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試驗溫度對鎳基單晶高溫合金裂紋擴展行為的影響
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中國航發(fā)北京航空材料研究院,北京 100095

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國家科技重大專項


Effect of Test Temperature on Crack Propagation Behavior of Nickel-Based Single-Crystal Superalloy
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AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China

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China's National Science and Technology Major Program (J2019-VI-0022-0138)

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    摘要:

    研究了DD6鎳基單晶高溫合金從530 ℃到850 ℃的疲勞裂紋穩(wěn)定擴展行為。疲勞裂紋擴展試樣沿[001]方向平行于受拉的加載軸。通過掃描電子顯微鏡研究疲勞裂紋擴展試驗后的斷口形貌,并根據形貌特點分為源區(qū)、預制裂紋區(qū)、穩(wěn)定擴展區(qū)以及快速擴展區(qū)。通過電子背散射衍射技術研究垂直于斷口的剖面塑性變形情況。通過透射電子顯微鏡觀察斷口附近位錯機制隨溫度的變化。結果表明,受溫度場、應力場以及暴露時間的作用,在650 ℃時發(fā)生氧化,且在650 ℃至760 ℃之間,由于γ′相的弱化,在γγ′相中形成大量連續(xù)的位錯,導致合金氧化加劇,同時760 ℃下疲勞擴展壽命顯著下降。

    Abstract:

    The fatigue crack propagation behavior of DD6 nickel-based single-crystal superalloy was investigated at temperatures ranging from 530 °C to 850 °C. The fatigue properties were assessed along the [001] direction, parallel to the loading axis in tension. After the fatigue crack propagation test, the fracture morphology was examined by scanning electron microscope and classified into four zones, including source zone, prefabricated crack zone, stable extension zone, and rapid extension zone. Electron backscatter diffraction was utilized to observe the profiles of plastic deformation perpendicular to the fracture. Additionally, the dislocation motion mechanism near the fracture was studied by transmission electron microscope. Results show that oxidation occurs at 650 °C under combined influences of the temperature field, stress field, and exposure time. Furthermore, due to weakened γ′ phase, a significant number of consecutive dislocations form in the γ and γ′ phases between 650 and 760 °C, resulting in increased oxidation of alloy. Besides, a notable decrease in fatigue propagation life can be observed at 760 °C.

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李樂宇,田福政,李振,張金剛,鄧志偉,陳星,劉新靈.試驗溫度對鎳基單晶高溫合金裂紋擴展行為的影響[J].稀有金屬材料與工程,2024,53(7):1874~1881.[Li Leyu, Tian Fuzheng, Li Zhen, Zhang Jingang, Deng Zhiwei, Chen Xing, Liu Xinling. Effect of Test Temperature on Crack Propagation Behavior of Nickel-Based Single-Crystal Superalloy[J]. Rare Metal Materials and Engineering,2024,53(7):1874~1881.]
DOI:10.12442/j. issn.1002-185X.20230618

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  • 收稿日期:2023-10-06
  • 最后修改日期:2024-06-11
  • 錄用日期:2023-11-13
  • 在線發(fā)布日期: 2024-07-16
  • 出版日期: 2024-07-12