航空发动机用蜂窝材料应变率相关本构模型及应用研究

孟卫华; 王建军; 米栋; 汪文君; 郭伟国

doi:10.21656/1000-0887.390087

航空发动机用蜂窝材料应变率相关本构模型及应用研究

doi: 10.21656/1000-0887.390087

¹中国航发湖南动力机械研究所, 湖南株洲 412002;²西北工业大学航天学院, 西安 710072;³西北工业大学航空学院, 西安 710072

详细信息

作者简介:
孟卫华（1987—），男，工程师，硕士(E-mail: mengweihua1234＠163.com);王建军（1987—），男，副研究员，博士(通讯作者. E-mail: jianjunw87＠126.com）.

中图分类号: V259
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出版历程
- 收稿日期: 2017-12-18
- 修回日期: 2018-05-12
- 刊出日期: 2018-06-15

Application of Strain-Rate-Dependent Material Models to Aero-Engine Honeycomb Casing Analysis

¹AECC Hunan Aviation Powerplant Research Institute, Zhuzhou, Hunan 412002, P.R.China;²School of Astronautics, Northwestern Polytechnical University, Xi’an 710072, P.R.China;³School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, P.R.China

摘要

摘要: 针对典型航空发动机涡轮机匣防叶片刮磨的蜂窝材料，阐述了常用的蜂窝等效模型和J-C(Johnson-Cook)模型，将两种材料模型应用于蜂窝冲击试验的仿真分析，并与试验结果进行了对比.结果表明，通过合理的参数标定及简化假设，J-C模型可提供满意的仿真结果，其中蜂窝损伤预测与试验结果很好地吻合.鉴于其使用相对简单，同时能够提供足够的预测精度，在航空发动机叶片与蜂窝的刮磨仿真分析工程应用中值得推荐.
- 航空发动机 /
- 蜂窝材料 /
- 应变率相关 /
- J-C模型
Abstract: For typical honeycomb materials used in turbine casings of aero-engines to prevent blades from scraping the casing, 2 commonly used material models, the Johnson-Cook model and the honeycomb equivalent model, and the relevant calibration methods were discussed. Then the 2 models were implemented in the simulation of a honeycomb impact test, and the simulation results were compared with the test results. It is shown that, through appropriate parameter calibrations and reasonable simplifications, the Johnson-Cook model provides satisfying results, in which the damage prediction is in good agreement with the test observation. Since the Johnson-Cook model is relatively easier to be implemented with enough prediction accuracy, it is recommended for blade-honeycomb scraping analysis of aero-engines.
- aero-engine /
- honeycomb material /
- strain rate dependency /
- Johnson-Cook model

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参考文献(9)

[1]	刘艳辉, 杜鹏. 金属蜂窝夹层板的研究进展[J]. 机械制造与自动化, 2013,41(1): 9-15.(LIU Yanhui, DU Peng. Research process of metal honeycomb sandwich boards[J]. Machine Building & Automation,2013,41(1): 9-15.(in Chinese))
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航空发动机用蜂窝材料应变率相关本构模型及应用研究

doi: 10.21656/1000-0887.390087

作者简介:
孟卫华（1987—），男，工程师，硕士(E-mail: mengweihua1234＠163.com);王建军（1987—），男，副研究员，博士(通讯作者. E-mail: jianjunw87＠126.com）.

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Application of Strain-Rate-Dependent Material Models to Aero-Engine Honeycomb Casing Analysis

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航空发动机用蜂窝材料应变率相关本构模型及应用研究

doi: 10.21656/1000-0887.390087

作者简介: 孟卫华（1987—），男，工程师，硕士(E-mail: mengweihua1234＠163.com);王建军（1987—），男，副研究员，博士(通讯作者. E-mail: jianjunw87＠126.com）.

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出版历程

Application of Strain-Rate-Dependent Material Models to Aero-Engine Honeycomb Casing Analysis

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出版历程

目录

作者简介:
孟卫华（1987—），男，工程师，硕士(E-mail: mengweihua1234＠163.com);王建军（1987—），男，副研究员，博士(通讯作者. E-mail: jianjunw87＠126.com）.