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Compaction processing method used for spray forming superhigh-intensity aluminum alloy material

An aluminum alloy material, spray forming technology, applied in the field of metal material processing, can solve the problems of structure defects, incomplete closure, flaky oxide layer defects, etc., to improve structure and performance, improve material density, and improve quality consistency Effects of Sex and Reliability

Inactive Publication Date: 2016-01-06
GENERAL RESEARCH INSTITUTE FOR NONFERROUS METALS BEIJNG
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Problems solved by technology

[0005] Aiming at a series of problems in the prior art such as the formation of new flake-like oxide layer defects during long-term high-temperature homogenization annealing of the defects in the deposited blank, and the incomplete closure of structural defects after thermal deformation processing, the purpose of the present invention is to provide A densification treatment method for spray-formed ultra-high-strength aluminum alloy materials to significantly improve the structure and properties of the material, and improve the quality consistency and reliability of the final product

Method used

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  • Compaction processing method used for spray forming superhigh-intensity aluminum alloy material
  • Compaction processing method used for spray forming superhigh-intensity aluminum alloy material
  • Compaction processing method used for spray forming superhigh-intensity aluminum alloy material

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Embodiment

[0025] The present invention is applied to the 7A93 aluminum alloy registered in China Nonferrous Metals and Alloy Trademark, and its nominal composition range (mass fraction, %) is: Si is not higher than 0.12, Fe is not higher than 0.15, Cu1.6~2.2, Ni is not high 0.08, Mg2.0~2.6, Zn9.8~11.0, Zr0.15~0.30, balance Al and other unavoidable impurities; among them, select a typical alloy composition: 10.8% Zn, 2.5% Mg, 1.9% Cu , 0.15% Zr, the balance Al and other inevitable impurities. Machine the vehicle body from the 7A93 alloy deposition blank prepared by spray forming, such as figure 1 Shown is an optical microstructural image of a 7A93 alloy deposited blank. The 7A93 alloy prepared by spray forming was subjected to different densification treatments. The densification treatment process parameters are shown in Table 1. The densification index of the material was obtained by testing the bulk density of the densified material. After the densification treatment, 440°C×12h+472°C...

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Abstract

The invention discloses a compaction processing method used for a spray forming superhigh-intensity aluminum alloy material, and belongs to the metal material processing technology field. A superhigh-intensity aluminum alloy blank after spraying forming is subjected to covering and air pumping processing and then is placed in a hot isostatic pressing furnace, vacuum-pumping, heating and pressurization are carried out, thermal insulation and pressure maintaining compaction processing is carried out, the scopes of the parameters of the compaction processing are as follows: the temperature is 440-475 DEG C, the pressure intensity is 80-120MPa, and the maintaining time is 0.5-24h. The provided method is advantageous in that structural defects in the spray forming ingot blank can be eliminated effectively, the material compactness is raised, the problem can be avoided that an exterior of a spray forming ingot blank is oxidized by a high temperature and defects are exacerbated further in a high temperature long-time homogenization thermal insulation process in the prior art, material structure and performances are improved substantially, and quality consistency and reliability of final products are raised.

Description

technical field [0001] The invention relates to a densification treatment method for spray-forming ultra-high-strength aluminum alloy materials, and belongs to the technical field of metal material processing. Background technique [0002] Al-Zn-Mg-Cu series (7xxx series) alloys are typical representatives of high-strength aluminum alloys, and their appearance can be traced back to the 1930s. The modernized 7075 and B95 high-strength aluminum alloys are widely used in the manufacture of aircraft parts instead of duralumin, which is commonly used in the aircraft industry. In the 1960s, on the basis of optimizing the traditional preparation and processing technology, by changing the types and contents of various trace elements in the 7xxx series aluminum alloys, and studying the new heat treatment process of the alloy, a variety of alloys with good performance were developed. High-strength aluminum alloys, including 7175, 7475, etc., are used to manufacture various aircraft f...

Claims

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Application Information

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IPC IPC(8): C22F1/053
Inventor 李志辉熊柏青张永安李锡武黄树晖刘红伟王锋
Owner GENERAL RESEARCH INSTITUTE FOR NONFERROUS METALS BEIJNG
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