阻尼结构对长扭叶片应力及振动频率的影响分析
Study on the Influence of Damping Structure on Stress and Eigenfrequency of Long Twisted Blade
郑飞逸 1张军辉 1林兵 1陈华梅 1徐阳 1何炜楠 1牛春燕1
作者信息
- 1. 杭州汽轮动力集团股份有限公司,杭州 310022
- 折叠
摘要
针对不同阻尼结构对长扭叶片应力及振动频率影响的问题,对仅具有围带阻尼的模型1和具有围带、中间阻尼的模型2展开分析.首先,利用ANSYS软件进行叶片结构分析,得到不同转速下叶片的应力和阻尼结构接触面的正压力;然后通过Greenwood-Williamson接触模型将正压力转化为接触刚度,使用Matrix27单元模拟接触刚度,进行叶片模态分析.研究表明,叶片最大应力出现在叶型顶截面与围带交接处,模型1与模型2的最大应力比为1.34∶1;模型1接触面的接触刚度比模型2小,其同阶次同节径振动频率比模型2低;通过坎贝尔图分析发现,模型1有3个共振转速,其中2阶7节径共振转速的避开率不满足要求;模型2有2个共振转速,避开率均满足要求.研究表明,与模型1相比,模型2的应力与振动频率更能满足设计要求.
Abstract
In order to study the influence of different damping structure on stress and eigenfrequency of long twisted blade,two models of long twisted blade,Model 1 with shroud only and Model 2 with shroud and snubber,were presented and analyzed in this paper.Firstly,the static stress analysis ofblade was conducted by ANSYS,stress of blade was obtained,and normal contact force of neighboring shroud and snubber contact surface of adjacent blade under different rotational speeds were also obtained.Then,the Greenwood Williamson contact model was used to convert normal contact force into contact stiffness.Contact stiffness was simulated by Matrix27 element in the finite analysis model,and blade's modal analysis was conducted by ANSYS.The results show that maximum stress onblade occurs at the intersection of the blade top section and the shroud,the ratio of maximum stress between Model 1 and Model 2 is 1.34∶1.Contact stiffness of Model 1's contact surface is smaller than that of Model 2's.Under the same order and same nodal diameter,model 1's eigenfrequency is lower than that of Model 2's.According to Campbell diagram,Model 1 has three resonance speeds,and the avoidance rate of resonance speed of the 2nd order nodal diameter 7 does not meet the requirements.Model 2 has two resonance speeds,and both avoidance rates meet the requirements.The results indicate that Model 2's stress and eigenfrequency meet the design requirements better than Model 1's.
关键词
长扭叶片/阻尼结构/接触刚度/应力分析/振动频率Key words
long twisted blade/damping structure/contact stiffness/stress analysis/eigenfrequency引用本文复制引用
基金项目
2021年杭州市高层次人才特殊支持计划项目()
杭州汽轮动力集团股份有限公司资助项目(C新23-01)
杭州汽轮动力集团股份有限公司资助项目(C研23-02)
出版年
2024
NETL
NSTL
万方数据