CN109706365A - A kind of aluminum alloy materials - Google Patents

A kind of aluminum alloy materials Download PDF

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Publication number
CN109706365A
CN109706365A CN201711012948.9A CN201711012948A CN109706365A CN 109706365 A CN109706365 A CN 109706365A CN 201711012948 A CN201711012948 A CN 201711012948A CN 109706365 A CN109706365 A CN 109706365A
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CN
China
Prior art keywords
parts
aluminum alloy
alloy materials
aluminium
present
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
CN201711012948.9A
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Chinese (zh)
Inventor
吕淑敏
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.)
Qingdao Sea Through Department Of Science And Technology Consulting Co Ltd
Original Assignee
Qingdao Sea Through Department Of Science And Technology Consulting 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.)
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Priority to CN201711012948.9A priority Critical patent/CN109706365A/en
Publication of CN109706365A publication Critical patent/CN109706365A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a kind of aluminum alloy materials, the raw material comprising following component: 3-5 parts of manganese, 2-4 parts of titanium, 6-8 parts of magnesium, 4-6 parts of chromium, 3-6 parts of bismuth, 1-3 parts of niobium, 2-3 parts of strontium, 5-6 parts of barium, 4-7 parts of nickel, 12-16 parts of iron, 8-13 parts of copper, 35-42 parts of aluminium.Hardness number of the present invention is high, and intensity good combination property, heat resistance is strong, and oxidation resistance is significant, high-wearing feature.

Description

A kind of aluminum alloy materials
Technical field
The present invention relates to technical field of alloy more particularly to a kind of aluminum alloy materials.
Background technique
Aluminium alloy is most widely used one kind non-ferrous metal structural material in industry, in Aeronautics and Astronautics, automobile, machinery It has been widely applied in manufacture, ship and chemical industry.The rapid development of industrial economy, the demand day to aluminum alloy piping welding structural member Benefit increases, and the Research on Weldability enabled aluminum alloy to is also goed deep into therewith, and aluminium alloy is to apply most alloys, but aluminium alloy is hard at present It spends the engineering properties or heat resistance etc. such as not high, its intensity to need to enhance, to adapt to the requirement of more high-tech sector.
Summary of the invention
Above-mentioned to solve the problems, such as, the present invention provides a kind of hardness number height, and intensity good combination property, heat resistance is strong, Oxidation resistance is significant, the aluminum alloy materials of high-wearing feature.
The present invention solves the technical solution that above-mentioned technical problem uses are as follows: a kind of aluminum alloy materials include following component Raw material:
3-5 parts of manganese, 2-4 parts of titanium, 6-8 parts of magnesium, 4-6 parts of chromium, 3-6 parts of bismuth, 1-3 parts of niobium, 2-3 parts of strontium, 5-6 parts of barium, 4-7 parts of nickel, 12-16 parts of iron, 8-13 parts of copper, 35-42 parts of aluminium.
Above-mentioned aluminum alloy materials, the raw material comprising following component:
4 parts of manganese, 3 parts of titanium, 7 parts of magnesium, 5 parts of chromium, 5 parts of bismuth, 2 parts of niobium, 2.6 parts of strontium, 5.5 parts of barium, 6 parts of nickel, 14 parts of iron, 11 parts of copper, 39 parts of aluminium.
The present invention solves beneficial effect brought by technical problem and is: hardness number of the present invention is high, intensity good combination property, Heat resistance is strong, and oxidation resistance is significant, high-wearing feature.
Specific embodiment
The present invention is described in further details combined with specific embodiments below.
Embodiment 1
A kind of aluminum alloy materials, the raw material comprising following component:
3 parts of manganese, 2 parts of titanium, 6 parts of magnesium, 4 parts of chromium, 3 parts of bismuth, 1 part of niobium, 2 parts of strontium, 5 parts of barium, 4 parts of nickel, 12 parts of iron, 8 parts of copper, aluminium 35 Part.
Embodiment 2
A kind of aluminum alloy materials, the raw material comprising following component:
4 parts of manganese, 3 parts of titanium, 7 parts of magnesium, 5 parts of chromium, 5 parts of bismuth, 2 parts of niobium, 2.6 parts of strontium, 5.5 parts of barium, 6 parts of nickel, 14 parts of iron, 11 parts of copper, 39 parts of aluminium.
Embodiment 3
A kind of aluminum alloy materials, the raw material comprising following component:
5 parts of manganese, 4 parts of titanium, 8 parts of magnesium, 6 parts of chromium, 6 parts of bismuth, 3 parts of niobium, 3 parts of strontium, 6 parts of barium, 7 parts of nickel, 16 parts of iron, 13 parts of copper, aluminium 42 Part.
Above-mentioned, although specific embodiments of the present invention have been described, not to the limit of the scope of the present invention System, those skilled in the art should understand that, based on the technical solutions of the present invention, those skilled in the art do not need to pay The various modifications or changes that creative work can be made out are still within protection scope of the present invention.

Claims (2)

1. a kind of aluminum alloy materials, it is characterised in that: the raw material comprising following component:
3-5 parts of manganese, 2-4 parts of titanium, 6-8 parts of magnesium, 4-6 parts of chromium, 3-6 parts of bismuth, 1-3 parts of niobium, 2-3 parts of strontium, 5-6 parts of barium, 4-7 parts of nickel, 12-16 parts of iron, 8-13 parts of copper, 35-42 parts of aluminium.
2. aluminum alloy materials according to claim 1, it is characterised in that: the raw material comprising following component:
4 parts of manganese, 3 parts of titanium, 7 parts of magnesium, 5 parts of chromium, 5 parts of bismuth, 2 parts of niobium, 2.6 parts of strontium, 5.5 parts of barium, 6 parts of nickel, 14 parts of iron, 11 parts of copper, 39 parts of aluminium.
CN201711012948.9A 2017-10-26 2017-10-26 A kind of aluminum alloy materials Pending CN109706365A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711012948.9A CN109706365A (en) 2017-10-26 2017-10-26 A kind of aluminum alloy materials

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711012948.9A CN109706365A (en) 2017-10-26 2017-10-26 A kind of aluminum alloy materials

Publications (1)

Publication Number Publication Date
CN109706365A true CN109706365A (en) 2019-05-03

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711012948.9A Pending CN109706365A (en) 2017-10-26 2017-10-26 A kind of aluminum alloy materials

Country Status (1)

Country Link
CN (1) CN109706365A (en)

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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20190503

WD01 Invention patent application deemed withdrawn after publication