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Rib titanium alloy hollow structural part and preparation method thereof

A hollow structure, titanium alloy technology, applied in building elements, sheets/boards, weight reduction, etc., to achieve the effect of small deformation and easy control

Active Publication Date: 2021-08-20
AVIC BEIJING AERONAUTICAL MFG TECH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] In order to solve the problems existing in the manufacture of the existing superplastic forming / diffusion bonding preparation method of the hollow sandwich structure of titanium alloy high ribs
A preparation method and structural parts of ribbed titanium alloy hollow structural parts are proposed

Method used

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  • Rib titanium alloy hollow structural part and preparation method thereof
  • Rib titanium alloy hollow structural part and preparation method thereof
  • Rib titanium alloy hollow structural part and preparation method thereof

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Embodiment Construction

[0033] The present invention will be described below in conjunction with the accompanying drawings, but it is not used to limit the scope of the present invention.

[0034] see figure 1 It is a flow chart of a method for preparing a ribbed titanium alloy hollow structural part of the present invention, including:

[0035] S1: The upper panel, the lower panel, the upper core plate and the lower core plate are preformed by the superplastic forming method, and the ribs are processed by the numerical control processing method.

[0036] In order to avoid ribs from breaking during the forming process, two outer skin structures (ie, upper panel and lower panel) are superplastically formed. Then two core plates are formed by superplastic forming, and the ribs are processed by numerical control, but the height of the ribs is lower than the height of the ribs after actual forming.

[0037] S2: Pickling the upper panel, lower panel, upper and lower core panels, and ribs to remove surfa...

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Abstract

An embodiment of the invention provides a preparation method of a rib titanium alloy hollow structural part. The method comprises the steps that an upper core plate, a lower core plate and ribs are designed, the space of the upper core plate, the lower core plate and the ribs is filled with BaCl2, after combined welding, the upper core plate, the lower core plate and the ribs are placed in the space of an upper panel and a lower panel, wherein the lower panel and the lower core plate are basically attached, and when diffusion connection between the core plates and the ribs is carried out, the upper core plate cannot collapse, and the ribs cannot be bent. Furthermore, in the superplastic forming process of the upper core plate, deformation is small, the height of the ribs can be adjusted to conveniently control the superplastic deformation amount of the upper core plate, and the circumstance that the core plates are broken due to the fact that forming limit is exceeded cannot occur, so that titanium alloy hollow structures with various heights can be formed as long as mold and equipment conditions are allowed.

Description

technical field [0001] The invention relates to the technical field of metal plastic forming, in particular to a method for preparing a rib titanium alloy hollow structural part and the structural part. Background technique [0002] When the superplastic forming / diffusion bonding process is used to prepare the four-layer titanium alloy hollow sandwich structure, when the height of the ribs is high, it is easy to cause the core plate to break during the forming process due to the large local deformation of the core plate when the height of the ribs is high. The structural parts of the ribs, and the higher the ribs, the more difficult the forming technology is, and some even cannot be formed at all. In order to solve this problem, the only way is to optimize the forming process, but the degree of improvement is limited. Therefore, the superplastic forming / diffusion bonding process is limited in the preparation of high-rib structural parts, and it is generally impossible to fo...

Claims

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Application Information

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IPC IPC(8): B23P15/00F16S1/10
CPCB23P15/00F16S1/10Y02T50/40
Inventor 李志强赵冰陈福龙
Owner AVIC BEIJING AERONAUTICAL MFG TECH RES INST
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