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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Fatigue and Strength Studies of Titanium 6Al-4V Fabricated by Direct Metal Laser Sintering
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Fatigue and Strength Studies of Titanium 6Al-4V Fabricated by Direct Metal Laser Sintering

机译:直接金属激光烧结钛6Al-4V的疲劳强度研究

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摘要

Vibratory bending fatigue behavior of titanium 6Al-4V plate specimens manufactured via direct metal laser sintering (DMLS), powder bed fusion additive manufacturing (AM), is assessed. Motivation for the work is based on unprecedented performance demands for sixth-generation gas turbine engine technology that requires complex, lightweight components. Due to cost, schedule, and feasibility limitations associated with conventional manufacturing, AM aims to address ubiquitous component concepts. Though AM has promise in the engine community, process controls necessary for consistent material properties remain an enigma. The following manuscript compares variability of DMLS fatigue and strength to cold-rolled data. Results show discrepancies between DMLS and cold-rolled for fatigue and microstructure characteristics.
机译:评估了通过直接金属激光烧结(DMLS),粉末床熔合增材制造(AM)制造的6Al-4V钛板试样的振动弯曲疲劳行为。开展这项工作的动力是基于对第六代燃气涡轮发动机技术的空前性能要求,该技术需要复杂,轻便的部件。由于与常规制造相关的成本,进度和可行性限制,AM的目标是解决普遍存在的组件概念。尽管AM在发动机领域有前途,但保持一致的材料特性所必需的过程控制仍然是一个谜。以下手稿将DMLS疲劳和强度的变化与冷轧数据进行了比较。结果表明,DMLS和冷轧之间的疲劳和显微组织特征存在差异。

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  • 来源
    《Journal of Engineering for Gas Turbines and Power 》 |2016年第2期| 022101.1-022101.7| 共7页
  • 作者单位

    Air Force Research Laboratory, Aerospace Systems Directorate, Wright-Patterson AFB, OH 45433;

    Air Force Research Laboratory, Aerospace Systems Directorate, Wright-Patterson AFB, OH 45433;

    Air Force Research Laboratory, Aerospace Systems Directorate, Wright-Patterson AFB, OH 45433;

    Air Force Research Laboratory, Aerospace Systems Directorate, Wright-Patterson AFB, OH 45433;

    Perceptive Engineering Analytics, Lino Lakes, MN 55014;

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