CN107012591A - Dry laminating vacuum insulation core material and preparation method thereof - Google Patents

Dry laminating vacuum insulation core material and preparation method thereof Download PDF

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Publication number
CN107012591A
CN107012591A CN201710224522.3A CN201710224522A CN107012591A CN 107012591 A CN107012591 A CN 107012591A CN 201710224522 A CN201710224522 A CN 201710224522A CN 107012591 A CN107012591 A CN 107012591A
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China
Prior art keywords
vacuum insulation
dry laminating
core material
insulation core
ultra
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CN201710224522.3A
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Chinese (zh)
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CN107012591B (en
Inventor
翟富强
郭茂
秦大江
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XUANHAN ZHENGYUAN MICRO GLASS FIBER Co Ltd
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XUANHAN ZHENGYUAN MICRO GLASS FIBER Co Ltd
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Publication of CN107012591A publication Critical patent/CN107012591A/en
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Classifications

    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/002Inorganic yarns or filaments
    • D04H3/004Glass yarns or filaments
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03CCHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C1/00Ingredients generally applicable to manufacture of glasses, glazes, or vitreous enamels
    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03CCHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
    • C03C13/00Fibre or filament compositions
    • DTEXTILES; PAPER
    • D04BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04HMAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/08Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating

Abstract

The present invention relates to dry laminating vacuum insulation core material, by mass percentage, including 1~5wt% of ultra-fine fibre glass 70~80wt% of cotton, 15~25wt% of nanometer grade silica powder and processing aid;The nanometer grade silica diameier is 50~100nm;Na in the ultra-fine fibre glass cotton2O and K2O total content is controlled in 11~17wt%.The invention further relates to the preparation method of dry laminating vacuum insulation core material, ultra-fine fibre glass cotton and nanometer grade silica powder are combined together, vacuum insulation core material is prepared using dry method hot pressing, thermal conductivity factor is low, intensity is high, life-span increase.

Description

Dry laminating vacuum insulation core material and preparation method thereof
Technical field
The invention belongs to functional composite material technical field, it is related to dry laminating vacuum insulation core material and preparation method thereof.
Background technology
Vacuum heat-insulating plate (Vacuum Insulation Panel:VIP) it is thermal insulation material of new generation, thermal conductivity coefficient Can as little as 2.0mW/ (mK) below, equivalent to the 1/10 of traditional material thermal conductivity factor, be at present in the world thermal conductivity factor it is minimum Heat preserving and insulating material.VIP is widely used in refrigerator, refrigerator-freezer, refrigerating box, freezer, construction wall insulation, naval vessels, ship, vapour The fields such as car, electric heater.
Core is as part most crucial vacuum heat-insulating plate VIP, and itself is made up of porous material, limits residual aqueous vapor The free movement of molecule, and prevent convection current and the heat transfer of gas.In vacuum encapsulation process, the core of support frame is used as The pressure more than 98KPa can be born, it is ensured that Obstruct membrane is with core good fit without caving in.For what is made with fibrous material Vacuum heat-insulating plate VIP cores, the aperture size of core is collided with each other by molecule and caused closer to gas molecule mean free path Gas heat transfer just it is smaller, so the factor such as porosity, fibre diameter and aperture size has together decided on vacuum heat-insulating plate VIP Thermal conductivity factor.With the extension of use time, the gas adsorbed in core can be discharged, interior in vacuum heat-insulating plate VIP Pressure can increase to a certain extent, and interior pressure increases with thermal conductivity factor to have a great impact.For being made with silica Vacuum heat-insulating plate VIP cores, because it has nano-pore structure feature, the conduction heat transfer of gas can be reduced.
Publication No. CN104747862 has glass fibre sheet and gas phase SiO2It is open in the patent of the VIP cores of layer The middle core that multilayer laminated glass fibre sheet is constituted, the upper surface and/or lower surface of middle core be covered with gas phase SiO2Plate, or the periphery of the middle core are coated with gas phase SiO2Bisque.
In the patent of the method for Publication No. CN104628239 dry process core material of vacuum heat insulation plate, disclose a kind of dry The method that method prepares core material of vacuum heat insulation plate.Prepare first and collect glass fibre, glass fibre is heated to certain temperature, applied Plus appropriate pressure and the compound for maintaining the class silica gel of half melt of fiberglass surfacing formation after a period of time, this partly melts state Compound causes glass fiber to be cross-linked with each other, and finally cooling obtains VIP cores to overlap joint.
It is open in a kind of patent of glass cores of flyash doping of Publication No. CN104291772 and preparation method thereof It is made using wet processing in blanket of glass wool, drying process in its surface even application silane coupler, after after its solidification, A vibration powder filling machine is placed above glass core, fly ash grain is placed wherein, fly ash grain is evenly distributed on core In the hole of material fiber.
In above-mentioned three patent of invention, disclosed vacuum heat-insulating plate VIP cores be sheet fiberglass lamella core with Powder lamella core laying is composited, or individually fiberglass plies core or independent powder lamella core composition;Wherein institute The fiberglass plies core stated is prepared from using wet method mashing mode, compared to dry method thermoforming way, wet method Pulping process can destroy fiber, and complex forming technology, energy consumption cost is higher;For powder lamella core difficult forming, intensity compared with Difference, it is just increasingly difficult especially for nano-scale particle powder compacting, core in vacuum can be caused to deform, surface is recessed Convex not gentle thermal conductivity factor increase.Therefore, the composite core material of dry method hot pressing glass fibre and nanometer grade powder how is prepared, It is to prepare ultra-low thermal conductivity vacuum heat-insulating plate VIP urgent problems to be solved.
The content of the invention
In view of this, it is an object of the invention to provide a kind of surfacing, intensity is high and the low dry method of thermal conductivity factor is answered Vacuum insulation core material is closed, the preparation method of the dry laminating vacuum insulation core material is also provided.
To reach above-mentioned purpose, the present invention provides following technical scheme:
1st, dry laminating vacuum insulation core material, by mass percentage, including following component:Ultra-fine fibre glass cotton 70~ 1~5wt% of 80wt%, 15~25wt% of nanometer grade silica powder and processing aid;The ultra-fine fibre glass cotton presses matter Percentages are measured, it is composed of the following components:SiO2:58.5~65wt%;Na2O:10.5~16wt%;K2O:0.5~3wt%; Al2O3:2.4~7wt%;MgO:1~4.5wt%;CaO:3~7.5wt%;B2O3:6~8wt%;Fe2O3:0.05~ 0.2wt%;ZnO:0~2wt%;BaO:0.5~3.5wt%.
Further, the nanometer grade silica diameier is 50~100nm.
Further, Na in the ultra-fine fibre glass cotton2O and K2O total content is controlled in 11~17wt%.
Further, the nanometer grade silica powder selects aerosil, precipitated silica or aeroge two One or more in silica.
Further, the processing aid selects KH792, KH550, KH560 silane coupler, NDZ-101 or NDZ-311 titaniums One or more in acid esters coupling agent.
2nd, the preparation method of dry laminating vacuum insulation core material, comprises the following steps:
(1) quartz sand, soda ash, potassium feldspar, albite, calcite, boron are chosen according to ultra-fine fibre glass cotton constituent Sand, dolomite, barium carbonate and zinc oxide uniformly mix and are smelted into the transparent glass metal of free from admixture;
(2) glass metal throws away ultra-fine fibre glass by the centrifugal pan of high speed rotation;
(3) the nanometer grade silica powder uniform atomizing for being blended with processing aid is sprayed on ultra-fine fibre glass table Face, formation dry laminating ultra-fine fibre glass cotton in cotton collecting machine is drawn onto by negative pressure induced wind;
(4) by obtained dry laminating ultra-fine fibre glass cotton through excess temperature for 550~650 DEG C curing oven hot pressing 3~ 10min, obtains dry laminating vacuum insulation core material.
Further, the normal distribution of diameter 95% of the ultra-fine fibre glass is in 2.5~4 μm, the ultra-fine fibre glass The normal distribution of length 90% in 15~30mm.
Further, the thickness control of step (4) the dry laminating vacuum insulation core material is in 15~35mm, and density domination exists 150~300Kg/m3
Further, the injection Stress control that uniform atomizing is sprayed in step (3) is in 0.3~0.5Mpa, injection flow control In 150~250Kg/h.
The beneficial effects of the present invention are:Ultra-fine fibre glass cotton chemical composition neutral and alkali metal Na of the present invention2O+ K2O content is controlled in 11~17wt%, can effectively improve the comprehensive mechanical property of fiber, reduces thermal conductivity factor;Superfine glass is fine B in dimension2O3Content is 6~8wt%, can effectively reduce thermal conductivity factor;The all normal state point of ultra-fine fibre glass diameter 95% prepared Cloth is at 2.5~4 μm, and all normal distributions of fibre length 90% are controlled in 15~35mm, density domination in 15~30mm, core thickness In 150~300Kg/m3, can effectively reduce the thermal conductivity factor for preparing dry laminating vacuum insulation core material.The present invention is by heat conduction system The low-down ultra-fine fibre glass cottons of number and nanometer grade silica powder are effectively combined together, and using dry method hot pressing come Vacuum insulation core material is prepared, has broken destruction of traditional wet method mashing to fiber, the dry laminating vacuum insulation core prepared Material service life is greatly increased, and is combined, is prepared by dry method hot pressing using nanometer grade silica and ultra-fine fibre glass cotton Composite evacuated adiabatic core, the single material core standby compared to other dry method hot pressings, its thermal conductivity factor is lower, and intensity is high, Life-span is longer;The core prepared is beaten compared to wet method, its preparation process does not destroy fiber, and moulding process is simple, energy consumption cost It is low, while realizing effective addition of nano silicon.Put down on the dry laminating vacuum insulation core material surface that the present invention is prepared Whole, intensity is high and thermal conductivity factor is low, be highly suitable for refrigerator, refrigerator-freezer, refrigerating box, freezer, construction wall insulation, naval vessels, ship, The fields such as automobile, electric heater.
Embodiment
The preferred embodiments of the present invention will be described in detail below.
Embodiment 1
By weight choose 23.5 parts of quartz sands, 11 parts of soda ash, 4.5 parts of potassium feldspars, 5.5 albites, 2.5 parts of calcites, Input kiln calcining, melts composition uniform after 8.5 boraxs, 6 dolomites, 1.5 parts of barium carbonates and 1 part of zinc oxide are uniformly mixed The transparent glass metal of free from admixture;Then glass metal throws away ultra-fine fibre glass by the centrifugal pan of high speed rotation, and for preparing is super The all normal distributions of thin glass fiber diameter 95% are at 2.5~3 μm, and all normal distributions of fibre length 90% are in 20~30mm;Will be mixed The nano grade gas phase silicon dioxide powder uniform atomizing that closing has content 1%KH560 silane couplers is sprayed on ultra-fine fibre glass The control of surface, wherein injection pressure is controlled in 200Kg/h in 0.4Mpa, injection flow;Then cotton collecting machine is drawn onto by negative pressure induced wind Interior formation dry laminating ultra-fine fibre glass cotton;It is finally 600 through excess temperature by obtained dry laminating ultra-fine fibre glass cotton DEG C solidification 8min;
Dry laminating vacuum insulation core material thickness 15mm, density 245Kg/m after testing3, core compression ratio 18% measures and leads Hot coefficient is compared with other vacuum insulation core materials, and concrete outcome is as follows:
It can be seen that the thermal conductivity factor for the dry laminating vacuum insulation core material prepared will be less than single dry method glass Glass fiber core and silica lamella fiberglass plies core, while being also less than wet glass fibers core.
Embodiment 2
By weight selection 26.5 parts of quartz sands, 12 parts of soda ash, 4 parts of potassium feldspars, 6 albites, 3 parts of calcites, 7.5 boron Input kiln calcining, melts composition uniform without miscellaneous after sand, 6 dolomites, 2 parts of barium carbonates and 1.5 parts of zinc oxide are uniformly mixed The transparent glass metal of matter;Then glass metal throws away ultra-fine fibre glass by the centrifugal pan of high speed rotation, the ultra-fine glass prepared The all normal distributions of glass fibre diameter 95% are at 2.5~3 μm, and all normal distributions of fibre length 90% are in 15~25mm;It is blended with The nanometer grade silica aerogel powder uniform atomizing of content 3%KH792 silane couplers is sprayed on ultra-fine fibre glass table The control of face, wherein injection pressure is controlled in 250Kg/h in 0.5Mpa, injection flow;Then it is drawn onto by negative pressure induced wind in cotton collecting machine Form dry laminating ultra-fine fibre glass cotton;It it is finally 630 DEG C through excess temperature by obtained dry laminating ultra-fine fibre glass cotton Solidification 5min;
Dry laminating vacuum insulation core material thickness 17mm, density 255Kg/m after testing3, core compression ratio 20% measures and leads Hot coefficient is compared with other vacuum insulation core materials, and concrete outcome is as follows:
It can be seen that the dry laminating vacuum insulation formed by nano silicon and ultra-fine fibre glass cotton hot pressing The thermal conductivity factor of core will be less than single dry method glass fibre core, while being also less than wet glass fibers core.Prove The dry laminating vacuum insulation core material that the present invention is prepared has cost low, the low feature of thermal conductivity factor.Therefore, in refrigerator, ice The fields such as cabinet, refrigerating box, freezer, construction wall insulation have wide market prospects.
Finally illustrate, preferred embodiment above is merely illustrative of the technical solution of the present invention and unrestricted, although logical Cross above preferred embodiment the present invention is described in detail, it is to be understood by those skilled in the art that can be Various changes are made to it in form and in details, without departing from claims of the present invention limited range.

Claims (9)

1. dry laminating vacuum insulation core material, it is characterised in that by mass percentage, including following component:Superfine glass is fine 1~5wt% of 70~80wt% of vinylon and cotton blend, 15~25wt% of nanometer grade silica powder and processing aid;The superfine glass is fine Vinylon and cotton blend is by mass percentage, composed of the following components:SiO2:58.5~65wt%;Na2O:10.5~16wt%;K2O:0.5 ~3wt%;Al2O3:2.4~7wt%;MgO:1~4.5wt%;CaO:3~7.5wt%;B2O3:6~8wt%;Fe2O3:0.05 ~0.2wt%;ZnO:0~2wt%;BaO:0.5~3.5wt%.
2. dry laminating vacuum insulation core material as claimed in claim 1, it is characterised in that the nanometer grade silica powder A diameter of 50~100nm.
3. dry laminating vacuum insulation core material as claimed in claim 1, it is characterised in that in the ultra-fine fibre glass cotton Na2O and K2O total content is controlled in 11~17wt%.
4. dry laminating vacuum insulation core material as claimed in claim 1, it is characterised in that the nanometer grade silica powder From the one or more in aerosil, precipitated silica or aeroge silica.
5. dry laminating vacuum insulation core material as claimed in claim 1, it is characterised in that the processing aid from KH792, One or more in KH550, KH560 silane coupler, NDZ-101 or NDZ-311 titanate coupling agents.
6. the preparation method of any described dry laminating vacuum insulation core materials of claim 1-5, it is characterised in that including as follows Step:
(1) quartz sand is chosen according to ultra-fine fibre glass cotton constituent, it is soda ash, potassium feldspar, albite, calcite, borax, white Marble, barium carbonate and zinc oxide uniformly mix and are smelted into the transparent glass metal of free from admixture;
(2) glass metal throws away ultra-fine fibre glass by the centrifugal pan of high speed rotation;
(3) the nanometer grade silica powder uniform atomizing for being blended with processing aid is sprayed on ultra-fine fibre glass surface, leads to Cross negative pressure induced wind and be drawn onto formation dry laminating ultra-fine fibre glass cotton in cotton collecting machine;
(4) by obtained dry laminating ultra-fine fibre glass cotton through excess temperature for 550~650 DEG C curing oven hot pressing 3~ 10min, obtains dry laminating vacuum insulation core material.
7. the preparation method of dry laminating vacuum insulation core material as claimed in claim 6, it is characterised in that the superfine glass The normal distribution of diameter 95% of fiber at 2.5~4 μm, the normal distribution of length 90% of the ultra-fine fibre glass 15~ 30mm。
8. the preparation method of dry laminating vacuum insulation core material as claimed in claim 6, it is characterised in that step (4) is described Dry laminating vacuum insulation core material thickness control is in 15~35mm, and density domination is in 150~300Kg/m3
9. the preparation method of dry laminating vacuum insulation core material as claimed in claim 6, it is characterised in that in step (3) The injection Stress control of even atomized spray is controlled in 150~250Kg/h in 0.3~0.5Mpa, injection flow.
CN201710224522.3A 2017-04-07 2017-04-07 Dry laminating vacuum insulation core material and preparation method thereof Active CN107012591B (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107512851A (en) * 2017-08-31 2017-12-26 宣汉正原微玻纤有限公司 A kind of high-specific surface area AGM dividing plates modified superfine glass fibre cotton and preparation method thereof
CN107558289A (en) * 2017-09-20 2018-01-09 宣汉正原微玻纤有限公司 A kind of high intensity low thermal conductivity ultra-fine fibre glass cotton dry method hot pressing core and preparation method thereof
CN107639920A (en) * 2017-09-20 2018-01-30 宣汉正原微玻纤有限公司 A kind of compound dry method hot pressing core material of vacuum heat insulation plate of low thermal conductivity and preparation method thereof
CN108101374A (en) * 2017-12-08 2018-06-01 重庆纤维研究设计院股份有限公司 A kind of environmentally friendly low thermal conductivity ultra-fine fibre glass spraying cotton particle for building and preparation method thereof
CN108468907A (en) * 2018-04-20 2018-08-31 宿迁南航新材料与装备制造研究院有限公司 A kind of vacuum heat-insulating plate and preparation method thereof of fiber reinforcement nano-powder material
CN109249507A (en) * 2018-09-27 2019-01-22 佛山齐安建筑科技有限公司 A kind of preparation method of core material of vacuum heat insulation plate
CN110159873A (en) * 2019-06-06 2019-08-23 四川迈科隆真空新材料有限公司 A kind of vacuum heat-insulating plate and preparation method thereof
CN110846927A (en) * 2019-07-01 2020-02-28 重庆文理学院 Hydrophobic oleophylic modified superfine glass fiber cotton for oil product purification filter membrane and preparation method thereof
CN110845145A (en) * 2019-07-01 2020-02-28 重庆文理学院 Composite heat-resistant material for automobile engine heat shield and preparation method thereof
CN111268995A (en) * 2019-11-19 2020-06-12 重庆文理学院 Honeycomb nano-pore structure composite heat insulation material and preparation method thereof
CN111268917A (en) * 2019-11-19 2020-06-12 重庆文理学院 Two-step primary nanopore dry-process composite vacuum heat-insulation core material and preparation method thereof
CN111893652A (en) * 2019-05-05 2020-11-06 南京和润隆环保科技有限公司 Preparation method of storage tank ceiling cold insulation glass cotton felt
CN112032475A (en) * 2020-09-03 2020-12-04 盱眙润新材料技术服务中心 Core material for dry-process vacuum insulation panel and preparation method thereof

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107512851A (en) * 2017-08-31 2017-12-26 宣汉正原微玻纤有限公司 A kind of high-specific surface area AGM dividing plates modified superfine glass fibre cotton and preparation method thereof
CN107558289A (en) * 2017-09-20 2018-01-09 宣汉正原微玻纤有限公司 A kind of high intensity low thermal conductivity ultra-fine fibre glass cotton dry method hot pressing core and preparation method thereof
CN107639920A (en) * 2017-09-20 2018-01-30 宣汉正原微玻纤有限公司 A kind of compound dry method hot pressing core material of vacuum heat insulation plate of low thermal conductivity and preparation method thereof
CN107558289B (en) * 2017-09-20 2019-01-11 宣汉正原微玻纤有限公司 A kind of high intensity low thermal conductivity ultra-fine fibre glass cotton dry method hot pressing core material and preparation method thereof
CN108101374A (en) * 2017-12-08 2018-06-01 重庆纤维研究设计院股份有限公司 A kind of environmentally friendly low thermal conductivity ultra-fine fibre glass spraying cotton particle for building and preparation method thereof
CN108468907A (en) * 2018-04-20 2018-08-31 宿迁南航新材料与装备制造研究院有限公司 A kind of vacuum heat-insulating plate and preparation method thereof of fiber reinforcement nano-powder material
CN109249507A (en) * 2018-09-27 2019-01-22 佛山齐安建筑科技有限公司 A kind of preparation method of core material of vacuum heat insulation plate
CN111893652A (en) * 2019-05-05 2020-11-06 南京和润隆环保科技有限公司 Preparation method of storage tank ceiling cold insulation glass cotton felt
CN110159873A (en) * 2019-06-06 2019-08-23 四川迈科隆真空新材料有限公司 A kind of vacuum heat-insulating plate and preparation method thereof
CN110846927A (en) * 2019-07-01 2020-02-28 重庆文理学院 Hydrophobic oleophylic modified superfine glass fiber cotton for oil product purification filter membrane and preparation method thereof
CN110845145A (en) * 2019-07-01 2020-02-28 重庆文理学院 Composite heat-resistant material for automobile engine heat shield and preparation method thereof
CN111268995A (en) * 2019-11-19 2020-06-12 重庆文理学院 Honeycomb nano-pore structure composite heat insulation material and preparation method thereof
CN111268917A (en) * 2019-11-19 2020-06-12 重庆文理学院 Two-step primary nanopore dry-process composite vacuum heat-insulation core material and preparation method thereof
CN112032475A (en) * 2020-09-03 2020-12-04 盱眙润新材料技术服务中心 Core material for dry-process vacuum insulation panel and preparation method thereof

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