Progressive damage analysis of double-layer variable thickness 3D woven composite scaled engine casing

Author:

Wang Kun1,Kong Weiyi2,Xu Liming1,Zhang Nan1,Li Chao3,Cai Deng’an1,Zhou Guangming1ORCID

Affiliation:

1. State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing, China

2. Commercial Aviation Engine Company Limited, AECC, Shanghai, China

3. Nanjing Fiberglass Research & Design Institute, Nanjing, China

Abstract

Due to the excellent mechanical properties and strong design flexibility, the 3D woven composite engine casing shows great potential in high performance fields. This article adopted the method of double-layer weaving and adding yarn to achieve the variable thickness of the 3D woven composite engine casing. The purpose of this article is to study the compression performance and failure mechanism of this variable thickness casing in different thickness zones through experiments and numerical simulations to lay a foundation for future optimization and inclusiveness research on this casing with complex thickness changes. Three types of representative volume cells are established for progressive damage analysis. 3D-Hashin criteria and von-Mises stress criterion are used as damage criteria for yarns and matrix. The progressive damage process and the proportion of damage in the inner and outer layers of three types of 3D woven tubes under axial compression load are analyzed. Results show that the main failure modes of the three types of tubes are yarn-matrix compressive cracking along direction 3 and matrix failure. The damages are mostly concentrated in the warp bending area. The proportions of warp yarn damage in the inner and outer layers of three tubes are different.

Funder

National Natural Science Foundation of China

the Carbon Peaking and Carbon Neutrality Technology Innovation Special Fund of Jiangsu Province

Priority Academic Program Development of Jiangsu Higher Education Institutions

Publisher

SAGE Publications

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2. Improved analytical model to predict the effective elastic properties of 2.5D interlock woven fabrics composite

3. Quasi-Static Compression Response of Carbon Fiber Reinforced 2.5D Woven Composites at Different Loading Directions

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