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Effects of Casting and Process Designs on Shrinkage Porosity in Nozzle Segments Investment Casting of Ren6 77 Alloy

机译:铸造和工艺设计对戒指区段收缩孔隙率的影响REN6 77合金

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In this study, the effects of casting and process designs on the occurrence of shrinkage porosity in nozzle segments investment casting of Rene 77 alloy are systematically investigated by using the Design of Experiment (DOE) method. The ultimate goal is to reach an optimal design to produce castings which are free from porosity defects. The casting under investigation is a 6-vane turbine muki-nozzle segment with item dimensions of 230mmL 180mmH 51mmW. The casting conditions under consideration include seven gate positions, two blade trailing edge directions, two outer shroud directions, three ceramic shell thicknesses, four insulation wrap methods, five chiller thicknesses, and three pouring temperatures. Macro-porosity content and distribution of the castings are measured using visual examination, Fluorescent Penetrant Inspection (FPI), and X-ray inspection. Those castings without macro-porosity are then dissected into 21 specimens. The specimens are grounded, polished, and observed under an optical microscope. The worst area for microporosity formation is identified. The extent of micro-porosity in that area is quantified by an image analyzer. A microporosity map is then drawn for each and every casting. The results show that for the original casting design, where the inner shroud is 3 mm thick, without the employment of steel chiller born linear shrinkage and through porosity can be found in the inner shroud of the castings regardless of the casting conditions. By the employment of room temperature chiller, not only the macro-porosity can be eliminated but also the micro-porosity can be significantly reduced. The optimal casting and process designs are to stay with the design of 3 mm thick for the inner shroud and to use steel chiller of room temperature on the inner shroud area, inward TE direction, upward outer shroud direction, 6 1/2 shell coats, pouring temperature of 1440 deg C, and wrapping the mold from the bottom of airfoils to the pouring cup by 6.35 mm thick insulation. For this optimal design, the worst micro-porosity formation is around 4 percent for the casting.
机译:在这项研究中,通过使用实验(DOE)方法的设计,系统地研究了铸造和工艺设计对rene 77合金的投资铸造的收缩孔隙率的影响。最终目标是达到最佳设计,以生产没有孔隙缺陷的铸件。正在调查的铸件是一个6叶片涡轮机Muki-喷嘴段,其中物品尺寸为230mml 180mm 551mm。所考虑的铸件条件包括七个栅极位置,两个叶片后缘方向,两个外护罩方向,三个陶瓷壳厚度,四个绝缘包装方法,五个冷却器厚度和三个浇注温度。宏观孔隙率和铸件的分布是使用视觉检查,荧光渗透检查(FPI)和X射线检测的测量。然后将那些没有宏观孔隙率的铸件分解成21个样本。在光学显微镜下接地,抛光并观察标本。鉴定了微孔形成的最差区域。通过图像分析仪量化该区域中的微孔隙率的程度。然后为每个铸件绘制微孔隙度图。结果表明,对于原始的铸造设计,其中内护罩厚3毫米,而不会就采用钢冷却器出生的线性收缩,并且通过孔隙率可以在铸件的内护罩中找到,而不管浇铸条件如何。通过采用室温冷却器,不仅可以消除宏观孔隙,而且可以显着降低微孔隙率。最佳的铸造和工艺设计是保持内部护罩的3毫米厚的设计,并在内护罩区域上使用钢冷却器,向上的TE方向,向上外护罩方向,6 1/2壳涂层,浇注1440°C的温度,将模具从翼型底部缠绕在浇注杯中,厚的绝缘浓度为6.35毫米。对于这种最佳设计,最差的微孔隙率形成为铸造的4%。

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