CN108437306B - Composite material microwave indirect heating mold and curing method - Google Patents

Composite material microwave indirect heating mold and curing method Download PDF

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CN108437306B
CN108437306B CN201810325089.7A CN201810325089A CN108437306B CN 108437306 B CN108437306 B CN 108437306B CN 201810325089 A CN201810325089 A CN 201810325089A CN 108437306 B CN108437306 B CN 108437306B
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CN108437306A (en
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李迎光
周靖
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Nanjing University of Aeronautics and Astronautics
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C35/00Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding

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  • Oral & Maxillofacial Surgery (AREA)
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  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
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  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

A microwave indirect heating mould for composite material and its solidifying method features that the microwave is absorbed by the microwave absorbing surface of said indirect heating mould, and the microwave energy is converted into heat energy for heating and solidifying the part made of composite material. The invention can realize the effective heating and curing of the multi-directional layering carbon fiber reinforced resin matrix composite material and the glass fiber reinforced resin matrix composite material, has a series of advantages of short curing time, low energy consumption and the like, greatly improves the microwave curing efficiency of the composite material parts, and provides theoretical basis and technical support for the industrial application of the composite material microwave curing technology.

Description

复合材料微波间接加热模具及固化方法Composite material microwave indirect heating mold and curing method

技术领域technical field

本发明涉及一种复合材料加热模具及固化方法,尤其是一种复合材料微波加热模具及固化方法,具体地说是一种复合材料微波间接加热模具及固化方法。The invention relates to a composite material heating mold and a curing method, in particular to a composite material microwave heating mold and a curing method, in particular to a composite material microwave indirect heating mold and a curing method.

背景技术Background technique

先进复合材料具有比强度和比模量高、抗疲劳性能好、耐腐蚀性能好和整体成型性好等许多优异特性,飞机上大量应用复合材料不仅可以明显减轻飞机的结构重量,提高飞机性能,还可以大大减少零部件数量,简化装配工序,缩短制造周期。目前复合材料已广泛用于机翼和机身的主承力零件,在进气道等复杂曲面零件上的用量越来越多,并向整体成型、共固化方向发展。Advanced composite materials have many excellent properties, such as high specific strength and specific modulus, good fatigue resistance, good corrosion resistance and good overall formability. It can also greatly reduce the number of parts, simplify the assembly process, and shorten the manufacturing cycle. At present, composite materials have been widely used in the main load-bearing parts of wings and fuselage, and are used more and more in complex curved parts such as air intakes, and are developing towards integral molding and co-curing.

目前,复合材料主要采用热压罐工艺加热加压固化成型。热压罐固化工艺以电阻丝加热空气后在风机作用下循环流动,以对流换热和热传导的方式加热复合材料,复合材料表面先加热,然后传热至内部。复材零件的加热速率缓慢、零件厚度方向温差大,成型周期长,且空气和模具均需加热至高温,能耗高。申请人前期提出的微波固化方法以电磁波直接穿透、内外同时均匀加热复合材料,加热速度快,成型周期短,微波选择性加热复合材料,空气与模具均不加热,能耗低。At present, composite materials are mainly formed by heating and pressure curing in the autoclave process. In the autoclave curing process, the air is heated by a resistance wire and circulated under the action of a fan, and the composite material is heated by convection heat exchange and heat conduction. The surface of the composite material is heated first, and then the heat is transferred to the interior. The heating rate of composite parts is slow, the temperature difference in the thickness direction of the parts is large, the molding cycle is long, and both the air and the mold need to be heated to high temperatures, resulting in high energy consumption. The microwave curing method proposed by the applicant in the early stage uses electromagnetic waves to directly penetrate and uniformly heat the composite material inside and outside at the same time. The heating speed is fast, the molding cycle is short, the microwave selectively heats the composite material, neither the air nor the mold is heated, and the energy consumption is low.

然而,通过大量研究,申请人发现微波难以穿透加热多向铺层碳纤维增强树脂基复合材料,以及微波固化玻璃纤维增强树脂基复合材料加热效率低等问题。针对上述问题,本发明提出一种复合材料微波间接加热模具及固化方法,采用微波间接加热模具的吸波型面吸收微波,将微波能转化为热能用于加热固化复合材料零件。本发明可以实现多向铺层碳纤维增强树脂基复合材料和玻璃纤维增强树脂基复合材料的有效加热固化,具有固化时间短、能耗低等一系列优点,大大提高了这类复合材料零件的微波固化效率,为复合材料微波固化技术的工业应用提供了理论依据与技术支撑。However, through extensive research, the applicant found that microwaves are difficult to penetrate and heat the multi-directional layered carbon fiber reinforced resin matrix composites, and the microwave-cured glass fiber reinforced resin matrix composites have problems such as low heating efficiency. In view of the above problems, the present invention proposes a composite material microwave indirect heating mold and a curing method. The microwave absorbing surface of the microwave indirect heating mold is used to absorb microwaves, and the microwave energy is converted into heat energy for heating and curing composite material parts. The invention can realize effective heating and curing of multi-directional layered carbon fiber reinforced resin matrix composite materials and glass fiber reinforced resin matrix composite materials, has a series of advantages such as short curing time and low energy consumption, and greatly improves the microwave power of such composite material parts. The curing efficiency provides theoretical basis and technical support for the industrial application of composite microwave curing technology.

发明内容SUMMARY OF THE INVENTION

本发明的目的是针对微波难以穿透加热多向铺层碳纤维增强树脂基复合材料,以及微波固化玻璃纤维增强树脂基复合材料加热效率低等问题,发明一种复合材料微波间接加热模具及固化方法。The purpose of the present invention is to invent a microwave indirect heating mold for composite materials and a curing method in view of the problems that microwaves are difficult to penetrate and heat multi-directional layered carbon fiber reinforced resin-based composite materials, and the heating efficiency of microwave-cured glass fiber reinforced resin-based composite materials is low. .

本发明的技术方案之一是:One of the technical solutions of the present invention is:

一种复合材料微波间接加热模具,其特征在于:模具由支撑桁架、透波面板、隔热层和吸波型面组成;支撑桁架与透波面板间采用机械连接,用于支撑透波面板;透波面板的表面设有放置隔热层和吸波型面的凹槽,隔热层位于凹槽的底部,待加热固化的复合材料放置在所述的吸波型面上。吸波型面的高度与透波面板四周的高度保持一致,即吸波型面的上表面与透波面板的上表面齐平。A composite material microwave indirect heating mold is characterized in that: the mold is composed of a supporting truss, a wave-transmitting panel, a heat insulating layer and a wave-absorbing profile; the supporting truss and the wave-transmitting panel are mechanically connected to support the wave-transmitting panel; The surface of the wave-transmitting panel is provided with a groove for placing the heat-insulating layer and the wave-absorbing surface, the heat-insulating layer is located at the bottom of the groove, and the composite material to be heated and cured is placed on the wave-absorbing surface. The height of the wave-absorbing profile is consistent with the height around the wave-transmitting panel, that is, the upper surface of the wave-absorbing profile is flush with the upper surface of the wave-transmitting panel.

所述的支撑桁架由圆滑过渡的金属结构组成,如不锈钢圆管,支撑桁架表面及连接处不存在任何尖角和毛刺。The supporting truss is composed of a smooth transition metal structure, such as a stainless steel round tube, and there are no sharp corners and burrs on the surface and the connection of the supporting truss.

所述的透波面板由透波性能良好且具有一定刚度和硬度的材料组成,如玻璃纤维增强树脂基复合材料、陶瓷、聚四氟乙烯等;透波面板表面的凹槽四周采用直径不小于5mm的圆弧过渡,不存在过渡尖角。The wave-transmitting panel is composed of materials with good wave-transmitting performance and certain stiffness and hardness, such as glass fiber reinforced resin-based composite materials, ceramics, polytetrafluoroethylene, etc.; 5mm arc transition, there is no transition sharp corner.

所述的隔热层由隔热性能良好的材料组成(如玻璃纤维布、石棉布等),用于降低吸波型面向透波面板和周围环境的热量损耗。The thermal insulation layer is composed of materials with good thermal insulation properties (such as glass fiber cloth, asbestos cloth, etc.), and is used to reduce the heat loss of the wave absorbing type facing the wave-transmitting panel and the surrounding environment.

所述的吸波型面由短切碳纤维毡增强树脂基复合材料组成,短切碳纤维的长度为3mm~20mm(优选4mm~6mm),短切碳纤维的体积分数为42%~58%(优选48.5%~52.5%),吸波型面的厚度为5mm~15mm(优选8mm~12mm);当使用温度在150℃以下时,吸波型面的树脂基体采用环氧树脂或双马树脂等低温树脂体系,当使用温度在150℃以上时,吸波型面的树脂基体采用聚酰亚胺树脂等高温树脂体系;吸波型面四周采用半径不小于5mm的圆弧过渡,不存在过渡尖角;吸波型面四周边缘应至少大于待固化复合材料零件四周边缘50mm。The wave-absorbing profile is composed of chopped carbon fiber felt reinforced resin-based composite material, the length of the chopped carbon fiber is 3mm~20mm (preferably 4mm~6mm), and the volume fraction of the chopped carbon fiber is 42%~58% (preferably 48.5mm). %~52.5%), the thickness of the absorbing surface is 5mm~15mm (preferably 8mm~12mm); when the operating temperature is below 150 °C, the resin matrix of the absorbing surface adopts low temperature resin such as epoxy resin or double horse resin. When the operating temperature is above 150 °C, the resin matrix of the absorbing surface adopts a high-temperature resin system such as polyimide resin; the surrounding of the absorbing surface adopts an arc transition with a radius of not less than 5mm, and there is no transition sharp corner; The surrounding edge of the wave absorbing profile should be at least 50mm larger than the surrounding edge of the composite part to be cured.

本发明的技术方案之二是:The second technical solution of the present invention is:

一种复合材料微波间接固化方法,其特征在于:当待固化复合材料零件的厚度不大于5mm时,直接在所述的微波间接加热模具上依次放置脱模布、待固化复合材料零件、脱模布、吸胶布、无孔隔离膜、透气毡、真空袋等;当待固化复合材料零件的厚度大于5mm时,在所述的微波间接加热模具上依次放置脱模布、待固化复合材料零件、脱模布、吸胶布、无孔隔离膜、吸波层、透气毡、真空袋等;真空袋采用密封胶带密封进行抽真空;对于待固化复合材料零件为零吸胶复合材料体系时,无需设置吸胶布等辅助材料;当待固化复合材料零件为平板或单曲率层合板等简单结构时,所述的吸波层与模具吸波型面的材料、形状、厚度一致,当待固化复合材料零件为双曲率或多曲率层合板等复杂结构时,所述的吸波层采用与模具吸波型面吸波性能相当的柔性吸波隔膜组成(如碳黑硅胶隔膜等);所述的微波间接加热模具放置在微波腔体内,模具上的金属结构与微波腔体的金属壁面接触良好(共地),避免强电磁环境下放电打火和拉弧现象;固化时,实时测量复合材料零件和吸波型面的温度,采用吸波型面的测量温度与设定固化温度间的差值实时调节微波腔体内的功率,直至复合材料零件完全固化。A microwave indirect curing method for composite materials, which is characterized in that: when the thickness of the composite material parts to be cured is not greater than 5 mm, a mold release cloth, the composite material parts to be cured, and the mold release cloth are directly placed on the microwave indirect heating mold in sequence. cloth, absorbent cloth, non-porous isolation film, breathable felt, vacuum bag, etc.; when the thickness of the composite material part to be cured is greater than 5mm, place release cloth, composite material part to be cured, Release cloth, absorbent cloth, non-porous isolation film, wave absorbing layer, breathable felt, vacuum bag, etc.; the vacuum bag is sealed with sealing tape for vacuuming; for the composite material to be cured, there is no need to set the zero-adhesive composite material system Auxiliary materials such as absorbent cloth; when the composite material to be cured is a simple structure such as a flat plate or a single-curvature laminate, the material, shape and thickness of the absorbing layer and the absorbing surface of the mold are consistent. When the part is a complex structure such as a double-curvature or multi-curvature laminate, the wave-absorbing layer is composed of a flexible wave-absorbing diaphragm (such as a carbon black silicone diaphragm, etc.) with the wave-absorbing performance of the wave-absorbing surface of the mold; the microwave The indirect heating mold is placed in the microwave cavity, and the metal structure on the mold is in good contact with the metal wall surface of the microwave cavity (common ground) to avoid the phenomenon of discharge ignition and arc drawing in a strong electromagnetic environment; during curing, real-time measurement of composite parts and For the temperature of the absorbing surface, the difference between the measured temperature of the absorbing surface and the set curing temperature is used to adjust the power in the microwave cavity in real time until the composite parts are completely cured.

本发明的有益效果:Beneficial effects of the present invention:

本发明可以实现多向铺层碳纤维增强树脂基复合材料和玻璃纤维增强树脂基复合材料的有效加热固化,具有固化时间短、能耗低等一系列优点,大大提高了这类复合材料零件的微波固化效率,为复合材料微波固化技术的工业应用提供了理论依据与技术支撑。The invention can realize effective heating and curing of multi-directional layered carbon fiber reinforced resin matrix composite materials and glass fiber reinforced resin matrix composite materials, has a series of advantages such as short curing time and low energy consumption, and greatly improves the microwave power of such composite material parts. The curing efficiency provides theoretical basis and technical support for the industrial application of composite microwave curing technology.

附图说明Description of drawings

图1是本发明的复合材料微波间接加热模具及真空封装系统;1 is a composite microwave indirect heating mold and a vacuum packaging system of the present invention;

图中:1为支撑桁架,2为透波面板,3为隔热层,4为吸波型面,5为脱模布、6为复合材料零件、7为吸胶布、8为无孔隔离膜,9为吸波层,10为透气毡,11为真空袋、12为密封胶带。In the figure: 1 is the supporting truss, 2 is the wave-transmitting panel, 3 is the thermal insulation layer, 4 is the wave-absorbing profile, 5 is the release cloth, 6 is the composite material part, 7 is the absorbent cloth, and 8 is the non-porous isolation film , 9 is the absorbing layer, 10 is the air felt, 11 is the vacuum bag, 12 is the sealing tape.

具体实施方式Detailed ways

下面结合附图和实施例对本发明作进一步的说明。The present invention will be further described below with reference to the accompanying drawings and embodiments.

实施例一。Example 1.

本实施例采用24层碳纤维增强的双马树脂复合材料层合板作为待固化的复合材料零件(6),铺层顺序为[0/+45/-45/90]5,零件尺寸为300mm×300mm×3mm,固化温度为200℃。微波间接加热模具由支撑桁架(1)、透波面板(2)、隔热层(3)和吸波型面(4)组成。其中,支撑桁架(1)由外径为40mm,内径为36mm的不锈钢管焊接制成;透波面板(2)采用透波陶瓷制作,尺寸为500mm×500mm×30mm,凹槽尺寸为400mm×400mm×12mm,凹槽四周的转角为半径为8mm的四分之一圆弧;支撑桁架(1)与陶瓷透波面板(2)间采用螺纹机械连接,连接处表面打磨光滑,不存在尖角和毛刺;隔热层(3)由16层玻璃纤维布组成,厚度为2mm;吸波型面(4)采用短切碳纤维毡增强聚酰亚胺树脂复合材料制成,短切碳纤维的长度为5mm,碳纤维的体积分数为50%,吸波型面尺寸为399mm×399mm×10mm,四周转角为半径为7.8mm的四分之一圆弧,最高使用温度为350℃。In this example, 24 layers of carbon fiber reinforced bismuth resin composite material laminates are used as the composite material parts ( 6 ) to be cured. ×3mm, curing temperature is 200°C. The microwave indirect heating mold is composed of a supporting truss (1), a wave-transmitting panel (2), a heat insulating layer (3) and a wave-absorbing surface (4). Among them, the support truss (1) is welded by stainless steel pipes with an outer diameter of 40mm and an inner diameter of 36mm; the wave-transmitting panel (2) is made of wave-transmitting ceramics, with a size of 500mm×500mm×30mm, and a groove size of 400mm×400mm ×12mm, the corners around the groove are quarter arcs with a radius of 8mm; the support truss (1) and the ceramic wave-transmitting panel (2) are mechanically connected with threads, and the surface of the connection is polished smoothly without sharp corners and Burr; the heat insulation layer (3) is composed of 16 layers of glass fiber cloth, with a thickness of 2mm; the wave absorbing surface (4) is made of chopped carbon fiber felt reinforced polyimide resin composite material, and the length of the chopped carbon fiber is 5mm , the volume fraction of carbon fiber is 50%, the size of the absorbing surface is 399mm × 399mm × 10mm, the surrounding corner is a quarter arc with a radius of 7.8mm, and the maximum operating temperature is 350 ℃.

铺层完毕后,在复合材料零件(6)周围粘贴铝箔胶带,预留流胶孔,并将复合材料零件(6)和一系列真空辅助材料放置在微波间接加热模具上。放置顺序依次为脱模布(5)、待固化复合材料零件(6)、脱模布(5)、无孔隔离膜(8)、透气毡(10)、真空袋(11)等;真空袋(11)采用密封胶带(12)密封进行抽真空,真空度为-0.098MPa。将准备好的微波间接加热模具放置在微波腔体内,不锈钢支撑桁架(1)与微波腔体的金属壁面接触良好;固化时,实时测量复合材料零件(6)和吸波型面(4)的温度,采用吸波型面(4)的测量温度与设定固化温度间的差值实时调节微波腔体内的功率,直至复合材料零件(6)完全固化。After the lamination is completed, the aluminum foil tape is pasted around the composite material part (6), the flow glue hole is reserved, and the composite material part (6) and a series of vacuum auxiliary materials are placed on the microwave indirect heating mold. The order of placement is the release cloth (5), the composite material part to be cured (6), the release cloth (5), the non-porous isolation film (8), the air felt (10), the vacuum bag (11), etc.; the vacuum bag (11) Use sealing tape (12) to seal and vacuumize, and the vacuum degree is -0.098MPa. The prepared microwave indirect heating mold is placed in the microwave cavity, and the stainless steel support truss (1) is in good contact with the metal wall of the microwave cavity; during curing, real-time measurement of the composite material part (6) and the wave absorbing profile (4) temperature, using the difference between the measured temperature of the wave absorbing profile (4) and the set curing temperature to adjust the power in the microwave cavity in real time until the composite material part (6) is completely cured.

实施例二。Example two.

本实施例采用200层玻璃纤维增强的环氧树脂复合材料层合板作为待固化的复合材料零件(6),铺层顺序为[0/90]100,零件尺寸为300mm×300mm×20mm,固化温度为120℃。微波间接加热模具由支撑桁架(1)、透波面板(2)、隔热层(3)和吸波型面(4)组成。其中,支撑桁架(1)由外径为40mm,内径为36mm的不锈钢管焊接制成;透波面板(2)采用玻璃纤维增强环氧树脂复合材料制成,尺寸为500mm×500mm×30mm,凹槽尺寸为400mm×400mm×12mm,凹槽四周的转角为半径为8mm的四分之一圆弧;支撑桁架(1)与玻璃纤维增强环氧树脂复合材料透波面板(2)间采用螺纹机械连接,连接处表面打磨光滑,不存在尖角和毛刺;隔热层(3)由厚度为2mm的石棉布组成;吸波型面(4)采用短切碳纤维毡增强双马树脂复合材料制成,短切碳纤维的长度为5mm,碳纤维的体积分数为50%,吸波型面尺寸为399mm×399mm×10mm,四周转角为半径为7.8mm的四分之一圆弧,最高使用温度为180℃。In this example, 200 layers of glass fiber reinforced epoxy resin composite material laminates are used as the composite material parts (6) to be cured, the layering sequence is [0/90] 100 , the size of the parts is 300mm×300mm×20mm, and the curing temperature is is 120°C. The microwave indirect heating mold is composed of a supporting truss (1), a wave-transmitting panel (2), a heat insulating layer (3) and a wave-absorbing surface (4). Among them, the supporting truss (1) is made of stainless steel pipes with an outer diameter of 40mm and an inner diameter of 36mm; The size of the groove is 400mm×400mm×12mm, and the corners around the groove are quarter arcs with a radius of 8mm; a screw machine is used between the supporting truss (1) and the glass fiber reinforced epoxy resin composite wave-transmitting panel (2). Connection, the surface of the connection is polished and smooth, and there are no sharp corners and burrs; the heat insulation layer (3) is composed of asbestos cloth with a thickness of 2mm; the wave absorbing surface (4) is made of chopped carbon fiber felt reinforced Shuangma resin composite material , the length of the chopped carbon fiber is 5mm, the volume fraction of the carbon fiber is 50%, the size of the absorbing surface is 399mm×399mm×10mm, the surrounding corner is a quarter arc with a radius of 7.8mm, and the maximum operating temperature is 180℃ .

铺层完毕后,将复合材料零件(6)和一系列真空辅助材料放置在微波间接加热模具上。放置顺序依次为脱模布(5)、待固化复合材料零件(6)、脱模布(5)、吸胶布(7)、无孔隔离膜(8)、吸波层(9)、透气毡(10)、真空袋(11)等;真空袋(11)采用密封胶带(12)密封进行抽真空,真空度为-0.098MPa。吸波层(9)采用碳黑含量为45%的硅胶隔膜制成,尺寸为300mm×300mm×8mm。将准备好的微波间接加热模具放置在微波腔体内,不锈钢支撑桁架(1)与微波腔体的金属壁面接触良好;固化时,实时测量复合材料零件(6)和吸波型面(4)的温度,采用吸波型面(4)的测量温度与设定固化温度间的差值实时调节微波腔体内的功率,直至复合材料零件(6)完全固化。After the layup is complete, the composite part (6) and a series of vacuum-assisted materials are placed on the microwave indirect heating mold. The order of placement is demoulding cloth (5), composite parts to be cured (6), demoulding cloth (5), absorbent cloth (7), non-porous isolation film (8), wave absorbing layer (9), air felt (10), a vacuum bag (11), etc.; the vacuum bag (11) is sealed with a sealing tape (12) for vacuuming, and the vacuum degree is -0.098MPa. The wave absorbing layer (9) is made of a silica gel diaphragm with a carbon black content of 45%, and the size is 300mm×300mm×8mm. The prepared microwave indirect heating mold is placed in the microwave cavity, and the stainless steel support truss (1) is in good contact with the metal wall of the microwave cavity; during curing, real-time measurement of the composite material part (6) and the wave absorbing profile (4) temperature, using the difference between the measured temperature of the wave absorbing profile (4) and the set curing temperature to adjust the power in the microwave cavity in real time until the composite material part (6) is completely cured.

以上仅是本发明的具体应用范例,对本发明的保护范围不构成任何限制。凡采用等同变换或是等效替换而形成的技术方案,均落在本发明权利保护范围之内。The above are only specific application examples of the present invention, and do not constitute any limitation to the protection scope of the present invention. All technical solutions formed by equivalent transformation or equivalent replacement fall within the protection scope of the present invention.

本发明未涉及部分与现有技术相同或可采用现有技术加以实现。The parts not involved in the present invention are the same as or can be implemented by using the prior art.

Claims (6)

1. A composite microwave indirect heating mould is characterized in that: the mould consists of a supporting truss, a wave-transmitting panel, a heat-insulating layer and a wave-absorbing molded surface; the supporting truss is mechanically connected with the wave-transmitting panel and is used for supporting the wave-transmitting panel; the surface of the wave-transmitting panel is provided with a groove for placing a heat insulation layer and a wave-absorbing molded surface, the heat insulation layer is positioned at the bottom of the groove, and the composite material to be heated and cured is placed on the wave-absorbing molded surface; the support truss is a smooth transition metal structural part, and the metal structural part is well contacted with the metal wall surface of the microwave cavity and is grounded so as to avoid the phenomena of discharging, igniting and arcing in a strong electromagnetic environment; the wave-transmitting panel is made of materials with good wave-transmitting performance and certain rigidity and hardness, the periphery of the groove on the surface of the wave-transmitting panel is in arc transition with the diameter not less than 5mm, and transition sharp corners do not exist; the wave-absorbing profile is made of chopped carbon fiber felt reinforced resin matrix composite materials, the length of the chopped carbon fibers is 4 mm-6 mm, the volume fraction of the chopped carbon fibers is 48.5% -52.5%, and the thickness of the wave-absorbing profile is 8 mm-12 mm; when the use temperature is below 150 ℃, the resin matrix of the wave-absorbing profile adopts epoxy resin or bismaleimide resin, and when the use temperature is above 150 ℃, the resin matrix of the wave-absorbing profile adopts polyimide resin; the periphery of the wave-absorbing molded surface is in arc transition with the radius not less than 5mm, and a transition sharp corner does not exist; the peripheral edge of the wave-absorbing molded surface is at least 50mm larger than the peripheral edge of the composite material part to be cured;
when the thickness of the composite material part to be cured is not more than 5mm, directly and sequentially placing demoulding cloth, the composite material part to be cured, the demoulding cloth, the adhesive absorption cloth, the nonporous isolation film, the breathable felt and the vacuum bag on the microwave indirect heating mould; when the thickness of the composite material part to be cured is more than 5mm, sequentially placing demoulding cloth, the composite material part to be cured, the demoulding cloth, the adhesive absorption cloth, the nonporous isolation film, the wave absorbing layer, the breathable felt and the vacuum bag on the microwave indirect heating mould; the vacuum bag is sealed by a sealing adhesive tape and vacuumized; when the composite material part to be cured is a zero-adhesive-absorption composite material system, an adhesive absorption cloth does not need to be arranged; when the composite material part to be cured is of a flat plate or single-curvature laminated plate structure, the wave-absorbing layer is consistent with the wave-absorbing profile of the die in material, shape and thickness, and when the composite material part to be cured is of a double-curvature or multi-curvature laminated plate structure, the wave-absorbing layer is formed by a flexible wave-absorbing diaphragm which has equivalent wave-absorbing performance to the wave-absorbing profile of the die; the microwave indirect heating mould is arranged in the microwave cavity; and during curing, measuring the temperature of the composite part and the wave-absorbing profile in real time, and adjusting the power in the microwave cavity in real time by adopting the difference between the measured temperature of the wave-absorbing profile and the set curing temperature until the composite part is completely cured.
2. The composite microwave indirect heated mold of claim 1, wherein: the metal structural part is a stainless steel round pipe, and the surface and the joint of the metal structural part are free of sharp corners and burrs.
3. The composite microwave indirect heated mold of claim 1, wherein: the wave-transparent panel is made of glass fiber reinforced resin matrix composite, ceramic, polytetrafluoroethylene or glass.
4. The composite microwave indirect heated mold of claim 1, wherein: the heat insulation layer is made of materials with good heat insulation performance and used for reducing heat loss of the wave-absorbing molded surface to the wave-transmitting panel and the surrounding environment.
5. The composite microwave indirect heated mold of claim 4, wherein: the heat insulation layer is made of glass fiber cloth and asbestos cloth.
6. The composite microwave indirect heating mold of claim 1, wherein the flexible wave-absorbing membrane is a carbon black silica gel membrane.
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