航空发动机轮盘优化设计的策略与纲要(轮盘优化设计系统TDSOS简介)
STRATEGIES FOR OPTIMAL DESIGN OF GAS TURBINE DISKS
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摘要: 轮盘结构形状复杂,完全按照实际结构进行结构分析也非常困难。为此,将榫头沿根部从轮盘中分离出来,作为三维问题处理;剩下的盘体简化为轴对称问题。由于简化了盘体,忽略了局部的应力集中,为此,适当降低被简化部位的屈服应力以做补偿。这样处理是否合适,需要从得到的优化设计中取出被简化的部分进行三维弹塑性计算来校核。如不满足给定条件,调整后重新进行优化直至满足要求。Abstract: A number of strategies for optimal design of the gas turbine disks are proposed,which include separation of tenons design from disk design,rational simplification of structural model,check on local constraints,optimal design based on elastic analysis and further check based on elastoplastic analysis,multi level optimization by grouping design variables.According to the strategies a computer program TDSOS is developed for practical use.By applying the strategies and the program TDSOS,shape optimization of gas turbine disk with light mass and low stress level can be obtained and the contradiction among high performance index,reliability and long life expectation is better solved.
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