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TiAl合金高溫疲勞小裂紋與長裂紋擴展行為
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1.北京航空材料研究院 材料檢測與評價航空科技重點實驗室;2.北京航空材料研究院 先進鈦合金航空科技重點實驗室

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中圖分類號:

TG146.2

基金項目:

國家自然科學(xué)基金(項目號:51401195)和航空科學(xué)基金(項目號:2013ZF21014)資助


Behavior of small and long fatigue crack propagration of TiAl alloy at elevated temperature
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Aviation Key Laboratory of Science and Technology on Materials Testing and Evaluation,Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation,Beijing Institute of Aeronautical Matarials

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    摘要:

    本研究利用原位觀察疲勞試驗方法研究了變形TiAl合金在650℃下的三維小裂紋擴展行為,利用傳統(tǒng)疲勞裂紋擴展試驗方法研究了合金在650~800 ℃溫度范圍內(nèi)的長裂紋擴展行為。結(jié)果顯示,650℃下,變形TiAl合金的三維小裂紋在低于長裂紋擴展門檻值的區(qū)域依然能夠擴展,并且擴展速率高于長裂紋;試樣棱邊平直橫向加工刻痕是合金三維小裂紋萌生的主要位置之一,小裂紋在擴展過程中發(fā)生偏折并在偏折處合并,合金的疲勞壽命對試樣表面的不規(guī)則條狀加工缺陷不敏感;在650~800 ℃溫度范圍內(nèi),合金的疲勞長裂紋穩(wěn)態(tài)擴展速率對溫度變化不敏感,裂紋擴展過程均顯示解理斷裂,裂紋擴展門檻值受韌脆轉(zhuǎn)變溫度影響,韌脆轉(zhuǎn)變溫度以下溫度的門檻值較低。

    Abstract:

    Three-dimensional small crack propagation behavior of deforming TiAl alloy at 650℃ is studied by in-situ observation fatigue testing, and then long crack propagation behavior of the alloy in temperature range from 650℃ to 800℃ is studied by fatigue crack propagation tests. It shows that, the three-dimensional small cracks can still grow even though in the stress intensity factor region that below the long crack propagation threshold value, furthermore, the growth rates of small cracks are higher than long cracks in this region; The sample edge straight horizontal manufacturing nick is one of the main positions of three-dimensional small crack initiation of the alloy. Small cracks merge at the position of bends that occur during the fatigue testing. The fatigue life of the alloy is not sensitive to irregular strip manufacturing defects on the surface of the sample; The steady propagation rates of long fatigue cracks of the alloy are not sensitive to temperature changes in temperature range from 650℃ to 800℃. All the long crack propagation processes exhibit the cleavage fracture. Crack propagation threshold values are related to ductile-brittle transition temperature, the temperatures below the ductile-brittle transition temperature have lower threshold values.

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焦?jié)奢x,于慧臣,董成利,魯原,高帆. TiAl合金高溫疲勞小裂紋與長裂紋擴展行為[J].稀有金屬材料與工程,2019,48(2):538~544.[Jiao Zehui, Yu Huichen, Dong Chengli, Lu Yuan, Gao Fan. Behavior of small and long fatigue crack propagration of TiAl alloy at elevated temperature[J]. Rare Metal Materials and Engineering,2019,48(2):538~544.]
DOI:10.12442/j. issn.1002-185X.20170477

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  • 收稿日期:2017-06-05
  • 最后修改日期:2017-09-27
  • 錄用日期:2017-10-12
  • 在線發(fā)布日期: 2019-03-15
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