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运用ANSYS软件对某航空涡轮发动机压气机盘进行了模态分析,得到了压气机盘的前10阶固有频率和振型,确定了压气机盘的振动特性,为压气机盘的结构优化和动力修改提供了参考依据。
The ANSYS software was used to analyze the modal analysis of an aero-turbo engine compressor disk. The first ten natural frequencies and vibration modes of the compressor disk were obtained. The vibration characteristics of the compressor disk were determined, which were the structural optimization and power of the compressor disk Modify provides a reference.