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Method for obtaining fine and fully lamellar structure of β-type γ-tial-based alloy

A base alloy and full-lamellar technology, which is applied in the field of obtaining fine full-lamellar structures in β-type γ-TiAl-based alloys, can solve the problem of low alloy plasticity, achieve high alloy plasticity, uniform distribution, and improve alloy performance.

Active Publication Date: 2018-03-09
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

This method uses high-temperature cyclic heat treatment to obtain fine and uniform full-lamellar structures, which solves the disadvantages of low plasticity of the alloy caused by ordinary heat treatment that is difficult to obtain fine full-lamellar structures. The size of the layer grain group improves the room temperature plasticity of the alloy and provides a theoretical basis for the practical application of the alloy

Method used

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  • Method for obtaining fine and fully lamellar structure of β-type γ-tial-based alloy
  • Method for obtaining fine and fully lamellar structure of β-type γ-tial-based alloy
  • Method for obtaining fine and fully lamellar structure of β-type γ-tial-based alloy

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Experimental program
Comparison scheme
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Embodiment 1

[0029] The chemical composition of the β-type γ-TiAl-based alloy used in this embodiment is calculated according to atomic percentage: Al 45%, Ta 3.0%, W 0.2%, Cr 2%, and the balance is Ti, and the β-type γ-TiAl-based alloy is Phase transition temperature T 1 is 1283°C, the eutectoid point temperature T 2 The temperature is 1190°C; the ingot is smelted by the vacuum self-consumption three-time melting process, and then the ingot is extruded to obtain the processed β-type γ-TiAl-based alloy rod, along the 1 / 2 radius of the cross-section of the rod Cut out a sample of 8mm×8mm×8mm, and process the sample as follows:

[0030] Step 1. Place the β-type γ-TiAl-based alloy sample in a heat treatment furnace, heat-preserve it at 1288°C for 20 minutes, cool the furnace to 1070°C, take out the alloy sample and air-cool it to room temperature;

[0031] Step 2. Place the β-type γ-TiAl-based alloy sample that was air-cooled to room temperature in step 1 in a heat treatment furnace, heat-t...

Embodiment 2

[0040] Adopt the β-type γ-TiAl based alloy bar of the processing state identical with embodiment 1, cut out the sample of 10mm * 10mm * 10mm along the 1 / 2 radius place of bar cross section, this sample is carried out as follows:

[0041] Step 1. Place the β-type γ-TiAl-based alloy sample in a heat treatment furnace, heat-preserve it at 1283°C for 30 minutes, cool the furnace to 1030°C, take out the alloy sample and air-cool it to room temperature;

[0042] Step 2. Place the β-type γ-TiAl-based alloy sample that was air-cooled to room temperature in step 1 in a heat treatment furnace, heat-treat it at 1190°C for 20 minutes, and take it out and air-cool it to room temperature;

[0043] Step 3. According to the method of step 2, repeat the heat preservation heat treatment and air cooling of the β-type γ-TiAl-based alloy sample that was air-cooled to room temperature in step 2 for 3 times, and then place it in a heat treatment furnace for heat preservation and heat treatment at 128...

Embodiment 3

[0048] Adopt the β-type γ-TiAl based alloy bar of the processing state identical with embodiment 1, cut out the sample of 15mm * 15mm * 15mm along the 1 / 2 radius place of bar cross section, this sample is carried out as follows:

[0049] Step 1. Place the β-type γ-TiAl-based alloy sample in a heat treatment furnace, heat-preserve it at 1278°C for 30 minutes, cool the furnace to 1030°C, take out the alloy sample and air-cool it to room temperature;

[0050] Step 2. Place the β-type γ-TiAl-based alloy sample that was air-cooled to room temperature in step 1 in a heat treatment furnace, heat-treat it at 1185°C for 20 minutes, and take it out and air-cool it to room temperature;

[0051] Step 3. According to the method of step 2, repeat heat preservation and heat treatment and air cooling of the β-type γ-TiAl-based alloy sample in step 2 to room temperature for 3 times, and then place it in a heat treatment furnace for heat preservation and heat treatment at 1283°C for 10 minutes ...

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Abstract

The invention discloses a method for obtaining a small fully lamellar structure by using beta type gamma-TiAl-based alloy. The method comprises the following steps of 1. putting beta type gamma-TiAl-based alloy into a thermal treatment furnace for heat insulation thermal treatment, taking out the beta type gamma-TiAl-based alloy after the furnace is cooled to 1030-1070 DEG C, and performing air cooling until reaching room temperature; 2. putting the beta type gamma-TiAl-based alloy air-cooled to room temperature into a thermal treatment furnace for heat insulation thermal treatment, and then directly taking out and performing air cooling until reaching room temperature; and 3. carrying out repeated heat insulation thermal treatment and air cooling for 3-5 times on the beta type gamma-TiAl-based alloy air-cooled to room temperature according to the method of step 2, then putting into the thermal treatment furnace for heat insulation thermal treatment, taking out and then air cooling to room temperature, thus obtaining the beta type gamma-TiAl-based alloy with the small fully lamellar structure. According to the invention, the small and uniform fully lamellar structure can be obtained by adopting high temperature circulating thermal treatment, the defect of low plasticity of the alloy caused by the fact that small fully lamella structures are hard to obtain by common thermal treatment is overcome, and simultaneously the structure is optimized and the alloy performances are improved.

Description

technical field [0001] The invention belongs to the technical field of heat treatment of metal materials, and in particular relates to a method for obtaining a fine full-lamellar structure of a β-type γ-TiAl-based alloy. Background technique [0002] TiAl intermetallic compounds have become a promising high-temperature structural material due to their high specific strength, specific modulus, good oxidation resistance, creep resistance, and excellent high-temperature strength, stiffness, and low density. Different from the strengthening mechanisms of traditional superalloys such as solid solution strengthening, dispersion strengthening, and fine-grain strengthening, the high-temperature strength of TiAl alloys comes from the long-range ordered arrangement of its atoms and special bonds. However, the existence of this structure makes the room temperature ductility and fracture toughness of TiAl alloys low, which also becomes the main factor limiting its application. [0003]...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C22F1/18
CPCC22F1/183
Inventor 罗媛媛毛小南吴金平苏航标杨英丽郭荻子杨帆
Owner NORTHWEST INSTITUTE FOR NON-FERROUS METAL RESEARCH