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6082 aluminum alloy plate for aviation and production process thereof

A technology of aluminum alloy sheet and production process, applied in the field of aluminum alloy sheet manufacturing, can solve the problems of aluminum alloy sheet fracture, poor bending performance, affecting the application of 6082 aluminum alloy sheet, etc., and achieve the effect of improving stamping and forming performance

Active Publication Date: 2020-01-21
河南明晟新材料科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, most of the 6082 aluminum alloy sheets currently used in the aviation field are in the T6 state after solution heat treatment and aging. This state has high strength. The current conventional 6082-T6 aluminum alloy sheets have poor bending performance. The aluminum alloy sheet prepared by the method is stamped and formed, the aluminum alloy sheet will break, and the stamping performance of the aluminum alloy sheet is poor, which affects the application of the 6082 aluminum alloy sheet in the aviation field

Method used

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  • 6082 aluminum alloy plate for aviation and production process thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0020] A 6082 aluminum alloy sheet for aviation, including the following components by weight percentage: Si=0.9%, Fe≤0.4%, Cu≤0.05%, Mn=0.7%, Mg=1.0%, Cr≤0.1%, Zn≤0.1 %, Ti=0.025%, AL and other unavoidable elements, the other unavoidable single elements are ≤0.05%, and the total is ≤0.15%.

[0021] The production process of the 6082 aluminum alloy sheet for aviation includes the following preparation steps:

[0022] S1. Weigh the aforementioned ingredients according to weight percentages and put them in a melting furnace for smelting at 700-750°C. After refining, degassing, slagging, and filtering, the molten aluminum is cast into aluminum alloy ingots;

[0023] S2. After uniformly thermalizing the aluminum alloy ingot obtained in step S1, the head and tail are cut off and milled to obtain a pretreated alloy ingot;

[0024] S3. Preheat the preheated alloy ingot obtained in step S2 and then undergo hot rolling to a hot-rolled plate with a thickness of 5.5 mm, and the final hot-rolling...

Embodiment 2

[0029] A 6082 aluminum alloy plate for aviation, including the following components by weight percentage: Si=1.1%, Fe≤0.4%, Cu≤0.05%, Mn=0.65%, Mg=0.95%, Cr≤0.1%, Zn≤0.1 %, Ti=0.03%, AL and other inevitable elements, the other inevitable individual elements are ≤0.05%, and the total is ≤0.15%.

[0030] The production process of the 6082 aluminum alloy sheet for aviation includes the following preparation steps:

[0031] S1. Weigh the aforementioned ingredients according to weight percentages and put them in a melting furnace for smelting at 700-750°C. After refining, degassing, slagging, and filtering, the molten aluminum is cast into aluminum alloy ingots;

[0032] S2, after uniform thermal treatment of the aluminum alloy ingot obtained in step S1, the head and tail are cut off and milled to obtain a pretreated alloy ingot;

[0033] S3. Preheat the preheated alloy ingot obtained in step S2 and then undergo hot rolling to a hot-rolled plate with a thickness of 5.0mm, and the final hot...

Embodiment 3

[0038] A 6082 aluminum alloy sheet for aviation, including the following components by weight percentage: Si=0.95%, Fe≤0.4%, Cu≤0.05%, Mn=0.75%, Mg=1.1%, Cr≤0.1%, Zn≤0.1 %, Ti=0.02%, AL and other unavoidable elements, the other unavoidable single elements are ≤0.05%, and the total is ≤0.15%.

[0039] The production process of the 6082 aluminum alloy sheet for aviation includes the following preparation steps:

[0040] S1. Weigh the aforementioned ingredients according to weight percentages and put them in a smelting furnace for smelting at 700-750°C. After refining, degassing, slagging and filtering, the molten aluminum is cast into aluminum alloy ingots;

[0041] S2. After uniformly thermalizing the aluminum alloy ingot obtained in step S1, the head and tail are cut off and milled to obtain a pretreated alloy ingot;

[0042] S3. Preheat the preheated alloy ingot obtained in step S2 and then undergo hot rolling to a hot-rolled plate with a thickness of 6.0 mm, and the final hot-rollin...

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Abstract

The invention relates to a 6082 aluminum alloy plate for aviation and a production process thereof. The 6082 aluminum alloy plate comprises the following components in percentage by weight: 0.95-1.1%of Si, less than or equal to 0.4% of Fe, less than or equal to 0.05% of Cu, 0.65-0.75.75% of Mn, 0.95-1.1% of Mg, less than or equal to 0.1% of Cr, less than or equal to 0.1% of Zn, 0.02-0.03% of Ti,and less than or equal to 0.15% of Al and other inevitable elements, wherein the other inevitable elements are less than or equal to 0.05%. The production process comprises the following steps: smelting and casting the elements into an aluminum alloy ingot in a smelting furnace, performing hot rolling at a temperature of greater than or equal to 320 DEG C, performing cold rolling until the thickness is 0.9-1.0mm, and performing solution hardening on a continuous quenching line at a speed of 9-14m / min at a temperature of 500-520 DEG C; and the aluminum alloy plate prepared by the process effectively improves the stamping forming performance of the aluminum alloy plate and realizes 180-degree bending of the aluminum alloy plate.

Description

Technical field [0001] The invention belongs to the technical field of aluminum alloy sheet manufacturing, and specifically relates to a 6082 aluminum alloy sheet for aviation and a production process thereof. Background technique [0002] Aluminum alloy sheet is the most widely used non-ferrous metal structural material in the industry. It is used in various industries according to different materials. Among them, 6082 alloy is widely used in the aviation field. However, most of the 6082 aluminum alloy sheets currently used in the aviation field are in the T6 state after solution heat treatment and aging. This state has high strength. The current conventional 6082-T6 aluminum alloy sheet has poor bending performance. If you continue to use the traditional The aluminum alloy sheet prepared by the method is subjected to stamping forming, the aluminum alloy sheet will be broken, and the aluminum alloy sheet has poor stamping performance, which affects the application of the 6082 al...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C22C21/02C22C21/08C22C1/02C22F1/05
CPCC22C1/026C22C21/02C22C21/08C22F1/05
Inventor 宋喜波李克振
Owner 河南明晟新材料科技有限公司