CN108660342A - A kind of aluminum matrix composite - Google Patents

A kind of aluminum matrix composite Download PDF

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Publication number
CN108660342A
CN108660342A CN201810637125.3A CN201810637125A CN108660342A CN 108660342 A CN108660342 A CN 108660342A CN 201810637125 A CN201810637125 A CN 201810637125A CN 108660342 A CN108660342 A CN 108660342A
Authority
CN
China
Prior art keywords
weight percent
matrix composite
aluminum matrix
aluminum alloy
nickel
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
CN201810637125.3A
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Chinese (zh)
Inventor
叶燕青
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.)
Taicang Source Metal Technology Co Ltd
Original Assignee
Taicang Source Metal Technology 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 Taicang Source Metal Technology Co Ltd filed Critical Taicang Source Metal Technology Co Ltd
Priority to CN201810637125.3A priority Critical patent/CN108660342A/en
Publication of CN108660342A publication Critical patent/CN108660342A/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
    • C22C21/16Alloys based on aluminium with copper as the next major constituent with magnesium
    • 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
    • C22C21/18Alloys based on aluminium with copper as the next major constituent with zinc

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Arc Welding In General (AREA)

Abstract

The invention discloses a kind of aluminum matrix composites, the aluminum matrix composite includes zinc, copper, aluminium, magnesium and nickel, weight percent based on the aluminum matrix composite is counted for 100wt%, the weight percent of copper is more than 1wt% and is not more than 10wt%, the weight percent of zinc is more than 0.5wt% and is not more than 3wt%, the weight percent of magnesium is more than 0.02wt% and is not more than 3wt%, and the weight percent of nickel is more than 1wt% and is not more than 5wt%, and surplus is aluminium.The beneficial effects of the invention are as follows:The mechanics and welding performance of aluminum alloy materials are effectively improved, aluminum alloy materials good combination property preferably meets requirement of the modern development in science and technology to aluminum alloy junction component top load and lighting.

Description

A kind of aluminum matrix composite
Technical field
The present invention relates to a kind of composite material more particularly to a kind of aluminum matrix composites.
Background technology
With the fast development of communication and microelectric technique, integrated circuit is constantly to high power, micromation and lightweight side To development, this greatly improves circuit and device itself cooling requirements, while also mating electronic package material being given to propose higher Requirement.Not requiring nothing more than material has outside high-termal conductivity and adjustable coefficient of thermal expansion, and it is also desirable to have smaller heavy Amount and volume, higher consistency and better air-tightness.
The features such as high strength alumin ium alloy has intensity high, and plasticity is good, and solderability is good and fine corrosion resistance, is answered extensively It is many dual-use at present for the various structural members and the high high stress welding structural element of other intensity requirements of aircraft Indispensable important feature material in aircraft, transport facility.As the development of space flight and aviation technology is to the day of material requirements Benefit improves, and researcher is just putting forth effort mining inetesity higher, and the high-strength weldable aluminum alloy of high comprehensive performance is at present raising weldering The comprehensive performance of the high strength alumin ium alloy connect is reduced and is fought since intensity improves mainly while pursuing material high intensity Stress corrosion performance, fracture toughness and fatigue strength etc. cause harmful effect.
Therefore, to solve the above problems, providing a kind of new technical solution.
Invention content
The present invention provides a kind of aluminum matrix composite.
The technical solution adopted by the present invention is:
A kind of aluminum matrix composite, the aluminum matrix composite include zinc, copper, aluminium, magnesium and nickel, the weight based on the aluminum matrix composite It measures percentage to count for 100wt%, the weight percent of copper is more than 1wt% and is not more than 10wt%, and the weight percent of zinc is more than 0.5wt% and it is not more than 3wt%, the weight percent of magnesium is more than 0.02wt% and is not more than 3wt%, and the weight percent of nickel is big In 1wt% and it is not more than 5wt%, surplus is aluminium.
Further, the weight percent of the copper is more than 2wt% and is not more than 8wt%.
Further, the weight percent of the zinc is more than 1wt% and is not more than 2wt%.
Further, the weight percent of the magnesium is more than 0.5wt% and is not more than 2wt%.
Further, the weight percent of the nickel is more than 2wt% and is not more than 5wt%.
The beneficial effects of the invention are as follows:Effectively improve the mechanics and welding performance of aluminum alloy materials, aluminum alloy materials Good combination property preferably meets requirement of the modern development in science and technology to aluminum alloy junction component top load and lighting.
Specific implementation mode
In order to deepen the understanding of the present invention, below in conjunction with embodiment, the invention will be further described, the embodiment It is only used for explaining the present invention, not restrict the protection scope of the present invention.
Embodiment 1
A kind of aluminum matrix composite, the aluminum matrix composite include zinc, copper, aluminium, magnesium and nickel, the weight based on the aluminum matrix composite It measures percentage to count for 100wt%, the weight percent of copper is more than 2wt%, the weight percent 0.5wt% of zinc, the weight hundred of magnesium Divide than 0.05wt%, the weight percent 1.5wt% of nickel, surplus is aluminium.
The beneficial effects of the invention are as follows:Effectively improve the mechanics and welding performance of aluminum alloy materials, aluminum alloy materials Good combination property preferably meets requirement of the modern development in science and technology to aluminum alloy junction component top load and lighting.
Embodiment 2
A kind of aluminum matrix composite, the aluminum matrix composite include zinc, copper, aluminium, magnesium and nickel, the weight based on the aluminum matrix composite It measures percentage to count for 100wt%, the weight percent 5wt% of copper, the weight percent 1.5wt% of zinc, the weight percent of magnesium 2wt%, the weight percent 3wt% of nickel, surplus is aluminium.
The beneficial effects of the invention are as follows:Effectively improve the mechanics and welding performance of aluminum alloy materials, aluminum alloy materials Good combination property preferably meets requirement of the modern development in science and technology to aluminum alloy junction component top load and lighting.
Embodiment 3
A kind of aluminum matrix composite, the aluminum matrix composite include zinc, copper, aluminium, magnesium and nickel, the weight based on the aluminum matrix composite It measures percentage to count for 100wt%, the weight percent 10wt% of copper, the weight percent 3wt% of zinc, the weight percent of magnesium 3wt%, the weight percent 5wt% of nickel, surplus is aluminium.
The beneficial effects of the invention are as follows:Effectively improve the mechanics and welding performance of aluminum alloy materials, aluminum alloy materials Good combination property preferably meets requirement of the modern development in science and technology to aluminum alloy junction component top load and lighting.
The above described is only a preferred embodiment of the present invention, being not the limit for making any other form to the present invention System, and according to the technical essence of the invention made by any modification or equivalent variations, still fall within present invention model claimed It encloses.

Claims (5)

1. a kind of aluminum matrix composite, it is characterised in that:The aluminum matrix composite includes zinc, copper, aluminium, magnesium and nickel, is based on the aluminium The weight percent of based composites is counted for 100wt%, and the weight percent of copper is more than 1wt% and is not more than 10wt%, zinc Weight percent is more than 0.5wt% and is not more than 3wt%, and the weight percent of magnesium is more than 0.02wt% and is not more than 3wt%, nickel Weight percent be more than 1wt% and be not more than 5wt%, surplus is aluminium.
2. a kind of aluminum matrix composite according to claim 1, it is characterised in that:The weight percent of the copper is more than 2wt% and be not more than 8wt%.
3. a kind of aluminum matrix composite according to claim 1, it is characterised in that:The weight percent of the zinc is more than 1wt% and be not more than 2wt%.
4. a kind of aluminum matrix composite according to claim 1, it is characterised in that:The weight percent of the magnesium is more than 0.5wt% and be not more than 2wt%.
5. a kind of aluminum matrix composite according to claim 1, it is characterised in that:The weight percent of the nickel is more than 2wt% and be not more than 5wt%.
CN201810637125.3A 2018-06-20 2018-06-20 A kind of aluminum matrix composite Pending CN108660342A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810637125.3A CN108660342A (en) 2018-06-20 2018-06-20 A kind of aluminum matrix composite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810637125.3A CN108660342A (en) 2018-06-20 2018-06-20 A kind of aluminum matrix composite

Publications (1)

Publication Number Publication Date
CN108660342A true CN108660342A (en) 2018-10-16

Family

ID=63772162

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810637125.3A Pending CN108660342A (en) 2018-06-20 2018-06-20 A kind of aluminum matrix composite

Country Status (1)

Country Link
CN (1) CN108660342A (en)

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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20181016

WD01 Invention patent application deemed withdrawn after publication