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METHOD OF VIBRATION TESTS OF TURBOMASHINE LARGE-SIZE PARTS

机译:汽轮机大尺寸零件振动测试方法

摘要

FIELD: machine engineering.;SUBSTANCE: method includes preparing a part and setting it on a vibration table, adjusting the vibration excitation frequency of the vibration table before it coincides with the natural vibration frequency of the part, and impact on the part by vibrating at a resonant frequency. At the same time, to determine the fatigue endurance limit of the monowheel blades of a turbomachine compressor, in the preparation of a monowheel and mounting on the vibration table, the frequency of the natural vibrations of at least one of its blades and the exciting vibration frequency of the vibration table are adjusted until they coincide. Impact on the blade by vibration with a resonant frequency is performed under a load providing variables in the blade without destruction, close to the limiting ones, dynamic stresses during N-loading cycles corresponding to the material of the monowheel production. The coincidence of the natural vibration frequency of at least one of its blades and the excitation frequency of the vibration table is additionally provided by dampening the blades and / or loading with loads.;EFFECT: reduced number of blades to be destroyed and maintained operability of most of the structure.;2 cl, 5 dwg
机译:领域:机械工程。;实体:方法包括准备零件并将其放置在振动台上,在与零件的固有振动频率重合之前调节振动台的振动激发频率,并通过在以下位置振动来对零件产生冲击共振频率。同时,为了确定涡轮机压缩机的单轮叶片的疲劳寿命极限,在准备单轮并将其安装在振动台上时,至少要考虑其中一个叶片的固有振动频率和激励振动调整振动台的频率,直到它们一致为止。在载荷下,叶片会产生共振频率的振动,从而对叶片产生冲击,而叶片中的变量不会破坏(接近极限值)在N加载循环期间对应于单轮生产材料的动应力。至少一个叶片的固有振动频率与振动台的激发频率的重合是通过对叶片进行阻尼和/或施加载荷来实现的;效果:减少了要破坏的叶片数量并保持了其可操作性大部分结构。; 2 cl,5 dwg

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