CN100532069C - Thermal forming method for PMI foam laminated structure - Google Patents
Thermal forming method for PMI foam laminated structure Download PDFInfo
- Publication number
- CN100532069C CN100532069C CNB200510021884XA CN200510021884A CN100532069C CN 100532069 C CN100532069 C CN 100532069C CN B200510021884X A CNB200510021884X A CN B200510021884XA CN 200510021884 A CN200510021884 A CN 200510021884A CN 100532069 C CN100532069 C CN 100532069C
- Authority
- CN
- China
- Prior art keywords
- pmi
- foam
- vacuum bag
- splicing
- thermoforming process
- 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.)
- Expired - Fee Related
Links
Landscapes
- Laminated Bodies (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
The present invention discloses a thermoforming method of PMI foam sandwich structure. Said method mainly includes the following steps: adopting vacuum bag/drying oven or vacuum bag/thermocompression tank forming technique, placing aeration felt on the surface of PMI foam plate, making vacuum bag, heating to the temperature capable of making PMI be formed and softened, heat-insulating for 30-60 min according foam thickness, heat-insulating and vacuum-pumping, for foam with large thickness applying external pressure of below 0.3MPa for 15 min, then retaining pressure and cooling, demoulding and taking out finished product.
Description
Technical field
The present invention relates to a kind of thermoforming process of PMI foamed sandwich structure, especially alleviate bullet train, aircraft weight with the PMI foamed sandwich structure, reduce the noise that travels, improve metal decking or the interlayer intensity of composite material face foam layer member and the thermoforming process method of heat resisting temperature.
Background technology
In the known technology, for strengthening rigidity, the intensity of hot-short, aircraft metal decking sandwich component, weight reduction reduces noise, all will adopt metal or non-metal honeycomb sandwich to it usually.Though paper wasp nest sandwich has Machining of Curved Surface performance preferably, its intensity, rigidity, hear resistance, sound insulation and anti-flammability are not as extensively adopting the panel-sandwich foam plastics at aircraft, high-speed maglev train in recent years.And the PF that generally uses at present, the deficiency that the PU unicellular foamed plastic cores still exists low-intensity, fragility.Along with the development of technology, high strength, high tenacity, high rigidity, anti-combustion and the PEI PEI or the polyesterimide PMI foamed plastics that can heat or be machined into Special-Shaped Surface arise at the historic moment as the sandwich of sandwich material.This polyesterimide PMI foamed plastics (hereinafter to be referred as the PMI foam) is the highest heat-resisting foamed plastics of present strength and stiffness, it at high temperature has very high creep-resistant property, the co-curing technology that can bear 190 ℃ is to the requirement of foam size stability, and have good cementability and isotropism between the resin, and the shape of the easy various complexity of machine-shaping, and not fluorine-containing Lyons, fire protecting performance can reach standards such as FAR25.8 and AITM, is the novel core that can replace honeycomb.Its combination property is very outstanding, and using value is high.But polyesterimide PMI foamed plastics is as a kind of thermoset macromolecule material, and itself is insoluble not molten, even can not melt under any high temperature, is not dissolved in any solvent yet, does not almost have softening possibility.Thereby make polyesterimide PMI foamed plastics form the fixed pattern prejudice of can only the thermoforming curvature very little product.Aspect splicing, also there is the inboard contact interface glue-joint strength of foam layer and metal, the problem how compound back bubble is got rid of smoothly.In order to solve the problems referred to above that polyesterimide PMI foamed plastics exists, the Adtranz company that can make the company of Japanese East Japan Railway of high-speed magnetic levitation vehicle, Canadian Bombardier (Bombadier Inc) and Germany has at present adopted more advanced vacuum thermoforming technology, vacuum bag/solidification of hot-press tank technology, vacuum aided injection technique, whole winding technology, resin transfer moulding (RTM) technology to the manufacturing that relates to head, skirtboard, roof panels, floor, framed side wallboard.These technology all are to adopt under the softening condition of foam, utilize the adhesive technology of vacuum suction moulding special equipment formed product and HTHP.Very high of the equipment that is shaped, and complicated, and process conditions require also high.China also is in the primary stage of groping to study in the development of PEI and PMI foamed plastics, goes back neither one and can satisfy the especially ultra-large type of the method for the ripe manufacturing process that relates to metal decking or composite material face and the combination of PMI foamed sandwich structure and relevant foam and metal bonding technology (size reaches the bibliographical information of 5m * 4m) and uses example.
Summary of the invention:
It is simple to the purpose of this invention is to provide a kind of equipment, cheap, and process conditions are less demanding, can the certain curvature profile of thermoforming, and the thermoforming process that metal decking that no bubble glueds joint or composite material face combine with the PMI foamed sandwich structure.
The thermoforming process of a kind of PMI foamed sandwich structure provided by the invention comprises the following steps:
(1). the PMI cystosepiment is placed on the curved surface forming mould, and airfelt is put on the surface, is sealed in the vacuum bag, puts into baking oven or autoclave then, is warmed to 170～210 ℃ and carries out softening before the moulding;
(2)., vacuumize simultaneously or press molding more than 15 minutes according to depth of foam insulation, to be formed after demoulding pickup, to thickness big add pressurize cooling after at least 15 minutes below the external pressure 0.3MPa;
(3). the metallic plate that surface treatment is good or the PMI foam of composite material face and forming are put into the frock of metal or nonmetal band curvature die cavity or are gluedd joint frock, finish splicing with glued membrane or adhesive laying again;
(4). the PMI cystosepiment sealing of laying being finished splicing with vacuum bag is put into autoclave or is put into baking oven with the PMI cystosepiment sealing that vacuum bag is finished splicing with laying and is cured moulding.
The present invention puts into the epoxy resin glued membrane or glueds joint PMI foam that frock glueds joint can be the splicing that the multilayer laying is finished composite material face or metal decking and the inboard interface of PMI cystosepiment, and the PMI cystosepiment sealing of laying being finished splicing with vacuum bag is put into PMI cystosepiment that autoclave or vacuum bag finish splicing with laying and sealed and put into baking oven and carry out the co-curing moulding again.
Of the present invention according to the depth of foam temperature retention time preferably by empirical equation: t 〉=15+ δ (t in the formula: insulation the number of minutes, δ is a depth of foam, unit: mm) determine by experience.
Glued membrane of the present invention can be the epoxy resin glued membrane.
The present invention can also glued joint press molding by splicing for superhuge sandwich PMI foam.
Composite of the present invention can be that glass fabric/unsaturated polyester (UP) or epoxy resin composite material mix, and also can be glass-reinforced plastic material.
The present invention has following good effect than prior art.
The present invention adopts baking oven or autoclave prior art equipment, the PMI cystosepiment is sealed in vacuum bag to be warmed to 170～210 ℃ and to carry out before the moulding softening, especially 190 ℃～205 ℃ softening temperatures, avoided the too high easy decomposition of polyesterimide PMI foamed plastics temperature rightly, temperature is crossed low not softening defective.It not only avoided can only with external high equipment could formed product dependence, and simplified technology, and accelerated the shaping process of product, shortened the production cycle, reduce cost, simultaneously also overcome the fixed pattern prejudice of can only the thermoforming curvature very little product of PMI foam.The processing step of wherein the PMI foam being put into curved surface forming mould press molding has solved the shaping than complex profile.The method of finishing splicing with the glued membrane laying has solved metal decking and the problem that needs to get rid of bubble is gluedd joint with adhesive in the inboard interface of PMI cystosepiment, and it is smooth reliable to glued joint the interface, the intensity height.Superhuge sandwich PMI foam glueds joint the manufacturing that pressing/molding method has taken the lead in solving ultra-large type complex profile, high strength, high rigidity, high temperature resistant, maglev vehicle car body wallboard that sound insulation is good at home by splicing.
The specific embodiment
The invention will be further described below in conjunction with embodiment.
At first the PMI cystosepiment is put into mould, airfelt is put on the surface, be sealed in the vacuum bag, then the PMI cystosepiment is put into baking oven or autoclave is heated, heat make it softening to 170～210 ℃ after, softening optimum temperature is 190 ℃～205 ℃, empirical equation according to the depth of foam temperature retention time: t 〉=15+ δ (t: insulation the number of minutes, δ depth of foam (unit: mm) calculate and rely on working experience to determine the time of insulation, to time of the PMI cystosepiment of 20mm～40mm thickness insulation usually about 30～60 minutes, simultaneously the PMI cystosepiment after softening is vacuumized or pressurizes, to be formed after the demoulding take out.Can add pressurize cooling after at least 15 minutes below the external pressure 0.3MPa to the big PMI cystosepiment of thickness.Then with well-oxygenated non-ferrous metal board or aluminium alloy panel, or the PMI foam of composite panel and forming puts into metal or nonmetally the frock of curvature die cavity arranged or glued joint frock, glueds joint with glued membrane or adhesive laying again.Be cured with vacuum bag/autoclave or vacuum bag/baking oven at last.The co-curing adhesive bonding technique can be used the curing of composite and use and glued joint frock.
Putting into rubber moulding or glued joint the PMI foam that frock glueds joint can be to adopt the multilayer laying, after glued joint by specification requirement at metal decking and interface, PMI cystosepiment inboard, carries out the co-curing moulding with vacuum bag/autoclave or vacuum bag/baking oven again.Described glued membrane can be the epoxy resin glued membrane.Because the specification of present PMI cystosepiment has only 1.25m * 2.5m.For superhuge sandwich PMI foam, be about 12.2m * 2.6m such as high-speed magnetic levitation vehicle full-size, the compartment top board of curvature maximum; Be about most 25m, the sidewall paneling of wide about 0.8m; Be shaped as the cylinder of R6.0m, can glued joint vacuum or press molding by the butt joint splicing.
In sum, the thermoforming of PMI foam is to adopt vacuum bag/baking oven or vacuum bag/autoclave molding technology, put airfelt, system vacuum bag on PMI cystosepiment surface, be warmed to PMI moulding softening temperature (200～210 ℃), according to depth of foam insulation 30～60 minutes, insulation take out vacuum, to thickness big add pressurize cooling after at least 15 minutes, demoulding pickup below the external pressure 0.3MPa.
The splicing of composite material face and PMI foam layer composite construction can be adopted composite co-curing technology, use to glued joint frock, PMI foam, epoxy resin compound cutan or the adhesive of the composite material face of laying and forming and other composite construction such as inserts laying are finished vacuum bag/autoclave or vacuum bag/curing oven moulding.
Claims (8)
1. the thermoforming process of a PMI foamed sandwich structure comprises the following steps:
(1). the PMI cystosepiment is placed on the curved surface forming mould, and airfelt is put on the surface, is sealed in the vacuum bag, puts into baking oven or autoclave then, is warmed to 170～210 ℃ and carries out softening before the moulding;
(2)., vacuumize simultaneously or press molding more than 15 minutes according to depth of foam insulation, to be formed after demoulding pickup, to thickness big add pressurize cooling after at least 15 minutes below the external pressure 0.3MPa;
(3). the metallic plate that surface treatment is good or the PMI foam of composite material face and forming are put into the frock of metal or nonmetal band curvature die cavity or are gluedd joint frock, finish splicing with glued membrane or adhesive laying again;
(4). the PMI cystosepiment sealing of laying being finished splicing with vacuum bag is put into autoclave or is put into baking oven with the PMI cystosepiment sealing that vacuum bag is finished splicing with laying and is cured moulding.
2. thermoforming process according to claim 1 is characterized in that, the softening temperature of heating that described PMI cystosepiment carries out in baking oven or autoclave is 190 ℃～205 ℃.
3. thermoforming process according to claim 1 and 2, it is characterized in that putting into the epoxy resin glued membrane or glued joint PMI foam that frock glueds joint can be the splicing that the multilayer laying is finished composite material face or metal decking and the inboard interface of PMI cystosepiment, and the PMI cystosepiment sealing of laying being finished splicing with vacuum bag is put into PMI cystosepiment that autoclave or vacuum bag finish splicing with laying and sealed and put into baking oven and carry out the co-curing moulding again.
4. thermoforming process according to claim 1 and 2 is characterized in that described (t in the formula: insulation the number of minutes, δ is a depth of foam, unit: mm) experience is determined by empirical equation: t 〉=15+ δ according to the depth of foam temperature retention time.
5. thermoforming process according to claim 1 and 2 is characterized in that glued membrane is the epoxy resin glued membrane.
6. thermoforming process according to claim 1 and 2 is characterized in that glueing joint press molding for superhuge sandwich PMI foam by splicing.
7. thermoforming process according to claim 1 and 2 is characterized in that described composite is a glass-reinforced plastic material.
8. thermoforming process according to claim 1 and 2 is characterized in that described composite is mixing of glass fabric and unsaturated polyester (UP) or epoxy resin composite material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB200510021884XA CN100532069C (en) | 2005-10-18 | 2005-10-18 | Thermal forming method for PMI foam laminated structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB200510021884XA CN100532069C (en) | 2005-10-18 | 2005-10-18 | Thermal forming method for PMI foam laminated structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1775507A CN1775507A (en) | 2006-05-24 |
| CN100532069C true CN100532069C (en) | 2009-08-26 |
Family
ID=36765286
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB200510021884XA Expired - Fee Related CN100532069C (en) | 2005-10-18 | 2005-10-18 | Thermal forming method for PMI foam laminated structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100532069C (en) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101905528B (en) * | 2010-07-16 | 2012-07-04 | 沈阳飞机工业（集团）有限公司 | Wedge-shaped autoclave forming process of composite material I-shaped section |
| CN102092137B (en) * | 2010-11-12 | 2013-06-26 | 航天材料及工艺研究所 | High-temperature high-pressure vacuum nozzle and sealing method thereof |
| CN105620712A (en) * | 2014-10-28 | 2016-06-01 | 中国航空工业集团公司西安飞机设计研究所 | Large bend air inflow channel of foam interlayer structure and forming method for foam core of foam interlayer structure |
| CN106738815A (en) * | 2016-11-30 | 2017-05-31 | 江西洪都航空工业集团有限责任公司 | A kind of rigid foam core thermoforming process |
| CN109687159A (en) * | 2018-12-27 | 2019-04-26 | 上海复合材料科技有限公司 | Ultralight high-precision rapid shaping antenna reflective face and preparation method thereof |
| CN112297401A (en) * | 2020-10-10 | 2021-02-02 | 江西洪都航空工业集团有限责任公司 | Hot bending forming method for PMI foam of aviation interlayer composite material |
-
2005
- 2005-10-18 CN CNB200510021884XA patent/CN100532069C/en not_active Expired - Fee Related
Non-Patent Citations (1)
| Title |
|---|
| US5443884A 1995.08.22 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1775507A (en) | 2006-05-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103895315B (en) | Glare component prepare manufacturing process | |
| CN110481059B (en) | Composite material foam sandwich structure and forming method thereof | |
| CN112454938A (en) | Forming method of carbon fiber honeycomb sandwich composite material member | |
| CN110641088A (en) | Lightweight composite board for railway vehicle | |
| CN101407168A (en) | Passenger car skylight sunshading board and production process thereof | |
| CN110561792B (en) | Low-cost composite material large cabin integral forming method | |
| CN100532069C (en) | Thermal forming method for PMI foam laminated structure | |
| CN111002603A (en) | Manufacturing method of integrally formed automobile rear wing | |
| CN204701616U (en) | High-speed trains ceiling board | |
| CN109591329A (en) | A kind of carbon fiber full-height foam core filled composite material rudder face structure and preparation method thereof | |
| WO2020122260A1 (en) | Production method for fiber-reinforced resin molded article | |
| CN101653997A (en) | Process for producing low-density polyurethane foam sound insulating pad | |
| CN114074436B (en) | Composite control arm for vehicle and forming method thereof | |
| CN106476330A (en) | A kind of rail vehicle aramid fiber honeycomb side top board and preparation method thereof | |
| CN211000274U (en) | Lightweight composite board for railway vehicle | |
| CN111114037A (en) | Carbon fiber composite material interlayer and method for manufacturing automobile body by adopting interlayer | |
| CN114055807B (en) | Method for forming composite material part, formed part and aircraft | |
| CN110299598A (en) | A kind of aramid fiber covering-paper honeycomb interlayer barrel shell structure and its preparation method and application | |
| CN206154811U (en) | Novel compound panel | |
| CN214477707U (en) | Battery pack | |
| CN112123810B (en) | Process method for improving forming quality of large-thickness composite material rudder | |
| CN210590660U (en) | Rail transit equipment cabin bottom plate forming die | |
| CN104477252A (en) | Heat preservation compartment plate for refrigerator truck | |
| CN210161714U (en) | Rail transit decoration panel based on thermosetting prepreg and sandwich structure | |
| CN204296557U (en) | A kind of without bottom girder refrigerated semitrailer |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090826 Termination date: 20181018 |