Ti-6Al-4V合金の疲労き裂伝ぱに及ぼすき裂開閉口とき裂付近残留応力の相関

抄録

There are very few reports concerning X-ray residual stress measurements near the fatigue crack for Ti-6Al-4V alloys. The residual stress near the crack was measured by an X-ray method for the annealed materials of Ti-6Al-4V alloys and their aging treatment materials, in which the X-ray residual stress was confirmed to exist by comparing with loading stresses under tension. The compressive residual stress, measured in the wake of the propagating fatigue crack, was larger in the aging treatment material. In addition, the crack opening displacement was measured along the real fatigue crack, which was different from the theoretical one. This made it possible to evaluate the effective stress intensity factors K_eff depending on the residual stress near the fatigue crack. The fatigue crack propagation rate under the same K_eff-value was smaller in the annealed than in the aging treatment material. This was probably related not only to the zig-zag crack path in the annealed material, but also to the heavier plastic deformation accompanying the large compressive residual stress in the aging treatment material.