CN103952589A - Copper alloy - Google Patents

Copper alloy Download PDF

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Publication number
CN103952589A
CN103952589A CN201410206768.4A CN201410206768A CN103952589A CN 103952589 A CN103952589 A CN 103952589A CN 201410206768 A CN201410206768 A CN 201410206768A CN 103952589 A CN103952589 A CN 103952589A
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CN
China
Prior art keywords
alloy
copper alloy
copper
nickel
rare earth
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
CN201410206768.4A
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Chinese (zh)
Inventor
王新海
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Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201410206768.4A priority Critical patent/CN103952589A/en
Publication of CN103952589A publication Critical patent/CN103952589A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a copper alloy and relates to the technical field of alloy materials. The copper alloy comprises the following components by weight percent: 7.5%-8.5% of aluminum, 2.5%-3.0% of iron, 2% of phosphorus, 0.1%-0.3% of rare earth, 1%-2% of nickel and the balance of copper. The copper alloy disclosed by the invention is a six-element alloy, not only has the performances of an aluminum-bronze alloy, but also integrates a nickel alloy and rare earth; the copper alloy disclosed by the invention has relatively high hardness and toughness, good mechanical properties and manufacturability and relatively high stability and can be used after processing without any thermal treatment, so that the processing time is shortened and the production cost is reduced.

Description

Copper alloy
Technical field
The present invention relates to technical field of alloy material, be specifically related to a kind of copper alloy with high rigidity and high tenacity.
Background technology
Copper alloy has the history of several thousand in China, people do arms, pot for cooking rice, the armor, tripod etc. with it in ancient times, and modern is mainly used in copper alloy the various machineries such as Aeronautics and Astronautics, military project, high ferro, has mechanical place just to have copper alloy.Xantal is a kind of important Cu alloy material, aluminum content is generally no more than 11.5%, aluminum current bronze is generally made up of aluminium, iron and copper component, after processing, need to heat-treat strengthening, can cause like this process period long higher with cost, although its strength ratio tinbronze is high, high temperature oxidation resistance is also better, and hardness and the toughness of current xantal material can't be satisfactory.
Summary of the invention
The invention provides an Albatra metal-, need the poor problem of heat treatment reinforcement, hardness and toughness to solve the processing of existing copper alloy.
The technical solution adopted for the present invention to solve the technical problems is:
One Albatra metal-, by mass percentage, comprises following component:
Aluminium: 7.5%~8.5%;
Iron: 2.5%~3.0%;
Phosphorus: 2%;
Rare earth: 0.1%~0.3%;
Nickel: 1%~2%;
Surplus is copper.
Preferably, above-mentioned copper, aluminium, iron, nickel are electrolytic metal, can ensure the purity of copper alloy, can ensure, not containing cobalt, therefore, to have radiation-resistant advantage.
Copper alloy of the present invention is a kind of hexa-atomic alloy, in possessing McGill metals performance, also increase incorporating of nickelalloy and rare earth, nickel is a kind of noble metal, its feature is to have higher intensity and plasticity, high solidity to corrosion, infusibility (1455 DEG C of fusing points) and special physicals (ferromegnetism, high electrovacuum performance etc.), rare earth alloy can play the effect that improves toughness, thereby copper alloy of the present invention has higher hardness and toughness, good mechanical property and manufacturability, higher stability, this alloy need not any thermal treatment, process and can use, shorten process period, reduce production cost.
Embodiment
Below in conjunction with specific embodiment, the present invention is described in further detail.
One Albatra metal-, by mass percentage, comprises following component:
Aluminium: 7.5%~8.5%;
Iron: 2.5%~3.0%;
Phosphorus: 2%;
Rare earth: 0.1%~0.3%;
Nickel: 1%~2%;
Surplus is copper.

Claims (2)

1. an Albatra metal-, is characterized in that by mass percentage, comprises following component:
Aluminium: 7.5%~8.5%;
Iron: 2.5%~3.0%;
Phosphorus: 2%;
Rare earth: 0.1%~0.3%;
Nickel: 1%~2%;
Surplus is copper.
2. copper alloy according to claim 1, is characterized in that copper, aluminium, iron, nickel are electrolytic metal.
CN201410206768.4A 2014-05-12 2014-05-12 Copper alloy Pending CN103952589A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410206768.4A CN103952589A (en) 2014-05-12 2014-05-12 Copper alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410206768.4A CN103952589A (en) 2014-05-12 2014-05-12 Copper alloy

Publications (1)

Publication Number Publication Date
CN103952589A true CN103952589A (en) 2014-07-30

Family

ID=51329935

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410206768.4A Pending CN103952589A (en) 2014-05-12 2014-05-12 Copper alloy

Country Status (1)

Country Link
CN (1) CN103952589A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106636710A (en) * 2016-11-08 2017-05-10 中航装甲科技有限公司 Preparation method of graphene composite armor material

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101643867A (en) * 2009-08-28 2010-02-10 镇江汇通金属成型有限公司 High performance copper casting alloy and preparation method thereof
CN101649858A (en) * 2009-08-20 2010-02-17 浙江中达轴承有限公司 Steel-based copper alloy dual-metal sliding bearing and preparation method thereof
CN102296206A (en) * 2011-09-08 2011-12-28 中南大学 High-strength abrasion-resistant wrought aluminum bronze alloy
CN102560187A (en) * 2012-03-10 2012-07-11 甘肃大鑫铜业有限责任公司 Copper alloy for electrified railway contact network and preparation method thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101649858A (en) * 2009-08-20 2010-02-17 浙江中达轴承有限公司 Steel-based copper alloy dual-metal sliding bearing and preparation method thereof
CN101643867A (en) * 2009-08-28 2010-02-10 镇江汇通金属成型有限公司 High performance copper casting alloy and preparation method thereof
CN102296206A (en) * 2011-09-08 2011-12-28 中南大学 High-strength abrasion-resistant wrought aluminum bronze alloy
CN102560187A (en) * 2012-03-10 2012-07-11 甘肃大鑫铜业有限责任公司 Copper alloy for electrified railway contact network and preparation method thereof

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106636710A (en) * 2016-11-08 2017-05-10 中航装甲科技有限公司 Preparation method of graphene composite armor material

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Application publication date: 20140730

RJ01 Rejection of invention patent application after publication