CN104532065A - Aluminum alloy - Google Patents

Aluminum alloy Download PDF

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Publication number
CN104532065A
CN104532065A CN201410661640.7A CN201410661640A CN104532065A CN 104532065 A CN104532065 A CN 104532065A CN 201410661640 A CN201410661640 A CN 201410661640A CN 104532065 A CN104532065 A CN 104532065A
Authority
CN
China
Prior art keywords
aluminium alloy
aluminum alloy
present
component
aluminium
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201410661640.7A
Other languages
Chinese (zh)
Inventor
王洪初
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuxi Hongsheng Aluminium Industry Co Ltd
Original Assignee
Wuxi Hongsheng Aluminium Industry Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wuxi Hongsheng Aluminium Industry Co Ltd filed Critical Wuxi Hongsheng Aluminium Industry Co Ltd
Priority to CN201410661640.7A priority Critical patent/CN104532065A/en
Publication of CN104532065A publication Critical patent/CN104532065A/en
Pending legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/12Alloys based on aluminium with copper as the next major constituent
    • C22C21/14Alloys based on aluminium with copper as the next major constituent with silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/12Alloys based on aluminium with copper as the next major constituent
    • C22C21/16Alloys based on aluminium with copper as the next major constituent with magnesium

Abstract

The invention discloses an aluminum alloy. The aluminum alloy comprises 1.4-1.6wt% of Mn, 0.7-2wt% of Cu, 0.4-0.7wt% of Fe, 0.2-0.5wt% of Mg, 0.1-0.2wt% of Ti, 0.03-0.07wt% of Si, and 0.02-0.03wt% of Cd. Compared with present aluminum alloys, the aluminum alloy disclosed in the invention has obviously better elongation by adjusting the content of components.

Description

A kind of aluminium alloy
Technical field
The present invention relates to a kind of aluminium alloy with good mechanical strength.
Background technology
Aluminium alloy is a most widely used class non-ferrous metal structured material in industry, widely applies in Aeronautics and Astronautics, automobile, machinofacture, boats and ships and chemical industry.Along with develop rapidly that is scientific and technical and industrial economy, increasing to the demand of aluminium alloy, make the research of aluminium alloy also thereupon deeply.
Summary of the invention
The object of this invention is to provide a kind of aluminium alloy with good mechanical strength.
In order to solve the problems of the technologies described above, the invention provides following technical scheme:
A kind of aluminium alloy, by weight, the component of described aluminium alloy comprises:
Mn1.4-1.6%,Cu 0.7-2%,Fe 0.4-0.7%,Mg 0.2-0.5%,Ti 0.1-0.2%,Si 0.03-0.07%,Cd 0.02-0.03%。
Compared with existing aluminium alloy, the present invention obviously can improve the unit elongation of aluminium alloy by adjustment component concentration.Can be used for the trolley part that manufacture requirements has good extension property.
Embodiment
Below the preferred embodiments of the present invention are described, should be appreciated that preferred embodiment described herein is only for instruction and explanation of the present invention, is not intended to limit the present invention.
embodiment 1
A kind of aluminium alloy, by weight, the component of this aluminium alloy is as follows: Mn1.43%, Cu 0.75%, Fe 0.56%, Mg 0.24%, Ti, 0.15%, Si 0.05%, Cd 0.02%, surplus is aluminium.This aluminium alloy is inevitable impurity under containing preparation condition.By each component 730 DEG C of meltings, be cast into the sheet material that thickness is 5.00mm, tensile strength 184MPa, unit elongation 13.6%.
embodiment 2
A kind of aluminium alloy, by weight, the component of this aluminium alloy is as follows: Mn1.41%, Cu1.7%, Fe 0.55%, Mg 0.24%, Ti 0.15%, Si, 0.05%, Cd 0.03%, surplus is aluminium.This aluminium alloy is inevitable impurity under containing preparation condition.By each component 730 DEG C of meltings, be cast into the sheet material that thickness is 5.00mm, tensile strength 213MPa, unit elongation 16.2%.
Comparative example
By weight, the component of aluminium alloy is as follows: Mn1.43%, Cu 0.75%, Fe 0.56%, Mg 0.24%, Ti, 0.15%, Si 0.05%, surplus is aluminium.This aluminium alloy is inevitable impurity under containing preparation condition.By each component 730 DEG C of meltings, be cast into the sheet material that thickness is 5.00mm, tensile strength 182MPa, unit elongation 11%.
Last it is noted that the foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, although with reference to previous embodiment to invention has been detailed description, for a person skilled in the art, it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature.Within the spirit and principles in the present invention all, any amendment done, equivalent replacement, improvement etc., all should be included within protection scope of the present invention.

Claims (1)

1. an aluminium alloy, by weight, the component of described aluminium alloy comprises:
Mn1.4-1.6%,Cu 0.7-2%,Fe 0.4-0.7%,Mg 0.2-0.5%,Ti 0.1-0.2%,Si 0.03-0.07%,Cd 0.02-0.03%。
CN201410661640.7A 2014-11-19 2014-11-19 Aluminum alloy Pending CN104532065A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410661640.7A CN104532065A (en) 2014-11-19 2014-11-19 Aluminum alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410661640.7A CN104532065A (en) 2014-11-19 2014-11-19 Aluminum alloy

Publications (1)

Publication Number Publication Date
CN104532065A true CN104532065A (en) 2015-04-22

Family

ID=52847682

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410661640.7A Pending CN104532065A (en) 2014-11-19 2014-11-19 Aluminum alloy

Country Status (1)

Country Link
CN (1) CN104532065A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105062292A (en) * 2015-08-06 2015-11-18 苏州好洁清洁器具有限公司 High-corrosion-resistance aluminum alloy pipe material

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5260213A (en) * 1975-11-12 1977-05-18 Sumitomo Aluminium Smelting Co Aluminium alloy for extending
JP2007031825A (en) * 2005-06-22 2007-02-08 Sumitomo Light Metal Ind Ltd Aluminum alloy sheet for battery housing and method for producing the same
CN101054642A (en) * 2006-04-13 2007-10-17 深圳市比克电池有限公司 Aluminum alloy for preparing battery shell
CN101210872A (en) * 2007-12-25 2008-07-02 西南铝业(集团)有限责任公司 3104Aluminum alloy spectral standard sample and preparation method
WO2008114587A1 (en) * 2007-03-20 2008-09-25 Kabushiki Kaisha Kobe Seiko Sho Aluminum alloy material and aluminum alloy brazing sheet
CN101538665A (en) * 2008-03-19 2009-09-23 株式会社神户制钢所 Aluminum alloy plate for battery box and manufacturing method thereof
CN102021457A (en) * 2010-10-27 2011-04-20 中国航空工业集团公司北京航空材料研究院 High-toughness aluminum lithium alloy and preparation method thereof
EP2546373A1 (en) * 2011-07-13 2013-01-16 Aleris Aluminum Koblenz GmbH Method of manufacturing an Al-Mg alloy sheet product

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5260213A (en) * 1975-11-12 1977-05-18 Sumitomo Aluminium Smelting Co Aluminium alloy for extending
JP2007031825A (en) * 2005-06-22 2007-02-08 Sumitomo Light Metal Ind Ltd Aluminum alloy sheet for battery housing and method for producing the same
CN101054642A (en) * 2006-04-13 2007-10-17 深圳市比克电池有限公司 Aluminum alloy for preparing battery shell
WO2008114587A1 (en) * 2007-03-20 2008-09-25 Kabushiki Kaisha Kobe Seiko Sho Aluminum alloy material and aluminum alloy brazing sheet
CN101631884A (en) * 2007-03-20 2010-01-20 株式会社神户制钢所 Aluminum alloy materials and aluminum alloy brazing sheet
CN101210872A (en) * 2007-12-25 2008-07-02 西南铝业(集团)有限责任公司 3104Aluminum alloy spectral standard sample and preparation method
CN101538665A (en) * 2008-03-19 2009-09-23 株式会社神户制钢所 Aluminum alloy plate for battery box and manufacturing method thereof
CN102021457A (en) * 2010-10-27 2011-04-20 中国航空工业集团公司北京航空材料研究院 High-toughness aluminum lithium alloy and preparation method thereof
EP2546373A1 (en) * 2011-07-13 2013-01-16 Aleris Aluminum Koblenz GmbH Method of manufacturing an Al-Mg alloy sheet product

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105062292A (en) * 2015-08-06 2015-11-18 苏州好洁清洁器具有限公司 High-corrosion-resistance aluminum alloy pipe material

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Application publication date: 20150422

RJ01 Rejection of invention patent application after publication