CN108501472A - A kind of high rigidity metal product - Google Patents
A kind of high rigidity metal product Download PDFInfo
- Publication number
- CN108501472A CN108501472A CN201810424537.9A CN201810424537A CN108501472A CN 108501472 A CN108501472 A CN 108501472A CN 201810424537 A CN201810424537 A CN 201810424537A CN 108501472 A CN108501472 A CN 108501472A
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- CN
- China
- Prior art keywords
- parts
- layer material
- ingredient
- high rigidity
- brass
- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
- B32B15/015—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium the said other metal being copper or nickel or an alloy thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/017—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of aluminium or an aluminium alloy, another layer being formed of an alloy based on a non ferrous metal other than aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C30/00—Alloys containing less than 50% by weight of each constituent
- C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
Abstract
The invention discloses a kind of high rigidity metal products, including：First layer material and the second layer material, first layer material are made of titanium valve, magnesium, brass, manganese and silicon, and second layer material is made of iron, aluminium, platinum and barium, parts by weight shared by each ingredient in first layer material：1.1 2.2 parts of 41 52 parts of titanium valve, 61 69 parts of magnesium, 16 22 parts of brass, 4.1 5.2 parts of manganese and silicon, parts by weight shared by each ingredient in second layer material：2.1 3.6 parts of 20 30 parts of iron, 10 19 parts of aluminium, 0.9 1.8 parts of platinum and barium.By the above-mentioned means, high rigidity metal product provided by the invention, has higher hardness.
Description
Technical field
The present invention relates to metal material fields, more particularly to a kind of high rigidity metal product.
Background technology
With the continuous progress of science, the place for using alloy is more and more extensive, and the either vehicles, life is used
Product, household items etc., such as：Automobile industry, building material industry, kitchen article, alloy articles for use have risen quite big in daily life
Effect, but now alloy materials many on the market, hardness is poor, of high cost, especially in the various traffic works being prone to wear out
Tool engine art is particularly acute.
Invention content
The invention mainly solves the technical problem of providing a kind of high rigidity metal products, have higher hardness.
In order to solve the above technical problems, one aspect of the present invention is：A kind of high rigidity metal product is provided,
Including：First layer material and the second layer material, first layer material are made of titanium valve, magnesium, brass, manganese and silicon, and described second
Layer material is made of iron, aluminium, platinum and barium, parts by weight shared by each ingredient in first layer material：41-52 parts of titanium valve, magnesium 61-
1.1-2.2 parts of 69 parts, 16-22 parts of brass, 4.1-5.2 parts of manganese and silicon, parts by weight shared by each ingredient in second layer material：
2.1-3.6 parts of 20-30 parts of iron, 10-19 parts of aluminium, 0.9-1.8 parts of platinum and barium, the first layer material exists in the high rigidity metal product
The top of second layer material, and connected by way of seamless welding.
In a preferred embodiment of the present invention, parts by weight shared by each ingredient in first layer material：41 parts of titanium valve,
1.1 parts of 61 parts of magnesium, 16 parts of brass, 4.1 parts of manganese and silicon, parts by weight shared by each ingredient in second layer material：20 parts of iron, aluminium
2.1 parts of 10 parts, 0.9 part of platinum and barium.
In a preferred embodiment of the present invention, parts by weight shared by each ingredient in first layer material：43 parts of titanium valve,
1.3 parts of 62 parts of magnesium, 17 parts of brass, 4.5 parts of manganese and silicon, parts by weight shared by each ingredient in second layer material：22 parts of iron, aluminium
2.3 parts of 11 parts, 1.1 parts of platinum and barium.
In a preferred embodiment of the present invention, parts by weight shared by each ingredient in first layer material：44 parts of titanium valve,
1.5 parts of 63 parts of magnesium, 18 parts of brass, 4.6 parts of manganese and silicon, parts by weight shared by each ingredient in second layer material：23 parts of iron, aluminium
2.5 parts of 12 parts, 1.3 parts of platinum and barium.
In a preferred embodiment of the present invention, parts by weight shared by each ingredient in first layer material：46 parts of titanium valve,
1.7 parts of 65 parts of magnesium, 19 parts of brass, 4.7 parts of manganese and silicon, parts by weight shared by each ingredient in second layer material：25 parts of iron, aluminium
2.7 parts of 17 parts, 1.5 parts of platinum and barium.
In a preferred embodiment of the present invention, parts by weight shared by each ingredient in first layer material：49 parts of titanium valve,
1.9 parts of 67 parts of magnesium, 20 parts of brass, 4.9 parts of manganese and silicon, parts by weight shared by each ingredient in second layer material：28 parts of iron, aluminium
2.9 parts of 19 parts, 1.6 parts of platinum and barium.
The beneficial effects of the invention are as follows：A kind of high rigidity metal product that the present invention points out has higher hardness.
Specific implementation mode
The technical scheme in the embodiments of the invention will be clearly and completely described below, it is clear that described implementation
Example is only a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, this field is common
All other embodiment that technical staff is obtained without making creative work belongs to the model that the present invention protects
It encloses.
Embodiment 1：
Parts by weight shared by each ingredient in first layer material：41 parts of titanium valve, 61 parts of magnesium, 16 parts of brass, 4.1 parts of manganese and silicon
1.1 parts, parts by weight shared by each ingredient in second layer material：2.1 parts of 20 parts of iron, 10 parts of aluminium, 0.9 part of platinum and barium.
Embodiment 2：
Parts by weight shared by each ingredient in first layer material：43 parts of titanium valve, 62 parts of magnesium, 17 parts of brass, 4.5 parts of manganese and silicon
1.3 parts, parts by weight shared by each ingredient in second layer material：2.3 parts of 22 parts of iron, 11 parts of aluminium, 1.1 parts of platinum and barium.
Embodiment 3：
Parts by weight shared by each ingredient in first layer material：44 parts of titanium valve, 63 parts of magnesium, 18 parts of brass, 4.6 parts of manganese and silicon
1.5 parts, parts by weight shared by each ingredient in second layer material：2.5 parts of 23 parts of iron, 12 parts of aluminium, 1.3 parts of platinum and barium.
Embodiment 4：
Parts by weight shared by each ingredient in first layer material：46 parts of titanium valve, 65 parts of magnesium, 19 parts of brass, 4.7 parts of manganese and silicon
1.7 parts, parts by weight shared by each ingredient in second layer material：2.7 parts of 25 parts of iron, 17 parts of aluminium, 1.5 parts of platinum and barium.
Embodiment 5：
Parts by weight shared by each ingredient in first layer material：49 parts of titanium valve, 67 parts of magnesium, 20 parts of brass, 4.9 parts of manganese and silicon
1.9 parts, parts by weight shared by each ingredient in second layer material：2.9 parts of 28 parts of iron, 19 parts of aluminium, 1.6 parts of platinum and barium.
Test case：
After sheet material is made in each metal product in embodiment 1-5, carries out heat treatment in 1.5 hours and after furnace cooling, use Rockwell hardness
Measurement tries its hardness, and the average hardness measured is shown in Table 1.
Table 1：
| Heat treatment temperature | Average hardness value（HRC） | |
| Embodiment 1 | 980-1000℃ | 68 |
| Embodiment 2 | 980-1000℃ | 66 |
| Embodiment 3 | 980-1000℃ | 67 |
| Embodiment 4 | 980-1000℃ | 69 |
| Embodiment 5 | 980-1000℃ | 70 |
| Existing product | 980-1000℃ | 43 |
In conclusion a kind of high rigidity metal product that the present invention points out, has higher hardness.
Example the above is only the implementation of the present invention is not intended to limit the scope of the invention, every to utilize this hair
Equivalent structure or equivalent flow shift made by bright description is applied directly or indirectly in other relevant technology necks
Domain is included within the scope of the present invention.
Claims (6)
1. a kind of high rigidity metal product, which is characterized in that including：First layer material and the second layer material, the first layer material
Material is made of titanium valve, magnesium, brass, manganese and silicon, and second layer material is made of iron, aluminium, platinum and barium, in first layer material
Parts by weight shared by each ingredient：41-52 parts of titanium valve, 61-69 parts of magnesium, 16-22 parts of brass, 4.1-5.2 parts of manganese and silicon 1.1-2.2
Part, parts by weight shared by each ingredient in second layer material：20-30 parts of iron, 10-19 parts of aluminium, 0.9-1.8 parts of platinum and barium 2.1-
3.6 parts, the first layer material is in the top of the second layer material in the high rigidity metal product, and by way of seamless welding
Connection.
2. high rigidity metal product according to claim 1, which is characterized in that in first layer material shared by each ingredient
Parts by weight：1.1 parts of 41 parts of titanium valve, 61 parts of magnesium, 16 parts of brass, 4.1 parts of manganese and silicon, in second layer material shared by each ingredient
Parts by weight：2.1 parts of 20 parts of iron, 10 parts of aluminium, 0.9 part of platinum and barium.
3. high rigidity metal product according to claim 1, which is characterized in that in first layer material shared by each ingredient
Parts by weight：1.3 parts of 43 parts of titanium valve, 62 parts of magnesium, 17 parts of brass, 4.5 parts of manganese and silicon, in second layer material shared by each ingredient
Parts by weight：2.3 parts of 22 parts of iron, 11 parts of aluminium, 1.1 parts of platinum and barium.
4. high rigidity metal product according to claim 1, which is characterized in that in first layer material shared by each ingredient
Parts by weight：1.5 parts of 44 parts of titanium valve, 63 parts of magnesium, 18 parts of brass, 4.6 parts of manganese and silicon, in second layer material shared by each ingredient
Parts by weight：2.5 parts of 23 parts of iron, 12 parts of aluminium, 1.3 parts of platinum and barium.
5. high rigidity metal product according to claim 1, which is characterized in that in first layer material shared by each ingredient
Parts by weight：1.7 parts of 46 parts of titanium valve, 65 parts of magnesium, 19 parts of brass, 4.7 parts of manganese and silicon, in second layer material shared by each ingredient
Parts by weight：2.7 parts of 25 parts of iron, 17 parts of aluminium, 1.5 parts of platinum and barium.
6. high rigidity metal product according to claim 1, which is characterized in that in first layer material shared by each ingredient
Parts by weight：1.9 parts of 49 parts of titanium valve, 67 parts of magnesium, 20 parts of brass, 4.9 parts of manganese and silicon, in second layer material shared by each ingredient
Parts by weight：2.9 parts of 28 parts of iron, 19 parts of aluminium, 1.6 parts of platinum and barium.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810424537.9A CN108501472A (en) | 2018-05-07 | 2018-05-07 | A kind of high rigidity metal product |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810424537.9A CN108501472A (en) | 2018-05-07 | 2018-05-07 | A kind of high rigidity metal product |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108501472A true CN108501472A (en) | 2018-09-07 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810424537.9A Pending CN108501472A (en) | 2018-05-07 | 2018-05-07 | A kind of high rigidity metal product |
Country Status (1)
| Country | Link |
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| CN (1) | CN108501472A (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107723505A (en) * | 2017-09-19 | 2018-02-23 | 浙江力博实业股份有限公司 | A kind of wear-resistant copper alloy and preparation method thereof |
| CN107824819A (en) * | 2017-12-19 | 2018-03-23 | 苏州中骏木工机械配件有限公司 | A kind of high intensity wear-resistant cutting tool |
-
2018
- 2018-05-07 CN CN201810424537.9A patent/CN108501472A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107723505A (en) * | 2017-09-19 | 2018-02-23 | 浙江力博实业股份有限公司 | A kind of wear-resistant copper alloy and preparation method thereof |
| CN107824819A (en) * | 2017-12-19 | 2018-03-23 | 苏州中骏木工机械配件有限公司 | A kind of high intensity wear-resistant cutting tool |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180907 |
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| RJ01 | Rejection of invention patent application after publication |