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A kind of 6082 aluminum alloy sheet for aviation and its preparation process

An aluminum alloy sheet and aluminum alloy technology, which is applied in the field of aluminum alloy sheet manufacturing, can solve the problems of aluminum alloy sheet fracture, poor stamping and forming performance of aluminum alloy sheet, poor bending performance, etc., and achieve the effect of improving stamping and forming performance.

Active Publication Date: 2021-06-01
河南明晟新材料科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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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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  • A kind of 6082 aluminum alloy sheet for aviation and its preparation process

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Experimental program
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Effect test

Embodiment 1

[0020] A 6082 aluminum alloy plate for aviation, comprising the following components in weight percent: 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, said other unavoidable individual elements≤0.05%, total≤0.15%.

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

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

[0023] S2. Homogenize and heat-treat the aluminum alloy ingot obtained in step S1, cut off the head and tail, and perform surface milling to obtain a pretreated alloy ingot;

[0024] S3. Preheating the pretreated alloy ingot obtained in step S2, and then hot-rolling it to a hot-rolled plate with a thickness of 5.5 mm, and the hot...

Embodiment 2

[0029] A 6082 aluminum alloy plate for aviation, comprising the following components in weight percent: 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 unavoidable elements, said other unavoidable individual elements≤0.05%, total≤0.15%.

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

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

[0032] S2. Homogenize and heat-treat the aluminum alloy ingot obtained in step S1, cut off the head and tail, and perform surface milling to obtain a pretreated alloy ingot;

[0033] S3. Preheating the pretreated alloy ingot obtained in step S2 and then hot rolling it to a hot rolled plate with a thickness of 5.0mm, and the fina...

Embodiment 3

[0038] A 6082 aluminum alloy plate for aviation, comprising the following components in weight percent: 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, said other unavoidable individual elements≤0.05%, total≤0.15%.

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

[0040] S1. Weigh the aforementioned ingredients according to weight percentage and put them into a smelting furnace for melting at 700-750°C. After refining, degassing, slag removal, and filtering, the molten aluminum is cast into an aluminum alloy ingot;

[0041] S2. Homogenize and heat-treat the aluminum alloy ingot obtained in step S1, cut off the head and tail, and perform surface milling to obtain a pretreated alloy ingot;

[0042] S3. Preheating the pretreated alloy ingot obtained in step S2, and then hot-rolling it to a hot-rolled plate with a thickness of 6.0 mm, and the ho...

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Abstract

The invention relates to a 6082 aluminum alloy plate for aviation and its production process, comprising the following components in weight percentage: Si=0.95-1.1%, Fe≤0.4%, Cu≤0.05%, Mn=0.65-0.75%, Mg= 0.95-1.1%, Cr≤0.1%, Zn≤0.1%, Ti=0.02-0.03%, Al and other unavoidable elements, said other unavoidable individual elements≤0.05%, total≤0.15%; The element ingredients are smelted and cast into aluminum alloy ingots in a smelting furnace, and then hot-rolled at a temperature ≥320°C, and then cold-rolled to a thickness of 0.9-1.0mm, at a temperature of 500-520°C at a rate of 9-14m / min The speed is solid solution quenching in the continuous quenching line; the aluminum alloy sheet prepared by the above process can effectively improve the stamping performance of the aluminum alloy sheet and realize the 180° bending of the aluminum alloy sheet.

Description

technical field [0001] The invention belongs to the technical field of aluminum alloy plate manufacturing, and in particular relates to a 6082 aluminum alloy plate for aviation and a preparation 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 sheets have poor bending performance. The aluminum alloy sheet prepared by the method is stamped and formed, and 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 ...

Claims

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Application Information

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Patent Type & Authority Patents(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