航空学报 > 1986, Vol. 7 Issue (4): 412-416

紧拉型试样的电位场及其在裂纹扩展试验中的应用

姜伟之, 王春生, 路民旭   

  1. 北京航空学院
  • 收稿日期:1985-08-30 修回日期:1900-01-01 出版日期:1986-09-25 发布日期:1986-09-25

THE ELECTRICAL POTENTIAL OF CT SPECIMEN AND ITS APPLICATION IN CRACK EXTENSION

Jiang Weizhi, Wang Chunsheng, Lu Mingxu   

  1. Beijing Institute of Aeronautics and Astronautics
  • Received:1985-08-30 Revised:1900-01-01 Online:1986-09-25 Published:1986-09-25

摘要:

疲劳裂纹扩展是预测结构疲劳寿命所必需的基本力学性能之一,而要取得有用的裂纹扩展速率数据,必有可靠的裂纹检测分析方法。在常温下,直读、柔度、涡流、超声、电阻及电位等方法均可应用,但在航空及其他动力装置用高温材料的试验研究中,则几乎只有紧拉(CT)试样的电位法可供使用。因此,较全面地分析CT型试样的电位分布,探讨优先的试验方案和给出相应的裂纹电位标定函数是非常必要的。

Abstract:

The electric potential field calculations under all useful current boundary conditions for compact tension specimen show that varying current input point on boundary evidently affects the electric potential drop-crack extension calibration function. Therefore, although Johnson's formula can be applied to three-point bend specimen, it can't be adapted to compact tension specimen as the current input location is at different point on its boundary.The initial electric potential drop V0 is constant for a given geometry and current boundary condition, but for different current boundary conditions V0 may change greatly, so the relative sensitivity for the latter situation must be based on by directly and not on the normalized exporssion V/V0, then we can get the preferential order for choosing the current input point, i e. from crack mouth along front face, tip/bottom face and finally to back face. This order also agrees with the order of current density intensity near the notch root or crack tip.Of course, when making one's option in practice it is also necessary to consider technical feasibility and convenience. Since both geometry and current boundary condition influence the calibration function, the applied function had better be offered by finite element method individually after making the preferential option mentioned above.