CN106929715A - A kind of antiwear heat resisting aluminium alloy - Google Patents
A kind of antiwear heat resisting aluminium alloy Download PDFInfo
- Publication number
- CN106929715A CN106929715A CN201511004553.5A CN201511004553A CN106929715A CN 106929715 A CN106929715 A CN 106929715A CN 201511004553 A CN201511004553 A CN 201511004553A CN 106929715 A CN106929715 A CN 106929715A
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- Prior art keywords
- aluminium alloy
- heat resisting
- alloy
- antiwear heat
- aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/06—Alloys based on aluminium with magnesium as the next major constituent
- C22C21/08—Alloys based on aluminium with magnesium as the next major constituent with silicon
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
Abstract
The invention belongs to field of aluminum alloys, and in particular to a kind of antiwear heat resisting aluminium alloy.The alloy constitutes and is by weight:Silicon 5-12%, magnesium 3-8%, iron 0.8-1.2%, titanium 2-5%, manganese 0.1-0.5%, strontium 0.8-1.5%, ytterbium 0.01-0.05%, tungsten 0.5-0.8%, copper 0.5-0.8%, aluminium 3-5%, cerium 0.2-0.3%, zinc 0.5-1.8%, chromium 0.8-1.5%.Using composition of the invention, the rub proofness and temperature capability of aluminium alloy can be significantly improved, its hardness has reached 600 or so.
Description
Technical field
The invention belongs to field of aluminum alloys, and in particular to a kind of antiwear heat resisting aluminium alloy.
Background technology
Alusil alloy is a kind of common aluminium alloy, and the change of alumina silica ratio can make hardness produce very big influence, such as silicone content
When less than 7%, alusil alloy has good ductility, and after silicone content exceedes al-si eutectic point (11.7% silicon), alloy
Middle silicon grain substantially increases, and the hardness and wearability of alloy also significantly increase, and existing method carries out electrification by alusil alloy
Learn treatment and the silicon in matrix is retained with etch top layer aluminium, its wearability and hardness are improved to carry out a step, but the method is present
Complex operation, the treatment uppity problem of quality, the research simultaneously for the high temperature fatigue strength of aluminium alloy is also people's research
Emphasis, have at present it is many with good heat resistance can aluminium alloys, but the aluminium alloy with antiwear heat resisting performance is more rare.
The content of the invention
In order to solve the above problems, the invention provides a kind of aluminium alloy of antiwear heat resisting.
Technical scheme is as follows:
A kind of antiwear heat resisting aluminium alloy, the alloy constitutes and is by weight:Silicon 5-12%, magnesium 3-8%, iron 0.8-1.2%, titanium
2-5%, manganese 0.1-0.5%, strontium 0.8-1.5%, ytterbium 0.01-0.05%, tungsten 0.5-0.8%, copper 0.5-0.8%, aluminium 3-5%,
Cerium 0.2-0.3%, zinc 0.5-1.8%, chromium 0.8-1.5%.
Further, above-mentioned antiwear heat resisting aluminium alloy, the preparation method of aluminium alloy is:Described all elements are existed in proportion
Melting at 700-900 DEG C, pours shaping at 800-850 DEG C.
Beneficial effects of the present invention:
Compared with prior art, the aluminium alloy that the present invention is provided, using composition of the invention, can significantly improve the resistance to of aluminium alloy
Mill degree and temperature capability, its hardness have reached 600 or so.
Specific embodiment
Embodiment 1
A kind of antiwear heat resisting aluminium alloy, the alloy constitutes and is by weight:Silicon 5%, magnesium 3%, iron 0.8%, titanium 2%, manganese 0.1%,
Strontium 0.8%, ytterbium 0.01%, tungsten 0.5%, copper 0.5%, aluminium 3%, cerium 0.2%, zinc 0.5%, chromium 0.8%.
Further, above-mentioned antiwear heat resisting aluminium alloy, the preparation method of aluminium alloy is:Described all elements are existed in proportion
Melting at 700-900 DEG C, pours shaping at 800-850 DEG C.
Embodiment 2
A kind of antiwear heat resisting aluminium alloy, the alloy constitutes and is by weight:Silicon 12%, magnesium 8%, iron 1.2%, titanium 5%, manganese 0.5%,
Strontium 1.5%, ytterbium 0.05%, tungsten 0.8%, copper 0.8%, aluminium 5%, cerium 0.3%, zinc 1.8%, chromium 1.5%.
Further, above-mentioned antiwear heat resisting aluminium alloy, the preparation method of aluminium alloy is:Described all elements are existed in proportion
Melting at 900 DEG C, pours shaping at 850 DEG C.
Embodiment 3
A kind of antiwear heat resisting aluminium alloy, the alloy constitutes and is by weight:Silicon 10%, magnesium 7%, iron 1.0%, titanium 3%, manganese
0.4%th, strontium 1.2%, ytterbium 0.02%, tungsten 0.7%, copper 0.7%, aluminium 3-5%, cerium 0.25%, zinc 1.0%, chromium 1.25.
Further, above-mentioned antiwear heat resisting aluminium alloy, the preparation method of aluminium alloy is:Described all elements are existed in proportion
Melting at 800 DEG C, pours shaping at 820 DEG C.
Claims (2)
1. a kind of antiwear heat resisting aluminium alloy, it is characterised in that the alloy constitutes and is by weight:Silicon 5-12%, magnesium 3-8%,
Iron 0.8-1.2%, titanium 2-5%, manganese 0.1-0.5%, strontium 0.8-1.5%, ytterbium 0.01-0.05%, tungsten 0.5-0.8%, copper 0.5-0.8%,
Aluminium 3-5%, cerium 0.2-0.3%, zinc 0.5-1.8%, chromium 0.8-1.5%.
2. as claimed in claim 1, a kind of antiwear heat resisting aluminium alloy, it is characterised in that the preparation method of described aluminium alloy is:
By the melting at 700-900 DEG C in proportion of described all elements, shaping is poured at 800-850 DEG C.
Priority Applications (1)
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CN201511004553.5A CN106929715A (en) | 2015-12-29 | 2015-12-29 | A kind of antiwear heat resisting aluminium alloy |
Applications Claiming Priority (1)
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CN201511004553.5A CN106929715A (en) | 2015-12-29 | 2015-12-29 | A kind of antiwear heat resisting aluminium alloy |
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CN106929715A true CN106929715A (en) | 2017-07-07 |
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CN201511004553.5A Pending CN106929715A (en) | 2015-12-29 | 2015-12-29 | A kind of antiwear heat resisting aluminium alloy |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113637882A (en) * | 2021-08-13 | 2021-11-12 | 贵州电网有限责任公司 | Aluminum alloy corrosion-resistant structural member material for electric power facilities and preparation method thereof |
-
2015
- 2015-12-29 CN CN201511004553.5A patent/CN106929715A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113637882A (en) * | 2021-08-13 | 2021-11-12 | 贵州电网有限责任公司 | Aluminum alloy corrosion-resistant structural member material for electric power facilities and preparation method thereof |
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PB01 | Publication | ||
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WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170707 |