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A review on ultra-high cycle fatigue of CFRP

机译:CFRP超高周期疲劳综述

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摘要

Ultra-high cycle fatigue problem has received more and more attention with the continuous improvement of the reliability and life index of modern equipment, and has become a hot spot in fatigue research. As the non-metallic material with the most application potential in the modern aviation industry, the ultra-high cycle fatigue problem of carbon fiber reinforced plastic (CFRP) is the most prominent. In this paper, the research progress of ultra-high cycle fatigue research of CFRP has been systematically sorted out and summarized from three dimensions of test method, fatigue fracture macro-micro characteristics and fatigue damage model construction, including the adopted technical methods, the mechanism of fatigue crack initiation, the characteristics of S-N curve, Goodman diagram and the influence of humidity and other influence factors. The mechanism, evolution and model of CFRP ultra-high cycle fatigue damage are expounded, and the problems existing in the ultra-high cycle fatigue research of CFRP are presented.
机译:超高周期疲劳问题因现代设备的可靠性和生命指数而越来越多地受到关注,并已成为疲劳研究的热点。作为现代航空工业中最具应用潜力的非金属材料,碳纤维增强塑料(CFRP)的超高周疲劳问题是最突出的。本文从测试方法的三个维度,疲劳断裂宏观微观特性和疲劳损伤模型结构的三维超高周疲劳研究的研究进展已经过系统地分析并概述了疲劳损伤模型结构,包括采用技术方法,机制疲劳裂纹启动,Sn曲线的特点,善意图和湿度和其他影响因素的影响。阐述了CFRP超高周疲劳损伤的机制,演化和模型,并提出了CFRP超高周疲劳研究中存在的问题。

著录项

  • 来源
    《Composite Structures》 |2021年第1期|113058.1-113058.17|共17页
  • 作者单位

    Air Force Engn Univ Aeronaut Engn Coll Xian 710038 Peoples R China;

    Air Force Engn Univ Aeronaut Engn Coll Xian 710038 Peoples R China;

    Air Force Engn Univ Aeronaut Engn Coll Xian 710038 Peoples R China;

    Air Force Engn Univ Aeronaut Engn Coll Xian 710038 Peoples R China;

    Air Force Engn Univ Aeronaut Engn Coll Xian 710038 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    CFRP; Test method; Macro-micro characteristics; Fatigue model; Ultra-high cycle fatigue;

    机译:CFRP;测试方法;宏观微观特征;疲劳模型;超高循环疲劳;

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