Preparation method of precision-investment casting single-crystal high-temperature alloy thin-wall sample

A technology of investment precision casting and high-temperature alloys, which is applied in casting molding equipment, single crystal growth, single crystal growth, etc., can solve the problems of reduced fluidity, reduced shell collapse, bending and warping, etc. The effect of crystallization occurrence rate, reduction of solidification residual stress, and improvement of fluidity

Active Publication Date: 2016-10-12
AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the wax mold preparation process, when the thickness of the pressed wax mold is less than 1mm, the strength of the wax mold is low. If there is no core support, the wax mold is easily deformed during the process of taking out from the mold, trimming, and shell coating, resulting in The finally prepared single crystal superalloy precision cast thin-walled sample has large deformation, even bending and warping, which cannot meet the requirements of parallelism and coaxiality for the thin-walled sample in the mechanical performance test; in the process of shell preparation, Although increasing the number of coating layers is beneficial to improve the high temperature strength of the shell, too many coating layers will significantly reduce the collapse of the shell and increase the solidification residual stress of thin-walled samples. Recrystallization is easy to occur during the process, resulting in the scrapping of precision cast thin-walled samples; during the directional solidification process, when the temperature of the upper and lower heaters is low and the holding time of the mold shell is too short, the flow of the alloy metal liquid in the mold shell Insufficient pouring and under-casting of thin-walled samples are prone to occur, and when the pulling speed control is unreasonable, thin-walled samples are prone to defects such as miscellaneous crystals and large-angle grain boundaries

Method used

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  • Preparation method of precision-investment casting single-crystal high-temperature alloy thin-wall sample

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Experimental program
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Effect test

Embodiment approach

[0016] The preparation process of the invention is core preparation→wax mold pressing→wax mold machining thinning→model shell preparation→directional solidification.

[0017] Using the ceramic core as support, put the plate-shaped ceramic core into the mold, close the mold, inject wax into the mold, and form a certain wax pattern on both sides of the plate-shaped ceramic core to make the wax pattern tight. Attached to the surface of the ceramic core, according to the thickness of the designed thin-walled sample, the wax model of the thin-walled sample is prepared by milling and thinning the wax model. Thin-walled sample wax molds are formed into modules, and then shells are coated to prepare mold shells, and directional solidification casting is completed in a vacuum induction single crystal furnace. Since the ceramic core is used as a support to thin the wax pattern by machining and increase the temperature control during the directional solidification process, the deformatio...

Embodiment 1

[0029] Prepare a plate-shaped ceramic core of 25mm×5mm×150mm, put the core into the ceramic core die of the single crystal superalloy thin-wall sample wax mold pressing mold, close the mold, and align the wax injection port of the mold with the wax pressure Machine injection nozzle, inject wax into the mold, set the wax temperature to 65°C, wax injection pressure 8bar, pressure holding time 70s, and press the wax to the two sides of the plate-shaped ceramic core to make the wax tightly Attached to the surface of the ceramic core.

[0030] Put the pressed wax pattern on the special fixture, according to the thickness of the designed thin-walled sample, use the CNC machine tool to machine and thin the wax pattern, control the spindle speed to 5000r / min, the feed speed to 280mm / min, and the axial The cutting depth is 0.3mm, and the thickness of the wax after thinning is 0.5mm. Trim thinned thin-walled sample wax molds to remove wax chips and burrs generated during machining, and...

Embodiment 2

[0035] Prepare a plate-shaped ceramic core with a size of 25mm×5mm×150mm, put the core into a wax mold of a thin-walled sample of a single crystal superalloy, press the mold, and set the wax temperature at 70°C and the wax injection pressure 5bar, holding time 120s, press the wax to the two sides of the plate-shaped ceramic core, so that the wax is closely attached to the surface of the ceramic core.

[0036] Use CNC machine tools to machine and thin the wax pattern, control the spindle speed to 1000r / min, the feed speed to 45mm / min, and the axial cutting depth to 0.05mm. The thickness of the wax after thinning is 1.5mm. The sample wax models form a group, and the number of sand-hanging layers of the thin-walled sample model shell is 5 layers.

[0037] Directional solidification pouring of single crystal superalloy precision casting thin-walled samples is carried out in a vacuum induction single crystal furnace. The temperature of the upper heater is set to 1540 °C, the temper...

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Abstract

The invention relates to a preparation method of a precision-investment casting single-crystal high-temperature alloy thin-wall sample. In the wax mould preparation process, a plate-shaped ceramic core is put into a mould, and the ceramic core is used as a support of wax; the mould is closed, the wax is injected into the mould, the injection pressure of the wax ranges from 5 bar to 8 bar, the temperature of the wax ranges from 60 DEG C to 80 DEG C, and the pressure maintaining time ranges from 60 s to 120 s; and wax moulds of a certain thickness are formed on the two sides of the plate-shaped ceramic core, and the wax moulds are closely attached to the surface of the ceramic core. According to the thickness of the designed thin-wall sample, the wax moulds on the two sides of the ceramic core are thinned, the rotating speed of a spindle is controlled to range from 500 r/min to 6,000 r/min, the feed speed is controlled to range from 30 mm/min to 450 mm/min, and the axial cutting depth is controlled to range from 0.03 mm to 0.5 mm. The wax moulds of the thin-wall sample are prepared, after a mould set is formed by the wax moulds of the thin-wall sample, a shell is prepared through shell coating, directional solidification pouring is completed in a vacuum induction single crystal furnace, and therefore the single-crystal high-temperature alloy precision casting thin-wall sample is prepared. According to the preparation method, the problems of short run and undercasting of the wax moulds in the deformation and directional solidification process in the mould pick-up and finishing process can be completely avoided.

Description

technical field [0001] The invention relates to a method for preparing a thin-walled sample of a single-crystal superalloy by investment casting precision casting. Background technique [0002] With the continuous improvement of the thrust-to-weight ratio (power-to-weight ratio) of aviation gas turbine engines, the temperature in front of the turbine is getting higher and higher, which makes the inner cavity structure design of single crystal superalloy air-cooled turbine blades more complex, and the blade wall thickness is getting thinner and thinner. And adopt thin trailing edge structure to reduce aerodynamic loss. Whether the performance of the single crystal superalloy will change under the condition of thin-walled structure, whether it can reach the performance of the standard sample, that is, whether the single crystal superalloy has a thin-wall effect, this is important for the reliability design and performance of single crystal superalloy turbine blades. Long life...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B22D27/04B22C9/04C30B11/00C30B29/52
CPCB22C9/04B22D27/045C30B11/00C30B29/52
Inventor 杨亮李嘉荣韩梅刘世忠赵金乾
Owner AVIC BEIJING INST OF AERONAUTICAL MATERIALS
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