CN207916217U - A kind of fiber reinforcement type high performance composite film - Google Patents
A kind of fiber reinforcement type high performance composite film Download PDFInfo
- Publication number
- CN207916217U CN207916217U CN201721632940.8U CN201721632940U CN207916217U CN 207916217 U CN207916217 U CN 207916217U CN 201721632940 U CN201721632940 U CN 201721632940U CN 207916217 U CN207916217 U CN 207916217U
- Authority
- CN
- China
- Prior art keywords
- layer
- external protection
- basal layer
- high performance
- type high
- 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.)
- Active
Links
Landscapes
- Laminated Bodies (AREA)
Abstract
The utility model is related to a kind of fiber reinforcement type high performance composite films, including external protection, basal layer and enhancement layer, external protection is PVDF thin film, and basal layer is aluminium foil, and enhancement layer is the fibre bundle being laid with along warp-wise and broadwise;The external protection is arranged by binder in the side of basal layer; enhancement layer is in the latticed another side for being layed in base layer by through broadwise; the interlaminar strength of external protection and basal layer is not less than 3 pounds per inch, and the whole overall thickness of external protection, basal layer and enhancement layer is 35 μm 100 μm;The fiber reinforcement type high performance composite film of the utility model is film as external protection using PVDF, the layer based on aluminium foil, using fibre bundle as enhancement layer, makes whole have the basic properties such as good weatherability, durability;External protection is bonded with basal layer by special binder, improves peel strength, and using fibre bundle as enhancement layer, improve integral strength.
Description
Technical field
The utility model is related to a kind of fiber reinforcement type high performance composite films.
Background technology
Composite membrane material has low table due to having the performances such as weatherability, durability, good non-adhesive
Face tension, low frictional properties hate repellency, hate the special surface propertys such as reprimand oiliness, and are produced in aerospace and precise electronic
The encapsulation field of product is widely used;And existing composite membrane material is due to the limitation of material and structure, it is whole
Body intensity and peel strength still do not reach requirement in special use environment.
Utility model content
For the above technical problems, the purpose of this utility model is:Propose a kind of fiber reinforcement type high-performance
Laminated film.
What the technical solution of the utility model was realized in:A kind of fiber reinforcement type high performance composite film, packet
Containing external protection, basal layer and enhancement layer, external protection is PVDF thin film, and basal layer is aluminium foil, and enhancement layer is along warp-wise and latitude
To the fibre bundle of laying;The external protection is arranged by binder in the side of basal layer, and it is in net that enhancement layer, which is pressed through broadwise,
Trellis is layed in the another side of base layer, and the interlaminar strength of external protection and basal layer is not less than 3 pounds per inch, outer protection
The whole overall thickness of layer, basal layer and enhancement layer is 35 μm -100 μm.
Preferably, the thickness of the external protection is 18-25 microns.
Preferably, the thickness of the basal layer is 6.5-12 μm.
Preferably, the fibre bundle is nylon or aramid fiber, and parallel and spacing distance is between fibre bundle
2.5mm-10mm, fibre bundle pass through binder-impregnated before being laid with and handle.
Preferably, the binder is made of acetone, VMA and polyurethane, and the ratio of acetone, VMA and polyurethane is 1:3:
0.4。
Due to the application of the above technical scheme, the utility model has following advantages compared with prior art:
The fiber reinforcement type high performance composite film of the utility model is film as external protection using PVDF, is with aluminium foil
Basal layer makes entirety have the basic properties such as good weatherability, durability using fibre bundle as enhancement layer;External protection with
Basal layer is bonded by special binder, improves peel strength, and using fibre bundle as enhancement layer, is improved whole strong
Degree.
Description of the drawings
Technical solutions of the utility model are described further below in conjunction with the accompanying drawings:
Attached drawing 1 is a kind of structural schematic diagram of fiber reinforcement type high performance composite film of the utility model.
Specific implementation mode
Illustrate the utility model below in conjunction with the accompanying drawings.
As shown in Fig. 1, a kind of fiber reinforcement type high performance composite film described in the utility model, including external protection
1, basal layer 2 and enhancement layer 3;The external protection 1 is PVDF thin film, and the thickness of external protection 1 is 18-25 microns;The base
Plinth layer 2 is aluminium foil, and the thickness of basal layer 2 is 6.5-12 μm;The enhancement layer 3 is the fibre bundle being laid with along warp-wise and broadwise,
Fibre bundle is nylon or aramid fiber, and parallel and spacing distance is 2.5mm-10mm between fibre bundle, and fibre bundle is laid with
Preceding binder-impregnated of passing through is handled;The external protection 1 is arranged by binder in the side of basal layer 2, and enhancement layer 3 is by warp
Broadwise is in the latticed another side for being layed in base layer, and external protection 1 and the interlaminar strength of basal layer 2 are not less than 3 pounds/English
Very little, the whole overall thickness of external protection 1, basal layer 2 and enhancement layer 3 is 35 μm -100 μm;The binder is by acetone, VMA
Ratio with the glue of polyurethane composition, acetone, VMA and polyurethane is 1:3:0.4.
The preparation method of the laminated film is as follows:Glue is laid on aluminium foil, by PVDF and aluminium foil hot melt compounding machine
Compound, temperature is 75-85 DEG C, drum pressure 4kg, is then placed on curing 2 days in curing chamber, and curing temperature is 35-45 DEG C;Most
Combination product is placed on hot press afterwards, glue is layed on aluminium foil, fibre bundle is placed on aluminium foil, hot pressing temperature 90
DEG C, time 45s is spaced 20min, repeats hot pressing 3 times.
The specific application example that the above is only the utility model does not constitute the scope of protection of the utility model any limit
System.Any technical scheme formed by adopting equivalent transformation or equivalent replacement, all fall within the utility model rights protection scope it
It is interior.
Claims (4)
1. a kind of fiber reinforcement type high performance composite film, it is characterised in that:Including external protection(1), basal layer(2)And enhancing
Layer(3), external protection(1)For PVDF thin film, basal layer(2)For aluminium foil, enhancement layer(3)For along the fiber of warp-wise and broadwise laying
Tow;The external protection(1)It is arranged in basal layer by binder(2)Side, enhancement layer(3)It is in latticed by through broadwise
It is layed in the another side of base layer, external protection(1)With basal layer(2)Interlaminar strength be not less than 3 pounds per inch, outer guarantor
Sheath(1), basal layer(2)And enhancement layer(3)Whole overall thickness be 35 μm -100 μm.
2. fiber reinforcement type high performance composite film according to claim 1, it is characterised in that:The external protection(1)
Thickness be 18-25 microns.
3. fiber reinforcement type high performance composite film according to claim 1, it is characterised in that:The basal layer(2)'s
Thickness is 6.5-12 μm.
4. fiber reinforcement type high performance composite film according to claim 1, it is characterised in that:The fibre bundle is Buddhist nun
Dragon or aramid fiber, parallel and spacing distance is 2.5mm-10mm between fibre bundle, fibre bundle be laid with before by bonding
Agent impregnation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721632940.8U CN207916217U (en) | 2017-11-30 | 2017-11-30 | A kind of fiber reinforcement type high performance composite film |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721632940.8U CN207916217U (en) | 2017-11-30 | 2017-11-30 | A kind of fiber reinforcement type high performance composite film |
Publications (1)
Publication Number | Publication Date |
---|---|
CN207916217U true CN207916217U (en) | 2018-09-28 |
Family
ID=63613240
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201721632940.8U Active CN207916217U (en) | 2017-11-30 | 2017-11-30 | A kind of fiber reinforcement type high performance composite film |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN207916217U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107791629A (en) * | 2017-11-30 | 2018-03-13 | 苏州市君悦新材料科技股份有限公司 | A kind of fiber reinforcement type high performance composite film |
CN109827645A (en) * | 2018-12-26 | 2019-05-31 | 江苏日托光伏科技股份有限公司 | A kind of MWT component conducting resinl quota test method |
-
2017
- 2017-11-30 CN CN201721632940.8U patent/CN207916217U/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107791629A (en) * | 2017-11-30 | 2018-03-13 | 苏州市君悦新材料科技股份有限公司 | A kind of fiber reinforcement type high performance composite film |
CN109827645A (en) * | 2018-12-26 | 2019-05-31 | 江苏日托光伏科技股份有限公司 | A kind of MWT component conducting resinl quota test method |
CN109827645B (en) * | 2018-12-26 | 2021-06-18 | 江苏日托光伏科技股份有限公司 | MWT assembly conductive adhesive quota testing method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US9969146B2 (en) | Layered substrate and method for manufacturing same | |
CN103649015B (en) | Carbon fiber-reinforced carbon complex and manufacture method thereof | |
RU2017101000A (en) | PRELIMINARY IMPREGNATED CONDUCTIVE COMPOSITE SHEET AND METHOD FOR ITS MANUFACTURE | |
CN207916217U (en) | A kind of fiber reinforcement type high performance composite film | |
JP5533320B2 (en) | Sandwich structure | |
EP2922685A2 (en) | Bonding of composite materials | |
EP3110623A1 (en) | Composite sandwich panel having curable composite skins with asymmetrical resin distributions | |
WO2017016436A1 (en) | Preimpregnated fiber cloth and preparation method therefor | |
JP6700049B2 (en) | Carbon fiber sheet material, prepreg, laminated body, molded body and manufacturing method thereof | |
US20130280470A1 (en) | Thermal Management For Aircraft Composites | |
JP2015174807A (en) | Carbon fiber-based heat insulation material, and manufacturing method of the same | |
CN101786356A (en) | Preparation method of a co-cured high damping composite material | |
CN106785415A (en) | The polymer matrix composites antenna house of body containing stereoscopic radiation and its forming method | |
WO2019163633A1 (en) | Cfrp sheet, frp-metal composite, and method for manufacturing same | |
JP4164572B2 (en) | Composite material and manufacturing method thereof | |
WO2012086471A1 (en) | Composite material molding tool | |
CA2968081C (en) | Epoxy-based resin composition for composite materials | |
CN107791629A (en) | A kind of fiber reinforcement type high performance composite film | |
CN104786575B (en) | A kind of asbestos base lamilate, its manufacturing method and its application | |
JPWO2020009125A1 (en) | CFRP sheet, laminate using CFRP sheet, and method for manufacturing CFRP sheet | |
JP6035084B2 (en) | Intermediate material for carbon / carbon composite | |
CN109676951A (en) | Fibrous composite and its preparation method | |
Singh et al. | Investigation of bending properties of E-Glass fiber reinforced polymer matrix composites for applications in micro wind turbine blades | |
US10647452B2 (en) | Ablator, re-entry vehicle and method of manufacturing them | |
CN209869584U (en) | Light high-strength unidirectional carbon fiber laminated board |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |