首页> 外文期刊>Journal of aerospace engineering >Residual Stress Measurement and Fatigue Crack Growth Prediction after Cold Expansion of Cracked Fastener Holes
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Residual Stress Measurement and Fatigue Crack Growth Prediction after Cold Expansion of Cracked Fastener Holes

机译:开裂的紧固件孔冷扩后的残余应力测量和疲劳裂纹扩展预测

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摘要

The cold expansion technique is often used to introduce beneficial compressive stress at fastener holes, and can be used for remedial work where cracks already exist. In this paper, results are presented showing the effect of preexisting cracks on the residual stress field produced by cold expanding a fastener hole, and on subsequent fatigue crack growth. The effect on the residual stresses was experimentally evaluated in two ways: indirectly, in terms of retained expansion and directly, by measurement of the stresses using the X-ray and neutron diffraction techniques. The retained expansion ratio showed that cold expansion is more sensitive to the existence of precracks at lower levels of applied interference, and the inlet and outlet faces have different behavior. The stress measurements showed that preexisting cracks reduce the compressive residual stresses more on the mandrel inlet face than on the outlet face and in the middle of the specimen. The effect on fatigue crack growth rates was modeled using a linear-elastic fracture mechanics approach. It was found that cold expansion of a hole containing a preexisting crack longer than 1 mm introduces little benefit for subsequent fatigue crack growth behavior.
机译:冷膨胀技术通常用于在紧固件孔处引入有益的压缩应力,并可用于已经存在裂缝的补救工作。在本文中,结果显示了预先存在的裂纹对冷胀紧固件孔所产生的残余应力场以及随后疲劳裂纹扩展的影响。对残余应力的影响通过两种方法进行了实验评估:间接地,根据保留的膨胀,以及直接地,通过使用X射线和中子衍射技术测量应力。保留的膨胀率表明,在较低的施加干扰水平下,冷膨胀对预裂纹的存在更加敏感,并且入口和出口面的行为不同。应力测量表明,预先存在的裂纹在心轴入口面上的压缩残余应力比出口表面和试样中间的压缩残余应力更大。使用线性弹性断裂力学方法对疲劳裂纹扩展速率进行了建模。已发现,包含预先存在的裂纹的孔长于1 mm的孔的冷膨胀对随后的疲劳裂纹扩展行为几乎没有好处。

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