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High-flux method for powder alloy preparation and thermal consolidation forming process development

A forming process and powder alloy technology, which is applied in the high-throughput field of powder alloy preparation and thermal consolidation forming process development, can solve the problems of unverified accuracy of simulation, coarse second phase, and easy-to-crack available materials, etc., to achieve sufficient The effect of accurate data guidance, shortening the test cycle, and saving test costs

Active Publication Date: 2020-06-05
CENT SOUTH UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, methods such as hot extrusion, hot isostatic pressing, and sintering are usually used to prepare the alloy powder to the alloy block. When the powder is hot-extruded and consolidated, the selection of process parameters is unreasonable, which will cause the microstructure of the material to be deformed. Uniform, if the temperature is too high, it will lead to coarse grains and second phases, resulting in a decrease in alloy performance; when the temperature is too low, the deformation resistance becomes larger, and dislocations are easy to coil at the grain boundary, resulting in an increase in local stress and intergranular cracking , the alloy is cracked and scrapped
At present, the determination of the powder alloy thermal consolidation forming process is still mainly based on the trial and error method. The thermal consolidation forming often requires the cooperation of multiple large-scale equipment to complete, so the cost of a test is tens of thousands or even tens of millions of yuan, which is high. It takes several weeks or months to complete a test, the cycle is long, and the amount of powder used in a test needs several kilograms, which further increases the test cycle and cost. The high test cost and long cycle eventually lead to a very wide choice of test process parameters, resulting in alloy heat The development of the consolidation forming process is not accurate, and the optimal thermal consolidation forming process of the alloy cannot be accurately obtained
At the same time, different alloy powders have different optimal thermal consolidation forming processes, which add great difficulties to the development of powder alloys
[0003] Traditional powder alloy preparation and process development have problems such as long process development cycle and high cost
In recent years, some new powder metallurgy rapid prototyping methods have emerged, such as 3D printing (Chinese patent 201310011857.9), but there are still many problems in the production process, such as difficult to control the structure, easy to crack, and continuous expansion of available materials. It is difficult to replace traditional methods
The development of computers has promoted the research and development of materials in some aspects, and some forming simulation software has played a certain role in process development. For example, DEFORM software can simulate the thermal consolidation forming process by computer, which reduces the cost of expensive field tests to a certain extent. , which shortens the development cycle of the powder thermal consolidation forming process, but there are problems such as high software cost and the accuracy of simulation to be verified, and it cannot cover the whole process from composition design to performance extraction

Method used

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  • High-flux method for powder alloy preparation and thermal consolidation forming process development
  • High-flux method for powder alloy preparation and thermal consolidation forming process development
  • High-flux method for powder alloy preparation and thermal consolidation forming process development

Examples

Experimental program
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Effect test

Embodiment 1

[0043] This implementation case is a nickel alloy high-throughput composition design and hot extrusion process development steps are:

[0044] (1) adopt argon gas atomization to prepare nickel alloy powder, powder composition Ni-21Cr-0.7Fe-0.6Ti-0.3Al, cross 100 mesh sieves;

[0045] (2) Put the powder into a bag and shake it;

[0046] (3) The sheath is sealed and welded by vacuum electron beam;

[0047] (4) Use a thermal simulation testing machine to conduct a thermal compression simulation test, the thermal compression temperature is 850°C, 950°C, 1050°C, 1150°C, and the strain rate is 1S -1 , 0.1S -1 、5S -1 , the deformation amount is 80%, and the alloy small block is obtained;

[0048] (6) Observe the macroscopic surface conditions of the sample, such as Figure 5 As shown, the hot-pressing temperature of 850℃ alloy is all cracked, and the strain rate is 5S -1 Cracking occurs at a temperature of 950°C. When the temperature is too low, the deformation resistance becom...

Embodiment 2

[0052] This implementation case is a nickel alloy high-throughput composition design and hot extrusion process development steps are:

[0053] (1) Nickel alloy powder is prepared by argon atomization, and the powder composition is Ni-21Cr-0.7Fe-0.6Ti-0.3Al;

[0054] (2) Nickel alloy powder with 0.6% YH 2 The powder is ball milled, using argon protection during the ball milling process, adding 0.5% ethanol as a process control agent, ball milling for 36 hours, and passing through a 50-mesh sieve after ball milling;

[0055] (3) Put the ball mill powder into the bag and shake it;

[0056] (4) The sheath is sealed and welded by vacuum electron beam;

[0057] (5) Use a thermal simulation testing machine to conduct a thermal compression simulation test, the thermal compression temperature is 850°C, 950°C, 1050°C, 1150°C, and the strain rate is 1S -1 , 0.1S -1 、5S -1 , the deformation amount is 80%, and the alloy small block is obtained;

[0058] (6) Observe the macroscopic su...

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Abstract

The invention relates to a high-flux method for powder alloy preparation and thermal consolidation process development, covers the whole process of powder alloy component design, preparation, thermalconsolidation forming process development and performance detection, and provides a rapid process for powder alloy development. Alloy powder is prepared through a ball milling method; alloy powder orelement powder with different elements and different contents can be added in the process, and alloy powder with different components is prepared. The invention discloses a powder thermal consolidation forming sheath. Alloy powder is contained in the sheath, vacuum electron beam or laser seal welding is adopted after compaction, the powder sheath is subjected to thermal consolidation forming underdifferent process conditions, then hardness detection is conducted, the alloy component-thermal consolidation process-performance relation is established, optimal components, processes and other dataare screened, and a test basis is provided for alloy component design and thermal consolidation forming process development. The invention aims to solve the problems of long powder alloy developmentperiod, high cost, unreasonable thermal consolidation process and the like in the prior art.

Description

technical field [0001] The invention discloses a high-throughput method for powder alloy preparation and thermal consolidation forming process development, which belongs to the technical field of powder metallurgy material preparation. Background technique [0002] At present, methods such as hot extrusion, hot isostatic pressing, and sintering are usually used to prepare the alloy powder to the alloy block. When the powder is hot-extruded and consolidated, the selection of process parameters is unreasonable, which will cause the microstructure of the material to be deformed. Uniform, if the temperature is too high, it will lead to coarse grains and second phases, resulting in a decrease in alloy performance; when the temperature is too low, the deformation resistance becomes larger, and dislocations are easy to coil at the grain boundary, resulting in an increase in local stress and intergranular cracking , Alloy cracking and scrapping phenomenon. At present, the determina...

Claims

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Application Information

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IPC IPC(8): G01N3/18G01N3/54G01N3/06G01N1/28B22F3/14
CPCB22F3/14G01N1/286G01N3/06G01N3/18G01N3/54G01N2001/2873G01N2203/0019G01N2203/0076G01N2203/0226
Inventor 何武强刘锋谭黎明展鑫何英杰王国伟
Owner CENT SOUTH UNIV
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