发 动 机 外 涵 道 机 匣 加 筋 布 局 轻 量 化 设 计

Liang Meng, Jing Zhang, Yadong Wang, Yang Yu, Fan Zhang, Jihong Zhu, Weihong Zhang

科研成果: 期刊稿件文章同行评审

1 引用 (Scopus)

摘要

This study focuses on the lightweight design of a specific bypass engine casing,considering the complex effects. A topology optimization approach is first employed to determine the optimal layout of stiffening ribs under various loading conditions. Additionally,taking into account the buckling stability requirements for the casing,the correlation between four common reinforcement configurations and structural buckling resistance is systematically studied. A hierarchical stiffening strategy on the basis of triangle and hexagonal patterns is proposed,and built a parametric model for the periodically stiffened casing. A comprehensive optimization design objective,based on stress levels of stiffening ribs and structural buckling resistance,is finally developed. The optimized reinforcement design for the bypass engine casing achieves a weight reduction of approximately 40% compared to the original design model. Moreover,it surpasses the structural stiffness and strength requirements and exhibits a significant enhancement of 212. 9% in the critical buckling load when compared to a structure with a wall thickness of 1. 3 mm. These advancements effectively ensure the operational stability of the bypass engine casing under severe load conditions.

投稿的翻译标题Lightweight design of stiffening ribs layout of a bypass engine casing
源语言繁体中文
文章编号529021
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
45
11
DOI
出版状态已出版 - 15 6月 2024

关键词

  • buckling
  • bypass engine casing
  • parametric modeling
  • reinforcement design
  • structure optimization

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