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A method for two-pass secondary equal channel corner cold extrusion of high strength and toughness titanium alloy

A technology of equal channel angle and tough titanium alloy, applied in the field of material processing, can solve problems such as shear fracture, reduce friction resistance, improve plastic deformation ability, and reduce interference factors.

Active Publication Date: 2019-08-30
NORTHWEST INSTITUTE FOR NON-FERROUS METAL RESEARCH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, high-strength and tough titanium alloys are prone to shear fracture at room temperature due to their large deformation resistance and high friction during equal-channel extrusion. The service state under deformation conditions is an urgent scientific problem to be solved in the current engineering application of high-strength and tough titanium alloys

Method used

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  • A method for two-pass secondary equal channel corner cold extrusion of high strength and toughness titanium alloy
  • A method for two-pass secondary equal channel corner cold extrusion of high strength and toughness titanium alloy
  • A method for two-pass secondary equal channel corner cold extrusion of high strength and toughness titanium alloy

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] This embodiment includes the following steps:

[0033] Step 1: Load the solid solution Ti-1300 alloy bar from the bottom of the 1060 industrial pure aluminum sheath and inlay it inside the 1060 industrial pure aluminum sheath to obtain an extruded billet with an arc-shaped head, such as Figure 1a and Figure 1b As shown; the size of the Ti-1300 alloy rod is: 8.7mm×8.7mm×85mm, the size of the extrusion billet is: 12.7mm×12.7mm×90mm; the room temperature of the Ti-1300 alloy rod The yield strength is 1310MPa, the tensile strength is 1370MPa, the elongation is 17%, and the fracture toughness is 55MPa m 1 / 2 ;

[0034] Step 2. Spread the lubricant evenly on the surface of the extruded billet obtained in Step 1, then let it stand in the air for 1 hour, then wrap it with graphite paper, put it into a channel with a corner angle of 90° and a corner arc of 20°, etc. channel in an angular extrusion die; the lubricant consists of graphite milk and MoS 2 Prepared by magnetic st...

Embodiment 2

[0042] This embodiment includes the following steps:

[0043] Step 1. Load the annealed Ti-1300 alloy bar from the bottom of the T2 industrial pure copper sheath and inlay it inside the T2 industrial pure copper sheath to obtain an extruded billet with an arc-shaped head, such as Figure 1a and Figure 1b As shown; the size of the Ti-1300 alloy rod is: 8.7mm×8.7mm×85mm, the size of the extrusion billet is: 12.7mm×12.7mm×90mm; the room temperature of the Ti-1300 alloy rod The yield strength is 1039MPa, the tensile strength is 1078MPa, the elongation is 20.5%, and the fracture toughness is 72MPa m 1 / 2 ;

[0044] Step 2. Spread the lubricant evenly on the surface of the extruded billet obtained in Step 1, then let it stand in the air for 2 hours, then wrap it with graphite paper, and put it into a channel with a corner angle of 90° and a corner arc of 20°, etc. channel in an angular extrusion die; the lubricant consists of graphite milk and MoS 2 It is prepared by magnetic sti...

Embodiment 3

[0048] This embodiment includes the following steps:

[0049] Step 1: Load the annealed Ti-1300 alloy bar from the bottom of the 1060 industrial pure aluminum sheath and inlay it inside the 1060 industrial pure aluminum sheath to obtain an extruded billet with an arc-shaped head, such as Figure 1a and Figure 1b As shown; the size of the Ti-1300 alloy rod is: 8.7mm×8.7mm×85mm, the size of the extrusion billet is: 12.7mm×12.7mm×90mm; the room temperature of the Ti-1300 alloy rod The yield strength is 1039MPa, the tensile strength is 1078MPa, the elongation is 20.5%, and the fracture toughness is 72MPa m 1 / 2 ;

[0050] Step 2: Spread the lubricant evenly on the surface of the extruded billet obtained in Step 1, then let it stand in the air for 3 hours, then wrap it with graphite paper, put it into a channel with a corner angle of 90° and a corner arc of 20°, etc. channel in an angular extrusion die; the lubricant consists of graphite milk and MoS 2 Prepared by magnetic stirr...

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Abstract

The invention discloses a method for two-pass equal channel angular cold extrusion on high strength and toughness titanium alloy. The method comprises the following steps: one, placing the high strength and toughness titanium alloy in a sheath from the bottom of the sheath and embedding the high strength and toughness titanium alloy in the sheath to obtain an extrusion blank; two, uniformly smearing the surface of the extrusion blank with a lubricating agent, standing and then wrapping the extrusion blank with graphite paper, and placing the extrusion blank in an equal channel angular extrusion die; and three, carrying out two-pass cold extrusion on the extrusion blank which is placed in the equal channel angular extrusion die under the condition of the room temperature, then taking out the extrusion blank, and removing the sheath and the graphite paper to obtain the extruded high strength and toughness titanium alloy. According to the method, the high strength and toughness alloy is placed in the sheath to form a semi-sheath structure, the lubricating agent smears the semi-sheath structure, two-pass equal channel angular cold extrusion is carried out at the room temperature, frictional resistance in a cold extrusion process is relieved, plastic deformation capability of the high strength and toughness alloy is improved, shearing and breakage of the high strength and toughnesstitanium alloy in a shearing process is avoided, and the service condition of the high strength and toughness titanium alloy under the shearing effect is researched favorably.

Description

technical field [0001] The invention belongs to the technical field of material processing, and in particular relates to a two-pass secondary equal-channel corner cold extrusion method for high-strength and tough titanium alloys. Background technique [0002] Due to its high specific strength, good fracture toughness, high hardenability, excellent thermal processing performance and machining performance, high-strength titanium alloy meets the requirements of high structural efficiency and high reliability structural parts of aerospace materials. , is an ideal metal structure material. High-strength and tough titanium alloys are currently mainly used in aerospace and aerospace fields that require high-strength and high-toughness load-bearing components, especially aerospace vehicles, aero-engines, and high-tech weapons and equipment. The main structural material for aircraft carrier catapults and car armor. In recent years, with the rapid development of the aviation industr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21C23/00B21C23/32
Inventor 卢金文张伟赵永庆霍望图张于胜
Owner NORTHWEST INSTITUTE FOR NON-FERROUS METAL RESEARCH