苏国征1,2 ,孙丹1,2 ,郁丽3,4 ,唐超3,4 ,李玉1,2 ,金俊臣 1,2.封严环蜂窝结构哈氏合金材料等效杨氏模量[J].航空发动机,2024,50(6):107-112
Equivalent Young's Modulus of Hastelloy Material with Honeycomb Structure for Seal Ring
DOI:
Key Words:Hastelloy material with honeycomb structure  equivalent Young's modulus  seal ring assembly  modal analysis  bisection method  aeroengine
作者单位
苏国征1,2 ,孙丹1,2 ,郁丽3,4 ,唐超3,4 ,李玉1,2 ,金俊臣 1,2 1.沈阳航空航天大学 航空发动机学院 2.辽宁省航空推进系统先进测试技术重点实验室:沈阳 110136 3.中国航发沈阳发动机研究所 4.航空发动机动力传输航空科技重点实验室:沈阳 110015 
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Abstract:In order to study the equivalent Young's modulus of Hastelloy material with honeycomb structure suitable for the dynamic analysis of the seal ring assembly, a modal testing device for the seal ring assembly was built and the finite element model of the seal ring assembly was established. Based on modal analysis and bisection approximation theory, taking the natural frequency derived from the modal testing as the reference value, numerical modal analyses of Young's modulus of Hastelloy material were consecutively carried out using the bisection method to approximate the reference natural frequency, and obtain equivalent Young's modulus of the Hastelloy mate? rial with honeycomb structure. The results show that when the equivalent Young's modulus of Hastelloy material with honeycomb structure is 0.304GPa, the maximum relative error between the natural frequencies from numerical modal analyses and test results is less than 1.3%, which can be used to analyze the dynamic characteristics of the seal ring assembly. The equivalent Young's modulus with 0.304GPa is veri? fied by seal ring assemblies with different structural parameters, and the maximum relative error is less than 3%, indicating that the equivalent Young's modulus of 0.304GPa for Hastelloy material with honeycomb structures has high accuracy and universality in analyzing the dynamic characteristics of seal ring assemblies.
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