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ASSESSMENT OF FATIGUE RELIABILITY OF POWER TRANSMISSION GEARING FOR AEROSPACE PROPULSION APPLICATIONS

机译:航空推进应用动力传动齿轮的疲劳可靠性评估。

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The fatigue strength in presence of inclusions is one of the main topics for the fatigue of high strength steels, especially the case hardened ones adopted for power transmission. In this paper we analyze the fatigue strength of carburized gears in presence of inclusions in order to develop the reliability assessment of a power transmission for aerospace propulsion. The high cycle fatigue properties of a high strength carburizing steel have been experimentally determined by conducting bending fatigue tests with specimens with artificial defects and a coherent model for the assessment of fatigue crack growth thresholds by taking into account of the residual stresses due to carburizing has been developed. In parallel, the distribution of non-metallic inclusions has been estimated by carrying out high cycle fatigue tests onto cylindrical smooth specimens and by inspection of mirror polished sections of the material. Eventually, by employing a simplified finite element model of a highly loaded gear wheel, the bending fatigue strength of gear teeth and the reliability of a turbo-propeller power transmission was determined by incorpo- rating the fatigue crack growth thresholds, the measured residual stress profiles and the statistics of extreme non-metallic inclusions into a competing risks model applied to FE discretization.
机译:存在夹杂物时的疲劳强度是高强度钢疲劳的主要主题之一,特别是用于动力传递的表面硬化钢。在本文中,我们分析了存在夹杂物时渗碳齿轮的疲劳强度,以发展用于航空航天推进的动力传动装置的可靠性评估。高强度渗碳钢的高周疲劳性能已通过对具有人工缺陷的试样进行弯曲疲劳试验,并通过考虑渗碳引起的残余应力来评估疲劳裂纹扩展阈值的连贯模型而得到了确定。发达。同时,通过对圆柱状光滑试样进行高周疲劳试验并检查材料的镜面抛光截面,可以估算出非金属夹杂物的分布。最终,通过采用高负荷齿轮的简化有限元模型,通过结合疲劳裂纹扩展阈值,测得的残余应力曲线来确定轮齿的弯曲疲劳强度和涡轮螺旋桨动力传递的可靠性。并将极端非金属夹杂物的统计数据应用到有限元离散化的竞争风险模型中。

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