A processing method for thin-wall special-shaped metal castings

A special-shaped metal and casting technology, which is applied in the field of casting processing, can solve the problems of uneven wall thickness and out-of-tolerance profile of products

Active Publication Date: 2021-08-17
HUBEI SANJIANG AEROSPACE GRP HONGYANG ELECTROMECHANICAL
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The embodiment of the present application provides a processing method for thin-walled special-shaped metal castings, which solves the technical problems of the existing overall molding processing method for thin-walled special-shaped metal castings, such as excessive contour and uneven wall thickness.

Method used

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  • A processing method for thin-wall special-shaped metal castings
  • A processing method for thin-wall special-shaped metal castings
  • A processing method for thin-wall special-shaped metal castings

Examples

Experimental program
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experiment example 1

[0141] Such as figure 2 As shown, it is a schematic view of the structure of an aluminum alloy casting with a cross-sectional dimension of 1170×821 and an axial dimension of 1200 mm, which is integrally cast and processed from aluminum alloy. The figure includes the end 1 of the aluminum alloy casting, the inner cavity 2 of the aluminum alloy casting and the shell 3 of the aluminum alloy casting, wherein the end 1 of the aluminum alloy casting includes a half end face, an end face connecting hole, a high-precision hole system and an end face.

[0142] Such as image 3 shown, for figure 2 A schematic diagram of the local structure of the inner cavity of the aluminum alloy casting, which includes: the inner cavity surface 21 of the aluminum alloy casting and the inner cavity mounting part 22 of the aluminum alloy casting, and the inner cavity surface 21 of the aluminum alloy casting has multiple inner nets of different sizes Grid curved surface, its thickness is 2.5mm ~ 3.5m...

experiment example 2

[0188] Such as figure 2 As shown, it is a schematic view of the structure of an aluminum alloy casting with a cross-sectional dimension of 1170×821 and an axial dimension of 1200 mm, which is integrally cast and processed from aluminum alloy. The figure includes the end 1 of the aluminum alloy casting, the inner cavity 2 of the aluminum alloy casting and the shell 3 of the aluminum alloy casting, wherein the end 1 of the aluminum alloy casting includes a half end face, an end face connecting hole, a high-precision hole system and an end face.

[0189] Such as image 3 shown, for figure 2 A schematic diagram of the local structure of the inner cavity of the aluminum alloy casting, which includes: the inner cavity surface 21 of the aluminum alloy casting and the inner cavity mounting part 22 of the aluminum alloy casting, and the inner cavity surface 21 of the aluminum alloy casting has multiple inner nets of different sizes Grid curved surface, its thickness is 2.5mm ~ 3.5m...

experiment example 3

[0234] Such as figure 2 As shown, it is a schematic view of the structure of an aluminum alloy casting with a cross-sectional dimension of 1170×821 and an axial dimension of 1200 mm, which is integrally cast and processed from aluminum alloy. The figure includes the end 1 of the aluminum alloy casting, the inner cavity 2 of the aluminum alloy casting and the shell 3 of the aluminum alloy casting, wherein the end 1 of the aluminum alloy casting includes a half end face, an end face connecting hole, a high-precision hole system and an end face.

[0235] Such as image 3 shown, for figure 2 A schematic diagram of the local structure of the inner cavity of the aluminum alloy casting, which includes: the inner cavity surface 21 of the aluminum alloy casting and the inner cavity mounting part 22 of the aluminum alloy casting, and the inner cavity surface 21 of the aluminum alloy casting has multiple inner nets of different sizes Grid curved surface, its thickness is 2.5mm ~ 3.5m...

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Abstract

The invention discloses a processing method of a thin-walled special-shaped metal casting. The method is first integrally cast and formed, and then performs machining of the outline, end and inner cavity installation parts of the casting blank according to the subsequent steps. , There are corresponding machining allowances in the process of rough machining, semi-finishing machining and finishing machining, and after each machining, the machining benchmark is adjusted in time according to the uniformity of wall thickness, and the process pin hole is reprocessed on the machine tool, Complete the physical correction of the machining benchmark. Therefore, for thin-walled special-shaped metal castings with large dimensions, the cumulative error of subsequent processing caused by small offsets can be eliminated as much as possible during the processing process, and the contour can be guaranteed while ensuring that the end and inner cavity mounting parts are processed in place. Contour, and can also ensure the uniformity of wall thickness.

Description

technical field [0001] The invention relates to the technical field of casting processing, in particular to a processing method for thin-wall special-shaped metal castings. Background technique [0002] In the aerospace manufacturing industry, large-sized, thin-walled, and special-shaped parts are often encountered. For large-sized, thin-walled, special-shaped parts, compared with the traditional skeleton + skin processing method, casting plus machining The overall molding method has the advantages of less material removal, pre-release of deformation, high processing efficiency, and less manual work. For example, currently common thin-walled special-shaped aluminum alloy castings are first formed by integral casting of aluminum alloy, and then the contour, end face, assembly surface, and assembly hole are machined through machining, and finally the formed product is obtained. [0003] However, there are still technical problems such as unqualified profile of the processed p...

Claims

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Application Information

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Patent Type & AuthorityPatents(China)
IPC IPC(8): B23P15/00
CPCB23P15/00
Inventor郭玉张守明邵峰
OwnerHUBEI SANJIANG AEROSPACE GRP HONGYANG ELECTROMECHANICAL