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High-Temperature Pre-deformation and Rejuvenation Treatment on the Microstructure and Creep Properties of Ni-Based Single-Crystal Superalloys

机译:高温预变形及恢复活性对Ni基单晶高温合金的微观结构和蠕变性能

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Unintentional plastic deformation during production of turbine blades made from Ni-based single-crystal superalloy has a huge risk on its durability. In the present study, a plastic deformation was applied at various temperatures to AM1 alloy and its effect on the alloy's microstructure and creep properties were analyzed. Microstructure evolution during aging treatment was different for plastic deformation at lower temperature (≤ 750°C) and higher temperature (950°C) because of different deformation mechanisms. AM1 with mild γ' directional coarsening after plastic deformation at 950°C and following aging treatments performed well in creep test at 1050°C/140 MPa, but poorly at 850°C/500 MPa. Rhenium containing CMSX-4 Plus was tested similarly to AM1. Pre-deformation has huge impact on creep durability of CMSX-4 Plus at 1150°C/110 MPa; however, the creep life debit at 1050°C/200 MPa was minor. In order to restore properties of pre-deformed single-crystal superalloys, rejuvenation heat treatment process was added after pre-deformation. Rejuvenation treatment successfully restored microstructure after room-temperature plastic deformation, and creep properties of rejuvenated specimens are equivalent to that of original AM1 and CMSX-4 Plus.
机译:在基于Ni的单晶高温合金制成的涡轮机叶片期间的无意塑性变形具有巨大的耐用性风险。在本研究中,在各种温度下施加塑性变形至AM1合金,分析了对合金的微观结构和蠕变性能的影响。由于不同的变形机制,在较低温度(≤750℃)和更高的温度(950℃)下,衰老处理过程中的微观结构演化是不同的。在950℃下塑性变形和在1050℃/ 140MPa的蠕变试验中表现出很细的蠕变试验后,具有温和γ'方向粗化,在1050℃/ 140MPa的蠕变试验中进行良好,但在850℃/ 500MPa的蠕变试验中进行良好。与AM1类似地测试含有CMSX-4 Plus的铼。预变形对1150°C / 110 MPa的CMSX-4加上的蠕变耐久性产生了巨大影响;但是,1050°C / 200 MPa的蠕变寿命借记是次要的。为了恢复预变形的单晶超合金的性能,在预变形后加入再生热处理过程。恢复治疗在室温塑性变形后成功恢复了微观结构,恢复活力的蠕变性能等同于原版AM1和CMSX-4 Plus。

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