数值模拟雾化气压对GH4169合金粉末粒径的影响

针对工艺参数与高温合金雾化粉末粒径间的复杂联系，采用ANSYS-Fluent数值模拟GH4169高温合金真空感应气雾化(VIGA)制粉过程中液滴的破碎行为，分析了雾化气压对金属熔体雾化过程和粉末粒度分布的影响.结果表明:一次雾化过程的带状液膜厚度和液滴面积逐渐减小；二次雾化对熔体的破碎作用逐渐增强，雾化所得粉末粒径越来越细小，中位径从81.10 μm减小到69.80，64.77，52.30，41.80μm；细粉收得率逐渐提高，由1.72%提高到12.62%，18.89%，56.50%，71.54%.     

High temperature tensile properties and fracture behavior of cast nickel-base K445 superalloy

The tensile properties and fracture behavior of a cast nickel-base superalloy K445 in the temperature range of 25-1 000℃were investigated.The microstructure and fracture surfaces of the alloy were investigated by OM,SEM and TEM.The results revealed that an anomalous yield strength phenomenon exists in the alloy at medium high temperature.The yield strength decreases gradually with the increase of temperature,reaches the minimum value at 650℃,and then increases again to obtain 940 MPa,which is almost the ...     

Effect of cyclic recovery heat treatment on surface recrystallization of a directionally solidified superalloy

Microstructural evolution and micro-har dness of a directionally solidified Ni-bas e superalloy subjected to shot-peening during cyclic recovery heat treatment was studied. It was found that γ′ dissolved and dislocation annih ilation occurred during heating, while γ′ re-precipitated when temperature dropped. Due to the formation of a stable dislocation network at γ/ γ′ interface, full recovery and therefore complete elimination of the surface recrystallization are difficult by the present cyclic recovery heat treatment .     

A comparative study of four modified Al coatings on Ni3Al-based single crystal superalloy

Four modified Al diffusion coatings (Al, Cr? Al, Al?Si and Cr? Al ? Si coatings) were prepared on Ni3Al based single crystal superalloy IC20. The oxidation tests were carried out at 1 150 °C for up to 100 h. Cyclic hot corrosion tests were carried out at 950 °C for 50 h. The results indicate that the oxidation and corrosion resistance s of IC20 alloy are improved significantly by the coatings, and both oxidation and hot corrosion resistances of the four coatings are rated in the order (from worst to best) of Cr ? Al, Al, Cr ? Al ? Si, Al? Si coatings. It is found that the degradations of Al and Cr ? Al coatings are very quick due to the serious inter-diffusion between the coatings and substrates. The inter-diffusion between Si-containing coatings and substrates is reduced since Si effe ctively retards the outward diffusion of Mo. The weak effects of Cr and benefit effects of Si to the oxidation and hot corrosion resistance were discussed. The hot corrosion degradation mechanism of superalloy IC20 was analyzed.     

高温合金GH3039铣削力实验研究

由于高温合金材料GH3039的切削加工性差,选取背吃刀量、铣削速度、每齿进给量等参数,研究其对高温合金数控铣削力的影响。利用线性回归方法建立了铣削力经验公式,并通过铣削实验得到了切削参数与铣削力的变化曲线。实证表明切削参数的选择在GH3039加工过程中的重要性。     

Deformation mechanism and quantitative characterization of Al2O3 inclusions in powder metallurgy superalloys

By means of implanting inclusions artificially, the evolution law of three-dimensional morphology and size of Al₂O₃ inclusions in FGH96 powder metallurgy (PM) superalloy during hot iso-static pressing (HIP), hot extrusion (HEX) and hot isothermal forging (HIF) process was investigated by SEM and quasi in situ Micronano-CT. The size change of inclusions during different stages was studied quantitatively, the three-dimensional (3D) morphology of the inclusions was characterized, and the deformation mechanism was proposed. The results showed that the inclusions in powder stage were long stripe or plate-like shape. During HIP, Al₂O₃ inclusions were mechanically bonded to the alloy matrix, and its chemical composition, morphology and size remained unchanged. During HEX, Al₂O₃ inclusions were broken and elongated into chain shape due to shear stress. The quantitative relationship between inclusion size after extrusion and extrusion ratio as well as original inclusion size was established. During HIF, the relationship between 3D morphology, size, orientation and deformation of a single inclusion during forging compression was quantitatively characterized by quasi in-situ micronano-CT for the first time. The above evolution law provides theoretical basis and technical support for improving the purity level of powder turbine disk.     

91211合金碳化物转变的试验研究

91211合金是结合我国资源自行设计的一种镍基铸造合金,其特点是无钻高钨,在高温下具有高强度,合金相的研究表明,合金铸态时存在MC、M_θC两种类型的碳化物,其总量为1.5％。本文应用热处理,电解萃取、化学分离方法,研究碳化物的稳定性及转变的数量关系。     

Effect of Grinding Temperatures on the Surface Integrity of a Nickel-based Superalloy

An experimental study was carried out to investigat e the influence of temperatures on workpiece surface integrity in surface grinding of a cast nickel-based superalloy with alumina abrasive wheels. Temperatur e response at the wheel-workpiece interface was measured using a grindable foil /workpiece thermocouple. Specimens with different grinding temperatures were obt ained through changing grinding conditions including depth of cut, workpiece fee d speed, and coolant supply. Changes in surface roughnes...     

Effect of the withdrawal rate on the microstructure and thermal durability of a third-generation single crystal superalloy

Single crystal Ni-based superalloys are the typical structural materials for high-pressure turbine blades, and their microstructure is critical in determining their mechanical properties. The withdrawal rate is a key parameter affecting the microstructure during the single crystal growth process. In the present work the effect of the withdrawal rate on the microstructure of a third-generation single crystal superalloy containing 6.8 ?wt% Re has been investigated, and the creep resistance of the alloy determined. The results showed that increased withdrawal rate refined the dendritic structure, reduced dendritic arm spacing, promoted the growth of secondary tertiary dendrites and decreased solidification segregation with a reduced size of γ′ phase. The porosity density of the as-cast alloy first decreased and then increased with the withdrawal rate, while the minimum porosity densityoccurred when the alloy was under the solidification condition of withdrawal rate of 4.5 ?mm/min. The maximum creep rupture life of 326.4 ?h of the heat-treated alloys under the test condition of 1100 ?°C/140 ?MPa also appeared at the alloys under the withdrawal rates of 4.5 ?mm/min. It is believed that the minimum porosity density and reduced size of the γ′ phase may be the main reasons for the enhanced creep rupture life of the alloys with withdrawal rates of 4.5 ?mm/min. This investigation provides theoretical support and a practical basis for the development of third-generation single crystal superalloys.     

Studies on thermally grown oxide as an interface between plasma-sprayed coatings and a nickel-based superalloy substrate

A thermally grown oxide layer formed by hot corrosion was investigated as an interface between plasma-sprayed coatings and a nickel-based superalloy substrate. The hot corrosion mechanism of NiCr-Cr₂O₃ and Al₂O₃-40wt% TiO₂ (A40T) plasma coated Inconel 617 was evaluated. The experiments were carried out at 1000℃ using a combination of Na₂SO₄, NaCl, and ₂O₅ salts to simulate the conditions of a gas turbine in a marine environment. The hot corrosion results revealed the spallation and dissolution of oxides upon prolonged exposure. Optical images and scanning electron micrographs of the exposed samples revealed the formation of oxide scale and provided details of its morphology in NiCr-Cr₂O₃ coated samples. Microstructure characterization of A40T coatings demonstrated a thermally grown oxide (TGO) layer at 1000℃. Increasing the thickness of the TGO layer decreased the corrosion resistance. The elemental analysis and image mapping revealed the migration of active elements from the substrate and coatings toward the corrosive environment.