CN106119643A - Heat insulation composite material - Google Patents
Heat insulation composite material Download PDFInfo
- Publication number
- CN106119643A CN106119643A CN201610505415.3A CN201610505415A CN106119643A CN 106119643 A CN106119643 A CN 106119643A CN 201610505415 A CN201610505415 A CN 201610505415A CN 106119643 A CN106119643 A CN 106119643A
- Authority
- CN
- China
- Prior art keywords
- composite material
- heat insulation
- component
- insulation composite
- rubidium
- 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
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Classifications
-
- 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
Abstract
The invention discloses a kind of heat insulation composite material, including percentage by weight shared by following component and each component being: titanium 1.76 6.18%, hafnium 0.11 0.17%, manganese 0.25 0.27%, copper 20 28%, rubidium 0.62 0.78%, indium 0.25 0.27%, molybdenum 19 25%, surplus is magnesium.
Description
Technical field
The invention belongs to technical field of metal, be specifically related to a kind of heat insulation composite material.
Background technology
In actual life, metal material is usually constructed with 100% metal ingredient and makes, the product that this metalloid material is made
It is commercially available and has been widely applied and promotes, but be but highly susceptible to the impact of extraneous factor and corrosion occurs, and
In the environment of some is specific, be often unable to reach the use demand of people, as winter metal material owing to being affected by weather,
Often decrease, and the metal material as tubing often causes breakage because of low temperature, thus cause various accident
The generation of situation, therefore it provides a kind of high-effect heat-insulation metal material becomes those skilled in the art's problem demanding prompt solution.
Therefore, need a kind of new technical scheme to solve the problems referred to above.
Summary of the invention
Goal of the invention: the problem and shortage existed for above-mentioned prior art, it is an object of the invention to provide a kind of heat insulation
Composite material.
Technical scheme: the invention discloses a kind of heat insulation composite material, including weight shared by following component and each component
Amount percentage ratio is: titanium 1 .76-6 .18%, hafnium 0 .11-0 .17%, manganese 0 .25-0 .27%, copper 20-28%, rubidium 0
.62-0 .78%, indium 0 .25-0 .27%, molybdenum 19-25%, surplus is magnesium.
As the further optimization of the present invention, of the present invention include percentage by weight shared by following component and each component
For: titanium 1 .83-5 .82%, hafnium 0 .13-0 .16%, manganese 0 .25-0 .265%, copper 23-27%, rubidium 0 .68-0 .73%,
Indium 0 .255-0 .265%, molybdenum 21-24 .5%, surplus is magnesium.
As the further optimization of the present invention, of the present invention include percentage by weight shared by following component and each component
For: titanium 2 .3-5 .1%, hafnium 0 .14-0 .15%, manganese 0 .25%, copper 25-26%, rubidium 0 .71-0 .72%, indium 0
.26%, molybdenum 23%, surplus is magnesium.
As the further optimization of the present invention, of the present invention include percentage by weight shared by following component and each component
For: titanium 2 .7-4 .2%, hafnium 0 .15%, manganese 0 .25%, copper 26%, rubidium 0 .72%, indium 0 .26%, molybdenum 23%, surplus is
Magnesium.
As the further optimization of the present invention, of the present invention include percentage by weight shared by following component and each component
For: titanium 3 .58%, hafnium 0 .14%, manganese 0 .26%, copper 28%, rubidium 0 .71%, indium 0 .26%, molybdenum 22%, surplus is magnesium.
Beneficial effect: the present invention compared with prior art, has the advantage that the composite material of the present invention can be fitted
Answer various variations in temperature, high temperature resistant and low temperature, there is preferable fatigue resistance and mechanicalness, applied widely.
Detailed description of the invention
Below in conjunction with specific embodiment, the present invention is described in detail, but protection scope of the present invention is described also simultaneously
Being not limited to the concrete scope of the present embodiment, based on the embodiment in the present invention, those of ordinary skill in the art are not making
The every other embodiment obtained under creative work premise, broadly falls into the scope of protection of the invention.
Embodiment 1
The heat insulation composite material of one of the present embodiment, including percentage by weight shared by following component and each component be: titanium 6
.18%, hafnium 0 .17%, manganese 0 .27%, copper 28%, rubidium 0 .78%, indium 0 .27%, molybdenum 25%, surplus is magnesium.
Embodiment 2
The heat insulation composite material of one of the present embodiment, including percentage by weight shared by following component and each component be: titanium 1
.83%, hafnium 0 .13%, manganese 0 .25%, copper 23%, rubidium 0 .68%, indium 0 .255%, molybdenum 21%, surplus is magnesium.
Embodiment 3
The heat insulation composite material of one of the present embodiment, including percentage by weight shared by following component and each component be: titanium 5
.82%, hafnium 0 .16%, manganese 0 .265%, copper 27%, rubidium 0 .73%, indium 0 .265%, molybdenum 24 .5%, surplus is magnesium.
Embodiment 4
The heat insulation composite material of one of the present embodiment, including percentage by weight shared by following component and each component be: titanium 2
.3%, hafnium 0 .14%, manganese 0 .25%, copper 25%, rubidium 0 .71%, indium 0 .26%, molybdenum 23%, surplus is magnesium.
Embodiment 5
The heat insulation composite material of one of the present embodiment, including percentage by weight shared by following component and each component be: titanium 5
.1%, hafnium 0 .15%, manganese 0 .25%, copper 26%, rubidium 0 .72%, indium 0 .26%, molybdenum 23%, surplus is magnesium.
Embodiment 6
The heat insulation composite material of one of the present embodiment, including percentage by weight shared by following component and each component be: titanium 2
.7%, hafnium 0 .15%, manganese 0 .25%, copper 26%, rubidium 0 .72%, indium 0 .26%, molybdenum 23%, surplus is magnesium.
Embodiment 7
The heat insulation composite material of one of the present embodiment, including percentage by weight shared by following component and each component be: titanium 4
.2%, hafnium 0 .15%, manganese 0 .25%, copper 26%, rubidium 0 .72%, indium 0 .26%, molybdenum 23%, surplus is magnesium.
Claims (5)
- The most heat insulation composite material, it is characterised in that: include that percentage by weight shared by following component and each component is: titanium 1 .76-6 .18%, hafnium 0 .11-0 .17%, manganese 0 .25-0 .27%, copper 20-28%, rubidium 0 .62-0 .78%, indium 0 .25- 0 .27%, molybdenum 19-25%, surplus is magnesium.
- Heat insulation composite material the most according to claim 1, it is characterised in that: include shared by following component and each component Percentage by weight is: titanium 1 .83-5 .82%, hafnium 0 .13-0 .16%, manganese 0 .25-0 .265%, copper 23-27%, rubidium 0 .68-0 .73%, indium 0 .255-0 .265%, molybdenum 21-24 .5%, surplus is magnesium.
- Heat insulation composite material the most according to claim 1, it is characterised in that: include shared by following component and each component Percentage by weight is: titanium 2 .3-5 .1%, hafnium 0 .14-0 .15%, manganese 0 .25%, copper 25-26%, rubidium 0 .71-0 .72%, indium 0 .26%, molybdenum 23%, surplus is magnesium.
- Heat insulation composite material the most according to claim 1, it is characterised in that: include shared by following component and each component Percentage by weight is: titanium 2 .7-4 .2%, hafnium 0 .15%, manganese 0 .25%, copper 26%, rubidium 0 .72%, indium 0 .26%, molybdenum 23%, surplus is magnesium.
- Heat insulation composite material the most according to claim 1, it is characterised in that: include shared by following component and each component Percentage by weight is: titanium 3 .58%, hafnium 0 .14%, manganese 0 .26%, copper 28%, rubidium 0 .71%, indium 0 .26%, molybdenum 22%, Surplus is magnesium.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610505415.3A CN106119643A (en) | 2016-07-01 | 2016-07-01 | Heat insulation composite material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610505415.3A CN106119643A (en) | 2016-07-01 | 2016-07-01 | Heat insulation composite material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106119643A true CN106119643A (en) | 2016-11-16 |
Family
ID=57467649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610505415.3A Pending CN106119643A (en) | 2016-07-01 | 2016-07-01 | Heat insulation composite material |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106119643A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108754265A (en) * | 2018-06-04 | 2018-11-06 | 芜湖征途电子科技有限公司 | A kind of corrosion-resistant unmanned plane case material |
| CN110656269A (en) * | 2019-10-25 | 2020-01-07 | 冯波 | Magnesium alloy forging and preparation process thereof |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105039771A (en) * | 2015-02-25 | 2015-11-11 | 上海交通大学 | Preparation method and application of three-dimensional interpenetrating porous magnesium-based material |
| CN105441772A (en) * | 2015-12-30 | 2016-03-30 | 太仓卡斯特姆新材料有限公司 | Heat-insulating composite metal material |
-
2016
- 2016-07-01 CN CN201610505415.3A patent/CN106119643A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105039771A (en) * | 2015-02-25 | 2015-11-11 | 上海交通大学 | Preparation method and application of three-dimensional interpenetrating porous magnesium-based material |
| CN105441772A (en) * | 2015-12-30 | 2016-03-30 | 太仓卡斯特姆新材料有限公司 | Heat-insulating composite metal material |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108754265A (en) * | 2018-06-04 | 2018-11-06 | 芜湖征途电子科技有限公司 | A kind of corrosion-resistant unmanned plane case material |
| CN110656269A (en) * | 2019-10-25 | 2020-01-07 | 冯波 | Magnesium alloy forging and preparation process thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161116 |
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| WD01 | Invention patent application deemed withdrawn after publication |