Method for forming Ti/Al dissimilar alloy based on laser selective melting technology

A laser selective melting and selective melting technology, which is applied in the improvement of process efficiency, additive manufacturing, additive processing, etc., can solve the problems of difficult connection of two alloys, low solubility, differences in thermal expansion coefficient and thermal conductivity, etc., to improve the solubility. , The effect of overcoming component segregation and improving forming efficiency

Active Publication Date: 2020-02-07
BEIJING UNIV OF TECH
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Problems solved by technology

[0006] The purpose of the present invention is to provide a forming method of Ti/Al dissimilar alloys based on laser selective melting technology, which solves the problem that the existing titanium/aluminum alloy dissim

Method used

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Embodiment Construction

[0030] The present invention will be described in detail below through specific embodiments.

[0031] A method for forming a Ti / Al dissimilar alloy based on laser selective melting technology of the present invention is specifically implemented according to the following steps:

[0032] Step 1, drying and pre-screening the titanium alloy and aluminum alloy powder;

[0033] Dry the TC4 titanium alloy and Al-Mg-Sc-Zr alloy powder in a vacuum environment oven with a temperature of 80-180°C and an air pressure not greater than -0.05MPa for 2-5h, then take it out after vacuum cooling for 2h, and then use it for 200- Sieve the powder with a 240-mesh sieve.

[0034] Step 2, before forming, preparation of program files and SLM equipment;

[0035] Step 2.1, preparation of program files;

[0036] First, use the 3D modeling software on the computer to design the overall 3D solid model of the required parts. According to the design requirements, the overall solid model is divided into ...

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Abstract

The invention discloses a method for forming a Ti/Al dissimilar alloy based on a laser selective melting technology. Drying and pre-screening treatment are carried out on aluminum alloy and titanium alloy powder; then program files and SLM equipment are prepared; the laser selective melting technology is used for forming a bottom titanium alloy part, after forming is completed, the titanium alloypowder in a powder supply chamber of the SLM equipment is replaced with the aluminum alloy powder, and the laser selective melting technology is continuously used for forming an upper aluminum alloy part on the titanium alloy substrate; and finally, wire cutting equipment is used for cutting parts from the substrate. The laser selective melting technology can directly form the complex parts, shortens the production cycle, improves the forming efficiency and has great production and application value in the aerospace field; and in addition, the laser selective melting technology is adopted, thecooling rate can reach 106 orders of magnitude, a molten pool rapidly solidifies, the solid solubility of aluminum in the titanium alloy is greatly improved, the phenomenon of component segregation is overcome, and the effect of refined crystalline strengthening is achieved.

Description

technical field [0001] The invention belongs to the technical field of laser selective melting technology rapid prototyping method, and in particular relates to a forming method of Ti / Al dissimilar alloy based on laser selective melting technology. Background technique [0002] Both aluminum alloy and titanium alloy have the advantages of light density, high specific strength (the strength of titanium alloy is close to that of medium-strength steel), good corrosion resistance and high temperature performance, etc. In aerospace applications, titanium-aluminum dissimilar alloy components can greatly reduce the overall weight , can significantly improve the economic efficiency. However, aluminum and titanium are very active metals, which are easily oxidized to form TiO in the air. 2 and Al 2 o 3 and other oxides. Moreover, there are large differences in physical and mechanical properties between aluminum and titanium, and there are large differences in the lattice type and ...

Claims

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Application Information

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IPC IPC(8): B22F3/105B22F7/06B33Y10/00
CPCB22F7/06B33Y10/00B22F10/00B22F10/34B22F10/28B22F10/36B22F10/366B22F10/32B22F10/80B22F10/73Y02P10/25
Inventor 曾勇黄昊
Owner BEIJING UNIV OF TECH
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