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A method for manufacturing an ultra-long thin-walled aluminum alloy sandwich rib double-skin integral empennage

A manufacturing method and aluminum alloy technology, applied in the field of mechanical processing and manufacturing, can solve problems such as poor quality stability of structural castings and imperfect precision casting molding methods, and achieve the effects of shortening the manufacturing cycle, reducing manufacturing costs, and ensuring overall quality

Active Publication Date: 2020-01-21
HUBEI SANJIANG AEROSPACE GRP HONGYANG ELECTROMECHANICAL
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In the prior art, the precision casting molding method of the super-long thin-walled aluminum alloy sandwich grid rib double-skin integral empennage is not perfect, and the quality stability of the produced structural castings is poor

Method used

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  • A method for manufacturing an ultra-long thin-walled aluminum alloy sandwich rib double-skin integral empennage
  • A method for manufacturing an ultra-long thin-walled aluminum alloy sandwich rib double-skin integral empennage
  • A method for manufacturing an ultra-long thin-walled aluminum alloy sandwich rib double-skin integral empennage

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Embodiment Construction

[0063] The embodiment of the present application improves the quality and precision of the product by providing a manufacturing method of an ultra-long thin-walled aluminum alloy sandwich grid rib double-skin integral empennage.

[0064] In order to better understand the above technical solutions, the above technical solutions will be described in detail below in conjunction with the accompanying drawings and specific implementation methods. It should be understood that the embodiments of the present invention and the specific features in the embodiments are detailed descriptions of the technical solutions of the present application. , rather than limiting the technical solutions of the present application, the embodiments of the present application and the technical features in the embodiments can be combined without conflict.

[0065] see figure 1 , a method for manufacturing an ultra-long thin-walled aluminum alloy sandwich rib double-skin integral empennage, comprising:

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Abstract

The invention belongs to the technical field of mechanical processing and manufacturing, and discloses a method for manufacturing a super-long thin-walled aluminum alloy sandwich grid rib double-skin integral tail, comprising: adopting ZL205AA high-strength aluminum alloy to form the integral tail; The integral tail is heat treated; the heat treated integral tail is processed by numerical control. The manufacturing method of the super-long thin-walled aluminum alloy sandwich grid rib double-skin integral empennage provided by the present invention can improve the overall quality of precision molding and manufacturing, reduce the manufacturing cost and shorten the manufacturing cycle.

Description

technical field [0001] The invention relates to the technical field of mechanical processing and manufacturing, in particular to a method for manufacturing an ultra-long thin-walled aluminum alloy sandwich grid rib double-skin integral empennage. Background technique [0002] Sandwich grid rib double-skin integral empennage is an important structural casting. The length specifications of this type of casting are mostly large and super long, and have high requirements for rigidity and processing precision. [0003] In the prior art, the precision casting molding method of the super-long thin-walled aluminum alloy sandwich grid rib double-skin integral empennage is not perfect, and the quality stability of the produced structural casting is poor. Therefore, it is necessary to improve the existing technology and design a precision casting molding method for an ultra-long thin-walled aluminum alloy sandwich grid rib double-skin integral tail that can make the quality and precisi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P15/00
CPCB23P15/00
Inventor 王华侨王春艳张权冯四伟冯凯李玉胜赵连君翟虎王宇飞赵华军肖星雨
Owner HUBEI SANJIANG AEROSPACE GRP HONGYANG ELECTROMECHANICAL
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