A device and method for preparing clad structural metal composite materials by bidirectional extrusion
A metal composite material and coating structure technology, applied in the direction of metal extrusion dies, etc., can solve the problems of long production process, low interface strength, and difficulty in ensuring strength, and achieve low cost, strong surface bonding, and short process Effect
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Embodiment 1
[0031] A device for preparing metal composite materials with clad structures by bidirectional extrusion, comprising: a fixed bracket 1, a composite extrusion die 5, an extrusion punch 4, an extrusion cylinder 10, a forward extrusion device 3 and a reverse extrusion device 13. The composite extrusion die 5 is set between the forward extrusion device 3 and the reverse extrusion device 13 .
[0032] The forward extrusion device 3 and the reverse extrusion device 13 provide extrusion driving power.
[0033] The outer side of the composite extrusion die 5 is covered with an installation base 12 , and the installation base 12 is fixedly connected with the fixed bracket 1 .
[0034] Wherein, the installation base 12 is fixedly connected with the composite extrusion die 5 through fastening screws 2 .
[0035] One end of the composite extrusion die 5 is provided with a forward extrusion die 51 , and the other end is provided with a reverse extrusion die 52 , and the forward extrusion ...
Embodiment 2
[0042] A method for preparing clad structural metal composite materials by bidirectional extrusion. This embodiment adopts the device for preparing clad structural metal composite materials by bidirectional extrusion provided in Example 1. The method includes the following steps:
[0043] S10, putting the inner layer blank 6 and the outer layer hollow blank 9 into the forward extrusion die 51 and the reverse extrusion die 52 respectively;
[0044] S20, start the first heating device 7 and the second heating device 11;
[0045] S30, the reverse extrusion device 13 is working, and the outer layer hollow blank 9 is compressed by the extrusion cylinder 10, and then stops moving toward the direction of the extrusion punch 4;
[0046] S40, select the first extrusion punch, and the forward extrusion device 3 starts to work, extruding the inner layer blank 6 into the outer layer hollow blank 9;
[0047] S50. When the inner layer billet 6 extrudes the outer layer hollow billet 9, the ...
Embodiment 3
[0051] This example is to prepare an aluminum-clad magnesium composite bar with a magnesium alloy diameter of 30 mm and an outer layer aluminum alloy thickness of 5 mm: AZ31 magnesium alloy inner layer blank 6 with an outer diameter of 90 mm, an inner diameter hole of 30 mm, and an outer diameter of 60 mm 7050 aluminum alloy The outer layer hollow blank 9.
[0052] S10, put the AZ31 magnesium alloy inner layer billet 6 with an outer diameter of 60 mm, the outer layer billet of 7050 aluminum alloy with an inner diameter hole of 30 mm and an outer diameter of 60 mm into the forward extrusion die 51 and reverse extrusion die in the composite extrusion die respectively Into the extrusion die 52;
[0053] S20, start the first heating device 7, heat up to 400°C; start the second heating device 11, heat up to 420°C, and keep warm for 30 minutes;
[0054] S30, the reverse extrusion device 13 is working, and the 7050 aluminum alloy outer layer billet is compressed by the extrusion cylin...
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