航空学报 > 1982, Vol. 3 Issue (2): 43-50

结构连接件常幅载荷下的无裂纹寿命预计

薛景川, 杨玉功   

  1. 飞机强度研究所
  • 收稿日期:1980-02-01 修回日期:1900-01-01 出版日期:1982-06-25 发布日期:1982-06-25

THE CRACK-FREE LIFE PREDICTION FOR STRUCTURAL JOINTS UNDER CONSTANT AMPLITUDE LOADS

Xue Jingchuan, Yang Yugong   

  1. Aircraft Strength Research Institute
  • Received:1980-02-01 Revised:1900-01-01 Online:1982-06-25 Published:1982-06-25

摘要: 本报告简明地介绍了用应力严重系数法预计常幅载荷下结构连接件的寿命的方法;介绍了基于应力严重系数概念确定α、β系数的方法;通过试验拟合导出考虑擦伤影响的方法;同时,通过一百多个铆接件的疲劳试验验证该方法的可靠性。

Abstract: This paper briefly describes a method of detailed designing and predicting the fatigue life for structural joints under constant amplitude loads by means of the Stress Severity Factor conceptBased on the Stress Severity Factor concept, an approach for determining factors α and β is developed and some of their values are derived from fatigue tests.An approach dealing with the cratch is created by fitting test data, and the relation between the corrective S-N curves of structural joints and the S-N curves of materials is defined.More than 100 specimens of revited joints were tested. The test data obtained were compared with the analytical results favorably and thereby testified the feasibility of this method.In addition, the present method was employed to predict the full-scale S-N curves of structural joints for their preliminary design and gave quite good results under the given conditions.