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封严环蜂窝结构哈氏合金材料等效杨氏模量

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为研究适用于封严环组件动力学特性分析的蜂窝结构哈氏合金材料等效杨氏模量,搭建了封严环组件模态试验装置,建立了封严环组件有限元模型.基于模态分析与二分逼近理论,以模态试验获得的固有频率为标准值,对哈氏合金材料杨氏模量采用二分法不断进行数值模态分析,以逼近固有频率标准值,获得蜂窝结构哈氏合金材料等效杨氏模量.结果表明:蜂窝结构哈氏合金材料等效杨氏模量为0.304 GPa时,数值模态分析固有频率与试验结果最大相对误差小于1.3%,可应用于封严环组件动力学特性分析.使用具有不同结构参数的封严环组件对等效杨氏模量为0.304 GPa进行了验证,最大相对误差小于3%,表明蜂窝结构哈氏合金材料等效杨氏模量取为0.304 GPa对于封严环组件动力学特性分析具有较高的准确性和普适性.
Equivalent Young's Modulus of Hastelloy Material with Honeycomb Structure for Seal Ring
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.

Hastelloy material with honeycomb structureequivalent Young's modulusseal ring assemblymodal analysisbisection methodaeroengine

苏国征、孙丹、郁丽、唐超、李玉、金俊臣

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沈阳航空航天大学 航空发动机学院:沈阳 110136

沈阳航空航天大学 辽宁省航空推进系统先进测试技术重点实验室:沈阳 110136

中国航发沈阳发动机研究所:沈阳 110015

中国航发沈阳发动机研究所 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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蜂窝结构哈氏合金材料 等效杨氏模量 封严环组件 模态分析 二分法 航空发动机

2024

航空发动机
中国工业沈阳发动机设计研究所

航空发动机

CSTPCD北大核心
影响因子:0.586
ISSN:1672-3147
年,卷(期):2024.50(6)