量4.6L/min,送粉器Ar气流量7.3L/min,激光头扫描速度12mm/s。 The laser head for laser forming adopts 4 coaxial discontinuous nozzles to feed powder around the molten pool so that the components of the laser molten pool can be evenly distributed; the digital graphics of the parts to be processed are sliced in layers, and the laser scanning path is established, and then The composition of the powder feeding is controlled, and the laser forming is carried out by the CNC machine tool to realize the laser forming of the internal and external layered structure of the component, forming a special structural part whose outer layer is wear-resistant Cr 3 C 2 -FeCr composite material, and the inner matrix is a metal matrix. Laser processing uses a fiber laser with an output power of 550W, a spot diameter of 0.35mm, an overlap rate of 38%, an Ar gas flow of the laser head of 4.6L/min, an Ar gas flow of the powder feeder of 7.3L/min, and a scanning speed of the laser head of 12mm/s. .

成形部件内部具有金属材料的韧性,表层具有耐磨、抗高温氧化的功能,且部件整体断裂韧度为同类金属部件的70%以上。 The inside of the formed part has the toughness of metal materials, and the surface layer has the functions of wear resistance and high temperature oxidation resistance, and the overall fracture toughness of the part is more than 70% of that of similar metal parts.

实施例二 Embodiment two

一种Cr3C2-FeCr复合材料热成型模具激光成形方法,包括以下流程: A Cr 3 C 2 -FeCr composite material thermoforming mold laser forming method, comprising the following processes:

(1)原料采用粉体形式,金属Fe、Cr、Mo粉和石墨粉的颗粒尺寸50~200微米以上;原料成分为:石墨5.19wt.%,Cr39.82wt.%,Mo5.16%,稀土氧化物0.71wt.%,Fe余量;将Cr粉、稀土氧化物球磨混合2.5小时。 (1) The raw material is in the form of powder, the particle size of metal Fe, Cr, Mo powder and graphite powder is 50-200 microns or more; the raw material composition is: graphite 5.19wt.%, Cr39.82wt.%, Mo5.16%, rare earth Oxide 0.71wt.%, Fe balance; Cr powder, rare earth oxide ball mill and mix for 2.5 hours.

(2)采用多料斗螺旋送粉混合系统进行送粉和即时混合,将Cr和稀土氧化物的混合粉末放入第1个料斗中,Fe粉置于第2料斗中,Mo粉置于第3料斗中,石墨粉置于第4个料斗中;4个送粉器同时送粉,并通过螺杆转速调整Cr3C2在粉体反应产物的含量。 (2) Use a multi-hopper screw powder feeding mixing system for powder feeding and instant mixing. Put the mixed powder of Cr and rare earth oxides into the first hopper, Fe powder in the second hopper, and Mo powder in the third In the hopper, graphite powder is placed in the fourth hopper; 4 powder feeders feed powder at the same time, and the content of Cr 3 C 2 in the powder reaction product is adjusted by the screw speed.

(3)激光成形 (3) Laser forming

激光成形的激光头采用4管同轴不连续喷嘴,对熔池环抱送粉以使得激光熔池的成分得以均匀分布;将待加工的部件的数字图形分层切片,并建立激光扫描路径,然后控制送粉成分和激光扫描路线,利用数控机床实现复合件内外分层结构的激光成形,形成外层为耐磨的Cr3C2-FeCr复合材料内部基体为金属基体的特殊结构件。激光加工使用CO2激光器,其输出功率800W,光斑直径0.25mm,搭接率55%,激光头Ar气流量3.8L/min,送粉器Ar气流量6.2L/min,激光头扫描速度14mm/s。 The laser head for laser forming adopts 4 coaxial discontinuous nozzles to feed powder around the molten pool so that the components of the laser molten pool can be evenly distributed; the digital graphics of the parts to be processed are sliced in layers, and the laser scanning path is established, and then Control the powder feeding composition and laser scanning route, use CNC machine tools to realize laser forming of the inner and outer layered structures of composite parts, and form special structural parts with wear-resistant Cr 3 C 2 -FeCr composite materials as the outer layer and the inner matrix as the metal matrix. Laser processing uses a CO 2 laser with an output power of 800W, a spot diameter of 0.25mm, an overlap rate of 55%, an Ar gas flow rate of the laser head of 3.8L/min, an Ar gas flow rate of the powder feeder of 6.2L/min, and a scanning speed of the laser head of 14mm/min. s.

成形部件内部具有金属材料的韧性,表层具有耐磨、抗高温氧化的功能,且部件整体断裂韧度为同类金属部件的70%以上。 The inside of the formed part has the toughness of metal materials, and the surface layer has the functions of wear resistance and high temperature oxidation resistance, and the overall fracture toughness of the part is more than 70% of that of similar metal parts.

实施例三 Embodiment Three

一种Cr3C2-FeCr复合材料热连轧输送辊激光成形方法,包括以下流程: A Cr 3 C 2 -FeCr composite material hot continuous rolling conveying roll laser forming method, comprising the following process:

(1)原料采用粉体形式,金属Fe、Cr、Mo粉和石墨粉的颗粒尺寸50~200微米以上;原料成分为:石墨6.31wt.%,Cr47.25wt.%,Mo4.86%,稀土氧化物0.64wt.%,Fe40.94wt.%;将Cr粉、稀土氧化物球磨混合3小时。 (1) The raw material is in the form of powder, the particle size of metal Fe, Cr, Mo powder and graphite powder is 50-200 microns or more; the raw material composition is: graphite 6.31wt.%, Cr47.25wt.%, Mo4.86%, rare earth Oxide 0.64wt.%, Fe40.94wt.%; Cr powder and rare earth oxides were ball milled and mixed for 3 hours.

(2)采用多料斗螺旋送粉混合系统进行送粉和即时混合,将Cr和稀土氧化物的混合粉末放入第1个料斗中,Fe粉置于第2料斗中,Mo粉置于第3料斗中,石墨粉置于第4个料斗中;4个送粉器同时送粉,并通过螺杆转速调整Cr3C2在粉体反应产物的含量。 (2) Use a multi-hopper screw powder feeding mixing system for powder feeding and instant mixing. Put the mixed powder of Cr and rare earth oxides into the first hopper, Fe powder in the second hopper, and Mo powder in the third In the hopper, graphite powder is placed in the fourth hopper; 4 powder feeders feed powder at the same time, and the content of Cr 3 C 2 in the powder reaction product is adjusted by the screw speed.

(3)激光成形工艺 (3) Laser forming process

激光成形的激光头采用4管同轴不连续喷嘴,对熔池环抱送粉以使得激光熔池的成分得以均匀分布;将待加工的部件的数字图形分层切片,并建立激光扫描路径,然后控制送粉成分和激光扫描路线,利用数控机床实现复合件内外分层结构的激光成形,形成外层为耐磨的Cr3C2-FeCr复合材料内部基体为金属基体的特殊结构件。激光加工使用光纤激光器,其输出功率900W,光斑直径0.40mm,搭接率30%,激光头Ar气流量7.8L/min,送粉器Ar气流量7.5L/min,激光头扫描速度28mm/s。 The laser head for laser forming adopts 4 coaxial discontinuous nozzles to feed powder around the molten pool so that the components of the laser molten pool can be evenly distributed; the digital graphics of the parts to be processed are sliced in layers, and the laser scanning path is established, and then Control the powder feeding composition and laser scanning route, use CNC machine tools to realize laser forming of the inner and outer layered structures of composite parts, and form special structural parts with wear-resistant Cr 3 C 2 -FeCr composite materials as the outer layer and the inner matrix as the metal matrix. Laser processing uses a fiber laser with an output power of 900W, a spot diameter of 0.40mm, an overlap rate of 30%, an Ar gas flow of the laser head of 7.8L/min, an Ar gas flow of the powder feeder of 7.5L/min, and a scanning speed of the laser head of 28mm/s. .

Claims (3)

1. a Cr 3c 2the laser forming method of-FeCr composite element, is characterized in that comprising the steps:
(1) composition of raw materials and pretreatment
Composition of raw materials is: graphite 4.23 ~ 6.31wt.%, Cr39.82 ~ 47.25wt.%, Mo3.26 ~ 5.16%, rare earth oxide 0.59 ~ 0.71wt.%, Fe surplus; Raw material adopts powder, the particle size of metal Fe, Cr, Mo powder and graphite powder 50 ~ 200 microns; By Metal Cr powder and RE oxide powder ball milling 0.5 ~ 5 hour;
(2) powder feeding and batch mixing
Adopt many hoppers spiral powder feeding hybrid system, described many hoppers spiral powder feeding hybrid system is connected to form respectively by powder feeding pipe and a common laser head by four powder feeders, the mixed-powder of Cr and rare earth oxide is put into the 1st hopper, Fe powder is placed in the 2nd hopper, Mo powder is placed in the 3rd hopper, graphite powder is placed in the 4th hopper, 4 powder feeder powder feedings simultaneously, and is controlled the ratio of powder by adjustment screw speed;
(3) laser forming
Described laser head adopts the coaxial discontinuous nozzle of 4 pipe, encircles powder feeding to molten bath, makes each uniform composition distribution in molten bath; To the digital figure hierarchy slicing of design part, set up laser beam scan path, in forming process, adjusting screw(rod) rotating speed, makes the wild phase Cr that local generates 3c 2ratio in component becomes gradient consecutive variations, and namely component skin is Cr 3c 2-FeCr composite, internal layer is metal matrix material, and the raw material of final utilization meets the proportion requirement of step (1).
2. the laser forming method according to patent requirements 1, is characterized in that, adopts optical fiber/CO in step (3) 2laser instrument, power output 100 ~ 3000W, spot diameter 0.2 ~ 4mm, overlapping rate 10 ~ 80%, laser head Ar throughput 0.2 ~ 13L/min, powder feeder Ar throughput 0.2 ~ 12L/min, laser head sweep speed 3 ~ 125mm/s.
3. the laser forming method according to patent requirements 1, is characterized in that, described powder feeder is made up of hopper, screw rod and Fluidizer, and described screw rod is promoted by DC stepper motor.
CN201510895530.1A 2015-12-08 2015-12-08 A Laser Forming Method for Cr3C2-FeCr Composite Components Pending CN105478762A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108994295A (en) * 2018-07-25 2018-12-14 吉林师范大学 A kind of 3D printing feed device
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
CN110480009A (en) * 2019-09-10 2019-11-22 淮浙煤电有限责任公司凤台发电分公司 A kind of probe tube structure of steel gradated material and preparation method thereof
CN115178734A (en) * 2022-05-16 2022-10-14 广州大学 Granular double/multi-metal composite material and preparation method thereof

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5453329A (en) * 1992-06-08 1995-09-26 Quantum Laser Corporation Method for laser cladding thermally insulated abrasive particles to a substrate, and clad substrate formed thereby
CN101818342A (en) * 2009-12-15 2010-09-01 江苏大学 Method and device for preparing working layer of metallurgical hot roll by laser direct deposition
CN103691949A (en) * 2014-01-09 2014-04-02 湖北工业大学 Laser forming method of WC (Wolfram Carbide)-metal composite material structural component
CN103993308A (en) * 2014-04-10 2014-08-20 江苏新亚特钢锻造有限公司 Method for re-manufacturing roller shaft part through laser cladding
CN104260360A (en) * 2014-07-28 2015-01-07 中国科学院重庆绿色智能技术研究院 Multi-material laser direct writing conformal system and method

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5453329A (en) * 1992-06-08 1995-09-26 Quantum Laser Corporation Method for laser cladding thermally insulated abrasive particles to a substrate, and clad substrate formed thereby
CN101818342A (en) * 2009-12-15 2010-09-01 江苏大学 Method and device for preparing working layer of metallurgical hot roll by laser direct deposition
CN103691949A (en) * 2014-01-09 2014-04-02 湖北工业大学 Laser forming method of WC (Wolfram Carbide)-metal composite material structural component
CN103993308A (en) * 2014-04-10 2014-08-20 江苏新亚特钢锻造有限公司 Method for re-manufacturing roller shaft part through laser cladding
CN104260360A (en) * 2014-07-28 2015-01-07 中国科学院重庆绿色智能技术研究院 Multi-material laser direct writing conformal system and method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108994295A (en) * 2018-07-25 2018-12-14 吉林师范大学 A kind of 3D printing feed device
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
CN110480009A (en) * 2019-09-10 2019-11-22 淮浙煤电有限责任公司凤台发电分公司 A kind of probe tube structure of steel gradated material and preparation method thereof
CN115178734A (en) * 2022-05-16 2022-10-14 广州大学 Granular double/multi-metal composite material and preparation method thereof

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