Integral precision casting method for large thin-wall casing part

A technology of precision casting and casing parts, which is used in casting molding equipment, casting molds, cores, etc., can solve the problems of heavy parts, large waste of metal materials, long processing cycles, etc., to save metal raw materials and improve internal metallurgy. Quality, the effect of ensuring dimensional accuracy

Active Publication Date: 2011-06-15
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This casing processing and forming method occupies a large amount of production resources, the processing cycle is long, the waste of metal materials is large, the cost is high, and the weight of the parts is heavy.
[0003] The outline size of a high-tempera

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 2

[0025] (1) First, use UG rapid prototyping technology to design a wax model computer model, and then prepare a wax model according to the computer model. The temperature of the wax material is 68°C, the injection pressure is 3 MPa; the pressure holding time is 200s;

[0026] (2) Apply the paint on the surface of the wax model, and apply a total of 15 layers. The specific process parameters are: silica sol is used as the adhesive in the paint slurry, corundum powder is used as the powder for the 1st to 7th layers, and corundum powder is used as the powder for the 8th to 15th layers. Corundum powder or bauxite, 80# or 100# corundum sand for the 1st to 2nd layers, 46# or 60# corundum sand for the 3rd to 7th layers, 16 / 24 coal gangue sand for the 8th to 15th layers, dry In the self-drying time of the parameters, the 1-2 layers are dried for 24-36 hours, the 3-7 layers are dried for 24 hours, the 8-15 layers are dried for 12-24 hours, and the air-drying time of all paint layers is 4...

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PUM

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Abstract

The invention relates to the field of precision casting methods, in particular to an integral precision casting method for a large thin-wall casing part. The production cost is saved, the production period is shortened, and the thrust-weight ratio of the casing part is greatly improved. The technical scheme comprises the following steps of: designing a computer model of a wax mould, and preparingthe wax mould according to the computer model, wherein the process parameters are that: the wax material temperature is 68DEG C, the injection pressure is 2-3MPa, and the hold up time is 180-200 seconds; coating 15 layers of coatings on the surface of the prepared wax mould, spreading sand on the surface after each layer is coated, naturally drying and finally performing air drying, wherein afterthe wax mould is coated with the seventh layer of coating, the coating layer is subjected to one-time hole plugging and net suspension; after the coating is finished, dewaxing and sintering to obtaina casing part shell; casting at the temperature of between 1,550 and 1,570DEG C for 22 to 27 seconds to obtain a casing casting; and performing hot shape correction on the casing casting.

Description

technical field [0001] The invention relates to the field of precision casting methods, in particular to an integral precision casting method for a large thin-wall casing. Background technique [0002] The casing parts in aero-engines have large diameters, generally above Φ800 mm, thin walls, complex structures, and high-temperature alloys. The traditional manufacturing process of this type of parts is: use different processing technology to process each single part, and then use welding processing method to assemble and weld the whole casing. This casing processing and forming method occupies a large amount of production resources, has a long processing cycle, a large waste of metal materials, high cost, and heavy parts. [0003] The outline size of a high-temperature alloy casing casting is Φ900mm, and the main body wall thickness is 2mm. Uneven, complex structure, one-time pouring of castings, internal metallurgical quality control, and size assurance of large thin-wall...

Claims

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Application Information

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IPC IPC(8): B22C9/04B22C3/00
Inventor 屠晓林王铁军梁岩陈震杨树林
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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