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激光沉積修復(fù)TA15鈦合金疲勞性能研究
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沈陽(yáng)航空航天大學(xué) 航空制造工藝數(shù)字化國(guó)防重點(diǎn)學(xué)科實(shí)驗(yàn)室; 沈陽(yáng)航空航天大學(xué) 機(jī)電工程學(xué)院,沈陽(yáng)航空航天大學(xué) 機(jī)電工程學(xué)院,沈陽(yáng)航空航天大學(xué) 航空制造工藝數(shù)字化國(guó)防重點(diǎn)學(xué)科實(shí)驗(yàn)室; 沈陽(yáng)航空航天大學(xué) 機(jī)電工程學(xué)院,沈陽(yáng)航空航天大學(xué) 航空制造工藝數(shù)字化國(guó)防重點(diǎn)學(xué)科實(shí)驗(yàn)室,沈陽(yáng)航空航天大學(xué) 航空制造工藝數(shù)字化國(guó)防重點(diǎn)學(xué)科實(shí)驗(yàn)室; 沈陽(yáng)航空航天大學(xué) 機(jī)電工程學(xué)院

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TG166.5

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國(guó)家自然科學(xué)基金資助項(xiàng)目(No.51405309);遼寧省自然科學(xué)基金資助項(xiàng)目(No.2013024011)


Fatigue properties of laser deposited repaired TA15 titanium alloy
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    摘要:

    采用激光沉積修復(fù)技術(shù)對(duì)銑切溝槽損傷的TA15鈦合金鍛件進(jìn)行修復(fù),研究了修復(fù)件的疲勞裂紋萌生和擴(kuò)展特性。采用光學(xué)顯微鏡和掃描電子顯微鏡分析了試樣疲勞斷口以及縱截面。結(jié)果表明,修復(fù)后試樣均斷裂于修復(fù)區(qū),其疲勞行為具有很強(qiáng)的組織敏感性,疲勞源區(qū)有與α片層集束尺寸和形貌相同的解理斷裂面和撕裂特征。穩(wěn)定擴(kuò)展區(qū)的裂紋沿著α片層邊界擴(kuò)展,有的垂直于α片層,有的平行于α片層;固溶時(shí)效熱處理后,組織敏感尺寸達(dá)到了單個(gè)片層尺寸的細(xì)小組織個(gè)體,表現(xiàn)為沿不同滑移方向分離的單個(gè)α/β片層撕裂和α′片層清晰排列的痕跡。細(xì)小、取向更多的片層集束使裂紋更容易偏轉(zhuǎn),增加了裂紋擴(kuò)展路徑的長(zhǎng)度,從而消耗更多的裂紋擴(kuò)展能量。

    Abstract:

    The technology of laser deposited repair was used to repair TA15 alloy with milling groove damage, and the fatigue crack nucleation and growth behaviors were investigated. Fatigue fracture surfaces and longitudinal sections of specimens were examined by optical microscopy and scanning electron microscopy. Results indicated that specimens were broken in the repaired zone and the fatigue properties are microstructure-sensitive. The crack nucleation region was characterized by the crystallographic cleavage facets of α lamellae and tearing of β matrix. The size and morphology of the cleavage facets were the same with α lamellae. The crack tended to propagate along the border of α lamellar and its propagation direction was parallel or perpendicular to α lamellar. After solution-aging treatment, the microstructure-sensitive size reached individual small units of a single lamellae, presenting a single α/β tearing deformation along the misalignment of silp direction in two colonies and a clear arrangement of bunch-α ". A finer, more oriented lamellar structure were obtained to make it easier for fatigue crack deflection, increased the length of the crack path, thereby consuming more crack propagation energy.

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許良,黃雙君,王磊,周松,回麗.激光沉積修復(fù)TA15鈦合金疲勞性能研究[J].稀有金屬材料與工程,2017,46(7):1943~1948.[Xu Liang, Huang Shuangjun, Wang Lei, Zhou Song, Hui Li. Fatigue properties of laser deposited repaired TA15 titanium alloy[J]. Rare Metal Materials and Engineering,2017,46(7):1943~1948.]
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  • 收稿日期:2016-05-18
  • 最后修改日期:2016-07-12
  • 錄用日期:2016-08-18
  • 在線發(fā)布日期: 2017-11-14
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