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A kind of anti-laser ablation coating for substrate surface and preparation method

A substrate surface, anti-laser technology, applied in metal material coating process, coating, superimposed layer plating and other directions, can solve the problems of reduced aircraft structural strength, increased temperature of stressed components, and decreased compressive strength, etc. Achieve good application prospects, controllable thickness, and low porosity

Active Publication Date: 2022-08-02
SHANGHAI AEROSPACE EQUIP MFG GENERAL FACTORY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

After the high-energy laser irradiates the aircraft, the temperature of the stress-bearing components will increase, and the tensile and compressive strength of the material will decrease, resulting in a decrease in the structural strength of the aircraft, causing the aircraft to be destroyed under its own stress

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  • A kind of anti-laser ablation coating for substrate surface and preparation method

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preparation example Construction

[0042] The preparation method of the anti-laser ablation coating for the surface of the substrate of embodiment 1-2, the steps of the method include:

[0043] (1) Degreasing and sandblasting: dip and wash with organic solvent, and dry naturally. Before spraying, the surface of the substrate is sandblasted to remove the surface oxide layer and increase the roughness of the substrate surface;

[0044] (2) Supersonic plasma spraying molybdenum layer on the surface of the substrate; the process parameters of supersonic plasma spraying are: the main gas is the inert gas Ar, the secondary gas is the reducing gas hydrogen, the current is 370-390A, and the voltage is 100-120V , the main air flow is 120~140L / min, the powder feeding and spraying distance is 90~110mm, and the powder feeding rate is 20~40g / min;

[0045] (3) Supersonic plasma spraying the zirconia layer on the molybdenum layer; the process parameters of the supersonic plasma spraying are: the main gas is the inert gas Ar, ...

Embodiment 1

[0049] The anti-laser ablation coating for the aluminum alloy surface of Example 1, the base material is an aluminum alloy substrate 1, the heat insulating layer includes a molybdenum layer 2 and a zirconia layer 3, the transition layer is a zirconia aluminum layer 4, and the reflective layer is Aluminum graphene layer 5, its specific structure can refer to figure 1 .

[0050] The preparation method of embodiment 1 is as follows:

[0051] (1) Degreasing and sandblasting: dip and wash with organic solvent, and dry naturally. Before spraying, the surface of the substrate is sandblasted to remove the surface oxide layer and increase the roughness of the substrate surface;

[0052] (2) Supersonic plasma spraying molybdenum layer on the surface of the substrate; the process parameters of supersonic plasma spraying are: the main gas is the inert gas Ar, the secondary gas is the reducing gas hydrogen, the current is 380A, the voltage is 110V, and the main gas flow rate is 380A. 130...

Embodiment 2

[0058] The anti-laser ablation coating for the aluminum alloy surface of Example 2, the base material is an aluminum alloy, the heat insulating layer is a molybdenum zirconia layer, the transition layer is a zirconia aluminum layer, and the reflective layer is an aluminum graphene layer, and its preparation The method is as follows:

[0059] (1) Degreasing and sandblasting: dip and wash with organic solvent, and dry naturally. Before spraying, the surface of the substrate is sandblasted to remove the surface oxide layer and increase the roughness of the substrate surface;

[0060] (2) Supersonic plasma spraying molybdenum layer on the surface of the substrate; the process parameters of supersonic plasma spraying are: the main gas is the inert gas Ar, the secondary gas is the reducing gas hydrogen, the current is 380A, the voltage is 110V, and the main gas flow rate is 380A. 130L / min, the powder feeding distance is 100mm, and the powder feeding rate is 30g / min;

[0061] (3) Su...

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Abstract

The invention discloses an anti-laser ablation coating on the surface of a base material and a preparation method, and belongs to the technical field of surface treatment engineering. The molybdenum zirconia thermal insulation layer was prepared on the surface of the aluminum alloy by supersonic plasma spraying technology, the gradient zirconia-aluminum transition layer was prepared by supersonic plasma spraying coupled with cold spraying, and the aluminum graphene reflective layer was prepared by cold spraying technology. The prepared anti-laser ablation coating has a controllable thickness, high bonding strength, low porosity, good thermal insulation performance and reflectivity, and can resist high power density laser ablation. In addition, the preparation method of the present invention has the characteristics of simple, convenient and flexible operation, stable process, controllable process and the like, and has good application prospects.

Description

technical field [0001] The invention relates to an anti-laser ablation coating for the surface of a substrate and a preparation method thereof, belonging to the technical field of surface treatment engineering, in particular to a method for preparing an anti-laser ablation coating on the surface of an aluminum alloy by cold spraying. The base material is aluminum or aluminum alloy. Background technique [0002] High-energy lasers have the characteristics of fast propagation speed, short interval time, high lethal power, high emission accuracy, and strong anti-interference ability. After the high-energy laser irradiates the aircraft, the temperature of the force-bearing components increases, and the tensile and compressive strength of the material decreases, resulting in a decrease in the structural strength of the aircraft, and the aircraft is damaged under its own stress. For example, according to the aircraft strength design criteria, if the aluminum alloy material is use...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C23C28/00C23C4/134C23C4/02C23C4/08C23C4/11C23C24/04
CPCC23C28/322C23C28/345C23C4/134C23C4/02C23C4/08C23C4/11C23C24/04
Inventor 鞠鹏飞许伟春臧旭升陈妍李忠建刘京周肖金涛
Owner SHANGHAI AEROSPACE EQUIP MFG GENERAL FACTORY