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Deformation heat treatment method for aluminum alloy

A technology of deformation heat treatment and aluminum alloy, which is applied in the field of aluminum alloy material manufacturing, can solve the problems of low strength of 6000 series aluminum alloy, inability to reflect the advantages of weight reduction, and sensitivity to intergranular corrosion, etc., and achieve the effect of high extrusion deformation strengthening effect

Inactive Publication Date: 2017-01-11
张家港市丰乐汽车设备有限公司
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Problems solved by technology

However, so far, the proportion of 6000-series aluminum alloys used in aircraft manufacturing is significantly lower than that of 7000-series and 2000-series aluminum alloys
The primary reason for this phenomenon is the relatively low strength of 6000 series aluminum alloys.
Although artificially aged to the peak state (T6), the strength of 6000-series aluminum alloys is still much lower than that of 7000-series and 2000-series aluminum alloys, which cannot reflect the advantages of weight reduction; at the same time, 6000-series aluminum alloys still have serious Inter-corrosion sensitivity, which seriously affects the life and safety of aircraft

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  • Deformation heat treatment method for aluminum alloy
  • Deformation heat treatment method for aluminum alloy
  • Deformation heat treatment method for aluminum alloy

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Embodiment Construction

[0020] The present invention is further illustrated by the following examples: According to the following examples, the present invention can be better understood. However, those skilled in the art can easily understand that the specific material ratios, process conditions and results described in the examples are only used to illustrate the present invention, and should not and will not limit the present invention described in the claims.

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Abstract

The invention discloses a deformation heat treatment method of an aluminum alloy, and a high-strength intergranular-corrosion-resistant aluminum alloy can be obtained by 550 DEG C / 1h solid solution treatment and water quenching, 180 DEG C / 2h under-aging and 85% rolling-reduction cold rolling of 6061 aluminum alloy as a raw material. The tensile strength of the aluminum alloy is 635MPa, the yield strength is 606MPa, the elongation at break is 3.4%, and the average elongation is 0.4%.

Description

technical field [0001] The application belongs to the field of aluminum alloy material manufacturing, and in particular relates to a deformation heat treatment method of aluminum alloy. Background technique [0002] Age-hardening aluminum alloy has low density, high specific strength, good corrosion resistance and plastic formability, and is an important lightweight structural material widely used in aircraft manufacturing, mainly including ultra-high strength 7000 series Al-Zn-Mg-Cu alloy (500-700MPa), high-strength 2000 series Al-Cu-Mg alloy (400-500MPa) and medium-strength 6000 series Al-Mg-Si-Cu alloy (300-400MPa), the representative alloy grades are 7075, 2024 and 6056. Compared with the 7000 series and 2000 series aluminum alloys, although the 6000 series aluminum alloys have the advantages of low material density and cost, ingot formability, plastic processing performance, excellent surface treatment performance and low tendency to stress corrosion cracking. However...

Claims

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Application Information

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IPC IPC(8): C22F1/043
Inventor 赵英
Owner 张家港市丰乐汽车设备有限公司
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