共查询到16条相似文献,搜索用时 156 毫秒
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针对透波性Si_3N_4陶瓷铣削加工过程中易出现边缘破损现象,通过不同铣削深度实验研究了边缘破损类型、产生位置以及切深对边缘破损影响,并分析了边缘破损产生机理,最后提出了边缘破损控制方法。结果表明:当切深为0.4~0.8 mm时,边缘破损主要集中于出口棱边和入刀侧边;且脆性域加工过程中随着切深的增加,边缘破损程度呈现增大趋势;降低切深至≤0.3 mm且采用跟随周边走刀方式,并保证入刀处刀尖线速度方向与进给方向夹角不小于90°,可以有效控制边缘破损。研究为提高透波性Si_3N_4陶瓷铣削加工表面质量提供了技术支撑。 相似文献
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使用PCD立式铣刀对聚合物浸渍裂解法(PIP)制备的SiC_(f)/SiC复合材料开展单因素铣削试验,通过对加工中产生的切削力和加工后的表面粗糙度进行测量,分析了铣削工艺参数对其的影响;对加工表面、纤维断口进行SEM分析,讨论了SiC_(f)/SiC复合材料加工表面的形成。研究结果表明,表面粗糙度与切削力的变化趋势相同,高主轴转速和小切削宽度有利于得到表面粗糙度较小的加工表面;近孔洞区域与远离孔洞区域的材料去除方式不同;材料中纤维发生面内偏移和层间屈曲,纤维存在多种去除方式。 相似文献
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钛合金径向超声振动铣削表面粗糙度研究 总被引:2,自引:0,他引:2
为提高钛合金零件加工质量,设计了径向超声振动辅助铣削试验装置,研究了切削速度、切削深度、进给速度和超声振动幅值对钛合金零件表面粗糙度的影响规律.试验结果表明,与普通铣削相比,径向超声振动铣削后工件上的刀痕更加平整、分布更加均匀,材料去除更彻底,有效减少了由于钛合金切屑粘刀造成的表面划痕和积屑瘤等现象.在不同的切削参数下,径向超声振动铣削均可以改善钛合金零件的表面粗糙度,这一点在低速切削时更为明显,而超声振动幅值过大或过小都会影响加工质量.对加工系统的切削力进行了分析,发现超声振动辅助铣削时系统的切削力明显减小,有助于提高加工系统的稳定性,从而能够获得较好的表面质量. 相似文献
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TiAl合金以其优异的性能被广泛应用于航空、航天制造领域,但由于TiAl合金自身的物理、化学特性,导致其切削性能较差,加工过程中容易出现工件表面烧伤、表面微裂纹等问题。为了研究TiAl合金铣削加工过程中切削工艺参数对加工表面裂纹的影响规律,设计了TiAl合金切削参数与加工表面裂纹之间的正交试验。结果表明:切削速度对TiAl合金铣削表面裂纹的影响最大,其次是切削深度和切削宽度,每齿进给量对表面裂纹的影响最小。基于遗传算法,以表面裂纹长度为目标函数,优化得到的最优参数组合为:ae=0. 2 mm、ap=0. 2003 mm/z、fz=0. 02001 mm/z、vc=20. 0004 m/min。采用优化后的参数铣削TiAl合金,发现工件表面的实际加工裂纹长度和经过算法优化的裂纹长度相差较小,该优化方法可行性较高,误差较小。 相似文献
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通过对TC21钛合金进行高速铣削加工试验,测量不同切削参数下的表面粗糙度.采用正交方法来安排试验和极差分析法对实验数据处理,分析了不同切削参数对粗糙度的影响.其中对TC21钛合金表面粗糙度影响最为显著的因素是每齿进给量,其次为切削深度和切削速率,最后为切削宽度.通过对粗糙度影响机理分析在加工中宜采用较小的进给量和切削深度、较大的切削速率和切削宽度. 相似文献
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TC4钛合金是 1种典型的不易加工材料,其切削加工表面质量很难控制。为实现面向侧铣加工表面形貌的切削工艺参数优选,开展了 TC4钛合金侧铣加工实验研究。首先,探究了加工表面微观缺陷特征及其形成机制;然后,采用粗糙度参数 Ra和 Sa对铣削表面形貌进行定量表征,并分析了切削速度、进给量和切削深度对表面粗糙度参数的影响;最后,基于遗传算法(Genetic Algorithm,GA)对铣削工艺参数进行了优化。研究发现,加工表面微观缺陷主要有进给刀痕等固有缺陷和黏附颗粒等随机缺陷。铣削表面粗糙度随主轴转速的增大先减小后增大;随径向切深的增大先增大后减小;随进给量先增大后减小。在主轴转速 n = 1 093 r/min、径向切深 ae = 0.2 mm、每转进给量 f = 0.06 mm/r的条件下可以获得较小的表面粗糙度。 相似文献
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石英纤维增强聚酰亚胺复合材料是一种非均匀的各向异性材料,采用传统铣削方法对其进行加工时存在刀具磨损严重、切削力较大、加工效率低等问题。为此本文采用超低温冷却铣削方法对石英纤维增强聚酰亚胺复合材料进行铣削实验,并与传统干铣削方式进行了对比,分析了包括加工表面形貌、粗糙度、切削力和刀具磨损等切削性能。结果表明:两种工况下,表面粗糙度随主轴转速的提高而降低,随切深的增加呈先降低后增大趋势;相对于干铣削,不同切削速度下超低温冷却铣削有效抑制了低速干铣削纤维起毛、高速干铣削黏结剂烧蚀缺陷,表面质量都得到改善,刀具耐用度得到提高。超低温冷却引起的复合材料切削力增大,纤维断屑方式的改变以及切削热的有效降低是提高加工质量的主要原因。 相似文献
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石英增强聚酰亚胺树脂基复合材料是一种非均匀的各向异性材料,其加工性能高度依赖于纤维铺层方向与加工进给方向所成角度,即纤维方向角。本文通过一系列不同纤维方向角的干切削和超低温冷却铣削实验,研究了纤维方向角对表面形貌、表面粗糙度、铣削力及刀具磨损的影响。结果表明:不同纤维方向角,剪应力形式不同,切削断屑形式也不同。纤维方向角为锐角时铣削表面质量均良好,但当纤维方向角增大到90°时,切削表面质量下降,切削力变化幅度增大。相同铣削时间内,在干切削工况下,刀具磨损严重,涂层脱落面积约为测量面积的70%;而在低温切削工况下,涂层未遭到严重破坏,刀具仍处于稳定磨损阶段,刀具耐用度优于干切削工况。 相似文献
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《中国航空学报》2020,33(4):1361-1374
In five-axis flank milling operations, the intersecting surfaces of different cutting edges create roughness on the milled surfaces that cannot be ignored in situations with strict requirements, especially in aeronautical manufacturing. To focus on motion problems in milling operations, this paper presents a new model that utilizes elliptical paths as cutting edge trajectories on 3D surface topography machined by peripheral milling. First, the cutter parallel axis offset and location angle are considered, which change the location of the ellipse center and intersection point of the cutting edges. Then, through the proposed model, the predicted surface topography is obtained, and the factors that affect the development tendency of roughness are analyzed. Next, the effects of the cutter location position (CLP) geometric parameters, cutter parallel axis offset and curvature on the roughness are evaluated by a numerical simulation. Finally, machining tests are carried out to validate the model predictions, and the results show that the surface topography predictions correspond well with the experimental results. 相似文献
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《中国航空学报》2023,36(6):402-419
Large-size thin-walled curved surface parts of pure iron are crucial in aerospace, national defense, energy and precision physical experiments. However, the high machining accuracy and surface quality are difficult to achieve due to the serious tool wear and deformation when machining the parts with conventional cutting tools. In this paper, an elliptical vibration cutting (EVC) with active cutting edge shift (ACES) based on a long arbor vibration device is proposed for ultra-precision machining the pure iron parts by using diamond tool. Compared with cutting at a fixed cutting edge, the influence of ACES on the EVC was analyzed. Experiments in EVC of pure iron with ACES were conducted. The evolutions of the surface roughness, surface topography, and chip morphology with tool wear in EVC with ACES are revealed. The reasonable parameters of ultra-precision machining the pure iron parts by EVC with ACES were determined. It shows that the ACES has a slight influence on the machined surface roughness and surface topography. The diamond tool life can be significantly prolonged in EVC of pure iron with ACES than that with a fixed cutting edge, so that high profile accuracy and surface quality could be obtained even at higher nominal cutting speed. A typical thin-walled curved surface pure iron part with diameter ∅240 mm, height 122 mm, and wall thickness 2 mm was fabricated by the presented method, and its profile error and surface roughness achieved PV 2.2 μm and Ra less than 50 nm, respectively. 相似文献
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《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