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1.
碳化硅铝基复合材料具有优良的导热性、较高的比强度和比刚度,在航空航天领域具有广泛的应用前景。由于此复合材料中含有增强相,导致材料的切削加工性能变差。通过试验分析了不同颗粒体积分数(纳米级5%、微米级25%)SiCp/Al复合材料和切削参数(切削速度、背吃刀量、进给量)对刀具磨损和工件表面质量的影响,并对刀具磨损机理进行了研究。试验结果表明,车削微米级25%SiCp/Al材料时聚晶金刚石PCD(Polycrystalline Diamond)刀具磨损更严重,且工件表面质量更差。随着进给量和背吃刀量的增大,工件表面粗糙度值增大,刀片前刀面磨损严重;随着切削速度的增大,工件表面粗糙度值减小,刀片前刀面磨损量增大。选取本文切削参数进行SiCp/Al复合材料的切削加工时,发现刀具磨粒磨损、微崩刃是PCD刀具后刀面磨损的主要成因,且刀具前刀面也会产生积屑瘤。研究结果可为SiCp/Al复合材料PCD车削工艺的优化提供理论基础。  相似文献   

2.
在研究了钛舍金材料切削性能的基础上,针对钛合金的特点,选用了五种国内常用的硬质舍金刀片材料,对钛合金进行深孔钻削刀具磨损试验。结果表明,确定了适合钻削钛合金TC11的硬质合金刀片材料。  相似文献   

3.
 本文介绍了用P18、M2Al、M42等三种高速钢拉刀低速拉削TC9钛合金时的刀具磨损、拉削表面完整性同拉削工艺条件的关系,同时也探讨了用H19硬质合金拉刀高速拉削TC9钛合金的可能性;并比较了两种拉削条件下的刀具磨损和表面完整性状况;分析了为提高钛合金拉削的表面完整性所应采取的措施。  相似文献   

4.
钛合金是一种典型难磨削加工材料,磨削表面易出现烧伤、裂纹等热损伤。本文开展了TC4-DT钛合金磨削实验,通过扫描电镜(SEM)、能谱(EDS)、X射线衍射(XRD)、显微硬度仪、金相显微镜及球-盘摩擦磨损实验仪研究了其表面特性及摩擦磨损性能。结果表明:低速磨削表面质量好,摩擦磨损性能较基体略提高;当砂轮线速度为80 m/s时,磨削表面质量良好,摩擦系数为0.38,较基体降低40%;而砂轮线速度为100 m/s时,磨削表面出现严重烧伤、网状裂纹。因此选择合理的高速磨削工艺可避免烧伤、裂纹等热损伤缺陷,并可有效改善表面摩擦磨损性能;磨削表面干摩擦磨损机制为磨粒磨损、粘着磨损和剥层磨损。  相似文献   

5.
张志强  杨凡  张宏伟  张天刚 《航空学报》2021,42(7):624115-624115
采用同轴送粉激光熔覆技术在Ti6Al4V合金表面成功制备了含稀土CeO2的碳化钛增强钛基激光熔覆层。运用渗透探伤、光学显微镜、X射线衍射仪、扫描电镜、能谱分析仪、电子探针、显微硬度计、摩擦磨损试验机等分析和测试方法研究了碳化钛增强钛基激光熔覆层的成形质量、微观组织、元素分布、硬度和摩擦磨损性能。结果表明,涂层内无裂纹缺陷,仅在层间过渡区分布有少量气孔(孔隙率为1.65%)。涂层中物相主要包括富Ti、Cr元素的β固溶体(CrTi4)、缺位型碳化钛(TiCx)和稀土氧化物(CeO2)。熔覆层各微区的碳化钛形貌存在显著差异,熔覆层顶部和中部区域呈发达树枝晶状和针状,而结合区由针状和小尺寸不发达枝晶组成。碳化钛枝晶中碳元素分布不均匀,一次枝晶含碳量高于二次枝晶。基体相中Ni和Cr元素呈现明显偏析,而Al和V元素分布相对均匀。此外,稀土氧化物CeO2主要分布于TiCx与CrTi4相界以及CrTi4晶粒边界处。与基材相比,尽管TiCx增强钛基复合涂层具有较高的摩擦系数,但其耐磨性显著增加(提高近52%)。熔覆层和基材磨损机制均为黏着磨损和磨粒磨损的复合磨损模式,但熔覆层的磨损程度较轻。  相似文献   

6.
为探索高硅氧玻璃纤维/酚醛树脂复合材料的切削加工性能,对该类材料进行大直径薄壁回转类零件的车削加工。采用四种不同刀具进行实验研究,获得了不同切削参数及不同刀具材料对切削力的影响规律。试验结果表明:切削用量三要素中,切削深度对切削力的影响最大,其次是进给量,而切削速度的影响很小。当切削速度为119.32 mm/min、进给量为0.1 mm/r、背吃刀量为0.5 mm时,为最优切削参数。Ti-Al-Si-N纳米涂层硬质合金和超硬材料F2HX无涂层硬质合金刀具适合于低速加工,而PCD刀具则适合于高速加工。  相似文献   

7.
氢对TC4合金物理力学性能的影响及其与切削性能的相关性   总被引:5,自引:0,他引:5  
分析研究了TC4合金经适当氢处理后的微观组织和物理力学性能变化规律,并通过切削试验研究了氢对切削加工性能和刀具磨损的影响,初步分析了二者的相关性.  相似文献   

8.
CFRP/TC4叠层板的钻削实验   总被引:1,自引:1,他引:0  
采用硬质合金麻花钻对碳纤维复合材料-钛合金叠层板进行钻削试验,分析了钛合金层加工参数对刀具磨损的影响和刀具磨损机制。刀具磨损对孔入口处最大撕裂长度的影响。结果表明:磨损的主要区域是横刃和后刀面,前刀面磨损不明显。钛合金层的低转速和低进给量可以降低刀具磨损;此外随着钻孔数的增加,钛合金层转速越低、进给量越大碳纤维复合材料孔入口处孔质量更好。  相似文献   

9.
TC4的铣削加工中铣削力和刀具磨损研究   总被引:2,自引:0,他引:2  
通过TC4铣削加工时的铣削力试验,研究了干切削时和有氮气介质铣削时影响铣削力大小的几个因素,为提高金属去除率优化了切削参数。同时通过刀具磨损试验,对上述两种铣削方式,比较了在不同的切削速度下铣削时铣刀后刀面的磨损,证实了以氮气为切削介质能够大大地改善刀具的磨损状况和提高刀具的寿命。  相似文献   

10.
使用硬质合金刀具对钛合金TB6进行正交铣削实验,对比分析不同切削参数下的刀具磨损情况,并用实验结果进行回归分析得到刀具磨损的回归公式。结果表明:刀具主要磨损在后刀面,其磨损大都呈现一条带状磨损带,在速度增大时大磨损带变长,刀具易发生脆性破损,且在刀具表面会出现钛合金粘连;对刀具耐用度的影响大小依次为切削速度、进给量、切削宽度和切削深度;刀具磨损回归方程具有良好的回归方差,能够很好的对刀具寿命进行预测。  相似文献   

11.
针对钛合金切削加工过程中切削力大、切削温度高和刀具磨损严重等问题,近年学者们尝试采用微织构刀具来解决。本文综述了微织构刀具在钛合金切削加工中的应用,分析了微织构刀具在改善表面质量,降低切削力、刀具磨损、摩擦因数和切削温度等方面的切削机理,并指出微织构刀具切削钛合金存在的问题。  相似文献   

12.
王珉  张幼桢 《航空学报》1988,9(9):495-498
 在钛合金铣削加工的过程中,伴随着产生各种物理、化学现象,如变形、切削热、切削力、摩擦与磨损等。而它们之间又是相互联系、相互影响、相互作用。同时又以各自独立的物理、化学和机械现象表现出来。因此只有同时从各个方面对它们进行研究,才能深入揭示其本质。弄清其作用机理,从而去指导生产实践。  相似文献   

13.
Tool Materials Rapid Selection Based on Initial Wear   总被引:1,自引:0,他引:1  
Based on a large amount of literature about tool wear research, 873 tool wear curves are taken as samples, and statistical analysis is carried out to select the most suitable tool from all the tool materials suggested by the tool manufacturers. Statistical relationships between the initial wear and uniform wear periods are obtained. The results show that there is qualitative relationship between wear rate during initial wear period (WRIWP) and wear rate in uniform wear period (WRUWP) to certain extent. On this basis, a tool material rapid selection method based on the initial wear is put forward, and suitable tool materials for machining titanium alloy are selected. The experimental results indicate that this method is effective and useful. The new tool materials rapid selection can be used to select suitable cutting tool materials quickly before carrying out systematic machinability tests with the most suitable tool materials. The technology can be applied to doing the initial selection of cutting tool materials in either the machinability research or the workshop production.  相似文献   

14.
Titanium alloys are widely used in aeronautics that demand a good combination of high strength, good corrosion resistance and low mass. The mechanical properties lead to challenges in machining operations such as high process temperature as well as rapidly increasing tool wear. The conventional tool materials are not able to maintain their hardness and other mechanical properties at higher cutting temperatures encountered in high speed machining. In this work, the new material tools, which are polycrystalline diamond (PCD) and polycrystalline cubic boron nitride (PCBN) tools, are used in high-speed milling of Ti-6.5Al-2Zr-1Mo-1V (TA15) alloy. The performance and wear mechanism of the tools are investigated. Compared to PCBN tool, PCD tool has a much longer tool life, especially at higher cutting speeds. Analyses based on the SEM and EDX suggest that attrition, adhesion and diffusion are the main wear mechanisms of PCD and PCBN tools in high-speed milling of TA15. Oxidation wear is also observed at PCBN tool/workpiece interface. Roughness, defects, micro-hardness and microstructure of the machined surface are investigated. The recorded surface roughness values with PCD/PCBN tools are bellow 0.3 μm at initial and steady cutting stage. Micro-hardness analysis shows that the machined surface hardening depth with PCD and PCBN tools is small. There is no evidence of sub-surface defects with PCD and PCBN tools. It is concluded that for TA15 alloy, high-speed milling can be carried out with PCD/PCBN tools.  相似文献   

15.
建立了一套便携式的在线刀具磨损图像检测装置及相应的计算程序,利用该装置观察到了涂层硬质合金刀具加工300M高强度钢过程的定性磨损规律,并确定了刀具磨损量的测量方法。  相似文献   

16.
砂带磨粒磨损直接影响磨削表面质量进而影响构件综合服役性能.以表面完整性为评估指标,对砂带磨损前后钛合金的表面加工质量进行了试验研究,揭示了砂带磨粒磨损对磨削TC17表面粗糙度、残余应力和表面硬度的影响规律及机制.结果表明,磨粒磨损后由于高度均匀化、单位面积切削磨粒数增加、磨削深度减小,使得表面粗糙度减小、纹理均匀细腻,...  相似文献   

17.
基于域对抗门控网络的变工况刀具磨损精确预测方法   总被引:1,自引:0,他引:1  
万鹏  李迎光  刘长青  华家玘 《航空学报》2021,42(10):524879-524879
刀具磨损的精确预测对保证零件加工质量、提高生产效率和降低制造成本具有重要作用。在实际加工过程中,切削参数、刀具几何参数、刀具材料等工况复杂多变,工况信息和刀具磨损量对监测信号的耦合作用为刀具磨损的精确预测带来了很大挑战。针对以上问题,提出了一种基于域对抗门控网络(DAGNN)的变工况刀具磨损精确预测方法。引入工况分类网络并利用无磨损量标签样本,通过域对抗和门控过滤机制自适应地从不同工况的原始监测信号中提取表征刀具磨损且对工况变化不敏感的关键信号特征。对信号特征提取网络和刀具磨损预测网络进行迭代优化,从而实现变工况刀具磨损的精确预测。实验结果表明:相比已有的方法,本文方法能够利用少量带磨损量标签的目标工况样本实现刀具材料和刀具直径变化情况下的刀具磨损量精确预测,预测精度大幅提高。  相似文献   

18.
《中国航空学报》2023,36(6):446-459
Cubic boron nitride (cBN) superabrasive grinding wheels exhibit unique advantages in the grinding of difficult-to-cut materials with high strength and toughness, such as titanium alloys and superalloys. However, grinding with multilayered metallic cBN superabrasive wheels faces problems in terms of grain wear resistance, the chip storage capability of the working layers and the stability and controllability of the dressing process. Therefore, in this work, novel metallic cBN superabrasive wheels with aggregated cBN (AcBN) grains and open pore structures were fabricated to improve machining efficiency and surface quality. Prior to the grinding trials, the air-borne abrasive blasting process was conducted and the abrasive blasting parameters were optimized in view of wear properties of cBN grains and metallic matrix materials. Subsequently, the comparative experiments were performed and then the variations in grinding force and force ratio, grinding temperature, tool wear morphology and ground surface quality of the multilayered AcBN grinding wheels were investigated during machining Ti–6Al–4V alloys. In consideration of the variations of grain erosion wear volume and material removal rate per unit of pure metallic matrix materials as the abrasive blasting parameters changes, the optimal abrasive blasting parameters were identified as the SiC abrasive mesh size of 60# and the abrasive blasting distance and time of 60 mm and 15 s, respectively. The as-developed AcBN grains exhibited better fracture toughness and impact resistance than monocrystalline cBN (McBN) grains because of the existence of metal-bonded materials amongst multiple cBN particles that decreased crack propagation inside whole grains. The metallic porous AcBN wheels had lower grinding forces and temperature and better ground surface quality than vitrified McBN wheels due to the constant layer-by-layer exposure of cBN particles in the working layer of AcBN wheels.  相似文献   

19.
《中国航空学报》2021,34(6):110-124
In-situ ceramics particle reinforced aluminum matrix composites are favored in the aerospace industry due to excellent properties. However, the hard ceramic particles as the reinforcement phase bring challenges to machining. To study the effect of in-situ TiB2 particles on machinability and surface integrity of TiB2/2024 composite and TiB2/7075 composite, milling experiments were performed, and compared with conventional 2024 and 7075 aluminum alloys. In-situ TiB2 particles clustered at the grain boundaries and dispersed inside the matrix alloy grains hinder the dislocation movement of the matrix alloy. Therefore, the milling force and temperature of the composites are higher than those of the aluminum alloys due to the increase of the strength and the decrease of the plasticity. In the milling of composites, abrasive wear is the main wear form of carbide tools, due to the scratching of hard nano-TiB2 particles. The composites containing in-situ TiB2 particles have machining defects such as smearing, micro-scratches, micro-pits and tail on the machined surface. However, in-situ TiB2 particles impede the plastic deformation of the composites, which greatly reduces cutting edge marks on the machined surface. Therefore, under the same milling parameters, the surface roughness of TiB2/2024 composite and TiB2/7075 composite is much less than that of 2024 and 7075 aluminum alloy respectively. Under the milling conditions of this experiment, the machined subsurface has no metamorphic layer, and the microhardness of the machined surface is almost the same as that of the material. Besides, compared with 2024 and 7075 aluminum alloy, machined surfaces of TiB2/2024 composite and TiB2/7075 composite both show tensile residual stress or low magnitude of compressive residual stress.  相似文献   

20.
采用PCD刀具对碳纤维复合材料(CFRP)进行了镗削加工试验,分析了切削用量对切削力、孔出口撕裂因子(撕裂值与孔直径的比值)的影响规律.试验结果表明,三向切削力随背吃刀量、进给量、切削速率的增大而增大.经分析认为,切削速率的增大引起待加工材料的屈服应力增大.由于刀尖圆弧半径较大,试验中出现背向力大于主切削力的现象;撕裂因子与背吃刀量基本无关;进给量与撕裂因子呈线性正相关;当切削速率增大时撕裂因子呈减小趋势,并且减小到一定程度后基本不变;采用PCD刀具镗削加工该材料能够有效地减小孔出口撕裂程度.  相似文献   

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