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PARAMETER ACQUISITION METHOD FOR CAST-PIECE SOLIDIFICATION SIMULATION AND CAST-IN-PLACE SYSTEM GRIDDING DESIGN METHOD

机译:铸造件凝固仿真的参数采集方法和铸造系统网格设计方法

摘要

The present invention provides a parameter acquisition method for cast-piece solidification simulation and a cast-in-place system gridding design method, comprising: calculating thermodynamic parameters of a superalloy; obtaining a cooling curve of the superalloy under different thickness conditions; measuring the change of the linear expansion coefficient of the superalloy with temperature. The design method comprises: simulating the solidification process of tubular features of different thicknesses, determining the compensation distance of features of different thicknesses; establishing a gridded casting system, dividing the cast piece into a plurality of modules according to thickness, dividing the inside of each module into units of a grid, and ensuring that the cell size is less than the compensation thickness of the feeding distance; performing filling and solidification simulation of the cast piece and the gridded cast-in-place system, and analyzing the defect simulation results. The present invention provides support for the development and manufacturing of large and complex thin-walled high-temperature alloy cast pieces for aeronautics and astronautics, and provides solutions for the development of diversified and complex thin-walled cast-in-place system design.
机译:本发明提供了一种用于铸造件凝固模拟的参数采集方法和浇注系统网格设计方法,包括:计算超合金的热力学参数;在不同厚度条件下获得超合金的冷却曲线;测量高温合金与温度的线性膨胀系数的变化。设计方法包括:模拟不同厚度的管状特征的凝固过程,确定不同厚度的特征的补偿距离;建立一个网格铸造系统,根据厚度将铸件分成多个模块,将每个模块的内部分成网格单元,确保电池尺寸小于供料距离的补偿厚度;执行铸造件和网格铸造系统的填充和凝固模拟,并分析缺陷仿真结果。本发明提供了对航空和航天器的大型和复杂薄壁高温合金铸件的开发和制造,并为多元化和复杂的薄壁制热系统设计提供了解决方案。

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