CN107690485A - A kind of brass alloys and its manufacture method - Google Patents
A kind of brass alloys and its manufacture method Download PDFInfo
- Publication number
- CN107690485A CN107690485A CN201680027394.7A CN201680027394A CN107690485A CN 107690485 A CN107690485 A CN 107690485A CN 201680027394 A CN201680027394 A CN 201680027394A CN 107690485 A CN107690485 A CN 107690485A
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- Prior art keywords
- brass alloys
- raw material
- manufacture method
- copper
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/01—Alloys based on copper with aluminium as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/04—Alloys based on copper with zinc as the next major constituent
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Prevention Of Electric Corrosion (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
- Manufacture And Refinement Of Metals (AREA)
Abstract
The invention discloses a kind of brass alloys and its manufacture method, brass alloys include by weight percentage:65%~70% copper, 5.5%~6.5% aluminium, 2%~2.5% iron, 2%~2.5% nickel, 2.8%~3.5% manganese, 0.25%~0.5% lead, 0.6%~1% silicon and 13.5%~19.8% zinc.The present invention increases substantially the intensity, corrosion resistance and wearability of brass alloys, reduces the usage amount and use cost of copper raw material.
Description
Technical field
The present invention relates to brass alloys field, and in particular to a kind of brass alloys and its manufacture method.
Background technology
Brass is most important alloy kind in copper alloy, is widely used in national economy due to inexpensive function admirable
Each field.With alpha+beta mutually for the complex brass of base, its performance can be greatly improved by adding polynary a small amount of alloying element, made
Material produces many new features with practical application foreground, as shape memory function, high resiliency, high intensity, high abrasion, it is anti-corrosion and
Wear vesistance etc..It is high to the content requirement of copper and aluminium because such alloy industry production difficulty is big, not only increase material into
This, and difficulty of processing is big, and especially preceding working procedure founding technology is difficult, produces the continuous casting working procedure that must be used in enormous quantities
Easily produce implosion or appearance cracking.Therefore, in order to avoid shortcoming present in prior art, it is necessary to which prior art is made
Improve.
The content of the invention
It is an object of the invention to overcome shortcoming and deficiency of the prior art, there is provided one kind can improve intensity, corrosion resistance
With the brass alloys of wearability.
It is a further object of the invention to provide a kind of manufacture method of brass alloys.
The present invention is realized by following technical scheme:
A kind of brass alloys, include by weight percentage:65%~70% copper, 5.5%~6.5% aluminium, 2%~
2.5% iron, 2%~2.5% nickel, 2.8%~3.5% manganese, 0.25%~0.5% lead, 0.6%~1% silicon and
13.5%~19.8% zinc.
Further, the brass alloys include by weight percentage:67% copper, 5.5% aluminium, 2% iron, 2.5%
Nickel, 3.5% manganese, 0.25% lead, 1% silicon and 18.25% zinc.
Further, the impurity content of the brass alloys is less than or equal to the 0.5% of brass alloys gross weight.
A kind of manufacture method of brass alloys, comprises the following steps:
(1) dispensing:Raw material are weighed by weight percentage;
(2) melting:The 50% of copper raw material are first put into, the first coverture is laid on copper raw material, carries out melting;Throw again
Enter manganese raw material, the second coverture is laid on manganese raw material;Nickel raw material and iron raw material are put into again, carry out melting;Throw again
Enter remaining 50% copper raw material, carry out melting, stirring;Zinc raw material and silicon material are put into again, carry out melting;Put into again
Aluminium raw material and lead raw material, carry out melting and obtain brass alloys liquation;Brass alloys liquid is stirred, then heating input
Refining agent carries out deslagging refining;Stand insulation and slagging-off;
(3) continuous casting:Insulation carries out horizontal casting billet, and casting speed is 2.5m/h~4m/h, and billet is sawed into spindle;
(4) extrude:Spindle be heated to 630 DEG C~750 DEG C carry out hot extrusions obtaining extruding pipe or extrude rod.
Further, the step (2) is 5min~10min to the mixing time of brass alloys liquid.
Further, a diameter of 140mm of the billet of the step (2).
Further, the first coverture of the step (2) is charcoal, and the second coverture is borax.
Further, the extrusion speed of the step (4) is 15mm/s~35mm/s, and extrusion ratio is 15~35.
Relative to prior art, the present invention produces big intensity by increasing silicon, nickel and the content of manganese, to matrix and consolidated
Molten reinforcing, corrosion resistance can be increased substantially, by the interaction between alloying element, make on brass base forming component it is complicated,
The high wear-resisting phase of uniform and stable distribution, hardness, advantageously reduce the raw material usage amount of copper.
Embodiment
It is clearly and completely described below in conjunction with the technical scheme in the embodiment of the present invention, it is clear that described reality
It is only part of the embodiment of the present invention to apply example, rather than whole embodiments.It is common based on the embodiment in the present invention, this area
The every other embodiment that technical staff is obtained under the premise of creative work is not made, belong to the model that the present invention protects
Enclose.
A kind of brass alloys, include by weight percentage:65%~70% copper, 5.5%~6.5% aluminium, 2%~
2.5% iron, 2%~2.5% nickel, 2.8%~3.5% manganese, 0.25%~0.5% lead, 0.6%~1% silicon and
13.5%~19.8% zinc.
As a kind of embodiment, brass alloys include by weight percentage:67% copper, 5.5% aluminium, 2%
Iron, 2.5% nickel, 3.5% manganese, 0.25% lead, 1% silicon and 18.25% zinc.
The impurity content of brass alloys is less than or equal to the 0.5% of brass alloys gross weight.
A kind of manufacture method of brass alloys, comprises the following steps:
(1) dispensing:Raw material are weighed by weight percentage.
(2) melting:The 50% of copper raw material are first put into, the first coverture is laid on copper raw material, carries out melting;Throw again
Enter manganese raw material, the second coverture is laid on manganese raw material;Nickel raw material and iron raw material are put into again, carry out melting;Throw again
Enter remaining 50% copper raw material, carry out melting, stirring;Zinc raw material and silicon material are put into again, carry out melting;Put into again
Aluminium raw material and lead raw material, carry out melting and obtain brass alloys liquation;Brass alloys liquid is stirred, then heating input
Refining agent carries out deslagging refining;Stand insulation and slagging-off;Mixing time to brass alloys liquid is 5min~10min.Billet
A diameter of 140mm.First coverture is charcoal, and the second coverture is borax.By putting into manganese, nickel and silicon successively in fusion process
Deng raw material, improve brass alloys performance.
(3) continuous casting:Insulation carries out horizontal casting billet, and casting speed is 2.5m/h~4m/h, and billet is sawed into spindle.
(4) extrude:Spindle be heated to 630 DEG C~750 DEG C carry out hot extrusions obtaining extruding pipe or extrude rod.Extrusion speed
For 15mm/s~35mm/s, extrusion ratio is 15~35.
By adjusting silicon, nickel and the proportional quantity of manganese, the corrosion resistance and wearability of brass alloys are adjusted, does not interfere with difficult processing
Degree, so as to reduce the proportional quantity of copper and aluminium, reduce use cost.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
God any modification, equivalent substitution and improvements made etc., should be included in the scope of the protection with principle.
Claims (8)
- A kind of 1. brass alloys, it is characterised in that:Include by weight percentage:65%~70% copper, 5.5%~6.5% Aluminium, 2%~2.5% iron, 2%~2.5% nickel, 2.8%~3.5% manganese, 0.25%~0.5% lead, 0.6%~ 1% silicon and 13.5%~19.8% zinc.
- 2. brass alloys according to claim 1, it is characterised in that:The brass alloys include by weight percentage: 67% copper, 5.5% aluminium, 2% iron, 2.5% nickel, 3.5% manganese, 0.25% lead, 1% silicon and 18.25% Zinc.
- 3. brass alloys according to claim 1, it is characterised in that:The impurity content of the brass alloys is less than or equal to The 0.5% of brass alloys gross weight.
- A kind of a kind of 4. manufacture method of brass alloys as described in any one of claims 1 to 3, it is characterised in that:Including with Lower step:(1) dispensing:Raw material are weighed by weight percentage;(2) melting:The 50% of copper raw material are first put into, the first coverture is laid on copper raw material, carries out melting;Manganese is put into again Raw material, the second coverture is laid on manganese raw material;Nickel raw material and iron raw material are put into again, carry out melting;Put into again remaining Under 50% copper raw material, carry out melting, stirring;Zinc raw material and silicon material are put into again, carry out melting;Aluminium original is put into again Material and lead raw material, carry out melting and obtain brass alloys liquation;Brass alloys liquid is stirred, then the refining of heating input Agent carries out deslagging refining;Stand insulation and slagging-off;(3) continuous casting:Insulation carries out horizontal casting billet, and casting speed is 2.5m/h~4m/h, and billet is sawed into spindle;(4) extrude:Spindle be heated to 630 DEG C~750 DEG C carry out hot extrusions obtaining extruding pipe or extrude rod.
- 5. the manufacture method of brass alloys according to claim 1, it is characterised in that:The step (2) is to brass alloys The mixing time of liquid is 5min~10min.
- 6. the manufacture method of brass alloys according to claim 4, it is characterised in that:The billet of the step (2) it is straight Footpath is 140mm.
- 7. the manufacture method of brass alloys according to claim 4, it is characterised in that:First covering of the step (2) Agent is charcoal, and the second coverture is borax.
- 8. the manufacture method of brass alloys according to claim 4, it is characterised in that:The extrusion speed of the step (4) For 15mm/s~35mm/s, extrusion ratio is 15~35.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/CN2016/103187 WO2018076161A1 (en) | 2016-10-25 | 2016-10-25 | Brass alloy and manufacturing method therefor |
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CN107690485A true CN107690485A (en) | 2018-02-13 |
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CN201680027394.7A Pending CN107690485A (en) | 2016-10-25 | 2016-10-25 | A kind of brass alloys and its manufacture method |
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WO (1) | WO2018076161A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110438355A (en) * | 2019-08-28 | 2019-11-12 | 福建工程学院 | A kind of brass alloys grain refiner and its preparation process and application method |
CN112695216A (en) * | 2020-12-08 | 2021-04-23 | 宁波正元铜合金有限公司 | Preparation method of manganese brass alloy with three strengthening phases |
CN114540665A (en) * | 2021-11-11 | 2022-05-27 | 佛山中国发明成果转化研究院 | Copper alloy with good bending performance and preparation method thereof |
CN115198139A (en) * | 2022-08-31 | 2022-10-18 | 宁波金田铜业(集团)股份有限公司 | Wear-resistant brass alloy bar and preparation method thereof |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115807175B (en) * | 2022-12-22 | 2023-12-26 | 上海太洋科技有限公司 | Preparation method of large-size beryllium copper alloy |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104894430A (en) * | 2015-06-29 | 2015-09-09 | 宁波金田铜业(集团)股份有限公司 | Wear-resistant easy-to-cut brass pipe material and method of using same to manufacture brass pipe |
CN105247085A (en) * | 2013-03-12 | 2016-01-13 | 迪尔金属合作两合公司 | Use of a copper-zinc alloy |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005087957A1 (en) * | 2004-03-12 | 2005-09-22 | Sumitomo Metal Industries, Ltd. | Copper alloy and method for production thereof |
DE102004058318B4 (en) * | 2004-12-02 | 2006-09-28 | Diehl Metall Stiftung & Co.Kg | Use of a copper-zinc alloy |
DE102005015467C5 (en) * | 2005-04-04 | 2024-02-29 | Diehl Brass Solutions Stiftung & Co. Kg | Using a copper-zinc alloy |
-
2016
- 2016-10-25 CN CN201680027394.7A patent/CN107690485A/en active Pending
- 2016-10-25 WO PCT/CN2016/103187 patent/WO2018076161A1/en active Application Filing
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105247085A (en) * | 2013-03-12 | 2016-01-13 | 迪尔金属合作两合公司 | Use of a copper-zinc alloy |
CN104894430A (en) * | 2015-06-29 | 2015-09-09 | 宁波金田铜业(集团)股份有限公司 | Wear-resistant easy-to-cut brass pipe material and method of using same to manufacture brass pipe |
Non-Patent Citations (2)
Title |
---|
郭莉等: "《冷凝管生产技术》", 28 February 2007, 冶金工业出版社 * |
钟卫佳: "《铜加工技术实用手册》", 31 January 2007, 冶金工业出版社 * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110438355A (en) * | 2019-08-28 | 2019-11-12 | 福建工程学院 | A kind of brass alloys grain refiner and its preparation process and application method |
CN110438355B (en) * | 2019-08-28 | 2021-04-02 | 福建工程学院 | Brass alloy grain refiner, and preparation process and use method thereof |
CN112695216A (en) * | 2020-12-08 | 2021-04-23 | 宁波正元铜合金有限公司 | Preparation method of manganese brass alloy with three strengthening phases |
CN112695216B (en) * | 2020-12-08 | 2021-12-28 | 宁波正元铜合金有限公司 | Preparation method of manganese brass alloy with three strengthening phases |
CN114540665A (en) * | 2021-11-11 | 2022-05-27 | 佛山中国发明成果转化研究院 | Copper alloy with good bending performance and preparation method thereof |
CN115198139A (en) * | 2022-08-31 | 2022-10-18 | 宁波金田铜业(集团)股份有限公司 | Wear-resistant brass alloy bar and preparation method thereof |
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WO2018076161A1 (en) | 2018-05-03 |
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