航空学报 > 2015, Vol. 36 Issue (3): 840-847   doi: 10.7527/S1000-6893.2014.0087

GH4169合金自然萌生小裂纹扩展行为的试验研究

张丽1,2, 吴学仁3, 黄新跃1,2   

  1. 1. 北京航空材料研究院 航空材料检测与评价北京市重点实验室, 北京 100095;
    2. 北京航空材料研究院 先进高温结构材料国防科技重点实验室, 北京 100095;
    3. 北京航空材料研究院, 北京 100095
  • 收稿日期:2014-02-27 修回日期:2014-05-05 出版日期:2015-03-15 发布日期:2015-03-31
  • 通讯作者: 吴学仁 男, 博士, 研究员, 北京航空材料研究院首席资深高级顾问。主要研究方向: 疲劳与断裂力学、 损伤容限技术、 材料力学性能。Tel: 010-62496005 E-mail: xrwu621@163.com E-mail:xrwu621@163.com
  • 作者简介:张丽 女, 博士,工程师。主要研究方向: 航空发动机材料的小裂纹行为研究与疲劳寿命预测。Tel: 010-62496718 E-mail: zli335@163.com
  • 基金资助:

    国家级项目

Experimental investigation on the growth behavior of naturally- initiated small cracks in superalloy GH4169

ZHANG Li1,2, WU Xueren3, HUANG Xinyue1,2   

  1. 1. Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, Beijing Institute of Aeronautical Materials, Beijing 100095, China;
    2. National Key Laboratory of Science and Technology on Advanced High Temperature Structure Materials, Beijing Institute of Aeronautical Materials, Beijing 100095, China;
    3. Beijing Institute of Aeronautical Materials, Beijing 100095, China
  • Received:2014-02-27 Revised:2014-05-05 Online:2015-03-15 Published:2015-03-31
  • Supported by:

    National Level Project

摘要:

为了研究镍基GH4169高温合金自然萌生小裂纹的扩展行为,采用单边缺口拉伸(SENT)试样进行了室温下应力比R=0.1, 0.5的小裂纹扩展试验。在长裂纹近门槛值区域,观察到明显的小裂纹效应,疲劳小裂纹扩展寿命占全寿命的大部分。利用扫描电子显微镜(SEM)和能谱分析仪(EDS)对试样断口表面进行微观分析,结果表明, 疲劳小裂纹起始于合金中的夹杂(Ti(C, N)或Nb(C, N)),并且倾向于以半圆形向试样内部扩展。试样的断裂模式存在由晶体学小平面断裂向疲劳条带断裂的转变,该断裂模式转变处对应小裂纹扩展速率曲线上裂纹加速扩展前的急速降低点。

关键词: 高温合金, 小裂纹效应, 断裂模式, 夹杂, 分散性

Abstract:

The growth behavior of naturally-initiated small cracks in single edge notched tensile (SENT) specimens of nickel-based superalloy GH4169 is studied. Fatigue experiments are conducted under constant amplitude loading with the stress ratios R of 0.1 and 0.5 at room temperature. A significant small crack effect is evident in this alloy, and the major part of total fatigue life is consumed in small crack propagation phase. Fracture mode under cyclic loading is established by scanning electron microscopy (SEM) and energy dispersive spectra (EDS) analysis on specimen fracture surfaces. Small cracks initiate from material inclusions, namely Ti(C, N) or Nb(C, N). A transition of fracture mode from faceted, crystallographic fracture to classical striation type of fracture occurs, corresponding to the minimum growth rate at small crack growth rate curve before crack growth acceleration.

Key words: superalloy, small crack effect, fracture mode, inclusion, scatter

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