首页> 外文会议>Pacific Rim International Conference on Advanced Materials and Processing >INFLUENCE OF MICROSTRUCTURAL CHANGES AND GRAIN BOUNDARY PRECIPITATION ON THE BEHAVIOR OF 25Ni-15Cr-2Ti SUPERALLOY DURING HIGH TEMPERATURE CREEP
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INFLUENCE OF MICROSTRUCTURAL CHANGES AND GRAIN BOUNDARY PRECIPITATION ON THE BEHAVIOR OF 25Ni-15Cr-2Ti SUPERALLOY DURING HIGH TEMPERATURE CREEP

机译:微观结构变化和晶界降水对高温蠕变期间25ni-15cr-2ti超合金的影响

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Iron-base superalloys are well known materials having excellent high temperature properties. They are used in turbo superchargers and turbine engines required for aerospace and power plants. In this investigation precipitation hardenable X5NiCrTi26-15 was used to study the influence of microstructural changes on the creep behavior at different conditions. Different creep cycles were applied for both base alloy and laser beam welded alloy (6kW CO2 ) namely at 600 , 625 and 650C at applied controlled creep stresses of 400 and 450 MPa . The base material sheet was used in as solution annealed state ( 30 min, 960 C, WQ ). The specimens were hardened in two steps (24h,760 C, FC and 16h, 705C,AC) before being investigated. The microstructural changes due to grain boundary sliding, intergranual fracture perpendicular to the metal flow axis, and the type, morphology of different secondary carbides were measured and discussed. To examine the changes in microstructure Philips EM 400 TEM with an acceleration voltage of 120KV, and SEM as well as light microscopy were used. It was found that, laser beam welded structure investigated after creep deformation at temperatures lower than 650C and at controlled stress of 400 and 450 MPa , showed a textured weld metal zone with dendrite having lower hardness combined with a higher creep resistance than that for base material. It was found also that creeping at 650C at the same stress values offsets any gain in creep resistance of welded joints as compared with that for the base material at the same conditions.
机译:铁基超合金是众所周知的材料具有优异的高温性能。它们用于航空航天和发电厂所需的涡轮增压器和涡轮发动机。在该研究中,沉淀沉淀可硬化X5nicRTi26-15用于研究微观结构变化对不同条件下蠕变行为的影响。在施加的受控蠕变应力为400和450MPa的施加控制的蠕变应力下,将不同的蠕变循环应用于基础合金和激光束焊接合金(6kW CO2),即600,625和650℃。基材片材用作溶液退火状态(30分钟,960℃,WQ)。在研究之前,将样品以两步(24小时,760℃,Fc和16h,705c,AC)硬化。测量并讨论了晶界滑动,垂直于金属流动轴的晶骨折,垂直于金属流动轴的晶状体的微观结构变化,并讨论了不同二级碳化物的形态。为了检查Microdructure Philips EM 400 TEM的变化,使用120kV的加速电压,并且使用SEM以及光学显微镜。发现,在低于650℃的温度下蠕变变形和400和450MPa的受控应力之后研究的激光束焊接结构显示出纹理化的焊接金属区,具有较低硬度的枝晶与基础材料的较高抗蠕变性相结合。发现还发现,在相同的应力值下在相同的应力值下爬行,与在相同条件下的基材相比,在相同的应力值下偏离焊接接头的蠕变电阻的任何增益。

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