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Bolt Design of Ceramic Matrix Composite and Superalloy Bolted Joint Based on Damage Failure Load

Chao Lv Shuyuan Zhao Zhengyu Li Zeliang Pu Jianglong Dong Xinyang Sun Wenjiao Zhang

哈尔滨工业大学学报（英文版）2021，Vol.28Issue(2)：55-61,7.

哈尔滨工业大学学报（英文版）2021，Vol.28Issue(2)：55-61,7.DOI:10.11916/j.issn.1005-9113.2019061

Bolt Design of Ceramic Matrix Composite and Superalloy Bolted Joint Based on Damage Failure Load

Chao Lv ¹Shuyuan Zhao ²Zhengyu Li ²Zeliang Pu ²Jianglong Dong ²Xinyang Sun ³Wenjiao Zhang⁴

作者信息

1. China Academy of Aerospace Aerodynamics, Beijing 100074, China
2. National Key Laboratory of Science and Technology for National Defense on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China
3. School of Aeronautics and Astronautics, Harbin Institute of Technology, Harbin 150001, China
4. Engineering College, Northeast Agricultural University, Harbin 150030, China
折叠

摘要

关键词

2D C/SiC composite/progressive damage analysis/tensile properties/bolted joint/bolt parameters

Key words

2D C/SiC composite/progressive damage analysis/tensile properties/bolted joint/bolt parameters

分类

航空航天

引用本文复制引用

Chao Lv,Shuyuan Zhao,Zhengyu Li,Zeliang Pu,Jianglong Dong,Xinyang Sun,Wenjiao Zhang..Bolt Design of Ceramic Matrix Composite and Superalloy Bolted Joint Based on Damage Failure Load[J].哈尔滨工业大学学报（英文版）,2021,28(2):55-61,7.

基金项目

Sponsored by the Pre-Research Foundation of Shenyang Aircraft Design and Research Institute,Aviation Industry Corporation of China(Grant No.JH20128255). （Grant No.JH20128255）

哈尔滨工业大学学报（英文版）

ISSN：1005-9113

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