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A kind of composite coating molding preparation method of ceramic core

A technology of ceramic cores and coatings, which is applied in the direction of casting molding equipment, cores, and mold components, which can solve the problems of low efficiency, high cost, and increased casting cost and reject rate of ceramic cores, so as to ensure removability , simple method, high cost effect

Active Publication Date: 2021-12-24
东营诚扬精密机械有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, ceramic cores are mostly alumina-based or silica-based materials, and the powder particles are relatively fine (greater than 200 mesh). They are often prepared by powder mixing, slurry preparation, injection molding and sintering processes. The process is cumbersome and lengthy. , there are certain process difficulties and deficiencies, such as the core is easily deformed during the injection molding and sintering process, and the core shrinks after sintering, resulting in out-of-tolerance or unqualified dimensions, etc.
In addition, during the use process, due to the large performance difference between the ceramic core and the mold shell, the core is often bent or broken, which leads to a significant increase in the cost of castings and the scrap rate
For castings with multiple small through-hole cross-sections and large concave cavity structures, the ordinary precision casting process cannot guarantee the accurate molding of the inner cavity
The normal coating, sanding and other processes used in the literature (coating core precision casting hollow blade castings, pages 11-13, "Special Casting and Nonferrous Alloys, Issue 1, 1994") have certain limitations. , if only the inner cavity is not very narrow, it is required that the internal cooling channel of the casting must be in a straight-through shape without twists and turns, and the length of the inner cavity is short and less than 100mm, otherwise it cannot be guaranteed to coat the central part
At the same time, it is very difficult to remove the corundum type core after pouring
Castings with multiple small through-hole cross-sections and large concave cavity structures cannot be prepared using the processes in the above literature
However, the preparation of ceramic cores by injection molding has low efficiency, high cost and limited performance. Therefore, it is necessary to develop a new process to prepare such structural castings.

Method used

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  • A kind of composite coating molding preparation method of ceramic core
  • A kind of composite coating molding preparation method of ceramic core
  • A kind of composite coating molding preparation method of ceramic core

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0041] 1) The inner cavity of the casting contains multiple through holes, the diameter of the through hole is 2mm, the height of the through hole (that is, the radial distance between the two ends of the through hole) is 2mm, the maximum diameter of the concave inner cavity is 50mm, and the height of the inner cavity of the casting is 150mm. Partitioning is carried out at the largest cross-section of the inner cavity structure of the casting, and the left and right half core wax molds are prepared that are completely consistent with the shape and size of the inner cavity structure of the casting (see image 3 ), wherein the inner dimensions corresponding to the concave parts of the left and right wax molds are exactly the same as the outer structure dimensions of the ceramic core. Prepared by injection molding process, the injection pressure is 3 atmospheres, the injection time is 10 seconds, and the pressure holding time is 10 seconds.

[0042]2) prepare the core slurry coat...

Embodiment 2

[0047] 1) The inner cavity of the casting contains multiple through holes, the diameter of the through hole is 10mm, the height is 12mm, the maximum diameter of the concave inner cavity is 50mm, and the height of the inner cavity of the casting is 300mm. Partitioning is carried out at the largest cross-section of the inner cavity structure of the casting, and the left and right half core wax molds are prepared that are exactly the same as the inner cavity structure of the casting. The structural dimensions are exactly the same. Prepared by injection molding process, the injection pressure is 3 atmospheres, the injection time is 10 seconds, and the pressure holding time is 20 seconds.

[0048] 2) prepare the core slurry coating, the coating is prepared by the mixed powder of quartz glass powder and zircon powder and silica sol, wherein the mass ratio of quartz glass powder and zircon powder is 90%: 10%, the mixed powder and The mass ratio of silica sol is 80%:20%, the particle...

Embodiment 3

[0053] 1) The inner cavity of the casting contains multiple through holes, the side length of the through holes is 20mm, the height is 20mm, the maximum diameter of the concave inner cavity is 100mm, and the height of the inner cavity of the casting is 100mm. Partitioning is carried out at the largest cross-section of the inner cavity structure of the casting, and the left and right half-core wax molds are prepared that are completely consistent with the shape and size of the inner cavity structure of the casting. The shape and size of the core are exactly the same. Prepared by injection molding process, the injection pressure is 5 atmospheres, the injection time is 60 seconds, and the pressure holding time is 60 seconds.

[0054] 2) prepare the core slurry coating, the coating is prepared by the mixed powder of quartz glass powder and zircon powder and silica sol, wherein the mass ratio of quartz glass powder and zircon powder is 60%:40%, the mixed powder and The mass ratio ...

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Abstract

The purpose of the present invention is to provide a preparation process of a ceramic core and superalloy cavity structure casting, wherein the preparation process of the ceramic core is: dividing the inner cavity into left and right half cavities at the maximum section of the casting inner cavity Structure, prepare the left and right half-core wax molds that are completely consistent with the shape and size of the internal cavity structure of the casting, and the inner dimensions corresponding to the concave parts of the left and right half-core wax molds are exactly the same as the outer structure dimensions of the ceramic core; The left and right half-model cores are prepared by the precision casting process. After the half-model cores are dried, they are dewaxed and roasted. After sintering, the largest cross-sections of the left and right half-model cores are trimmed. Negative tolerances are reserved for the left and right trimmed surfaces; bonding is used The left and right half-mold ceramic cores are combined into a monolithic ceramic core, and then dried for 4-8 hours to obtain a ceramic core for superalloy castings. The method can improve the comprehensive performance of the ceramic core, simplify the preparation process and process, ensure the matching between the core and the mold shell and reduce the casting cost.

Description

technical field [0001] The invention belongs to the technical field of high-temperature alloy precision casting, and particularly provides a preparation method of a ceramic core. Background technique [0002] High-temperature alloy precision castings are widely used in power generation, power industry and other fields. Such castings usually have complex inner cavity structures, which cannot be directly produced by traditional precision casting processes. Usually, ceramic cores are used to form the inner cavity structure, and then chemical methods are used. The core is removed, and finally the cavity of the casting is formed. [0003] At present, ceramic cores are mostly alumina-based or silica-based materials, and the powder particles are relatively fine (greater than 200 mesh). They are often prepared by powder mixing, slurry preparation, injection molding and sintering processes. The process is cumbersome and lengthy. , there are certain process difficulties and deficienc...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B22C3/00B22C9/10
CPCB22C3/00B22C9/10
Inventor 刘蓬波刘亦硕隋玉华
Owner 东营诚扬精密机械有限公司
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