Research on the dentiform basic parameters of aero-engine turbine joint structure
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Research on the dentiform basic parameters of aero-engine turbine joint structure
Vol. 26, Issue 4, (2011)
作者机构:
1. 北京航空航天大学 能源与动力工程学院,北京,100191
2. 中国航空工业集团公司 沈阳发动机设计研究所,沈阳,110015
作者简介:
基金信息:
DOI:
CLC:
Published:2011
稿件说明:
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SHEN Xiu-li, QI Xiao-dong, WANG Rong-qiao, et al. Research on the dentiform basic parameters of aero-engine turbine joint structure[J]. 2011, 26(4).
DOI:
SHEN Xiu-li, QI Xiao-dong, WANG Rong-qiao, et al. Research on the dentiform basic parameters of aero-engine turbine joint structure[J]. 2011, 26(4).DOI:
Research on the dentiform basic parameters of aero-engine turbine joint structure
The impacts on joint structure strength of the dentiform basic parameters
such as wedge angle
blade root neck width
disc groove height
top flank angle
bottom flank angle and skew angle
were studied by lots of finite element and optimization design numerical methods.Based on the calculated results
a new model was established and verified experimentally
indicating that the maximum stress has been reduced.Results show that two-dimensional finite element analysis can be used to study the influence of dentiform basic parameters on the joint structure stress distribution
but this does not reflect changes of the stress in the axial direction.