首页> 外文期刊>Materials Science and Engineering >An attempt to correlate the change of the swept area (ΔA/b~2) by mobile dislocations with the mechanism of the fatigue crack propagation rate (da/dN) in environmental hydrogen: Application in Inconel 690
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An attempt to correlate the change of the swept area (ΔA/b~2) by mobile dislocations with the mechanism of the fatigue crack propagation rate (da/dN) in environmental hydrogen: Application in Inconel 690

机译:尝试将移动位错的扫掠面积变化(ΔA/ b〜2)与环境氢中疲劳裂纹扩展速率(da / dN)的机理相关联:在Inconel 690中的应用

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The thermally activated dislocation motion due to plastic deformation in Inconel 690 has been carried out by performing tensile tests in air and in environmental hydrogen using the strain relaxation technique. The results show that the variation of - δ(ΔA/b~2) or ln(V_H/V_(Air)) with ε_p depends on the nickel content in the alloy and the microstructure, and generally increases with increasing Ni% for low value of ε_p (tensile test). The maximum increase in the rate change was observed for the austenized and aged microstructure. On the other hand, fatigue crack propagation rate (da/dN) has been measured in the same environments. An attempt has been carried out to correlate the rate change - δ(ΔA/b~2) or ln(V_H/V_(Air)) with the variation of (da/dN)_H against (da/dN)_(Air) (the variation of Ω) and has shown that for the austenized and aged microstructure, Ω is higher than those for stress relieved or only aged at 700 ℃. These results are similar to those obtained by the thermal activation parameter -δ(ΔA/b~2) or the ratio ln(V_H/V_(Air)). The maximum values of- δ(ΔA/b~2) and Ω are obtained when the density of precipitates on the grain boundaries is higher than that in the matrix. In this case, intergranular fractures with fin slip lines features on the grain surfaces were observed. Finally, in the presence of environmental hydrogen, about the fatigue crack propagation rate, two relationships were established and expressed as: 1) in stages Ⅰ and Ⅱ: (Δε_p/2) = θ ΔK + Γ and 2) only in stage Ⅱ: (da/dN)_(II) = c_(II) (Δε_p / 2)λ, where λ ≈ m = 2, the power factor in Paris' law.
机译:Inconel 690中由于塑性变形而引起的热活化位错运动已通过使用应变松弛技术在空气和环境氢气中进行拉伸测试来进行。结果表明-δ(ΔA/ b〜2)或ln(V_H / V_(空气))随ε_p的变化取决于合金中镍的含量和显微组织,通常在低值时随Ni%的增加而增加。 ε_p(拉伸测试)。对于奥氏体化和时效的显微组织,观察到速率变化的最大增加。另一方面,在相同环境下测量了疲劳裂纹扩展速率(da / dN)。已尝试将速率变化-δ(ΔA/ b〜2)或ln(V_H / V_(Air))与(da / dN)_H对(da / dN)_(Air)的变化相关联(Ω的变化),并且表明,对于奥氏体化和时效的显微组织,Ω高于缓解应力或仅在700℃时效的组织。这些结果类似于通过热活化参数-δ(ΔA/ b〜2)或比率ln(V_H / V_(Air))获得的结果。当晶界上的析出物密度高于基体中的析出物密度时,可获得-δ(ΔA/ b〜2)和Ω的最大值。在这种情况下,观察到晶粒表面具有鳍状滑移特征的晶间断裂。最后,在环境氢存在下,关于疲劳裂纹扩展速率,建立了两个关系,并表示为:1)在Ⅰ和Ⅱ阶段:(Δε_p/ 2)=θΔK+Γ和2)仅在Ⅱ阶段: (da / dN)_(II)= c_(II)(Δε_p/ 2)λ,其中λ≈m = 2,巴黎定律中的功率因数。

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