CN115723390A - An electrothermal composite material based on a nickel-chromium alloy wire weft-knitted structure and its preparation method - Google Patents
An electrothermal composite material based on a nickel-chromium alloy wire weft-knitted structure and its preparation method Download PDFInfo
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- 239000002131 composite material Substances 0.000 title claims abstract description 65
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 title claims description 41
- 238000002360 preparation method Methods 0.000 title abstract description 7
- 239000004744 fabric Substances 0.000 claims abstract description 52
- 238000005485 electric heating Methods 0.000 claims abstract description 42
- 239000002313 adhesive film Substances 0.000 claims abstract description 27
- 239000004593 Epoxy Substances 0.000 claims abstract description 16
- 238000010438 heat treatment Methods 0.000 claims abstract description 16
- 239000003365 glass fiber Substances 0.000 claims abstract description 12
- 229920006231 aramid fiber Polymers 0.000 claims abstract description 10
- 238000009940 knitting Methods 0.000 claims abstract description 6
- 229910001120 nichrome Inorganic materials 0.000 claims abstract 3
- 229920000728 polyester Polymers 0.000 claims description 10
- 239000000835 fiber Substances 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 7
- 238000002955 isolation Methods 0.000 claims description 4
- 238000007789 sealing Methods 0.000 claims description 4
- 238000009941 weaving Methods 0.000 claims description 4
- 229910052751 metal Inorganic materials 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 239000011347 resin Substances 0.000 claims description 3
- 229920005989 resin Polymers 0.000 claims description 3
- 239000004760 aramid Substances 0.000 abstract description 2
- 239000004753 textile Substances 0.000 abstract description 2
- 229920004933 Terylene® Polymers 0.000 abstract 1
- 239000005020 polyethylene terephthalate Substances 0.000 abstract 1
- 239000010410 layer Substances 0.000 description 69
- 239000000463 material Substances 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- 238000013461 design Methods 0.000 description 3
- 238000005056 compaction Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000011157 advanced composite material Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000009954 braiding Methods 0.000 description 1
- 239000000805 composite resin Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000032798 delamination Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 238000003856 thermoforming Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
- 230000037303 wrinkles Effects 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Abstract
Description
技术领域technical field
本发明属于纺织复合材料领域,具体涉及一种基于镍铬合金丝纬编结构的电热复合材料及制备方法。The invention belongs to the field of textile composite materials, and in particular relates to an electrothermal composite material based on a nickel-chromium alloy weft-knitted structure and a preparation method thereof.
背景技术Background technique
电热防冰是常用于旋翼飞机发动机进气管道、尾翼和风挡玻璃的防冰方式,基本原理是通过防冰材料内表面的加热元件将电能转化为热能,热量传导至部件表面使温度升高,以达到防冰的目的。虽然电加热防冰技术作为最可靠的防冰技术之一,但仍存在功耗高、热惯性大、反复结冰等缺陷,需要突破一系列关键的技术难点。为了解决上述问题,可实现快速热响应、重量轻的电加热织物及其复合材料被应用于电加热防冰技术中。Electrothermal anti-icing is an anti-icing method commonly used in rotorcraft engine intake ducts, tail fins and windshields. The basic principle is to convert electrical energy into heat energy through the heating element on the inner surface of the anti-icing material, and the heat is conducted to the surface of the component to increase the temperature. In order to achieve the purpose of anti-icing. Although electric heating anti-icing technology is one of the most reliable anti-icing technologies, it still has defects such as high power consumption, large thermal inertia, and repeated icing, and a series of key technical difficulties need to be overcome. In order to solve the above problems, fast thermal response, light-weight electrically heated fabrics and their composite materials are applied in electrically heated anti-icing technology.
在旋翼飞机轻量化技术的需求大背景下,同时实现结构性能和电热功能的兼顾,是复合材料的必然趋势。电热复合材料是含有电加热元件的先进复合材料,是旋翼飞机复合材料的理想材料。In the context of the demand for rotorcraft lightweight technology, it is an inevitable trend for composite materials to simultaneously achieve structural performance and electrothermal functions. Electrothermal composites are advanced composite materials containing electric heating elements, ideal for rotorcraft composites.
电热复合材料多为纤维增强复合材料,一般是由许多单层材料通过粘合制成的多层结构。由于增强纤维在复合材料层内沿不同方向的热、力学特性在空间上是各向异性的,工作时温度分布不均,电热防冰材料层内、层间会产生较大热应力,导致层合结构易发生变形及分层现象,所以电热复合材料应具有良好的力学性能、温度可控性和升温速率。Electrothermal composite materials are mostly fiber-reinforced composite materials, which are generally multi-layer structures made of many single-layer materials bonded together. Since the thermal and mechanical properties of the reinforcing fiber in different directions in the composite material layer are anisotropic in space, the temperature distribution is uneven during operation, and large thermal stress will be generated in and between the layers of the electrothermal anti-icing material, resulting in layer The composite structure is prone to deformation and delamination, so the electrothermal composite material should have good mechanical properties, temperature controllability and heating rate.
发明内容Contents of the invention
本发明从镍铬合金丝的排布设计、电加热织物的制备,到树脂基复合材料的设计与成型,为电热复合材料结构与功能一体化设计与制备提供方法。The invention provides a method for the integrated design and preparation of the structure and function of the electrothermal composite material from the layout design of the nickel-chromium alloy wire, the preparation of the electric heating fabric, to the design and molding of the resin-based composite material.
为了克服现有的电热复合材料承载性能低、升温速率低以及热量分布不均匀等问题,本发明提供了一种基于镍铬合金丝纬编结构的电热复合材料及制备方法。In order to overcome the problems of low bearing capacity, low heating rate and uneven heat distribution of the existing electrothermal composite materials, the present invention provides an electrothermal composite material based on a weft-knitted structure of nickel-chromium alloy wires and a preparation method thereof.
技术方案Technical solutions
一种基于镍铬合金丝纬编结构的电热复合材料,为五层结构,依次由第一复合结构层1、胶膜层2、电加热织物层3、胶膜层2、第二复合结构层4构成;厚度方向上以电加热织物层3为中心的对称结构。An electrothermal composite material based on the weft-knitted structure of nickel-chromium alloy wire, which is a five-layer structure, sequentially composed of the first
进一步的,所述电加热织物层3包括电热元件和绝缘纤维,电热元件为镍铬合金丝,镍铬合金丝尺寸为0.04mm~0.2mm。Further, the electric
进一步的,所述第一复合结构层1由4层平纹玻纤/环氧预浸料分别按铺层角度0°、45°、0°、45°铺设构成,复合结构层采用中高温预浸料,该种预浸料模压或热压成型。Further, the first
进一步的,所述第二复合结构层4由4层平纹玻纤/环氧预浸料分别按铺层角度45°、0°、45°、0°铺设构成。Further, the second
进一步的,所述胶膜层2是中高温环氧结构胶膜,与所属第一复合结构层1和第二复合结构层4所采用的树脂体系一直,固化温度相同。Further, the
进一步的,电加热织物层3的发热在预留出的镍铬合金丝顶端施加电流,金属丝通电流产生焦耳热,织物表面温度发生改变。Further, the heating of the electrically heated
进一步的,电加热织物层3的织物结构为平针组织、罗纹组织、双罗纹组织。Further, the fabric structure of the electric
进一步的,所述镍铬合金丝和涤纶或芳纶纤维并股喂入电脑横机进行共同织造,镍铬合金丝置于织物内部。Further, the nickel-chromium alloy wire and the polyester or aramid fiber are fed into a computerized flat knitting machine in parallel for weaving together, and the nickel-chromium alloy wire is placed inside the fabric.
一种基于镍铬合金丝纬编结构的电热复合材料的制备方法,包括如下步骤:A method for preparing an electrothermal composite material based on a nickel-chromium alloy wire weft-knitted structure, comprising the steps of:
1)用加粘度的底胶将胶膜层贴覆在电加热织物层上、下表面;1) Paste the adhesive film layer on the upper and lower surfaces of the electric heating fabric layer with a viscous primer;
2)分别将4层平纹玻纤/环氧预浸料铺设在两层胶膜层表面,形成多层结构;2) Lay 4 layers of plain glass fiber/epoxy prepreg on the surface of the two layers of adhesive film to form a multi-layer structure;
3)用密封胶条和隔离膜把组装的多层结构密封,通过透气毡和真空袋连接导管将多层结构内抽真空;3) Seal the assembled multi-layer structure with sealing tape and isolation film, and vacuum the inside of the multi-layer structure through the air felt and the vacuum bag connecting conduit;
4)利用密封真空袋将真空多层结构放入热压罐中加热固化,得到电热复合材料。4) Putting the vacuum multilayer structure into an autoclave for heating and curing by using a sealed vacuum bag to obtain an electrothermal composite material.
技术效果technical effect
一种电热复合材料,包括电加热织物层,所述电加热织物层包括镍铬合金丝、涤纶、芳纶纤维,在电加热织物层上下表面贴合胶膜,然后铺覆不同铺设角度的玻纤/环氧预浸料,形成多层结构,对其进行抽真空压实,放入热压罐中加热固化,得到基于纬编针织结构的电热复合材料。本发明中,该种电热复合材料可以应用于具有电加热需求的工程领域,例如直升机进气道防冰,该种复合材料不仅可以满足承载结构力学性能要求,还可以提供有效的加热效率和平衡温度。An electrothermal composite material, comprising an electric heating fabric layer, the electric heating fabric layer includes nickel-chromium alloy wire, polyester, and aramid fiber, and an adhesive film is pasted on the upper and lower surfaces of the electric heating fabric layer, and then covered with glass with different laying angles. fiber/epoxy prepreg to form a multi-layer structure, which is vacuumed and compacted, placed in an autoclave for heating and curing, and an electrothermal composite material based on a weft-knitted structure is obtained. In the present invention, this kind of electrothermal composite material can be applied to engineering fields that require electric heating, such as anti-icing of helicopter air inlets. This kind of composite material can not only meet the mechanical performance requirements of load-bearing structures, but also provide effective heating efficiency and balance temperature.
附图说明Description of drawings
图1为电热复合材料结构示意图。Figure 1 is a schematic diagram of the structure of the electrothermal composite material.
图2为图1的爆炸图。Figure 2 is an exploded view of Figure 1.
图3为制备方法流程图。Figure 3 is a flow chart of the preparation method.
具体实施方式Detailed ways
下面结合实施例对本发明作进一步描述。以下所述仅为本发明一部分实施例,非全部实施例。基于本发明实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The present invention will be further described below in conjunction with embodiment. The following descriptions are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.
首先使用电脑横机进行电加热织物织造。上机参数度目70,罗拉速度15,为提高编织效率,保证镍铬合金丝纬编织物顺利下机,机头速度参数值为10。测试镍铬合金丝纬编织物的厚度时,压脚面积选择100mm2,测试时间设为10s,所加压力为20cN,每块试样测试5次。最终,织造了面密度93.6g/cm2的平针组织结构织物,厚度为0.342mm;面密度74.1g/cm2的罗纹组织结构织物,厚度为0.352mm;面密度148.9g/cm2的双罗纹组织结构织物,厚度为0.550mm,线圈圈距为1mm。Firstly, a computerized flat knitting machine is used to weave electrically heated fabrics. The parameters of the upper machine are 70 stitches, and the roller speed is 15. In order to improve the weaving efficiency and ensure the smooth unloading of the nickel-chromium alloy weft knitted fabric, the parameter value of the machine head speed is 10. When testing the thickness of nickel-chromium alloy weft-woven fabrics, the area of the presser foot is selected to be 100mm 2 , the test time is set to 10s, the applied pressure is 20cN, and each sample is tested 5 times. In the end, we weaved a plain structure fabric with a surface density of 93.6g/ cm 2 and a thickness of 0.342mm; a rib structure fabric with a surface density of 74.1g/cm 2 and a thickness of 0.352mm; Rib structure fabric with a thickness of 0.550mm and a loop pitch of 1mm.
对于织造的三种电加热织物,加热区:0.06mm细度镍铬合金丝与50D芳纶并股;绝缘区:双股75D涤纶低弹丝;喂入比:4/2的喂入比排列交织。For the woven three kinds of electric heating fabrics, heating area: 0.06mm fineness nickel-chromium alloy wire and 50D aramid fiber parallel strands; insulation area: double-strand 75D polyester low elastic yarn; feeding ratio: 4/2 feeding ratio arrangement intertwined.
如图1是本发明的结构示意图,按照图1的爆炸图图2进行预浸料和胶膜铺层。将面积为300×300mm厚度0.25mm平纹结构玻纤/环氧预浸料按铺层角度按铺层角度0°、45°、0°、45°一一铺设在钢板模具表面,紧接铺设同面积厚度0.2mm胶膜,电加热织物下表面紧贴胶膜,接着按对称一一铺覆胶膜和玻纤/环氧预浸料。Figure 1 is a schematic structural diagram of the present invention, and the prepreg and adhesive film are laid up according to the exploded view of Figure 1 and Figure 2 . Lay the plain weave structure glass fiber/epoxy prepreg with an area of 300×300mm and a thickness of 0.25mm on the surface of the steel plate mold one by one according to the lay-up angle according to the lay-up angle of 0°, 45°, 0°, and 45°, and then lay the same The area thickness is 0.2mm adhesive film, the lower surface of the electric heating fabric is close to the adhesive film, and then the adhesive film and glass fiber/epoxy prepreg are laid symmetrically one by one.
铺覆完成后,形成多层结构,用密封胶条和隔离膜将多层结构密封,通过透气毡和真空袋连接导管,将多层结构内在室温下抽真空15~30min进行预压实,压力为0.07~0.1MPa。随后,再次进行真空压实10~20min。After the paving is completed, a multi-layer structure is formed, and the multi-layer structure is sealed with a sealing strip and an isolation film, and the conduit is connected through an air felt and a vacuum bag, and the multi-layer structure is vacuumed at room temperature for 15 to 30 minutes for pre-compaction, and the pressure It is 0.07~0.1MPa. Subsequently, vacuum compaction was carried out again for 10-20 minutes.
利用密封真空袋将真空多层结构放入热压罐中加热固化,具体条件为:热压罐室温下抽真空保持小于-0.097MPa真空度,加热时以30℃/小时的速率升温至180℃,保温4小时,随后停温停压,随炉降温,降温至60℃以下出罐脱模,得到镍铬合金丝纬编结构的电热复合材料。Use a sealed vacuum bag to put the vacuum multi-layer structure into an autoclave for heating and curing. The specific conditions are: the autoclave is vacuumed at room temperature to maintain a vacuum degree of less than -0.097MPa, and the temperature is raised to 180°C at a rate of 30°C/hour during heating. , keep warm for 4 hours, then stop the temperature and pressure, lower the temperature with the furnace, drop the temperature below 60°C, and release the tank to obtain an electrothermal composite material with a weft-knitted structure of nickel-chromium alloy wire.
本发明中,电热复合材料电加热织物层包括电热元件和绝缘纤维。电热元件为镍铬合金丝,绝缘纤维是涤纶、芳纶纤维。In the present invention, the electric heating fabric layer of the electric heating composite material includes electric heating elements and insulating fibers. The heating element is nickel-chromium alloy wire, and the insulating fiber is polyester or aramid fiber.
本发明中,将镍铬合金丝、涤纶、芳纶纤维通过共织的形式,以平针、1+1罗纹、双罗纹组织结构,利用电脑横机进行织造电加热织物。In the present invention, nickel-chromium alloy wire, polyester, and aramid fiber are co-woven to weave electric heating fabrics with plain stitch, 1+1 rib, and double rib weave structures.
本发明中,电加热织物的发热是在预留出的镍铬合金丝顶端施加电流,通电流产生焦耳热,织物表面温度发生改变,最终使电热复合材料电加热织物层可以均匀发热。In the present invention, the heat generation of the electrically heated fabric is to apply an electric current to the top of the reserved nickel-chromium alloy wire, and the electric current generates Joule heat, and the surface temperature of the fabric changes, so that the electrically heated fabric layer of the electrothermal composite material can generate heat evenly.
实施例1Example 1
基于镍铬合金丝纬编结构的电热复合材料,为五层结构,依次由第一复合结构层1、胶膜层2、电加热织物层3、胶膜层2、第二复合结构层4构成;厚度方向上以电加热织物层3为中心的对称结构。The electrothermal composite material based on the weft-knitted structure of nickel-chromium alloy wire has a five-layer structure, which is composed of the first
进一步的,所述电加热织物层3包括电热元件和绝缘纤维,电热元件为镍铬合金丝,镍铬合金丝尺寸为0.04mm~0.2mm,镍铬合金丝是具有良好的导电性,高温环境中强度高,不易变形,常温热塑性好,不带磁性,耐腐蚀性好,使用寿命长。绝缘纤维是涤纶或芳纶纤维,涤纶或芳纶纤维为75D低弹丝,涤纶或芳纶材料的弹性好,不易褶皱,耐热性好,耐光性和耐化学品功能性好。镍铬合金丝与绝缘纤维通过复合编织成型,具有柔性好,适应不规则双曲结构。Further, the electric
进一步的,所述第一复合结构层1由4层平纹玻纤/环氧预浸料分别按铺层角度0°、45°、0°、45°铺设构成,复合结构层一般采用中高温预浸料,该种预浸料可模压和热压成型,成型后结构稳定,具有均匀性和可重复性,从模具中产出的每个零件相同,成型后防水性和耐腐蚀性好,外观较好,与所述电加热织物层3共固化后,结合紧密,不易分层。Further, the first
进一步的,所述第二复合结构层4由4层平纹玻纤/环氧预浸料分别按铺层角度45°、0°、45°、0°铺设构成,此种铺设构成方式可以增加零件的结构强度。Further, the second
进一步的,所述胶膜层2是中高温环氧结构胶膜,与所属第一复合结构层1和第二复合结构层4所采用的树脂体系一直,固化温度相同,所述胶膜层2的主要作用是增加电热织物层3与第一复合结构层1和第二复合结构层4的粘接性,增加固化后的强度。Further, the
进一步的,电加热织物层3的发热功能是在预留出的镍铬合金丝顶端施加电流,金属丝通电流产生焦耳热,织物表面温度发生改变,镍铬合金丝是热的良导电,别且均匀排布,最终使电热复合材料电加热织物层可以均匀发热。Further, the heating function of the electrically
进一步的,电加热织物层3的织物结构为平针组织、罗纹组织、双罗纹组织。Further, the fabric structure of the electric
进一步的,所述镍铬合金丝和涤纶或芳纶纤维并股喂入电脑横机进行共同织造,镍铬合金丝置于织物内部,利于传热,并且不因承受高频振动与织物发生脱离。Further, the nickel-chromium alloy wire and polyester or aramid fiber are fed into the computerized flat knitting machine in parallel for weaving together, and the nickel-chromium alloy wire is placed inside the fabric, which is conducive to heat transfer and does not separate from the fabric due to high-frequency vibration .
一种基于镍铬合金丝纬编结构的电热复合材料的制备方法,包括如下步骤:A method for preparing an electrothermal composite material based on a nickel-chromium alloy wire weft-knitted structure, comprising the steps of:
1)用加粘度的底胶将胶膜层贴覆在电加热织物层上、下表面;1) Paste the adhesive film layer on the upper and lower surfaces of the electric heating fabric layer with a viscous primer;
2)分别将4层平纹玻纤/环氧预浸料铺设在两层胶膜层表面,形成多层结构;2) Lay 4 layers of plain glass fiber/epoxy prepreg on the surface of the two layers of adhesive film to form a multi-layer structure;
3)用密封胶条和隔离膜把组装的多层结构密封,通过透气毡和真空袋连接导管将多层结构内抽真空;3) Seal the assembled multi-layer structure with sealing tape and isolation film, and vacuum the inside of the multi-layer structure through the air felt and the vacuum bag connecting conduit;
4)利用密封真空袋将真空多层结构放入热压罐中加热固化,得到电热复合材料。4) Putting the vacuum multilayer structure into an autoclave for heating and curing by using a sealed vacuum bag to obtain an electrothermal composite material.
本技术领域技术人员可以理解的是,除非另外定义,这里使用的所有术语(包括技术术语和科学术语)具有与本发明所属领域中的普通技术人员的一般理解相同的意义。还应该理解的是,诸如通用字典中定义的那些术语应该被理解为具有与现有技术的上下文中的意义一致的意义,并且除非像这里一样定义,不会用理想化或过于正式的含义来解释。以上所述的具体实施方式,对本发明的目的、技术方案和有益效果进行了进一步详细说明,所应理解的是,以上所述仅为本发明的具体实施方式而已,并不用于限制本发明,凡在本发明的精神和原则之内,所做的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。Those skilled in the art can understand that, unless otherwise defined, all terms (including technical terms and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. It should also be understood that terms such as those defined in commonly used dictionaries should be understood to have a meaning consistent with the meaning in the context of the prior art, and will not be interpreted in an idealized or overly formal sense unless defined as herein explain. The specific embodiments described above have further described the purpose, technical solutions and beneficial effects of the present invention in detail. It should be understood that the above descriptions are only specific embodiments of the present invention and are not intended to limit the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included within the protection scope of the present invention.
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