Gamma prime crystal lattice orientation of turbine blades of the single crystal nickel based CMSX-4 superalloy (Conference Paper)

Onyszko A.

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Gamma prime crystal lattice orientation of turbine blades of the single crystal nickel based CMSX-4 superalloy (Conference Paper)

机译：单晶镍基CMSX-4高温合金的涡轮叶片的伽马素晶格取向（会议论文）

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The paper attempts to determine the changes in the γ' lattice orientation of aircraft engine turbine blades made of the CMSX-4 single crystal nickel superalloy. The solidification of a hollow assembly structure for 2 types of blades obtained at withdrawal rates of 3mm/min and 4 mm/min was carried out by the Bridgman method at the Research and Development Laboratory for Aerospace Materials at Rzeszow University of Technology using an ALD Vacuum Technologies vacuum furnace. Ceramic moulds made of Al_2O_3 were used. The alloy temperature during casting into the mould amounted to 1550°C. The blades withdrawal at a rate of 3 mm/min has a greater homogenity of disorientation angles distribution and γ' lattice constant values as compared with blades withdrawal at a rate 4 mm/min.

机译：本文试图确定由CMSX-4单晶镍超合金制成的飞机发动机涡轮叶片的γ'晶格取向的变化。使用ALD真空系统在热舒夫工业大学航空航天材料研究与发展实验室通过Bridgman方法对两种类型的叶片进行中空组装结构的固化，以3mm / min和4mm / min的抽出速度进行固化技术真空炉。使用由Al_2O_3制成的陶瓷模具。在铸模中的合金温度为1550℃。与以4mm / min的速率抽出的叶片相比，以3mm / min的速率抽出的叶片具有更大的取向角分布和γ′晶格常数值的均匀性。

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《Diffusion and Defect Data. Solid State Data, Part B. Solid State Phenomena》 |2013年第null期|共4页
作者
Onyszko A.;
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正文语种 eng
中图分类 53.632;
关键词
Bridgeman method; Single crystal; Structural perfection; Superalloys; Turbine blade;

机译：布里奇曼法;单晶;结构完善;高温合金;涡轮叶片;

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1. 取向偏离度对镍基第三代单晶高温合金DD9在760～1100℃ 横向拉伸性能的影响 [J] . 杨万鹏, 李嘉荣, 刘世忠, 中国有色金属学报（英文版） . 2019,第003期
2. 取向偏离度对镍基第三代单晶高温合金DD9在760~1100°C横向拉伸性能的影响 [J] . 杨万鹏, 李嘉荣, 刘世忠, 中国有色金属学报：英文版 . 2019,第003期
3. Gamma prime crystal lattice orientation of turbine blades of the single crystal nickel based CMSX-4 superalloy (Conference Paper) [J] . Onyszko A. Diffusion and Defect Data. Solid State Data, Part B. Solid State Phenomena . 2013,第Null期

机译：单晶镍基CMSX-4高温合金的涡轮叶片的伽马素晶格取向（会议论文）
4. Change in Gamma Prime Morphology and Dislocation Substructures of Single Crystal Nickel-based Superalloy, CMSX-4, Prior-crept at 1273 K-250 MPa with Simple Aging [J] . Nobuhiro MIURA, Kazunori KURITA, Yoshiaki HAYASHI, ISIJ international . 2011,第4期

机译：单晶镍基高温合金CMSX-4的γ初生形态和位错亚结构的变化，在1273 K-250 MPa时，先验蠕变，且时效简单
5. Change in Gamma Prime Morphology and Dislocation Substructures of Single Crystal Nickel-based Superalloy, CMSX-4, Prior-crept at 1273 K-250 MPa with Simple Aging [J] . Nobuhiro Miura, Kazunori Kurita, Yoshiaki Hayashi, ISIJ international . 2011,第4期

机译：单晶镍基高温合金CMSX-4的γ初生形态和位错亚结构的变化，并在1273 K-250 MPa的简单时效下先变
6. Gamma Prime Crystal Lattice Orientation of Turbine Blades of the Single Crystal Nickel Based CMSX-4 Superalloy [C] . ONYSZKO Arkadiusz Conference on applied crystallography . 2013

机译：基于单晶镍的CMSX-4高温合金的涡轮叶片的伽马素晶格取向
7. Eutectic gamma (Nickel)/gamma vprime(Nickel Aluminide) delta (Nickel Niobium) polycrystalline nickel-base superalloys: Chemistry, processing, microstructure and properties [D] . Xie, Mengtao 2012

机译：共晶γ（镍）/γvprime（镍铝化物）δ（镍铌）多晶镍基高温合金：化学，加工，显微组织和性能
8. The Effect of Withdrawal Rate on Crystal Structure Perfection Microstructure and Creep Resistance of Single Crystal Castings Made of CMSX-4 Nickel-Based Superalloy [O] . Kamil Gancarczyk, Maciej Zubko, Aneta Hanc-Kuczkowska, 2019

机译：撤离速率对CMSX-4镍基高温合金单晶铸件的晶体结构完善显微组织和抗蠕变性的影响
9. Change in Gamma Prime Morphology and Dislocation Substructures of Single Crystal Nickel-based Superalloy, CMSX-4, Prior-crept at 1273 K-250 MPa with Simple Aging [O] . Nobuhiro Miura, Kazunori Kurita, Yoshiaki Hayashi, 2011

机译：用简单的老化改变单晶镍高超合金，CMSX-4的伽马素形态和位错子结构，CMSX-4，在1273 k-250MPa下悄然悄然
10. Effect of Crystal Orientation on Analysis of Single-Crystal, Nickel-Based Turbine Blade Superalloys [R] . Swanson, G. R., Arakere, N. K. 2000

机译：晶体取向对单晶镍基涡轮叶片高温合金分析的影响

Gamma prime crystal lattice orientation of turbine blades of the single crystal nickel based CMSX-4 superalloy (Conference Paper)

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