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Influence of Assembly Parameters on Tensile Behavior of Hybrid CMC and Superalloy Bolted Joints by Progressive Damage Analysis

Chao Lv Feng Li Shuyuan Zhao Qian Sun Mingrui Li Xinyang Sun

哈尔滨工业大学学报（英文版）2021，Vol.28Issue(3)：53-60,8.

哈尔滨工业大学学报（英文版）2021，Vol.28Issue(3)：53-60,8.DOI:10.11916/j.issn.1005-9113.2021097

Influence of Assembly Parameters on Tensile Behavior of Hybrid CMC and Superalloy Bolted Joints by Progressive Damage Analysis

Chao Lv ¹Feng Li ¹Shuyuan Zhao ²Qian Sun ³Mingrui Li ²Xinyang Sun⁴

作者信息

1. China Academy of Aerospace Aerodynamics,Beijing 100074,China
2. National Key Laboratory of Science and Technology on Advanced Composites in Special Environments,Harbin Institute of Technology,Harbin 150080,China
3. Shenyang Aircraft Design and Research Institute,Aviation Industry Corporation of China,Shenyang 110000,China
4. School of Aeronautics and Astronautics,Harbin Institute of Technology,Harbin 150001,China
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摘要

关键词

ceramic matrix composite/progressive damage analysis/tensile performance/bolt preload/bolt-hole clearance

Key words

ceramic matrix composite/progressive damage analysis/tensile performance/bolt preload/bolt-hole clearance

分类

航空航天

引用本文复制引用

Chao Lv,Feng Li,Shuyuan Zhao,Qian Sun,Mingrui Li,Xinyang Sun..Influence of Assembly Parameters on Tensile Behavior of Hybrid CMC and Superalloy Bolted Joints by Progressive Damage Analysis[J].哈尔滨工业大学学报（英文版）,2021,28(3):53-60,8.

基金项目

Sponsored by the Pre-Research Foundation of Shenyang Aircraft Design and Research Institute,the Aviation Industry Corporation of China(Grant No.JH20128255),the National Defence Basic Research Program(Grant No.JZ20180032),and the Pre-Research Foundation of Equipment Development Department of People's Republic of China Central Military Commission(Grant No.ZJJSN20200001). （Grant No.JH20128255）

哈尔滨工业大学学报（英文版）

ISSN：1005-9113

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