CN106166873A - A kind of heat-resisting composite material - Google Patents
A kind of heat-resisting composite material Download PDFInfo
- Publication number
- CN106166873A CN106166873A CN201610539264.3A CN201610539264A CN106166873A CN 106166873 A CN106166873 A CN 106166873A CN 201610539264 A CN201610539264 A CN 201610539264A CN 106166873 A CN106166873 A CN 106166873A
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- CN
- China
- Prior art keywords
- composite material
- heat
- accounts
- body weight
- resisting
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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
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
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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
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
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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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
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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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/38—Layered products comprising a layer of synthetic resin comprising epoxy resins
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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
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/42—Layered products comprising a layer of synthetic resin comprising condensation resins of aldehydes, e.g. with phenols, ureas or melamines
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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
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide fibres
Abstract
The present invention discloses a kind of heat-resisting composite material, described heat-resisting composite material includes ferrous materials layer, organic polymer layers and polymer material layer, described ferrous materials layer is chromansil, described organic fibre layer is aramid fiber, described polymer material layer is synthetic resin, described chromansil accounts for the 10 21% of composite material body weight, described aramid fiber accounts for the 30 38% of composite material body weight, described synthetic resin accounts for the 31 36% of composite material body weight, the present invention provides a kind of heat-resisting composite material, there is light weight, heat-resisting, the features such as resistance to combustion and endurance.
Description
Technical field
The present invention relates to a kind of metal material, particularly relate to a kind of heat-resisting composite 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 intensity is high, 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, such as gradient composites (chemistry of material and crystallography group
The functional composite material that one-tenth, structure, space etc. become at Spatial continual ladder), Smart Composite (has sensation, processes and perform
Function, adapts to the functional composite material of environmental change), bionic composite material, camouflage composite material etc..
Summary of the invention
It is an object of the invention to provide a kind of heat-resisting composite material, there is light weight, heat-resisting, resistance to combustion and endurance
Etc. feature.
The technical scheme is that a kind of heat-resisting composite material, it is characterised in that: described heat-resisting composition metal material
Material includes that ferrous materials layer, organic polymer layers and polymer material layer, described chromansil account for composite material main body weight
The 10-21% of amount, described aramid fiber accounts for composite material body weight 30-38%, and described synthetic resin accounts for composition metal
The 31-36% of body of material weight.Described synthetic resin is phenolic resin, Lauxite or epoxy resin.
The heat-resisting composite material of one of the present invention, has light weight, heat-resisting, the feature such as resistance to combustion and endurance.
Detailed description of the invention
A kind of heat-resisting composite material, described heat-resisting composite material includes ferrous materials layer, organic polymer layers
And polymer material layer, described ferrous materials layer is chromansil, and described organic polymer layers is aramid fiber, described macromolecule
Material layer is synthetic resin, and described chromansil accounts for composite material body weight 10-21%, and described aramid fiber accounts for compound
Metal material body weight 30-38%, described synthetic resin accounts for the 31-36% of composite material body weight.Described synthesis
Resin is phenolic resin, Lauxite or epoxy resin.
Described chromansil accounts for the 10-21% of composite material body weight, and described aramid fiber accounts for composition metal material
The 30-38% of material body weight, described synthetic resin account for chromansil described in the 31-36% of composite material body weight
Compared with metallic nickel, crome metal fusing point is high (1860 DEG C), and specific strength is big (intensity and the ratio of density), has good antioxidation
Performance and anti-high-sulfur, diesel fuel, seawater corrosion performance.Described aramid fiber is a kind of novel high-tech synthetic fibers, has
Superhigh intensity, high-modulus and high temperature resistant, acid-fast alkali-proof, the premium properties such as lightweight, its intensity is 5～6 times of steel wire,
Modulus is 2～3 times of steel wire or glass fibre, and toughness is 2 times of steel wire, and weight is only about the 1/5 of steel wire,
At a temperature of 560 degree, do not decompose, do not melt.It has good insulating properties and ageing resistace, has the longest Life Cycle
Phase.Described fiberglass makees a kind of composite of matrix material with synthetic resin.Fibre reinforced composites are by reinforcing fiber
Form with matrix.The diameter of fiber (or whisker) is the least, and typically below 10 μm, defect is less the least, and breaking strain is about
Within 30/1000ths, it is fragile material, easy damaged, ruptures and corroded.Matrix for fiber, intensity, modulus
Will be much lower, but big strain can be withstood, often there is viscoelasticity and elastoplasticity, be toughness material.The present invention provides
A kind of heat-resisting composite material, has light weight, heat-resisting, the feature such as resistance to combustion and endurance.
Claims (3)
1. a heat-resisting composite material, it is characterised in that: described heat-resisting composite material includes ferrous materials layer, organic
Polymeric layer and polymer material layer, described ferrous materials layer is chromansil, and described organic fibre layer is aramid fiber, described
Polymer material layer is synthetic resin, and described chromansil accounts for the 10-21% of composite material body weight, and described aramid fiber is fine
Dimension accounts for the 30-38% of composite material body weight, and described synthetic resin accounts for the 31-of composite material body weight
36%, described synthetic resin is phenolic resin, Lauxite or epoxy resin.
2. according to the heat-resisting composite material described in claim 1, it is characterised in that: described chromansil be by chromium, manganese,
Ferrum and carbon composition.
3. according to the heat-resisting composite material described in claim 1, it is characterised in that: described chromansil accounts for composition metal
The 10-21% of body of material weight, described aramid fiber accounts for the 30-38% of composite material body weight, described synthesis tree
Fat accounts for the 31-36% of composite material body weight.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610539264.3A CN106166873A (en) | 2016-07-11 | 2016-07-11 | A kind of heat-resisting composite material |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610539264.3A CN106166873A (en) | 2016-07-11 | 2016-07-11 | A kind of heat-resisting composite material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106166873A true CN106166873A (en) | 2016-11-30 |
Family
ID=58066242
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610539264.3A Pending CN106166873A (en) | 2016-07-11 | 2016-07-11 | A kind of heat-resisting composite material |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106166873A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106782749A (en) * | 2016-12-22 | 2017-05-31 | 苏州缔绿电子科技有限公司 | A kind of corrosion-resistant composite of high connductivity and preparation method thereof |
| CN111013982A (en) * | 2019-11-06 | 2020-04-17 | 苏州胜禹材料科技股份有限公司 | High-temperature-resistant corrosion-resistant aluminum-zinc-plated plate and production method thereof |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2011161891A (en) * | 2010-02-15 | 2011-08-25 | Hitachi Chemical Techno Service Co Ltd | Heat-resistant gas barrier sheet |
| CN102963066A (en) * | 2012-11-28 | 2013-03-13 | 常熟市东涛金属复合材料有限公司 | Flame-retardant composite metal material |
-
2016
- 2016-07-11 CN CN201610539264.3A patent/CN106166873A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2011161891A (en) * | 2010-02-15 | 2011-08-25 | Hitachi Chemical Techno Service Co Ltd | Heat-resistant gas barrier sheet |
| CN102963066A (en) * | 2012-11-28 | 2013-03-13 | 常熟市东涛金属复合材料有限公司 | Flame-retardant composite metal material |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106782749A (en) * | 2016-12-22 | 2017-05-31 | 苏州缔绿电子科技有限公司 | A kind of corrosion-resistant composite of high connductivity and preparation method thereof |
| CN106782749B (en) * | 2016-12-22 | 2018-07-17 | 苏州缔绿电子科技有限公司 | A kind of highly conductive corrosion-resistant composite material and preparation method |
| CN111013982A (en) * | 2019-11-06 | 2020-04-17 | 苏州胜禹材料科技股份有限公司 | High-temperature-resistant corrosion-resistant aluminum-zinc-plated plate and production method thereof |
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Application publication date: 20161130 |