热处理工艺对铸造高温合金K480组织的影响

采用光学显微镜、扫描电镜对K480镍基高温合金的铸态组织和不同固溶、时效处理后的组织进行了观察。研究了不同固溶和时效处理对K480合金组织行为的影响。结果表明,合金经过1130℃亚固溶处理后,组织为大小两种尺寸的γ'相;经过1190、1210和1230℃过固溶处理后空冷,析出均匀的γ'相,并且随着固溶温度的升高,碳化物和共晶的含量逐渐降低。一次时效处理,固溶态γ'相平均尺寸随时效温度升高而增大,合金经1050、1090和1110℃×4 h时效后,γ基体通道中均有更细小的三次γ'相析出,而在之后的二次时效和全时效过程中,这些细小的三次γ'相又重新溶解到基体或周围的大尺寸γ'相中。

一种单晶镍基合金热处理制度的研究

通过对一种单晶镍基合金的差热曲线分析和不同条件热处理后的组织形貌观察，制定合金热处理工艺，并研究了热处理期间γ′相的组织演化规律．结果表明，实验用合金的热处理“窗口”是1272～1320℃，在1300℃时，γ′相有最大的溶解速度，1040℃析出的γ′相最为稳定，在该温度时效50h后。γ′相长大，且呈球状和条状形貌，γ′/γ两相之间出现界面位错．因此，确定出该合金的热处理工艺为1280℃，4h,A．C＋1300℃，4h，A．C＋1040℃，4h，A．C＋870℃，24h。A．C．一次时效促使γ′相长大呈立方体形貌；二次时效期间，γ′相略有长大，立方度增加，排列更加规则．

Creep properties and microstructure evolution of nickel-based single crystal superalloy at different conditions

The creep properties of nickel-based single crystal superalloy with [001] orientation was investigated at different test conditions. The microstructure evolution of γ′ phase, TCP phase and dislocation characteristic after creep rupture was studied by SEM and TEM. The results show that the alloy has excellent creep properties. Two different types of creep behavior can be shown in the creep curves. The primary creep is characterized by the high amplitude at test conditions of (760 °C, 600 MPa) and (850 °C, 550 MPa) and the primary creep strain is limited at (980 °C, 250 MPa), (1100 °C, 140 MPa) and (1120 °C, 120 MPa). A little change ofγ′precipitate morphology occurs at (760 °C, 600 MPa). The lateral merging of the γ′ precipitate has already begun at (850 °C, 550 MPa). Theγphase is surrounded by theγ′phase at (980 °C, 250 MPa). Theγphase is no longer continuous tested at (1070 °C, 140 MPa). At (1100 °C, 120 MPa), the thickness ofγphase continues to increase. No TCP phase precipitates in the specimens at (760 °C, 600 MPa), (850 °C, 550 MPa) and (980 °C, 250 MPa). Needle shaped TCP phase precipitates in the specimens tested at (1070 °C, 140 MPa) and (1100 °C, 120 MPa). The dislocation shear mechanism including stacking fault formation is operative at lower temperature and high stress. The dislocation by-passing mechanism occurs to form networks atγ/γ′interface under the condition of high temperature and lower stress.

Microstructure evolution of a new directionally solidified Ni-based superalloy after long-term aging at 950 ℃ upto 1 000 h

The microstructure evolution of a new directionally solidified（DS） Ni-based superalloy used for gas turbine blades after long-term aging at 950 ℃ was investigated.The results show that the γ ＇ phase becomes more regular in dendritic arm and interdendritic area,while both the mass fraction and the size of γ ＇ phase increase gradually with increasing aging time.During long-term aging,the MC carbide dissolves on the edge to provide the carbon for the formation of M23C6 carbide by the precipitation of Cr at the grain boundary.The rose-shaped γ ＇/γ eutectic partly dissolves into γ matrix and the aging promotes it transform into raft-shape γ ＇.The microstructure is generally stable and no needle-like topologically close-packed phase（TCP） can be found after aging for 1 000 h.

热处理过程中DD6单晶高温合金的组织演化规律与力学性能

研究了DD6单晶高温合金在热处理过程中的显微组织演化规律以及初熔组织的生成机理。通过研究不同固溶时效处理对γ′相形貌、尺寸分布和体积分数的影响且分析了完全热处理后合金的显微硬度和拉伸性能,从而确定了合金最佳的热处理工艺。结果表明,通过差热分析法和金相观察法确定合金的初熔温度在1300~1310℃。在1315℃固溶处理4 h,枝晶间/枝晶干γ′相尺寸趋于一致,呈立方状均匀排列。在固溶处理过程中,γ/γ′共晶组织熔化生成了不规则初熔组织。在不同的一次时效工艺下,1120℃时效4 h空冷后,γ′相立方度更好,尺寸分布更均匀。合金最佳的热处理工艺为1290℃×1 h+1300℃×2 h+1315℃×4 h,AC+1120℃×4 h,AC+870℃×32 h,AC。合金在完全热处理后,随拉伸温度从室温升高至850℃时,强度达到峰值,温度继续升高,强度下降;在760℃拉伸时塑性最差,随着拉伸温度从760℃升高到950℃,塑性提高。