2090 results about "Precision casting" patented technology

The present invention relates to a fusible pattern precision casting process for producing automobile H-shaped front axle. Said casting process includes the following steps; (1), preparing wax pattern; (2), applying coating material onto the wax pattern surface for several times, spreading sand and making the coating material hardened pattern shell be primarily formed, removing wax and forming pattern shell; (3), firing pattern shell; (4), pouring the molten steel into the pattern shell, before steel-smelting having to make analysis of charge mixture ratio, in the course of smelting steel having to make on-the-spot sample analysis and furnace rear analysis, adding required additive and deoxidant so as to make the molten steel be reached to the defined chemical components requirement; (5), removing pattern shell from obtained automobile H-shaped front axle casting, cleaning sand and cutting spure; (6), grinding, finishing and checking casting; (7), making quenching and tempering, heat treatment; (8), making correction and shot blasting treatment; and (9), making metalworking treatment.

A weight member for a golf club head is made of a WMoNi alloy by powder metallurgy or a precision casting process. The WMoNi alloy includes tungsten 1-70 wt %, molybdenum 4-55 wt %, and nickel 25-95 wt %. Molybdenum increases the density of the weight member and improves the rust-resisting property of the weight member. The tungsten, molybdenum, and nickel provide a uniform metallographic phase. Uniformity of shining finishing of the weight member is thus improved.

An antigravitational casting technology includes putting a lost mould in a bottom running type sand box, adding sand, vibration compacting, loading molten MgAl alloy in filler while introducing protecting gas, introducing the pressure controllable inertial gas to the filler, and pouring the molten alloy into said sand box to gasify said list mould. Its apparatus is composed of filler, sand box, pouring pipe, crucible in the filler, and heating coil surrounding said pouring pipe. It is suitable for precision casting.

The invention discloses a manufacturing method and a fixture of an integral bladed-disk wax mold. According to the invention, an integral bladed-disk wax pattern is divided into single blades and a disk shaft. Processes of separated pressing, precise fixture positioning and wax mold welding assembling are adopted. The integral wax pattern is precisely cast. According to the invention, the disk shaft is fixed on an assembling fixture; the blades are sequentially positioned on positioning points on the fixture, and are welded onto the disk shaft. Blade bodies and channel inner walls with high precisions are adopted in the positioning of the blades, such that good consistency is provided for the blades. When the wax pattern is assembled, positioning points are positioned on the blade bodies;blade body positioning points are consistent with processing positioning points, primary standards of cold and hot processing are consistent, such that blade dimensional precision of the whole cast is optimally improved, throat areas between blades are ensured, and flow rate homogeneity is ensured. Positioning parts of the fixture can be adjusted according to measured dimensions of parts, such that the volume of flow rate can be changed according to directional positions of angles of the blades. Therefore, repairing or even rejecting risks caused by unqualified integral mold dimensions are avoided, production period is saved, and production cost is reduced. With the method provided by the invention, hard processes are turned easy, product precision is improved, and production efficiency is improved.

A parametric machining method of air film cooling holes for precision casting turbine blades relates to turbine blades. The method provides errors including casting deformation of components, positioning errors of clamps, and blade movement and deformation during small hole machining so as to achieve parametric accurate machining of hollow turbine blade air film holes. Through solving and calculating propagation and accumulation of error during air film machining, correcting design parameters of air film holes and processing the air film holes according to air film hole shape and location parameters which are the center point of the film hole, the normal of the film hole, and the hole depth of the air film hole after correction, the processing accuracy of the air film holes is increased and the cooling efficiency of turbine blades is increased. This method has important theoretical significance and application value for precise forming of hollow turbine blade, avoids the present situation of air cooling efficiency reduction in the field of air film hole processing, ensures the precision of air film hole forming and achieves the air cooling effect consistent with the design requirements.