Aluminum alloy powder material for aviation additive manufacturing, preparation method and 3D printing method

A technology of additive manufacturing and aluminum alloy, which is applied in the field of preparation of aluminum alloy powder materials for aviation additive manufacturing, and can solve the problems of material cracking, uneven structure, strength, tensile strength in deposited state and low tensile strength in annealed state, etc. , to achieve the effect of solving easy oxidation and optimizing welding performance

Active Publication Date: 2021-06-25
BEIJING BAOHANG ADVANCED MATERIALS CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the traditional high-strength aluminum alloy material is designed for deformation processing, not for laser forming. It has a large tendency of stress cracking and cannot adapt to the 3D printing process. However, the current Al-Si alloys that can achieve 3D printing are in terms of mechanical properties. It is also difficult to assume the role of load-bearing parts, so there is an urgent need for an aluminum alloy material that can be used for additive manufacturing in the aviation field to meet the needs of laser forming performance
[0004] At present, the aluminum alloy powder materials that can be printed mainly include Al-Si materials such as AlSi10Mg, AlSi7Mg, and AlSi12. Their strength, tensile strength in the deposited state, and tensile strength in the annealed state are not high. application
[0005] Commonly used aluminum alloys such as Al-Cu-Mg series and Al-Zn-Mg-Cu series alloys can meet the requirements of aviation, but cannot adapt to additive manufacturing molding, such as Al-Cu-Mg series, Al-Zn-Mg -Cu-based alloy materials cannot adapt to the additive manufacturing process due to the composition
[0006] The main reason is that the aluminum alloy material has a high laser reflectivity, combined with the complex composition, the volatilization of low melting point components and the tearing of the matrix during the solidification of some components, resulting in severe cracking of the material after printing and the inability to form stably. Preparation makes a big impact
The existing improvement cases are not only difficult to prepare, but the design of some components violates the material design guidelines and restricts each other, which not only causes a waste of resources, but also restricts the applicability of materials
When a large amount of alloying elements are added to the material, it is easy to produce composition segregation, resulting in serious anisotropy of the material and uneven structure, which seriously affects the application of the material.

Method used

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  • Aluminum alloy powder material for aviation additive manufacturing, preparation method and 3D printing method
  • Aluminum alloy powder material for aviation additive manufacturing, preparation method and 3D printing method
  • Aluminum alloy powder material for aviation additive manufacturing, preparation method and 3D printing method

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preparation example Construction

[0047] Specifically this preparation method comprises the following steps:

[0048] Step S1: weighing a raw material of aluminum alloy powder with a preset content and placing it in a smelting device.

[0049] The raw materials for preparing aluminum alloy powder include: any one of pure magnesium, pure aluminum, aluminum-magnesium alloy, aluminum-scandium alloy, aluminum-zirconium alloy, aluminum-manganese alloy, aluminum-silicon alloy, aluminum-copper alloy or aluminum-titanium alloy or a combination thereof.

[0050] Step S2: After controlling the vacuum degree of the smelting device to be ≤300 Pa, fill the smelting device with inert gas until the smelting device reaches atmospheric pressure.

[0051] Specifically, the purpose of keeping the vacuum degree of the smelting device within 300 Pa is to draw away the air in the smelting chamber to ensure that the smelting device is in a vacuum state. When the inert gas is filled into the smelting device later, the atmosphere in ...

Embodiment 1

[0073] image 3 It is a schematic diagram of the raw material ratio of the aluminum alloy powder used for aviation additive manufacturing in Example 1 provided by the present invention, please refer to image 3 , the aluminum alloy powder material for aerospace additive manufacturing provided by the present invention contains the following components in mass percentage:

[0074] Mg: 4.8wt%, Sc: 0.8wt%, Zr: 0.35wt%, Mn: 0.55wt%, Si: 0.15wt%, Cu: 0.08wt%, Ti: 0.1wt%, Zn: 0.08wt%, Fe: <0.08wt%; the remaining content is Al.

[0075] According to the content of raw materials in the above aluminum alloy powder, weigh pure magnesium alloy, pure aluminum alloy, aluminum-scandium alloy, aluminum-zirconium alloy, aluminum-manganese alloy, aluminum-silicon alloy, aluminum-copper alloy and aluminum-titanium alloy, and place them in the melting device middle.

[0076] The smelting device is evacuated to a vacuum degree of 280 Pa, and then filled with nitrogen, so that the inside of the ...

Embodiment 2

[0087] Figure 4 It is a schematic diagram of the raw material ratio of the aluminum alloy powder used in the aviation additive manufacturing of the second embodiment provided by the present invention, please refer to Figure 4 , the aluminum alloy powder material for aerospace additive manufacturing provided by the present invention contains the following components in mass percentage:

[0088] Mg: 4.5wt%, Sc: 0.83wt%, Zr: 0.38wt%, Mn: 0.5wt%, Si: 0.2wt%, Cu: 0.05wt%, Ti: 0.15wt%; the remaining content is Al.

[0089] According to the content of raw materials in the above aluminum alloy powder, weigh pure magnesium alloy, pure aluminum alloy, aluminum-scandium alloy, aluminum-zirconium alloy, aluminum-manganese alloy, aluminum-silicon alloy, aluminum-copper alloy and aluminum-titanium alloy, and place them in the melting device middle.

[0090] The smelting device is evacuated to a vacuum degree of 300 Pa, and then filled with argon to make the inside of the smelting device...

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Abstract

The invention provides aluminum alloy powder for aviation additive manufacturing, a preparing method and a 3D printing method. The aluminum alloy powder comprises 4.0 wt%-6.0 wt% of Mg, 0.7 wt%-0.9 wt% of Sc, 0.3 wt%-0.5 wt% of Zr, 0.4 wt%-0.5 wt% of Mn, 0.1 wt%-0.2 wt% of Si, 0.02 wt%-0.1 wt% of Cu, 0.05 wt%-0.15 wt% of Ti, smaller than 0.1 wt% of Zn or smaller than 0.1 wt% of Fe and the balance Al. By doping elements with different components, the material has very high strength and toughness, the material characteristics of the aluminum alloy can be compensated, the high reflectivity of the aluminum alloy powder material to laser during laser forming is reduced, meanwhile, the problem of hot cracking of the aluminum alloy powder material is solved, and he aluminum alloy powder can be used for an additive manufacturing method in the aviation field.

Description

technical field [0001] The invention relates to the technical field of aluminum alloy powder, in particular to an aluminum alloy powder material for aviation additive manufacturing, a preparation method and a 3D printing method. Background technique [0002] As a light and high-strength material, aluminum alloy has been playing a pivotal role in various fields with its excellent specific strength. Especially in the field of aerospace, the requirements for aluminum alloys are increasing and becoming more and more stringent. In addition to the requirement of lightweight materials, there is also a demand for the flexibility and integration of component design. However, the additive manufacturing process in the current processing method, especially the additive manufacturing process of aluminum alloy, needs to meet the requirements of light weight and high strength of the material, and also needs to meet the design and molding requirements of complex parts. [0003] High-streng...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B22F9/08B22F1/00B33Y70/00C22C21/08
CPCB22F1/0003B22F9/082C22C21/08B33Y70/00B22F1/14Y02P10/25
Inventor 胡万谦李振民赵春禄邓韵琦王联波刘干
Owner BEIJING BAOHANG ADVANCED MATERIALS CO LTD
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