位錯(cuò);980℃拉伸,合金中出現(xiàn)了位錯(cuò)纏結(jié);1100℃拉伸,合金中形成了位錯(cuò)網(wǎng)絡(luò)。"/>

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一種鎳基第三代單晶高溫合金的橫向拉伸性能
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北京航空材料研究院 先進(jìn)高溫結(jié)構(gòu)材料重點(diǎn)實(shí)驗(yàn)室,北京航空材料研究院 先進(jìn)高溫結(jié)構(gòu)材料重點(diǎn)實(shí)驗(yàn)室,北京航空材料研究院 先進(jìn)高溫結(jié)構(gòu)材料重點(diǎn)實(shí)驗(yàn)室,北京航空材料研究院 先進(jìn)高溫結(jié)構(gòu)材料重點(diǎn)實(shí)驗(yàn)室,北京航空材料研究院 先進(jìn)高溫結(jié)構(gòu)材料重點(diǎn)實(shí)驗(yàn)室,北京航空材料研究院 先進(jìn)高溫結(jié)構(gòu)材料重點(diǎn)實(shí)驗(yàn)室

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Transverse Tensile Properties of a Nickel-based Third Generation Single Crystal Superalloy
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Science and Technology on Advanced High Temperature Structural Materials Laboratory,Beijing Institute of Aeronautical Materials,Science and Technology on Advanced High Temperature Structural Materials Laboratory,Beijing Institute of Aeronautical Materials,Science and Technology on Advanced High Temperature Structural Materials Laboratory,Beijing Institute of Aeronautical Materials,Science and Technology on Advanced High Temperature Structural Materials Laboratory,Beijing Institute of Aeronautical Materials,Science and Technology on Advanced High Temperature Structural Materials Laboratory,Beijing Institute of Aeronautical Materials,Science and Technology on Advanced High Temperature Structural Materials Laboratory,Beijing Institute of Aeronautical Materials

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    在760℃到1100℃條件下,研究了一種鎳基第三代單晶高溫合金的橫向拉伸性能。采用光學(xué)顯微鏡(OM)、場發(fā)射掃描電子顯微鏡(FESEM)與掃描透射電子顯微鏡(STEM)觀察了合金的顯微組織與斷口形貌。結(jié)果表明:隨著溫度的升高,合金的拉伸強(qiáng)度降低,而拉伸延伸率增加。在760℃與850℃條件下的拉伸斷裂均為類解理斷裂。在980℃,1070℃和1100℃條件下,試樣斷口出現(xiàn)了反映凝固方向的枝晶形貌特征,且隨著溫度的升高枝晶形貌在斷口上的面積增加。在980℃條件下,拉伸斷裂為類解理斷裂與韌窩斷裂的混合斷裂。在1070℃與1100℃條件下,拉伸斷裂均為韌窩斷裂。隨著溫度的升高,塑性變形過程中開動了更多滑移系,導(dǎo)致形成了不同的位錯(cuò)形貌。760℃拉伸,合金中出現(xiàn)了高密度大致平行分布的a/2<110>位錯(cuò);980℃拉伸,合金中出現(xiàn)了位錯(cuò)纏結(jié);1100℃拉伸,合金中形成了位錯(cuò)網(wǎng)絡(luò)。

    Abstract:

    At the temperature range of 760 °C to 1100 °C, the transverse tensile properties of a nickel-based third generation single crystal superalloy were studied. The microstructures and fracture surfaces were observed by optical microscopy (OM), field emission scanning electron microscopy (FESEM) and scanning transmission electron microscopy (STEM). The results show that the tensile strength of the alloy decreases as the temperature increases, while the tensile elongation of the alloy increases with the temperature increasing. The fracture surfaces of the tensile ruptured specimens are characterized by quasi-cleavage features at 760 °C and 850 °C. At the temperature range of 980 °C to 1100 °C, dendrites characteristics exhibiting the solidification direction are observed on the fracture surfaces and the proportion of dendrites characteristic on the fracture surfaces increases with the temperature increasing. The fracture surface displays mixed quasi-cleavage and dimple features at 980 °C. The fracture surfaces are characterized by dimple features at 1070 °C and 1100 °C. As the temperature increases, more slip systems tend to be activated during the plastic deformation, result in different dislocation configurations. At 760 °C, high density a/2<110> dislocations are found to distribute roughly parallel with each other in the tensile ruptured specimens. The dislocations are observed to be tangled at 980 °C and dislocation networks have formed at 1100 °C.

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楊萬鵬,李嘉榮,劉世忠,史振學(xué),趙金乾,王效光.一種鎳基第三代單晶高溫合金的橫向拉伸性能[J].稀有金屬材料與工程,2018,47(10):2964~2969.[Yang Wanpeng, Li Jiarong, Liu Shizhong, Shi Zhenxue, Zhao Jinqian, Wang Xiaoguang. Transverse Tensile Properties of a Nickel-based Third Generation Single Crystal Superalloy[J]. Rare Metal Materials and Engineering,2018,47(10):2964~2969.]
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  • 收稿日期:2017-03-07
  • 最后修改日期:2017-04-11
  • 錄用日期:2017-05-16
  • 在線發(fā)布日期: 2018-11-08
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