Method for refining additive manufactured titanium alloy grains

A technology of additive manufacturing and titanium alloy, which is applied in the field of additive manufacturing, can solve the problems of changing structure performance, limited improvement ability of structure performance, and cracking of parts, so as to refine grains, reduce the possibility of cracking, and reduce internal The effect of stress

Active Publication Date: 2019-01-04
SHENYANG AEROSPACE UNIVERSITY
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Problems solved by technology

[0005] In this method, due to the limitation of the power of the ultrasonic equipment, during the solidification process of the deposited metal, due to the low fluidity of the molten metal and rapid solidification, the ultrasonic wave cannot produce cavitation inside the molten metal, and cannot produce sufficient nucleation. On the other hand, due to the upward transmission of ultrasonic waves from the workbench, the ability of the deposited layer to receive ultrasonic waves is different at different heights, and the ability to control columnar crystals is limited.
[0006] 2. The electromagnetic stirring method, similar to the ultrasonic vibration method, suppresses the formation and growth of columnar crystals through the action of external force stirring the molten pool. Limited ability to improve organizational performance
[0007] 3. Heat treatment method, which is a common method for processing titanium alloys. However, during laser additive manufacturing, especially in the process of manufacturing large and thick parts, due to the extremely high energy density in the manufacturing process, extremely strong heat is generated inside the parts. The internal stress causes cracks on the surface of the part to cause the part to fail. This is a problem that needs to be solved before heat treatment. Stress relief annealing may cause the part to crack and fail directly. Therefore, when manufacturing large parts, the method of changing the structure and properties of heat treatment is not applicable.
However, due to the extremely high yield strength of titanium alloys, the external force deformation often uses heavy pressure and high impact to deform the forming layer, so the external force deformation system is usually very large, and the existing external force deformation system only improves the grain size of the surface layer of the part. However, it cannot achieve the improvement of the overall performance of alloy parts

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  • Method for refining additive manufactured titanium alloy grains
  • Method for refining additive manufactured titanium alloy grains
  • Method for refining additive manufactured titanium alloy grains

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Embodiment

[0038] A method for refining titanium alloy grains by additive manufacturing, which involves a device for refining titanium alloy grains by laser additive manufacturing, including an atmosphere protection box, a laser additive manufacturing system, an external force volume deformation system, and a control system. The working part of the laser additive manufacturing system and the working part of the external force volume deformation system are installed in the atmosphere protection box, and a high-precision hydrogen concentration monitoring device is installed outside the atmosphere protection box, and a hydrogen concentration alarm device is installed at the same time to prevent hydrogen The concentration reaches the deflagration point (when the volume percentage of hydrogen contained in the air is 4.0%-74.2% in the mixed gas, it will explode when ignited).

[0039] A method for refining and additively manufacturing titanium alloy grains, the flow chart of which is shown in ...

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Abstract

The invention relates to a method for refining additive manufactured titanium alloy grains, belonging to the field of v. The method comprises the following steps of: placing a titanium alloy substratein an atmosphere protection box of an additive manufacturing device; controlling the hydrogen concentration and environmental pressure in the atmosphere protection box to be favorable to hydrogen absorption of titanium alloy; adjusting the temperature of the titanium alloy substrate to be favorable for hydrogen absorption temperature of the titanium alloy; adopting an additive manufacturing system in the additive manufacturing device, after several layers are continuously deposited, introducing an external force volume deformation system to discharge hydrogen from the deposited layer by an external force, and controlling the temperature of the titanium alloy substrate to be unfavorable to hydrogen absorption temperature of the titanium alloy, and repeating the temperature control and deposition until a predetermined deposition form is obtained. The method is based on the hydrogen absorption principle of titanium alloy and exerts an external force to prevent the formation of columnar grain of titanium alloy and achieve the purpose of grain refinement. The method has the characteristics of further grain refinement, high efficiency and convenient realization.

Description

technical field [0001] The invention relates to 3D printing, in particular to a method for thinning and additively manufacturing titanium alloy grains, which belongs to the field of additive manufacturing. Background technique [0002] Laser additive manufacturing technology was developed in the 1980s. It combines laser additive manufacturing technology with the rapid prototyping principle of rapid prototyping technology to form a new rapid manufacturing technology. First, the solid model of the part is formed in the computer through 3D CAD software, and then the model established by CAD is layered according to a certain thickness, and then the 3D solid model is converted into a 2D outline model, and then under the control of the machine tool or robot , using methods such as synchronous powder feeding laser deposition to fill a given shape point by point with metal materials in a certain path until a three-dimensional solid shape is formed. [0003] It can be known from the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B22F3/105C22F1/18C22C14/00C22C1/04B33Y10/00B33Y50/02B33Y70/00
CPCC22C1/0458C22C14/00C22F1/183B33Y10/00B33Y50/02B33Y70/00B22F10/00B22F10/28Y02P10/25B22F10/20
Inventor 杨光王宝星钦兰云李长富王伟赵朔王超任宇航尚纯何波周思雨王维
Owner SHENYANG AEROSPACE UNIVERSITY
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