Forming and composite preparation method and device of a clad magnesium alloy multilayer structure

A multi-layer structure, magnesium alloy technology, applied in metal processing equipment, manufacturing tools, metal processing, etc., can solve the problems of serious layer interface cracking of multi-layer structural parts, decline in the formability of composite plates, and low quality of parts. High interface strength, improved efficiency, and good corrosion resistance

Active Publication Date: 2021-07-13
TAIYUAN UNIV OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

These three methods can successfully produce other metal-clad magnesium alloy composite panels, but hard and brittle intermetallic compounds will be formed at the interface, which will reduce the formability of the composite panel during subsequent processing and easily cause interlayer cracking.
Therefore, the process of preparing the composite plate first and then forming the parts is not only complicated, but also has large energy consumption, low production efficiency, high production cost, and the layer interface of the formed multi-layer structure is severely cracked, and the quality of the parts is not high.

Method used

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  • Forming and composite preparation method and device of a clad magnesium alloy multilayer structure
  • Forming and composite preparation method and device of a clad magnesium alloy multilayer structure
  • Forming and composite preparation method and device of a clad magnesium alloy multilayer structure

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preparation example Construction

[0039] A method for forming and compounding a coated magnesium alloy multilayer structure, comprising the following steps:

[0040]Step 1. Cut the magnesium alloy and clad alloy plates with a shearing machine or a wire cutting machine. The thickness, size and shape of the magnesium alloy and clad alloy plates are determined by the wall thickness, shape and size of the prepared parts. Magnesium alloys The thickness of the plate is generally less than 5mm, and the size and shape are not limited. The thickness of the cladding alloy plate is less than that of the magnesium alloy plate, and the size and shape are the same as the magnesium alloy plate;

[0041] The clad alloy plate includes one or more of aluminum alloy plate, titanium alloy plate, steel plate, nickel alloy plate, copper alloy plate and the like.

[0042] Step 2: Perform surface treatment on the trimmed magnesium alloy and the clad alloy plate, remove the oxide skin on the contact surface of the trimmed magnesium al...

Embodiment 1

[0058] combine Figure 1 to Figure 4 To illustrate this embodiment, the method for integrating the auxetic forming and compounding of the aluminum-clad magnesium box-shaped solid particle medium in this embodiment includes the following steps:

[0059] Step 1. According to the geometric size and performance requirements of the formed component, the selected magnesium alloy plate is AZ31 with a thickness of 2mm. In order to improve the corrosion resistance of the component, the cladding plate is an anti-rust aluminum alloy 5052 plate with a thickness of 0.5mm. Component geometry is determined.

[0060] Step 2. Use an electric wire brush to remove the oxide skin on the surface of the cut AZ31 and 5052 plates that are in contact with each other, so that the fresh substrate is exposed on the surface to promote the diffusion and bonding of the two;

[0061] Step 3. Put the AZ31 board in the middle, and put the 5052 board on the upper and lower sides of the AZ31 board to stack them...

Embodiment 2

[0068] A method for forming and compounding a coated magnesium alloy multilayer structure, comprising the following steps:

[0069] Step 1. According to the geometric size and performance requirements of the formed component, the selected magnesium alloy plate is AZ31 with a thickness of 5mm. In order to improve the corrosion resistance of the component, the cladding plate is a titanium alloy plate with a thickness of 1mm. The size of the plate is determined by the geometric size of the component .

[0070] Step 2. Use an electric wire brush to remove the oxide skin on the surface of the trimmed magnesium alloy and titanium alloy plates that are in contact with each other, so that the fresh substrate is exposed on the surface, so as to promote the diffusion and bonding of the two;

[0071] Step 3. Put the magnesium alloy plate in the middle, and stack the titanium alloy plate on the upper and lower sides of the magnesium alloy plate, place between the die and the barrel, and c...

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Abstract

The invention discloses a method and device for forming and compounding a clad magnesium alloy multilayer structural part. The steps are as follows: performing surface treatment on magnesium alloy and other alloy plates, stacking them alternately, and putting them between a die and a barrel , and apply blankholder force to the barrel; fill the barrel with an appropriate amount of solid particles as the pressure transmission medium; the press drives the pressure head to apply a certain pressure on the solid particle medium, and heats the mold and the blank to a certain temperature; the multi-layer board Forming under the action of pressure transmission of solid particle medium; heat preservation and pressure holding for a certain period of time to realize diffusion connection between multi-layer boards, open the mold, and obtain other metal-clad magnesium alloy multi-layer structural parts. Compared with the traditional method of preparing multi-layer composite boards first and then forming the composite boards, this invention saves the preparation process of composite boards and can avoid problems such as cracking between layers of composite boards, thereby significantly improving the quality and production of multi-layer structural parts efficiency and greatly reduce production costs.

Description

technical field [0001] The invention discloses a method and device for forming and compounding a clad magnesium alloy multilayer structural part, belonging to the technical field of composite plate forming. Background technique [0002] The poor corrosion resistance of magnesium and magnesium alloys is one of the main factors limiting their wide application. In order to improve its corrosion resistance, it can be modified on the surface. Commonly used methods include chemical conversion coating, anodic oxidation, vapor deposition, laser cladding, thermal spraying, etc. However, these methods require special equipment, and the process is complicated and the production cost is relatively high. In contrast, other metals such as aluminum and aluminum alloys usually have better corrosion resistance and plastic formability, and the surface is repairable and modifiable. Therefore, coating a layer of other alloys with good corrosion resistance on the surface of magnesium alloy pro...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21D22/10B23K20/02B23K20/22B23K20/24B23K20/26B23K101/18B23K103/18
CPCB21D22/10B23K20/023B23K20/22B23K20/24B23K20/26B23K2101/18B23K2103/18
Inventor 林鹏崔晓磊张晶
Owner TAIYUAN UNIV OF TECH
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