共查询到18条相似文献,搜索用时 78 毫秒
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碳纤维增强复合材料(CFRP)以其优越的性能被广泛应用于航空航天领域,然而其作为典型难加工材料,采用传统钻削加工时极易出现毛刺、撕裂、分层及加工表面质量差等现象,严重制约了CFRP的应用。采用纵扭复合超声振动钻削和普通钻削两种钻削方式加工CFRP板材,对比了两种钻削方式下的轴向力、扭矩及钻孔质量,研究了单向型和编织型CFRP板材的钻削轴向力特性,分析了转速、进给速度对钻削轴向力的影响规律。试验表明:纵扭复合超声振动辅助钻削可以更加有效切削CFRP,降低轴向力和扭矩,降低撕裂因子,抑制分层现象;钻削轴向力随着进给速度提高而增大,随着钻速的提高而降低,且当Vc/Vf增大时,钻削轴向力随之下降,试验拟合得到轴向力经验公式。 相似文献
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为避免或减少钻削出口分层缺陷,控制钻削轴向力不超过出口分层临界轴向力具有重要的实际意义.将钻头横刃上的轴向力分为两部分,其一是横刃前刀面与碳纤维增强复合材料(Carbon fiber reinforced polymers,CFRP)之间作用力的轴向分量,其二是横刃圆弧与CFRP接触力的轴向分量.基于复合材料的细观力学... 相似文献
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碳纤维复合材料(CFRP)钻孔出口缺陷的研究 总被引:10,自引:3,他引:7
对碳纤维复合材料(CFRP)钻孔出口的缺陷进行了试验研究,对其典型形式进行了模型总结,指出孔出口缺陷由撕裂和毛边两部分组成,其中撕裂比毛边的尺寸大。撕裂的形成过程包括两个作用阶段即横刃作用阶段和主切削刃作用阶段,其中横刃作用在撕裂形成中占主导成份。毛边缺陷通常出现在表层纤维被“顺向”切削的孔边缘部分。另外,以孔出口两侧撕裂长度平均值作为撕裂评价参数,在总结钻削试验结果的基础上探讨了钻削参数变化对撕裂大小的影响。指出随着进给速度、进给量、钻头直径和轴向力等因素的增大,撕裂缺陷将变得严重;钻头转速的增大将使撕裂值变小;将切削速度与进给速度比值控制在3000-4000以下,可以有效地减小撕裂值。 相似文献
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针对Kevlar复合材料纤维韧性足和剪切强度大的特点,分析切削过程的抗力来源,将钻削过程简化为同时切削多根Kevlar纤维并发生剪切破坏的力学模型,在瞬时切削速度方向和纤维方向所形成的平面上进行二维正交切削分析,建立最大轴向力预测模型;根据复合材料的分层缺陷机理,计算分层临界轴向力;设计单因素加工参数试验,并使用水浸超声检测设备检测分层缺陷。试验结果表明:预测最大轴向力大于分层临界轴向力时,发生分层缺陷的比例达到78%;预测最大轴向力小于分层临界轴向力时,均没有发生分层缺陷。 相似文献
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Composite laminates are used in many applications in ae-rospace/defense industries due to their high strength-to-weight ratio and corrosion resistance properties. In general, composite materials are hard-to-machine materials which exhibit low drilling efficiency and drilling-induced delamination damage at exit. Hence, it is important to understand the drilling processes for composite materials. This article presents a comprehensive study involving experimental characterization of drilling process to understand the cutting mechanism and relative effect of cutting parameters on delamination during drilling of carbon fiber reinforced plastic (CFRP). Thrust force and torque data are acquired for analyzing the cutting mechanism, initiation and propagation of delamination, and identification of critical thrust force below which no damage occurs. An FE model for prediction of critical thrust force has been developed and validated with experimental results. A [0/90] composite laminate is modeled simulating the last two plies in exit condition and a thin interface layer is inserted in between the plies to capture delamination extent. The tool geometry is modeled as “rigid body” with geometric features of twist drill used in experiments. The tool is indented on the workpiece to simulated tool feeding action into the workpiece. The FE model predicts the critical thrust force within 5% of the experimentally determined mean value. 相似文献
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In aeronautical industry, stringent requirements relate to the quality of drilled holes in carbon fiber reinforced plastic (CFRP) composite laminates as low hole quality determines poor assembly tolerance, structural properties reduction, and risk for long-term part performance. Non-destructive quality control techniques were applied to drilled CFRP laminate stacks for aeronautical applications to characterize the material damage induced by drilling in order to assess the hole quality for product acceptability. Experimental metrology procedures, including optical measurements and ultrasonic non-destructive evaluation, were employed to appraise both external and internal induced material damage in holes machined under diverse drilling conditions. The optical inspection procedure, comparable to the visual inspection method regularly utilized in industry, provided delaminated area evaluations that are underestimated in the case of severe drilling conditions by up to 7% for hole exit and up to 5% for hole entry. In the case of less severe drilling conditions, the underestimation was limited to <2.5% for both hole exit and hole entry, which can be considered a practically negligible disparity. 相似文献
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基于CFRP切削过程仿真的面下损伤形成分析 总被引:7,自引:1,他引:7
由于碳纤维增强树脂基复合材料(Carbon fiber reinforced plastic,CFRP)宏观上呈现非均质、各向异性,细观上表现为纤维和树脂的特殊混合形态,导致其制件加工过程中极易产生分层、开裂等损伤,严重影响其制件的加工精度及承载性能。研究CFPR加工损伤产生机理并以此降低加工损伤是提高其加工质量的关键。基于宏观各向异性本构、Hashin失效起始准则及损伤演化,建立了可实现任意纤维角度单向板连续动态切削过程仿真分析的直角切削有限元模型,分析了任意纤维角度CFRP单向板连续切削过程面下损伤,得到了纤维角度、切削参数、刀具结构对面下损伤深度的影响规律。具体结果:纤维角度为影响面下损伤的主要因素,随纤维角度增大,切削力增大同时面下损伤深度也明显增加;面下损伤的主要原因为切削力过大导致的基体破坏及扩展;对于135°单向板面下损伤深度随刀具前角增大呈先增大后减小的趋势。 相似文献
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采用超高压磨料水射流技术对碳纤维复合材料进行切割试验,借助μscan激光共聚焦显微镜重构样品切口的三维表面,测得样品切口表面粗糙度;研究了扫描分辨率对表面粗糙度测量的影响,以及切割速度、样品厚度对样品切口表面粗糙度的影响规律。试验结果表明:扫描分辨率对表面粗糙度的测量无明显的影响;当切割深度较小(0~0.6 mm)时,即在切口入口处,表面粗糙度随切割深度的增大而减小,当切割深度较大(大于0.6 mm)时,表面粗糙度随切割深度的增大而增大;当样品厚度一定时,随着切割速度的增大,切口最大表面粗糙度在整体趋势上是增大的,而样品厚度的大小对表面粗糙度的影响并无明显的规律。 相似文献
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