CN107471769A - A kind of carbon-based multiple Alloy Materials - Google Patents
A kind of carbon-based multiple Alloy Materials Download PDFInfo
- Publication number
- CN107471769A CN107471769A CN201710838839.6A CN201710838839A CN107471769A CN 107471769 A CN107471769 A CN 107471769A CN 201710838839 A CN201710838839 A CN 201710838839A CN 107471769 A CN107471769 A CN 107471769A
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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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/005—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile
- B32B9/007—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising one layer of ceramic material, e.g. porcelain, ceramic tile comprising carbon, e.g. graphite, composite carbon
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
-
- 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
- B32B9/00—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00
- B32B9/04—Layered products comprising a layer of a particular substance not covered by groups B32B11/00 - B32B29/00 comprising such particular substance as the main or only constituent of a layer, which is next to another layer of the same or of a different material
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- Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Carbon And Carbon Compounds (AREA)
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Abstract
The invention discloses a kind of carbon-based multiple Alloy Materials, it leads carrier layer by first surface layer and second and formed, and the first surface layer is made up of carbon zinc, graphene, nickel oxide, and the mass fraction of each component is：3.5 6 parts of carbon zinc, 6.8 10 parts of graphene, 5 12 parts of nickel oxide, described second leads carrier layer is made up of carborundum, calcium carbide, ferrocene, and the mass fraction of each component is：12 20 parts of carborundum, 3.5 8 parts of calcium carbide, 25 parts of ferrocene.By the above-mentioned means, a kind of carbon-based multiple Alloy Materials of the present invention, there is high-melting-point, chemical inertness and heat resistanceheat resistant performance of shaking are good.
Description
Technical field
The present invention relates to electronics new material technology field, more particularly to a kind of carbon-based multiple Alloy Materials.
Background technology
Carbofrax material is since being found, with its superior performance, Aero-Space, warship, high ferro,
The field extensive use such as iron, electric automobile, communication apparatus, the structural member and Chemical Engineering being applied to again now in mechanical engineering
In seal in.
The content of the invention
The present invention solves the technical problem of a kind of carbon-based multiple Alloy Materials are provided, there is high-melting-point, it is chemical lazy
Property and heat resistanceheat resistant performance of shaking are good.
In order to solve the above technical problems, a kind of carbon-based multiple Alloy Materials, it is characterised in that it is by first surface layer and the
Two lead carrier layer composition, and the first surface layer is made up of carbon zinc, graphene, nickel oxide, and the mass fraction of each component is：Carbon
Change zinc 3.5-6 parts, graphene 6.8-10 parts, nickel oxide 5-12 parts, described second leads carrier layer by carborundum, calcium carbide, two cyclopentadienyls
Iron forms, and the mass fraction of each component is：Carborundum 12-20 parts, calcium carbide 3.5-8 parts, ferrocene 2-5 parts.
In a preferred embodiments of the invention, the mass fraction of each component is in the first surface layer：Carbon zinc 3.5
Part, 6.8 parts of graphene, 5 parts of nickel oxide.
In a preferred embodiments of the invention, the mass fraction of each component is in the first surface layer：Carbon zinc 4.5
Part, 8 parts of graphene, 10 parts of nickel oxide.
In a preferred embodiments of the invention, the mass fraction of each component is in the first surface layer：6 parts of carbon zinc,
10 parts of graphene, 12 parts of nickel oxide.
In a preferred embodiments of the invention, second mass fraction for leading each component in carrier layer is：Carborundum 12
Part, 3.5 parts of calcium carbide, 2 parts of ferrocene.
In a preferred embodiments of the invention, second mass fraction for leading each component in carrier layer is：Carborundum 20
Part, 8 parts of calcium carbide, 5 parts of ferrocene.
The beneficial effects of the invention are as follows：Carbon-based multiple Alloy Materials of the invention a kind of, have a high-melting-point, chemical inertness and resist
Heat performance of shaking is good, there is good application prospect.
Embodiment
The technical scheme in the embodiment of the present invention will be clearly and completely described below, it is clear that described implementation
Example is only the part of the embodiment of the present invention, rather than whole embodiments.It is common based on the embodiment in the present invention, this area
All 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 carbon-based multiple Alloy Materials, it leads carrier layer by first surface layer and second and formed, the first surface layer
It is made up of carbon zinc, graphene, nickel oxide, the mass fraction of each component is：Carbon zinc 3.5-6 parts, graphene 6.8-10 parts, oxygen
Change nickel 5-12 parts, described second leads carrier layer is made up of carborundum, calcium carbide, ferrocene, and the mass fraction of each component is：Carbonization
Silicon 12-20 parts, calcium carbide 3.5-8 parts, ferrocene 2-5 parts.
In above-mentioned, the mass fraction of each component is in the first surface layer：3.5 parts of carbon zinc, 6.8 parts of graphene, oxygen
Change 5 parts of nickel.
In above-mentioned, the mass fraction of each component is in the first surface layer：4.5 parts of carbon zinc, 8 parts of graphene, oxidation
10 parts of nickel.
Further, the mass fraction of each component is in the first surface layer：6 parts of carbon zinc, 10 parts of graphene, oxidation
12 parts of nickel.
Further, second mass fraction for leading each component in carrier layer is：12 parts of carborundum, 3.5 parts of calcium carbide,
2 parts of ferrocene.
Further, second mass fraction for leading each component in carrier layer is：20 parts of carborundum, 8 parts of calcium carbide, two
Luxuriant 5 parts of iron.
The beneficial effects of the invention are as follows：Carbon-based multiple Alloy Materials of the invention a kind of, have a high-melting-point, chemical inertness and resist
Heat performance of shaking is good, there is good application prospect.
Embodiments of the invention are the foregoing is only, are not intended to limit the scope of the invention, it is every to utilize this hair
The equivalent structure or equivalent flow conversion that bright description is made, or directly or indirectly it is used in other related technology necks
Domain, similarly it is included in the scope of patent protection of the present invention.
Claims (6)
- A kind of 1. carbon-based multiple Alloy Materials, it is characterised in that it leads carrier layer by first surface layer and second and formed, and described the One superficial layer is made up of carbon zinc, graphene, nickel oxide, and the mass fraction of each component is：Carbon zinc 3.5-6 parts, graphene 6.8-10 parts, nickel oxide 5-12 parts, described second leads carrier layer is made up of carborundum, calcium carbide, ferrocene, the quality of each component Fraction is：Carborundum 12-20 parts, calcium carbide 3.5-8 parts, ferrocene 2-5 parts.
- 2. the carbon-based multiple Alloy Materials of one kind according to claim 1, it is characterised in that each group in the first surface layer Point mass fraction be：3.5 parts of carbon zinc, 6.8 parts of graphene, 5 parts of nickel oxide.
- 3. the carbon-based multiple Alloy Materials of one kind according to claim 1, it is characterised in that each group in the first surface layer Point mass fraction be：4.5 parts of carbon zinc, 8 parts of graphene, 10 parts of nickel oxide.
- 4. the carbon-based multiple Alloy Materials of one kind according to claim 1, it is characterised in that each group in the first surface layer Point mass fraction be：6 parts of carbon zinc, 10 parts of graphene, 12 parts of nickel oxide.
- 5. the carbon-based multiple Alloy Materials of one kind according to claim 1, it is characterised in that described second leads in carrier layer respectively The mass fraction of component is：12 parts of carborundum, 3.5 parts of calcium carbide, 2 parts of ferrocene.
- 6. the carbon-based multiple Alloy Materials of one kind according to claim 1, it is characterised in that described second leads in carrier layer respectively The mass fraction of component is：20 parts of carborundum, 8 parts of calcium carbide, 5 parts of ferrocene.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710838839.6A CN107471769A (en) | 2017-09-18 | 2017-09-18 | A kind of carbon-based multiple Alloy Materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710838839.6A CN107471769A (en) | 2017-09-18 | 2017-09-18 | A kind of carbon-based multiple Alloy Materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107471769A true CN107471769A (en) | 2017-12-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710838839.6A Pending CN107471769A (en) | 2017-09-18 | 2017-09-18 | A kind of carbon-based multiple Alloy Materials |
Country Status (1)
| Country | Link |
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| CN (1) | CN107471769A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103085372A (en) * | 2011-10-31 | 2013-05-08 | 深圳光启高等理工研究院 | Metamaterial dielectric substrate and processing method thereof |
| CN104309207A (en) * | 2014-09-26 | 2015-01-28 | 无锡一名精密铜带有限公司 | Copper strip for ship condenser tube |
| CN104877395A (en) * | 2015-04-29 | 2015-09-02 | 檀四华 | Ship steel plate coating with superhigh anticorrosive and self-cleaning functions |
-
2017
- 2017-09-18 CN CN201710838839.6A patent/CN107471769A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103085372A (en) * | 2011-10-31 | 2013-05-08 | 深圳光启高等理工研究院 | Metamaterial dielectric substrate and processing method thereof |
| CN104309207A (en) * | 2014-09-26 | 2015-01-28 | 无锡一名精密铜带有限公司 | Copper strip for ship condenser tube |
| CN104877395A (en) * | 2015-04-29 | 2015-09-02 | 檀四华 | Ship steel plate coating with superhigh anticorrosive and self-cleaning functions |
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171215 |