王晓放

个人信息Personal Information

教授

博士生导师

硕士生导师

任职 : 现任中国工程热物理学会流体机械专委员会委员、中国航空学会学轻型燃气轮机分会委员、教育部重型燃气轮机教学资源库专家委员会委员、辽宁省能动类专业教指委副主任、大连市核事故应急指挥部专家组成员等职。

性别:女

毕业院校:大连理工大学

学位:硕士

所在单位:能源与动力学院

电子邮箱:dlwxf@dlut.edu.cn

扫描关注

论文成果

当前位置: 中文主页 >> 科学研究 >> 论文成果

变厚度叶片对离心压缩机结构强度和性能影响

点击次数:

发表时间:2022-10-10

发表刊物:大连理工大学学报

所属单位:能源与动力学院

卷号:52

期号:1

页面范围:29-34

ISSN号:1000-8608

摘要:A systematic investigation to understand the impacts of the
   variable-thickness blade on the structural strength and performance of
   the first stage impeller for a domestic large flow centrifugal
   compressor is undertaken.The geometric models of 9 shrouded impellers
   with variable-thickness blade are mainly established by CAD software
   Solidworks,static structural analyses are carried out using finite
   element software ANSYS,and CFD simulations are performed with the CFX
   code.Emphases are placed on the variation of maximal von Mises stress in
   FEM analyses,and the distinction of impeller internal flow behavior in
   CFD simulations.The variable thickness of blade is found to exert the
   great influence on the structural strength and performance of a
   centrifugal compressor.Furthermore,the computational results indicate
   that the appropriate increase of blade thickness close to trailing edge
   can remarkably improve the strength and aerodynamic characteristics of a
   shrouded impeller.Finally,the theoretical bases are given for the
   structural optimization and the performance improvement of a large flow
   centrifugal compressor and a nuclear reactor coolant cycling pump
   impellers.

备注:新增回溯数据