Electric arc additional material manufacturing method of multi-material integral structural component

A technology of integral structural parts and additive manufacturing, applied in the direction of manufacturing tools, additive processing, arc welding equipment, etc., can solve the problems that deposition cannot be carried out continuously, it is not suitable for industrial applications, and the molding efficiency is low

Active Publication Date: 2020-03-20
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the arc additive manufacturing technology is usually a single-feed arc additive manufacturing technology, that is, one wire is used as a raw material for arc fuse each time. When it is used to prepare multi-material integral structural parts, it is necessary to replace the wire frequently

Method used

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  • Electric arc additional material manufacturing method of multi-material integral structural component
  • Electric arc additional material manufacturing method of multi-material integral structural component
  • Electric arc additional material manufacturing method of multi-material integral structural component

Examples

Experimental program
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Example Embodiment

[0043] Example 1

[0044] use figure 1 The shown device prepares a barrel for artillery breech block, in which the material of the cylinder part (ie the rigid connection part) is TA15 titanium alloy, and the material of the rocker part (ie the loading area) is TC18 titanium alloy. The specific steps are as follows:

[0045] Construct a three-dimensional solid model by solidworks software, then use 3D data processing software for slicing, then generate a processing program, and import the processing program into the control system; install two TC18 titanium alloy wires with a diameter of 1.6mm on the 1# wire feeder And 2# wire feeder, install two TA15 titanium alloy wires with a diameter of 1.6mm on the 3# wire feeder and 4# wire feeder, and connect the hot wire power supplies numbered Ⅰ, Ⅱ, Ⅲ, and Ⅳ. The positive pole is connected to the wires on the 1# wire feeder, 2# wire feeder, 3# wire feeder, and 4# wire feeder through a copper wire feed tube. The distance between the connecti...

Example Embodiment

[0054] Example 2

[0055] use figure 1 The shown device prepares TC4-TC11 titanium alloy thin-walled devices, wherein the lower layer is made of TC4 titanium alloy with a height of 25mm, and the upper layer is made of TC11 titanium alloy with a height of 45mm. The specific steps are as follows:

[0056] Build a three-dimensional solid model (such as image 3 (Shown), then use 3D data processing software for slicing processing, the layer height is 2.5mm, and then generate the processing program, and import the processing program into the control system;

[0057] Install two TC4 titanium alloy wires with a diameter of 1.6mm on 1# wire feeder and 2# wire feeder, and install two TC11 titanium alloy wires with a diameter of 1.6mm on 3# wire feeder and 4# On the wire feeder, pass the positive electrode of the hot wire power supply numbered Ⅰ, Ⅱ, Ⅲ, and Ⅳ with the wires on the 1# wire feeder, 2# wire feeder, 3# wire feeder and 4# wire feeder in turn Copper wire feeding tube is connected, t...

Example Embodiment

[0060] Example 3

[0061] use figure 1 The shown device prepares TC4-TC11 titanium alloy gradient blocks, where the lower layer is made of TC4 titanium alloy with a height of 35mm, and the upper layer is made of TC11 titanium alloy with a height of 35mm. The specific steps are as follows:

[0062] Build a three-dimensional solid model (such as Figure 5 (Shown), and then use 3D data processing software for slicing, the layer height is 3.5mm, and then generate the processing program, and import the processing program into the control system;

[0063] Install two TC4 titanium alloy wires with a diameter of 1.6mm on 1# wire feeder and 2# wire feeder, and install two TC11 titanium alloy wires with a diameter of 1.6mm on 3# wire feeder and 4# On the wire feeder, pass the positive electrode of the hot wire power supply numbered Ⅰ, Ⅱ, Ⅲ, and Ⅳ with the wires on the 1# wire feeder, 2# wire feeder, 3# wire feeder and 4# wire feeder in turn Copper wire feeding pipe is connected, the distance ...

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Abstract

The invention provides an electric arc additional material manufacturing method of a multi-material integral structural component, and belongs to the multi-material integral structural component manufacturing technology field. The electric arc additional material manufacturing method of the multi-material integral structural component comprises the following steps of constructing a three-dimensional solid model of a target structural component, then carrying out slicing processing, generating a machining program, and importing the machining program into a control system; and using electric arcadditional material manufacturing equipment provided with n sets of wire feeders to carry out electric arc additional material manufacturing according to the machining program, and acquiring the multi-material integral structural component, wherein the n is an integer greater than or equal to 2. In an electric arc additional material manufacturing process, the n sets of wire feeders are divided into m sets, the m is the integer greater than or equal to 2, each set of wire feeders feeds one kind of wire at the same time, the m sets of wire feeders are continuously and alternately used, and a molten drop transition mode is a contact type transition mode. The method of the invention has no obvious defects at an interface, and has an advantage of high forming efficiency.

Description

technical field [0001] The invention relates to the technical field of preparation of multi-material integral structural parts, in particular to an arc additive manufacturing method for multi-material integral structural parts. Background technique [0002] With the development of aerospace technology, the performance requirements of advanced aircraft for large and lightweight structural parts such as titanium alloys are also getting higher and higher. Due to the different service environments of different parts of the same structural part, the performance requirements of different parts are also different. For example, load-bearing structural parts such as aircraft frame beams, the upper part mainly bears high compressive stress, which requires high strength and rigidity of the material, while the lower part mainly bears high tensile stress, which requires the material to have excellent toughness, fatigue crack growth resistance and excellent performance. The damage tolera...

Claims

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Application Information

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IPC IPC(8): B23K9/04B23K9/167B33Y10/00
CPCB23K9/04B23K9/167B33Y10/00B23K2103/14
Inventor 刘长猛王贺陈倬宋文强刘家伟
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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