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Finite-element modeling of the failure of interference-fit planet carrier and shaft assembly

机译:过盈配合行星架和轴组件失效的有限元建模

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摘要

A planet carrier and shafts assembly with interference-fit was modeled based on 3-D finite element method by applying thermal loads to the shafts with orthotropic coefficients of thermal expansion. A 3-D finite element contact model verified that the contact pressure is identical compared with the calculated pressure by Lame's equations for the thick-wall cylinder interference-fit. A displacement history analysis by the 3-D finite element multi-contact simulation under alternate loads reveals the root cause for the interference-fit shafts coming out of the planet carrier after 65 h of planetary gear reducer working test.
机译:基于3-D有限元方法,通过向正交各向异性的热膨胀系数的轴施加热载荷,对具有过盈配合的行星齿轮架和轴组件进行建模。一个3-D有限元接触模型验证了与厚壁圆筒过盈配合的Lame方程所计算的压力相比,接触压力是相同的。通过在交替载荷下的3-D有限元多触点模拟进行的位移历史分析,揭示了在行星齿轮减速器工作65小时后,过盈配合轴从行星架中脱出的根本原因。

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