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Investment casting method for duplex overall-cast directional-solidified turbine guide blades

A technology of turbine guide vanes and investment casting, which is applied in casting molding equipment, casting molds, casting mold components, etc., to achieve the effect of large relative distance of seeding structure, favorable drying consistency and uniformity, and avoiding metallurgical defects

Active Publication Date: 2019-08-02
AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to address metallurgical defects such as inclusions, looseness, miscellaneous crystals, transverse grain boundaries, outcropping grains, and crystal orientation deviations existing in the preparation process of the existing duplex integrally cast hollow turbine guide vanes, as well as dimensions such as excessive wall thickness. The problem is to provide an investment casting method for double-integrated directional solidification turbine guide blades, the purpose of which is to improve the qualified rate and production efficiency of the blades, and shorten the development and production cycle of the blades

Method used

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  • Investment casting method for duplex overall-cast directional-solidified turbine guide blades

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Embodiment 1

[0025] When preparing the ceramic core, first press and sinter a ceramic core with a shape consistent with the ceramic core, with a circumferential dimension smaller than the ceramic core's design size by 0.5mm, then pre-place it in the core mold, and press the outer shell on the outside of the cold core , After sintering, a complete ceramic core is formed; the material of the cold core is the same as the ceramic slurry used to prepare the ceramic core shell;

[0026] After the completion of the ceramic core system, the blade wax mold is pressed. The feeding bending piece 6 is a wedge block with a length of 30mm, a height of 10mm, and a thickness of 1mm to 3mm;

[0027] The thickness of the core head of the seeding section 3 is 0.5~2mm;

[0028] Exhaust side wax sheet 8 has a width of 5mm and a thickness of 3mm;

[0029] The blade body 9, the inner edge plate 10 and the outer edge plate 11 in the blade wax mold are formed by integral injection molding. The injection temperature is 63~...

Embodiment 2

[0035] Compared with Example 1, this embodiment differs as follows:

[0036] The size of the cold core is 2mm smaller than the one side of the core;

[0037] The feed bending piece (6) is a wedge block with a length of 20mm, a height of 15mm, and a thickness of 2mm to 4mm;

[0038] Exhaust side wax sheet (8) has a width of 3mm and a thickness of 2mm;

[0039] The number of coating layers for the shell is 8;

[0040] The melting and casting equipment is a vacuum induction directional solidification furnace. After the shell reaches the temperature, it is held for 30 minutes. The IC10 alloy is selected for refining at 1535°C. Then the upper heater temperature is controlled at 1480°C, the lower heater temperature is 1490°C, and the casting temperature is 1480°C. The pulling rate is 8mm / min.

[0041] After the casting is out of the furnace, the shell is cleaned with high-pressure water, and the runner is removed and corroded in an aqueous solution of ferric chloride and hydrochloric acid. Th...

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Abstract

The invention discloses an investment casting method for duplex overall-cast directional-solidified turbine guide blades. The method comprises the steps of preparation of ceramic molding cores, placement of the ceramic molding cores in shape molds for pressing of blade wax molds, coating of molding shells after mold assembly and dewaxing roasting, smelting and pouring, shell removal, core removal,and cutting of redundant gate parts. The method is simple and feasible in process, can effectively reduce such metallurgic defect rejection rates as inclusion, looseness and crystal orientation deviation of the blades, improves the casting size precision, greatly improves the product pass percent, reduces the economical loss, and cam meet large-scale production demands.

Description

Technical field [0001] The invention is an investment casting method for double-unit integral casting directional solidification turbine guide blades, belonging to the technical field of investment precision casting high-temperature alloys. Background technique [0002] The increase of the temperature in front of the turbine is crucial to the increase of the engine thrust-to-weight ratio, and the high-pressure turbine guide blades directly bear the impact of high-temperature gas, which puts forward extremely high requirements for its temperature-bearing capacity and reliability. On the one hand, the improvement in temperature bearing capacity comes from the optimization of alloy composition and microstructure. Compared with traditional equiaxed crystal blades, columnar crystals eliminate the transverse grain boundaries that are prone to cracks, which greatly improves the fatigue performance of the blades. ; On the other hand, it comes from the optimization of structural design, i...

Claims

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Application Information

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IPC IPC(8): B22C9/04B22C9/08B22C9/10B22C9/22B22C7/02
CPCB22C7/02B22C9/043B22C9/082B22C9/10B22C9/22
Inventor 杨泽南王祯张强姜华陈昊彭子超王旭青罗学军马国君
Owner AVIC BEIJING INST OF AERONAUTICAL MATERIALS