40CrNi2Si2MoVA钢机械加工与喷丸试样旋转弯曲疲劳寿命的预测方法

TG111.7%TG668; 为了预测机械加工及喷丸强化后40CrNi2Si2MoVA钢试样在室温下的旋转弯曲疲劳寿命,结合商用有限元软件ABAQUS和疲劳寿命分析软件FE-SAFE对不同数值计算方法的适用性及准确性进行比较,提出了喷丸强化40CrNi2Si2MoVA钢的寿命预测经验公式.结果表明:对于机械加工试样,选择"Brown-Miller"算法和表面残余应力用于计算可获得比较准确的预测结果;对于喷丸强化试样,高应力水平下也可选用"Brown-Miller"算法及表面残余应力,而低应力水平下则应改用"Stress-based Brown...

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Published in航空材料学报 Vol. 40; no. 1; pp. 87 - 92
Main Authors 徐明波, 柳鸿飞, 高玉魁
Format Journal Article
LanguageChinese
Published 中国商用飞机有限责任公司上海飞机设计研究院,上海,200232%同济大学航空航天与力学学院,上海,200092 01.02.2020
Subjects
FE-SAFE
40CrNi2Si2MoVA钢
疲劳寿命预测
喷丸强化
Online AccessGet full text
ISSN1005-5053
DOI10.11868/j.issn.1005-5053.2019.000033

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Abstract TG111.7%TG668; 为了预测机械加工及喷丸强化后40CrNi2Si2MoVA钢试样在室温下的旋转弯曲疲劳寿命,结合商用有限元软件ABAQUS和疲劳寿命分析软件FE-SAFE对不同数值计算方法的适用性及准确性进行比较,提出了喷丸强化40CrNi2Si2MoVA钢的寿命预测经验公式.结果表明:对于机械加工试样,选择"Brown-Miller"算法和表面残余应力用于计算可获得比较准确的预测结果;对于喷丸强化试样,高应力水平下也可选用"Brown-Miller"算法及表面残余应力,而低应力水平下则应改用"Stress-based Brown Miller"算法及最大残余应力.基于上述两种方法提出的经验公式:σmax=-64.378?lg N+1449.268,可改善40CrNi2Si2MoVA钢喷丸强化试样疲劳寿命预测的准确性.
AbstractList TG111.7%TG668; 为了预测机械加工及喷丸强化后40CrNi2Si2MoVA钢试样在室温下的旋转弯曲疲劳寿命,结合商用有限元软件ABAQUS和疲劳寿命分析软件FE-SAFE对不同数值计算方法的适用性及准确性进行比较,提出了喷丸强化40CrNi2Si2MoVA钢的寿命预测经验公式.结果表明:对于机械加工试样,选择"Brown-Miller"算法和表面残余应力用于计算可获得比较准确的预测结果;对于喷丸强化试样,高应力水平下也可选用"Brown-Miller"算法及表面残余应力,而低应力水平下则应改用"Stress-based Brown Miller"算法及最大残余应力.基于上述两种方法提出的经验公式:σmax=-64.378?lg N+1449.268,可改善40CrNi2Si2MoVA钢喷丸强化试样疲劳寿命预测的准确性.
Author 高玉魁
徐明波
柳鸿飞
AuthorAffiliation 中国商用飞机有限责任公司上海飞机设计研究院,上海,200232%同济大学航空航天与力学学院,上海,200092
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GAO Yukui
LIU Hongfei
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DocumentTitle_FL Prediction method of rotating-bending fatigue life of 40CrNi2Si2MoVA steel specimens after machining and shot peening
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40CrNi2Si2MoVA钢
疲劳寿命预测
喷丸强化
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Publisher 中国商用飞机有限责任公司上海飞机设计研究院,上海,200232%同济大学航空航天与力学学院,上海,200092
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Snippet TG111.7%TG668; 为了预测机械加工及喷丸强化后40CrNi2Si2MoVA钢试样在室温下的旋转弯曲疲劳寿命,结合商用有限元软件ABAQUS和疲劳寿命分析软件FE-SAFE对不同数值计算方法的...
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Title 40CrNi2Si2MoVA钢机械加工与喷丸试样旋转弯曲疲劳寿命的预测方法
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