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
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[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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