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The unbiased propagation mechanism in laser cutting silicon wafer with laser induced thermal-crack propagation

机译:激光切割硅晶片中的非偏见传播机制,激光诱导热裂纹传播

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摘要

In the silicon dicing processes, the laser induced thermal-crack propagation (LITP) has been reported about its superiority over traditional dicing methods in aspect of crack surface quality and mechanical properties. However, this process may cause deviation of its propagation path especially under the condition of asymmetric linear cutting. Aiming to solve the path-deviation problem, a method of pre-crack on the surface of the silicon wafer has been proposed. A mathematical model which consists absorption of laser, heat transfer, generation of thermal stress, and crack initiation and propagation, has been established. Numerical simulation in the LITP of silicon wafer with respect to two pre-crack modes: pre-crack on the end and pre-crack on the surface were conducted to study the high-quality crack propagation mechanism. Unbiased crack propagation was found in the simulation of pre-crack on the surface process and the mechanism of it was revealed through the analysis of the tensile stress distribution. It was found that the three-dimensional shape of the tensile stress at the front of the crack tip would result in an uncertain propagation in conventional LITP of pre-crack on the end. Conversely, the slice shape of the tensile stress would induce a certain propagation direction that was along the plane of the pre-crack in the simulation of pre-crack on the surface. The experimental results verified the unbiased propagation mode and showed good crack surface quality.
机译:在硅切割工艺中,在裂纹表面质量和机械性能方面,据报道了激光诱导的热裂纹传播(LITP)对传统切割方法的优势。然而,该过程可能导致其传播路径的偏差,特别是在不对称线性切割的条件下。旨在解决路径偏差问题,提出了一种在硅晶片表面上的预裂缝的方法。已经建立了由激光,传热,热应力产生和裂纹启动和繁殖的吸收的数学模型。相对于两个预裂纹模式的硅晶片LITP中的数值模拟:表面上的预裂纹和表面上的预裂纹,以研究高质量的裂纹传播机制。在表面过程的预裂纹模拟中发现了不偏不倚的裂纹繁殖,并通过分析拉伸应力分布来揭示其机制。发现,裂纹尖端前部的拉伸应力的三维形状将导致在末端的常规预裂纹中的传统LITP中的不确定传播。相反,拉伸应力的切片形状将诱导沿着预裂纹平面的一定的传播方向,在模拟表面上的预裂纹上。实验结果验证了无偏的传播模式,并显示出良好的裂纹表面质量。

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  • 来源
    《Applied Physics 》 |2019年第7期| 479.1-479.11| 共11页
  • 作者单位

    Harbin Inst Technol Sch Mechatron Engn Dept Aeronaut & Astronaut Mfg Engn Mfg Bldg 525 92 West Dazhi St POB 422 Harbin 150001 Heilongjiang Peoples R China;

    Harbin Inst Technol Sch Mechatron Engn Dept Aeronaut & Astronaut Mfg Engn Mfg Bldg 525 92 West Dazhi St POB 422 Harbin 150001 Heilongjiang Peoples R China;

    Harbin Inst Technol Sch Mechatron Engn Dept Aeronaut & Astronaut Mfg Engn Mfg Bldg 525 92 West Dazhi St POB 422 Harbin 150001 Heilongjiang Peoples R China;

    Harbin Inst Technol Sch Mechatron Engn Dept Aeronaut & Astronaut Mfg Engn Mfg Bldg 525 92 West Dazhi St POB 422 Harbin 150001 Heilongjiang Peoples R China;

    Harbin Inst Technol Sch Mechatron Engn Dept Aeronaut & Astronaut Mfg Engn Mfg Bldg 525 92 West Dazhi St POB 422 Harbin 150001 Heilongjiang Peoples R China;

    Harbin Inst Technol Sch Mechatron Engn Dept Aeronaut & Astronaut Mfg Engn Mfg Bldg 525 92 West Dazhi St POB 422 Harbin 150001 Heilongjiang Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
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  • 正文语种 eng
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