長(zhǎng)期熱暴露對(duì)含鎢鈮γ-TiAl合金疲勞及表面損傷容限的影響
發(fā)布人：上海艾荔艾合金股份有限公司www.shailiai.cn
更新時(shí)間：2016-07-05
選取熱暴露(700 ℃，10000 h)前、后的Ti-44.5Al-5Nb-1W-1B(摩爾分?jǐn)?shù)，%)(5-1-1合金)，對(duì)其表面引入不同深度的缺口(0~800 μm)，研究熱暴露對(duì)該材料的疲勞性能及缺口損傷容限的影響，以Kitagawa-Takahashi線圖的形式對(duì)熱暴露引起的疲勞強(qiáng)化、長(zhǎng)裂紋擴(kuò)展門檻值以及合金在熱暴露影響下對(duì)表面損傷的容忍限度進(jìn)行定量分析。
長(zhǎng)期熱暴露對(duì)含鎢鈮γ-TiAl合金疲勞及表面損傷容限的影響Effects of long-term thermal exposure on fatigue behavior and surface defect tolerance of W+Nb containing γ-TiAl alloy?選取熱暴露(700 ℃，10000 h)前、后的Ti-44.5Al-5Nb-1W-1B(摩爾分?jǐn)?shù)，%)(5-1-1合金)，對(duì)其表面引入不同深度的缺口(0~800 μm)，研究熱暴露對(duì)該材料的疲勞性能及缺口損傷容限的影響，以Kitagawa-Takahashi線圖的形式對(duì)熱暴露引起的疲勞強(qiáng)化、長(zhǎng)裂紋擴(kuò)展門檻值以及合金在熱暴露影響下對(duì)表面損傷的容忍限度進(jìn)行定量分析。結(jié)果表明:熱暴露導(dǎo)致的回火穩(wěn)態(tài)良性效應(yīng)大于合金顯微組織出現(xiàn)脆化的有害效應(yīng)，使得熱暴露后無(wú)缺口樣品出現(xiàn)疲勞強(qiáng)度提高，而α2層片分解和組織細(xì)化能適當(dāng)提高疲勞長(zhǎng)裂紋擴(kuò)展門檻值。當(dāng)在熱暴露后引入缺口而無(wú)回火效應(yīng)時(shí)，長(zhǎng)期熱暴露導(dǎo)致的組織脆化成為控制性因素，材料的缺口敏感性增加，表現(xiàn)為出現(xiàn)短缺口效應(yīng)的尺寸范圍在熱暴露后明顯增大。
Single edge through thickness notch of different depths (0-800 μm) was introduced to the surface of Ti-44Al-5Nb-1W-1B alloy (5-1-1 alloy) before and after the thermal exposure at 700 ℃ for 10000 h. The effects of thermal exposure on the fatigue behaviour and the surface defect tolerance capability were studied. The exposure-induced fatigue strengthening, the fatigue threshold of long cracks and the surface defect tolerance under thermal exposure were quantitatively analysed and discussed in the form of Kitagawa-Takahashi diagram. The results show that the positive effect of the thermal exposure-induced tempering stability is greater than the harmful effect of the microstructural embrittlement. The fatigue strength of the non-notched is therefore improved after thermal exposure. On the other hand, the increase in threshold stress for long fatigue crack growth after the long-term exposure is attributed to the refinement of α2?lamellae. The introduction of the short notches after thermal exposure (hereby no tempering effect) has caused increased notch sensitivity, causing an increased notch size range within which the fatigue strength decreases significantly, due to microstructural embrittlement induced by the long-term thermal exposure.
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