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Topology Optimization Method Research on Hollow Wide-Chord Fan Blade of a High-bypass Turbofan Engine

机译:高旁通涡轮机发动机空洞宽弦风扇叶片的拓扑优化方法研究

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In order to realize lightweight design of a high-hypass turbofan engine, topology optimization of vacuum structure on a wide-chord fan blade was carried out regarding mixed loading conditions as static strength, vibration and bird-strike. Without changing the leaf shape, relationship of performance indices on vacuum structure was analyzed with simplified mechanical model of loading conditions. Topology optimization designs were carried out according to the highly sensitive conditions. Vacuum structure layout of fan blade was constructed integrating the major load transfer paths in each design proposal. Performance indices of different fan blade structures were compared. Result shown that optimized fan blade can realize lightweight as well as meeting the strength design requirement.
机译:为了实现高次丘比特发动机的轻量级设计,在宽弦扇叶片上的真空结构的拓扑优化是关于混合负载条件作为静态强度,振动和鸟击。 在不改变叶形形状的情况下,分析了在真空结构上的性能指标的关系,通过简化的装载条件进行了简化的机械模型。 拓扑优化设计根据高度敏感的条件进行。 风扇刀片的真空结构布局是在每个设计方案中的主要负载传输路径的构建。 比较了不同风扇叶片结构的性能指标。 结果表明,优化的风扇刀片可以实现轻量级,也可以满足强度设计要求。

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