CN106166870A - A kind of High-rigidity composite metal material - Google Patents
A kind of High-rigidity composite metal material Download PDFInfo
- Publication number
- CN106166870A CN106166870A CN201610529031.5A CN201610529031A CN106166870A CN 106166870 A CN106166870 A CN 106166870A CN 201610529031 A CN201610529031 A CN 201610529031A CN 106166870 A CN106166870 A CN 106166870A
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- Prior art keywords
- metal material
- composite
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- rigidity
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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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- 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
- B32B33/00—Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
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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
- B32B2250/00—Layers arrangement
- B32B2250/03—3 layers
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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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/30—Properties of the layers or laminate having particular thermal properties
- B32B2307/302—Conductive
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/536—Hardness
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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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/546—Flexural strength; Flexion stiffness
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- Carbon And Carbon Compounds (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
The open a kind of High-rigidity composite metal material of the present invention, described High-rigidity composite metal material includes light metal material layer, semi-metallic layer and Rare Metals Materials layer, described light metal material layer is almag, described semi-metallic layer is perovskite, described Rare Metals Materials layer is diamondite, described almag accounts for the 25% of composite material body weight, described perovskite accounts for the 20% of composite material body weight, described diamondite accounts for the 25% of composite material body weight, the present invention provides a kind of High-rigidity composite metal material, there is thermal diffusivity preferable, crushing resistance is relatively strong and the feature such as the hardness of superelevation.
Description
Technical field
The present invention relates to a kind of metal material, particularly relate to a kind of High-rigidity composite metal material.
Background technology
Composite is a kind of mixture.All play the biggest effect in a lot of fields, instead of the most traditional material
Material.Composite by its composition be divided into metal and metallic composite, nonmetal with metallic composite, nonmetal and nonmetal
Composite.It is divided into again by its construction features: 1. fibre reinforced composites.Various fibre reinforcements are placed in matrix material
It is composited.Such as fibre reinforced plastics, fibreglass-reinforced metal etc..2. interlayer composite material.The different surfacing of do as one likes matter and
Core material composition forms.Generally face material high rigidity, thin；Core light weight, intensity are low, but have certain rigidity and thickness.It is divided into solid
Interlayer and honeycomb interlayer two kinds.3. fine granule composite materials.Hard particulates is uniformly distributed in matrix, as strengthened dispersion alloy,
Ceramic metal etc..4. hybrid composite.Strengthened phase material by two or more and mix structure in a kind of matrix phase material
Become.Strengthening phase composite materials ratio with common single, its impact strength, fatigue strength and fracture toughness significantly improve, and have special
Hot expansibility.Be divided into interlaminar hybrid, interlayer to mix, sandwich mixes, in layer/interlayer mixes and superhybrid composite.Multiple
Condensation material sixties, for meeting the needs of the sophisticated technology material therefors such as Aero-Space, successively develop and produce with high-performance
Fiber (such as carbon fiber, boron fibre, aramid fiber, silicon carbide fibre etc.) is the composite of reinforcing material, and its specific strength is more than 4
× 106 centimetres (cm), specific modulus is more than 4 × 108cm.In order to first generation galss fiber reinforced resin composite phase region
Not, this composite is referred to as advanced composite material.Different by matrix material, advanced composite material is divided into resin base, metal
Base and ceramic matric composite.It uses temperature to reach 250～350 DEG C, 350～1200 DEG C and more than 1200 DEG C respectively.Advanced multiple
Condensation material, in addition to as structural material, also acts as functional material, but these material shortage thermal diffusivities, crushing resistance and hardness
Deng.
Summary of the invention
It is an object of the invention to provide a kind of High-rigidity composite metal material, have thermal diffusivity preferably, crushing resistance stronger
The features such as the hardness with superelevation.
The technical scheme is that a kind of High-rigidity composite metal material, described High-rigidity composite metal material includes
Light metal material layer, semi-metallic layer and Rare Metals Materials layer, described light metal material layer is almag, described half gold
Belonging to material layer is perovskite, and described Rare Metals Materials layer is diamondite, and described almag accounts for composite material master
The 25% of body weight, described perovskite accounts for the 20% of composite material body weight, and described diamondite accounts for composition metal
The 25% of body of material weight；Described perovskite includes sodium, cerium, ferrum and niobium.
A kind of High-rigidity composite metal material of the present invention, have thermal diffusivity preferably, crushing resistance is relatively strong and the hardness of superelevation
Etc. feature.
Detailed description of the invention
A kind of High-rigidity composite metal material, described High-rigidity composite metal material includes light metal material layer, semimetal
Material layer and Rare Metals Materials layer, described light metal material layer is almag, and described semi-metallic layer is perovskite, institute
Stating Rare Metals Materials layer is diamondite, and described almag accounts for the 25% of composite material body weight, described calcium
Titanium ore accounts for the 20% of composite material body weight, and described diamondite accounts for the 25% of composite material body weight；
Further illustrating, described perovskite includes sodium, cerium, ferrum and niobium..Described almag essential element is that aluminum mixes a small amount of magnesium again
Or other metal material strengthens its hardness.Aluminium alloy with Mg as main adding elements, owing to its corrosion stability is good, again
Claim rust-preventing aluminum alloy.Cause inherently metal, its heat conductivility and intensity are especially prominent.
Further illustrating, described perovskite has the crystal structure of uniqueness, the most doped rear crystal defect knot formed
Structure and performance, be employed maybe can be used in solid fuel cell, solid electrolyte, sensor, high temperature heated materials, solid
The numerous areas such as the oxidation reduction catalyst of resistor and replacement noble metal, become the research in the fields such as chemistry, physics and material
Focus.Due to this compounds have stable crystal structure, unique electromagnetic performance and the highest oxidoreduction, hydrogenolysis,
Isomerization, electro-catalysis isoreactivity, as a kind of novel functional material, have the biggest in the field such as environmental conservation and Industrial Catalysis
Potentiality to be exploited.
Further illustrating, described diamondite is one of the hardest metal, and hardness is at 8-9M(Mohs
Hardness standard) between, it is only second to diamond (10M).Tungsten is a kind of rare metal, tungsten ore through digging, grinding, water gravity treatment,
Refinement etc. is refined into the tungsten powder of purity 60% or 90%, then the finished product produced through high-temperature electric resistance furnace refinement molding is exactly tungsten rod.
The fusing point of tungsten rod about 3500 DEG C.A kind of High-rigidity composite metal material of the present invention, have thermal diffusivity preferably, crushing resistance stronger
The features such as the hardness with superelevation.
The detailed description of the invention of the present invention, but protection scope of the present invention is not limited thereto, any is familiar with this area
Technical staff in the technical scope that disclosed herein, the change can expected without creative work or replacement, all should contain
Cover within protection scope of the present invention.Therefore, the protection model that protection scope of the present invention should be limited with claims
Enclose and be as the criterion.
Claims (2)
1. a High-rigidity composite metal material, it is characterised in that: described High-rigidity composite metal material includes light metal material
Layer, semi-metallic layer and Rare Metals Materials layer, described light metal material layer is almag, and described semi-metallic layer is
Perovskite, described Rare Metals Materials layer is diamondite, and described almag accounts for composite material body weight
25%, described perovskite accounts for the 20% of composite material body weight, and described diamondite accounts for composite material main body
The 25% of weight.
High-rigidity composite metal material the most according to claim 1, its domestic animal is: described perovskite include sodium, cerium, ferrum and
Niobium.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610529031.5A CN106166870A (en) | 2016-07-07 | 2016-07-07 | A kind of High-rigidity composite metal material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610529031.5A CN106166870A (en) | 2016-07-07 | 2016-07-07 | A kind of High-rigidity composite metal material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106166870A true CN106166870A (en) | 2016-11-30 |
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ID=58065140
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610529031.5A Pending CN106166870A (en) | 2016-07-07 | 2016-07-07 | A kind of High-rigidity composite metal material |
Country Status (1)
| Country | Link |
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| CN (1) | CN106166870A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108859317A (en) * | 2018-06-14 | 2018-11-23 | 南通麦斯铁数控机床有限公司 | A kind of high hardness alloy material |
| CN109811238A (en) * | 2017-11-20 | 2019-05-28 | 遵义市播州区正立达铸造有限公司 | A kind of composite material |
| CN110920165A (en) * | 2018-09-20 | 2020-03-27 | 南通麦斯铁数控机床有限公司 | Pressure-resistant combined metal material |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050175843A1 (en) * | 2003-05-02 | 2005-08-11 | Johnson John R. | Bright formable metalized film laminate |
| CN103273690A (en) * | 2013-05-23 | 2013-09-04 | 昆山乔锐金属制品有限公司 | High-rigidity composite metal material |
-
2016
- 2016-07-07 CN CN201610529031.5A patent/CN106166870A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050175843A1 (en) * | 2003-05-02 | 2005-08-11 | Johnson John R. | Bright formable metalized film laminate |
| CN103273690A (en) * | 2013-05-23 | 2013-09-04 | 昆山乔锐金属制品有限公司 | High-rigidity composite metal material |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109811238A (en) * | 2017-11-20 | 2019-05-28 | 遵义市播州区正立达铸造有限公司 | A kind of composite material |
| CN108859317A (en) * | 2018-06-14 | 2018-11-23 | 南通麦斯铁数控机床有限公司 | A kind of high hardness alloy material |
| CN110920165A (en) * | 2018-09-20 | 2020-03-27 | 南通麦斯铁数控机床有限公司 | Pressure-resistant combined metal material |
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Application publication date: 20161130 |