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CN106003850B - Honeycomb sandwich structural part and preparation method thereof - Google Patents

Honeycomb sandwich structural part and preparation method thereof Download PDF

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Publication number
CN106003850B
CN106003850B CN201610334926.3A CN201610334926A CN106003850B CN 106003850 B CN106003850 B CN 106003850B CN 201610334926 A CN201610334926 A CN 201610334926A CN 106003850 B CN106003850 B CN 106003850B
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hot
adhesive film
fiber
melt adhesive
foam
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CN106003850A (en
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巫俊斌
文峰
汪应山
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Guangdong Xinxiu New Material Co ltd
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Guangdong Xinxiu New Material Co ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/12Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/30Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers
    • B32B27/304Layered products comprising a layer of synthetic resin comprising vinyl (co)polymers; comprising acrylic (co)polymers comprising vinyl halide (co)polymers, e.g. PVC, PVDC, PVF, PVDF
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/32Layered products comprising a layer of synthetic resin comprising polyolefins
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/08Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B33/00Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/06Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the heating method
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/08Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the cooling method
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/10Interconnection of layers at least one layer having inter-reactive properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties

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  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Laminated Bodies (AREA)

Abstract

The invention discloses a honeycomb sandwich structural member and a preparation method thereof. The method comprises the following steps: s1, selecting a honeycomb core and filling foam to form a foam honeycomb core; s2, selecting two non-woven fabric layers and two hot melt adhesive film layers, sequentially placing the non-woven fabric layers, the hot melt adhesive film layers, the foam honeycomb core, the hot melt adhesive film layers and the non-woven fabric layers in a first mold, and adjusting the temperature and the pressure to perform hot-pressing combination to obtain an intermediate core; s3, placing the middle core between two fiber reinforced thermoplastic panels, placing the two fiber reinforced thermoplastic panels in a second mold, adjusting the temperature and the pressure to perform hot-pressing combination, and rapidly cooling after the hot pressing is finished to obtain the honeycomb sandwich middle plate; s4, injection molding and edge covering are carried out on the periphery of the honeycomb sandwich intermediate plate, and the honeycomb sandwich structural member is obtained. The honeycomb sandwich structural member prepared by the method has strong mechanical property, is not easy to degum and delaminate and has long service life.

Description

蜂窝夹芯结构件及其制备方法Honeycomb sandwich structure and its preparation method

技术领域technical field

本发明涉及蜂窝夹芯板技术领域,具体涉及蜂窝夹芯结构件及其制备方法。The invention relates to the technical field of honeycomb sandwich panels, in particular to a honeycomb sandwich structure and a preparation method thereof.

背景技术Background technique

复合夹层结构一般由三层材料复合形成,上下面是高强度、高模量材料的面板或蒙皮,中间层是较厚的轻质材料,称为芯子,组成一个整体,使两个面板或蒙皮保持一定距离,从而增加截面的惯性矩,这样既提高结构的弯曲刚度,又充分利用了材料的强度。用蜂窝芯作为芯子可以制出高性能、轻质的层合板,称为蜂窝夹芯结构。The composite sandwich structure is generally composed of three layers of materials. The upper and lower layers are panels or skins of high-strength, high-modulus materials. Or the skin keeps a certain distance, thereby increasing the moment of inertia of the section, which not only improves the bending stiffness of the structure, but also makes full use of the strength of the material. Using the honeycomb core as the core can produce a high-performance, lightweight laminate, called a honeycomb sandwich structure.

现有蜂窝夹芯结构的机械性能不理想,如热固性蒙皮蜂窝夹芯结构存在韧性较差,抗冲击性能不好等问题,影响其使用范围。另外由于蒙皮与蜂窝芯的黏结面积非常小,难以保证蒙皮与蜂窝芯的必要黏结,极易发生脱胶分层,而直接影响产品的性能和使用寿命。The mechanical properties of the existing honeycomb sandwich structure are not ideal. For example, the thermosetting skin honeycomb sandwich structure has problems such as poor toughness and poor impact resistance, which affect its application range. In addition, because the bonding area between the skin and the honeycomb core is very small, it is difficult to ensure the necessary bonding between the skin and the honeycomb core, and degumming and delamination are very easy to occur, which directly affects the performance and service life of the product.

发明内容Contents of the invention

基于此,本发明提供一种蜂窝夹芯结构件的制备方法,其制备的蜂窝夹芯结构件机械性能强、不易脱胶分层,使用寿命长。Based on this, the present invention provides a method for preparing a honeycomb sandwich structure. The prepared honeycomb sandwich structure has strong mechanical properties, is not easy to be degummed and delaminated, and has a long service life.

本发明还提供一种蜂窝夹芯结构件。The invention also provides a honeycomb sandwich structure.

为了实现本发明的目的,本发明采用以下技术方案:In order to realize the purpose of the present invention, the present invention adopts following technical scheme:

蜂窝夹芯结构件的制备方法,其包括如下步骤:A preparation method for a honeycomb sandwich structure, comprising the steps of:

S1、选取蜂窝芯,在所述蜂窝芯的孔内填充泡沫,形成泡沫蜂窝芯;S1, selecting a honeycomb core, filling foam in the pores of the honeycomb core to form a foam honeycomb core;

S2、选取第一无纺布层、第二无纺布层、第一热熔胶膜层、第二热熔胶膜层并提供第一模具,然后加热第一模具到大于第一热熔胶膜层与第二热熔胶膜层的熔点温度1℃-100℃,依次将第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层以及第二无纺布层置于第一模具中,合模,调整第一模具的压力为0.1MPa-1MPa,保温保压3s-120s,使得第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层以及第二无纺布层热压结合,脱模后得到中间芯;S2, select the first non-woven fabric layer, the second non-woven fabric layer, the first hot-melt adhesive film layer, the second hot-melt adhesive film layer and provide the first mold, then heat the first mold to be larger than the first hot-melt adhesive The melting point temperature of the film layer and the second hot-melt adhesive film layer is 1°C-100°C, and the first non-woven fabric layer, the first hot-melt adhesive film layer, the foam honeycomb core, the second hot-melt adhesive film layer and the second Place the non-woven fabric layer in the first mold, close the mold, adjust the pressure of the first mold to 0.1MPa-1MPa, keep the heat and pressure for 3s-120s, so that the first non-woven fabric layer, the first hot-melt adhesive film layer, the foam The honeycomb core, the second hot-melt adhesive film layer and the second non-woven fabric layer are combined by heat and pressure, and the intermediate core is obtained after demoulding;

S3、选取纤维增强热塑性面板并提供第二模具,加热第二模具到纤维增强热塑性面板的成型温度,将所述中间芯置于两片纤维增强热塑性面板之间,并置于所述第二模具中,合模,调整第二模具的压力为0.2MPa-5MPa,保温保压15s-150s,使得纤维增强热塑性面板与中间芯热压结合在一起,在30s-90s内迅速冷却后脱模,得到蜂窝夹芯中间板;S3. Select a fiber-reinforced thermoplastic panel and provide a second mold, heat the second mold to the molding temperature of the fiber-reinforced thermoplastic panel, place the intermediate core between two fiber-reinforced thermoplastic panels, and place it in the second mold In the process of closing the mold, adjust the pressure of the second mold to 0.2MPa-5MPa, and keep the heat and pressure for 15s-150s, so that the fiber-reinforced thermoplastic panel and the middle core are hot-compressed together, and they are demoulded after rapid cooling within 30s-90s to obtain Honeycomb sandwich panel;

S4、将蜂窝夹芯中间板嵌入注塑模具内,对蜂窝夹芯中间板进行注塑,在所述蜂窝夹芯中间板的周部形成包边,得到蜂窝夹芯结构件。S4. Embedding the honeycomb sandwich middle plate into the injection mold, injecting the honeycomb sandwich middle plate, forming hemming on the periphery of the honeycomb sandwich middle plate, and obtaining the honeycomb sandwich structure.

在其中一些实施例中,所述步骤S3与步骤S4之间,还具有步骤S31:去除所述蜂窝夹芯中间板周部的飞边。In some of the embodiments, between the step S3 and the step S4, there is also a step S31: removing the burrs on the periphery of the honeycomb sandwich middle plate.

在其中一些实施例中,所述步骤S1中蜂窝芯为PE蜂窝芯、PP蜂窝芯、PVC蜂窝芯、PC蜂窝芯、PET蜂窝芯、纸蜂窝芯、Nomex蜂窝芯以及铝蜂窝芯其中的一种,厚度为3mm-30mm。In some of these embodiments, the honeycomb core in the step S1 is one of PE honeycomb core, PP honeycomb core, PVC honeycomb core, PC honeycomb core, PET honeycomb core, paper honeycomb core, Nomex honeycomb core and aluminum honeycomb core , the thickness is 3mm-30mm.

在其中一些实施例中,所述步骤S1中泡沫为PVC泡沫、PS泡沫、PU泡沫、PUR泡沫、PEI泡沫、PI泡沫、PMI泡沫、PPSU泡沫以及SAN泡沫其中的一种或几种的组合,所述泡沫的密度为40-200kg/m3In some of these embodiments, the foam in the step S1 is one or a combination of PVC foam, PS foam, PU foam, PUR foam, PEI foam, PI foam, PMI foam, PPSU foam and SAN foam, The foam has a density of 40-200 kg/m 3 .

在其中一些实施例中,所述步骤S2中第一无纺布层与第二无纺布层均选自丙纶、涤纶、锦纶、腈纶、乙纶、氯纶中的一种,平方克重为10g/m2-100g/m2In some of these embodiments, in the step S2, the first non-woven layer and the second non-woven layer are all selected from polypropylene, polyester, nylon, acrylic, polyethylene, and polyvinyl chloride, and the square grammage is 10g/m 2 -100g/m 2 .

在其中一些实施例中,所述步骤S2中第一热熔胶膜层与第二热熔胶膜层选用同种热熔胶膜层,且均选自PO热熔胶膜、TPU热熔胶膜、PA热熔胶膜、EVA热熔胶膜以及PES热熔胶膜其中的一种,厚度为0.05mm-0.3mm。In some of these embodiments, the first hot-melt adhesive film layer and the second hot-melt adhesive film layer in the step S2 use the same kind of hot-melt adhesive film layer, and are selected from PO hot-melt adhesive film, TPU hot-melt adhesive film Film, PA hot-melt adhesive film, EVA hot-melt adhesive film and PES hot-melt adhesive film, with a thickness of 0.05mm-0.3mm.

在其中一些实施例中,所述步骤S3中纤维增强热塑性面板的厚度为0.2mm-3mm,纤维的体积含量为35%-65%,所述纤维增强热塑性面板由树脂基体与增强相组成,所述树脂基体为HDPE、LDPE、PP、PE、PC、PC/ABS合金、PA、TPU、PA6、PA66、PA11、PA12、PPS、PEK、PEEK、PI、PEI、PMMA、PLA、POM、PET和PBT中的一种,所述增强相为连续玻璃纤维、碳纤维、芳纶纤维、玄武岩纤维、PBO纤维、UHMWPE纤维、PET纤维、氧化铝纤维、碳化硅纤维编织布、单向布、编织布与单向布的混合布中的一种或多种。In some of these embodiments, the thickness of the fiber-reinforced thermoplastic panel in the step S3 is 0.2mm-3mm, the volume content of fibers is 35%-65%, and the fiber-reinforced thermoplastic panel is composed of a resin matrix and a reinforcing phase, so The above resin matrix is HDPE, LDPE, PP, PE, PC, PC/ABS alloy, PA, TPU, PA6, PA66, PA11, PA12, PPS, PEK, PEEK, PI, PEI, PMMA, PLA, POM, PET and PBT The reinforcing phase is continuous glass fiber, carbon fiber, aramid fiber, basalt fiber, PBO fiber, UHMWPE fiber, PET fiber, alumina fiber, silicon carbide fiber woven cloth, unidirectional cloth, woven cloth and single One or more of mixed cloth to cloth.

在其中一些实施例中,所述步骤S4中注塑用塑料为玻璃纤维或碳纤维增强塑料,纤维的重量含量为5%-65%,所述玻璃纤维或碳纤维增强塑料中的塑料基体为HDPE、LDPE、PP、PE、PC、PC/ABS合金、PA、TPU、PA6、PA66、PA11、PA12、PPS、PEK、PEEK、PI、PEI、PMMA、PLA、POM、PET和PBT中的一种。In some of these embodiments, the plastic used for injection molding in the step S4 is glass fiber or carbon fiber reinforced plastic, the weight content of the fiber is 5%-65%, and the plastic matrix in the glass fiber or carbon fiber reinforced plastic is HDPE, LDPE , PP, PE, PC, PC/ABS alloy, PA, TPU, PA6, PA66, PA11, PA12, PPS, PEK, PEEK, PI, PEI, PMMA, PLA, POM, PET and PBT.

本发明还采用如下技术方案:The present invention also adopts following technical scheme:

一种蜂窝夹芯结构件,由上述的方法制成,包括蜂窝夹芯中间板以及包覆于所述蜂窝夹芯中间板周部的包边,所述蜂窝夹芯中间板包括依次贴合连接的第一纤维增强热塑性面板、第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层、第二无纺布层以及第二纤维增强热塑性面板,所述泡沫蜂窝芯由蜂窝芯以及填充于所述蜂窝芯的孔内的泡沫组成。A honeycomb sandwich structure, made by the above method, comprising a honeycomb sandwich middle plate and a wrapping covering the periphery of the honeycomb sandwich middle plate, the honeycomb sandwich middle plate includes sequentially bonded and connected The first fiber-reinforced thermoplastic panel, the first non-woven fabric layer, the first hot-melt adhesive film layer, the foam honeycomb core, the second hot-melt adhesive film layer, the second non-woven fabric layer and the second fiber-reinforced thermoplastic panel, so The foam honeycomb core is composed of a honeycomb core and foam filled in the pores of the honeycomb core.

在其中一些实施例中,所述第一纤维增强热塑性面板与第二纤维增强热塑性面板的厚度均为0.2mm-3mm,所述第一热熔胶膜层与第二热熔胶膜层的厚度均为0.05mm-0.3mm,所述蜂窝芯的厚度为3mm-30mm。In some of these embodiments, the thicknesses of the first fiber-reinforced thermoplastic panel and the second fiber-reinforced thermoplastic panel are both 0.2mm-3mm, and the thicknesses of the first hot-melt adhesive film layer and the second hot-melt adhesive film layer are Both are 0.05mm-0.3mm, and the thickness of the honeycomb core is 3mm-30mm.

本发明所述蜂窝夹芯结构件的制备方法,先在蜂窝芯中填充泡沫,形成泡沫蜂窝芯,加强了蜂窝芯的韧性、抗冲击性等机械性能;然后将第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层与第二无纺布层置于第一模具中进行热压贴合,形成中间芯,然后将中间芯置于两个纤维增强热塑性面板之间,并通过第二模具进行热压贴合,再进行注塑包边;在纤维增强热塑性面板与泡沫蜂窝芯之间具有无纺布层,由于无纺布本身韧性好,从而增强了整个结构件的机械性能;且纤维增强热塑性面板与泡沫蜂窝芯之间通过无纺布层进行粘结,增大了两者的粘结面积,注塑包边加固了结构件的稳固性,第二模具热压时采用急热急冷的手段,在热压稳固后迅速冷却,使得胶合稳固性更高,由此使得该结构件不易发生脱胶分层,提高了其使用寿命。The preparation method of the honeycomb sandwich structural part of the present invention first fills the honeycomb core with foam to form a foam honeycomb core, which strengthens the mechanical properties such as toughness and impact resistance of the honeycomb core; then the first non-woven fabric layer, the second A hot-melt adhesive film layer, a foam honeycomb core, a second hot-melt adhesive film layer and a second non-woven fabric layer are placed in the first mold for hot-press bonding to form an intermediate core, and then the intermediate core is placed on two fibers Reinforced thermoplastic panels are hot-pressed and laminated through the second mold, and then injection-molded; there is a non-woven fabric layer between the fiber-reinforced thermoplastic panels and the foam honeycomb core. The mechanical properties of the entire structural part are improved; and the fiber-reinforced thermoplastic panel and the foam honeycomb core are bonded through a non-woven layer, which increases the bonding area of the two, and the injection molding reinforcement strengthens the stability of the structural part. The means of rapid heating and rapid cooling is adopted in the hot pressing of the second mold, and the rapid cooling after the hot pressing is stable makes the bonding stability higher, thus making the structural part less prone to degumming and delamination, and improving its service life.

附图说明Description of drawings

图1是本发明一较佳实施例所述的蜂窝夹芯结构件的局部剖视图。Fig. 1 is a partial sectional view of a honeycomb sandwich structure according to a preferred embodiment of the present invention.

具体实施方式Detailed ways

为了便于理解本发明,下面将结合附图对本发明进行更全面的描述。本发明可以以许多不同的形式来实现,并不限于本文所描述的实施例。相反地,提供这些实施例的目的是使对本发明的公开内容的理解更加透彻全面。In order to facilitate the understanding of the present invention, the present invention will be described more fully below with reference to the accompanying drawings. The present invention can be implemented in many different forms and is not limited to the embodiments described herein. On the contrary, these embodiments are provided to make the understanding of the disclosure of the present invention more thorough and comprehensive.

需要说明的是,当元件被称为“固定于”另一个元件,它可以直接在另一个元件上或者也可以存在居中的元件。当一个元件被认为是“连接”另一个元件,它可以是直接连接到另一个元件或者可能同时存在居中元件。It should be noted that when an element is referred to as being “fixed” to another element, it can be directly on the other element or there can also be an intervening element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or intervening elements may also be present.

除非另有定义,本文所使用的所有的技术和科学术语与属于本发明的技术领域的技术人员通常理解的含义相同。本文中在本发明的说明书中所使用的术语只是为了描述具体的实施例的目的,不是旨在于限制本发明。Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the technical field of the invention. The terms used herein in the description of the present invention are for the purpose of describing specific embodiments only, and are not intended to limit the present invention.

本发明所述的蜂窝夹芯结构件的制备方法,其包括如下步骤:The preparation method of honeycomb sandwich structure of the present invention, it comprises the steps:

S1、选取蜂窝芯,蜂窝芯具有多个孔,在蜂窝芯的孔内填充泡沫,形成泡沫蜂窝芯。在本实施例中,蜂窝芯的厚度为3mm-30mm,厚度根据整体结构件需要的厚度而定。蜂窝芯的材料为PE蜂窝芯、PP蜂窝芯、PVC蜂窝芯、PC蜂窝芯、PET蜂窝芯、纸蜂窝芯、Nomex蜂窝芯以及铝蜂窝芯其中的一种。泡沫为PVC泡沫、PS泡沫、PU泡沫、PUR泡沫、PEI泡沫、PI泡沫、PMI泡沫、PPSU泡沫以及SAN泡沫其中的一种或几种的组合,泡沫的密度为40-200kg/m3。泡沫选用几种材料时,一个孔内可以填充不同种类的泡沫,或者同一孔内填充一种泡沫,其他孔内填充不同种类的其他泡沫。S1. A honeycomb core is selected. The honeycomb core has a plurality of holes, and the pores of the honeycomb core are filled with foam to form a foam honeycomb core. In this embodiment, the thickness of the honeycomb core is 3mm-30mm, and the thickness is determined according to the required thickness of the overall structural member. The material of the honeycomb core is one of PE honeycomb core, PP honeycomb core, PVC honeycomb core, PC honeycomb core, PET honeycomb core, paper honeycomb core, Nomex honeycomb core and aluminum honeycomb core. The foam is one or a combination of PVC foam, PS foam, PU foam, PUR foam, PEI foam, PI foam, PMI foam, PPSU foam and SAN foam, and the density of the foam is 40-200kg/m 3 . When several materials are selected for the foam, different types of foam can be filled in one hole, or one kind of foam can be filled in the same hole, and other foams of different types can be filled in other holes.

S2、选取第一无纺布层、第二无纺布层与第一热熔胶膜层、第二热熔胶膜层并提供第一模具,将第一无纺布层、第二无纺布层与第一热熔胶膜层、第二热熔胶膜层与泡沫蜂窝芯裁切成相同尺寸,以保证制作的结构件周部整齐,然后加热第一模具到大于热熔胶膜的熔点温度1℃-100℃,总体在80℃-180℃,如PES的熔点为135℃,热压时加热到145℃。依次将第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层以及第二无纺布层置于第一模具中,整理至各个层对齐,合模,热压温度为80℃-180℃,调整第一模具的压力为0.1MPa-1MPa,保温保压3s-120s,使得第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层以及第二无纺布层热压结合,脱模后得到中间芯。其中不同的热熔胶膜具有不同的熔点温度,根据热熔胶膜的熔点温度设定模具的温度,其中第一热熔胶膜层与第二热熔胶膜层需采用相同的热熔胶膜,以便更方便地设置第一模具的温度,防止第一热熔胶膜层与第二热熔胶膜层的熔点温度不同,而影响热压贴合的进程。第一热熔胶膜层与第二热熔胶膜层均选自PO热熔胶膜、TPU热熔胶膜、PA热熔胶膜、EVA热熔胶膜以及PES热熔胶膜其中的一种,且第一热熔胶膜层与第二热熔胶膜层的厚度为0.05mm-0.3mm。第一无纺布层与第二无纺布层均选自丙纶、涤纶、锦纶、腈纶、乙纶、氯纶中的一种,平方克重为10g/m2-100g/m2。第一无纺布层与第二无纺布层可选用相同或不同种类。S2, select the first non-woven fabric layer, the second non-woven fabric layer, the first hot-melt adhesive film layer, the second hot-melt adhesive film layer and provide the first mould, the first non-woven fabric layer, the second non-woven fabric layer The cloth layer is cut to the same size as the first hot-melt adhesive film layer, the second hot-melt adhesive film layer and the foam honeycomb core to ensure that the circumference of the manufactured structural parts is neat, and then the first mold is heated to a thickness larger than the hot-melt adhesive film. The melting point temperature is 1°C-100°C, generally 80°C-180°C. For example, the melting point of PES is 135°C, and it is heated to 145°C during hot pressing. Place the first non-woven fabric layer, the first hot-melt adhesive film layer, the foam honeycomb core, the second hot-melt adhesive film layer and the second non-woven fabric layer in the first mold in sequence, arrange until the layers are aligned, and close the mold , the hot pressing temperature is 80°C-180°C, the pressure of the first mold is adjusted to 0.1MPa-1MPa, and the heat preservation and pressure are kept for 3s-120s, so that the first non-woven fabric layer, the first hot-melt adhesive film layer, the foam honeycomb core, The second hot-melt adhesive film layer and the second non-woven fabric layer are bonded by heat and pressure, and the intermediate core is obtained after demoulding. Wherein different hot-melt adhesive films have different melting point temperatures, the temperature of the mold is set according to the melting point temperature of the hot-melt adhesive film, wherein the first hot-melt adhesive film layer and the second hot-melt adhesive film layer need to use the same hot-melt adhesive film, in order to set the temperature of the first mold more conveniently, and prevent the melting point temperature of the first hot melt adhesive film layer and the second hot melt adhesive film layer from being different, which will affect the process of hot-press bonding. Both the first hot-melt adhesive film layer and the second hot-melt adhesive film layer are selected from PO hot-melt adhesive film, TPU hot-melt adhesive film, PA hot-melt adhesive film, EVA hot-melt adhesive film and PES hot-melt adhesive film. species, and the thickness of the first hot-melt adhesive film layer and the second hot-melt adhesive film layer is 0.05mm-0.3mm. Both the first non-woven fabric layer and the second non-woven fabric layer are selected from polypropylene fiber, polyester fiber, nylon fiber, acrylic fiber, polyethylene fiber and polyvinyl chloride, and the square grammage is 10g/m 2 -100g/m 2 . The first non-woven fabric layer and the second non-woven fabric layer can be selected from the same or different types.

S3、选取纤维增强热塑性面板并提供第二模具,加热第二模具到纤维增强热塑性面板的成型温度,温度为150℃-400℃,如纤维增强TPU面板的成型温度为180℃。将中间芯置于相同的两片纤维增强热塑性面板之间,并置于第二模具中,合模,调整第二模具的压力为0.2MPa-5MPa,保温保压15s-150s,使得纤维增强热塑性面板与中间芯热压结合在一起,在30s-90s内迅速冷却后脱模,得到蜂窝夹芯中间板。纤维增强热塑性面板由树脂基体与增强相组成,不同种类纤维增强热塑性面板成型温度不同,例如选用树脂基体,玻璃纤维增强与碳纤维增强形成的面板成型温度不同。在本实施例中,纤维增强热塑性面板的厚度为0.2mm-3mm,纤维的体积含量为35%-65%,即增强相在树脂基体与增强相中体积占比35%-65%。树脂基体选用HDPE、LDPE、PP、PE、PC、PC/ABS合金、PA、TPU、PA6、PA66、PA11、PA12、PPS、PEK、PEEK、PI、PEI、PMMA、PLA、POM、PET和PBT中的一种,增强相选用连续玻璃纤维、碳纤维、芳纶纤维、玄武岩纤维、PBO纤维、UHMWPE纤维、PET纤维、氧化铝纤维、碳化硅纤维编织布、单向布、编织布与单向布的混合布中的一种或多种,当选用多种增强相时,为多种纤维增强的纤维增强热塑性面板。S3. Select a fiber-reinforced thermoplastic panel and provide a second mold, heat the second mold to the molding temperature of the fiber-reinforced thermoplastic panel, the temperature is 150°C-400°C, for example, the molding temperature of the fiber-reinforced TPU panel is 180°C. Place the middle core between the same two fiber-reinforced thermoplastic panels, and place it in the second mold, close the mold, adjust the pressure of the second mold to 0.2MPa-5MPa, keep the heat and pressure for 15s-150s, so that the fiber-reinforced thermoplastic The panel and the middle core are hot-pressed together, cooled rapidly within 30s-90s and demolded to obtain the honeycomb sandwich middle board. Fiber-reinforced thermoplastic panels are composed of a resin matrix and a reinforcement phase. Different types of fiber-reinforced thermoplastic panels have different molding temperatures. For example, if the resin matrix is selected, the molding temperatures of glass fiber-reinforced and carbon-fiber-reinforced panels are different. In this embodiment, the thickness of the fiber-reinforced thermoplastic panel is 0.2mm-3mm, and the volume content of fibers is 35%-65%, that is, the volume ratio of the reinforcing phase in the resin matrix and the reinforcing phase is 35%-65%. The resin matrix is selected from HDPE, LDPE, PP, PE, PC, PC/ABS alloy, PA, TPU, PA6, PA66, PA11, PA12, PPS, PEK, PEEK, PI, PEI, PMMA, PLA, POM, PET and PBT The reinforcing phase is made of continuous glass fiber, carbon fiber, aramid fiber, basalt fiber, PBO fiber, UHMWPE fiber, PET fiber, alumina fiber, silicon carbide fiber woven cloth, unidirectional cloth, woven cloth and unidirectional cloth One or more of the mixed cloth, when multiple reinforcement phases are selected, is a fiber-reinforced thermoplastic panel reinforced with multiple fibers.

S31、去除蜂窝夹芯中间板周部的飞边,以便使其表面光滑,更方便注塑。S31. Remove flashings around the middle plate of the honeycomb sandwich to make the surface smooth and more convenient for injection molding.

S4、将蜂窝夹芯中间板嵌入注塑模具内,对蜂窝夹芯中间板进行注塑,在蜂窝夹芯中间板的周部形成包边,得到蜂窝夹芯结构件。其中注塑用塑料为玻璃纤维或碳纤维增强塑料,纤维的重量含量为5%-65%,玻璃纤维或碳纤维增强塑料中的塑料基体为HDPE、LDPE、PP、PE、PC、PC/ABS合金、PA、TPU、PA6、PA66、PA11、PA12、PPS、PEK、PEEK、PI、PEI、PMMA、PLA、POM、PET和PBT中的一种。S4. Embedding the honeycomb sandwich middle plate into an injection mold, injecting the honeycomb sandwich middle plate, forming hemming around the periphery of the honeycomb sandwich middle plate, and obtaining a honeycomb sandwich structure. Among them, the plastic used for injection molding is glass fiber or carbon fiber reinforced plastic, and the weight content of fiber is 5%-65%. The plastic matrix in glass fiber or carbon fiber reinforced plastic is HDPE, LDPE, PP, PE, PC, PC/ABS alloy, PA , TPU, PA6, PA66, PA11, PA12, PPS, PEK, PEEK, PI, PEI, PMMA, PLA, POM, PET and PBT.

请参照图1,由上述蜂窝夹芯结构件的制备方法制备的蜂窝夹芯结构件100,包括蜂窝夹芯中间板10以及包覆于蜂窝夹芯中间板周部的包边20,蜂窝夹芯中间板10包括依次贴合连接的第一纤维增强热塑性面板11、第一无纺布层12、第一热熔胶膜层13、泡沫蜂窝芯14、第二热熔胶膜层15、第二无纺布层16以及第二纤维增强热塑性面板17,泡沫蜂窝芯14由蜂窝芯141以及填充于蜂窝芯的孔内的泡沫组成。其中第一纤维增强热塑性面板11与第二纤维增强热塑性面板17的厚度均为0.2mm-3mm,第一热熔胶膜层13与第二热熔胶膜层15的厚度均为0.05mm-0.3mm,蜂窝芯的厚度为3mm-30mm。Please refer to Fig. 1, the honeycomb sandwich structure 100 prepared by the preparation method of the above-mentioned honeycomb sandwich structure includes a honeycomb sandwich middle plate 10 and an edge 20 wrapped around the periphery of the honeycomb sandwich middle plate, the honeycomb sandwich The middle panel 10 includes a first fiber-reinforced thermoplastic panel 11, a first non-woven fabric layer 12, a first hot-melt adhesive film layer 13, a foam honeycomb core 14, a second hot-melt adhesive film layer 15, a second The non-woven fabric layer 16 and the second fiber-reinforced thermoplastic panel 17, the foam honeycomb core 14 is composed of a honeycomb core 141 and foam filled in the cells of the honeycomb core. The thicknesses of the first fiber reinforced thermoplastic panel 11 and the second fiber reinforced thermoplastic panel 17 are both 0.2mm-3mm, and the thicknesses of the first hot melt adhesive film layer 13 and the second hot melt adhesive film layer 15 are both 0.05mm-0.3 mm. mm, the thickness of the honeycomb core is 3mm-30mm.

本发明先在蜂窝芯中填充泡沫,形成泡沫蜂窝芯,加强了蜂窝芯的韧性、抗冲击性等机械性能;然后将第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层与第二无纺布层置于第一模具中进行热压贴合,形成中间芯,然后将中间芯置于两个纤维增强热塑性面板之间,并通过第二模具进行热压贴合,再进行注塑包边;在纤维增强热塑性面板与泡沫蜂窝芯之间具有无纺布层,由于无纺布本身韧性好,从而增强了整个结构件的机械性能;且纤维增强热塑性面板与泡沫蜂窝芯之间通过无纺布层进行粘结,增大了两者的粘结面积,注塑包边加固了结构件的稳固性,第二模具热压时采用急热急冷的手段,在热压稳固后迅速冷却,使得胶合稳固性更高,由此使得该结构件不易发生脱胶分层,提高了其使用寿命。In the present invention, foam is first filled in the honeycomb core to form a foam honeycomb core, which strengthens the mechanical properties of the honeycomb core such as toughness and impact resistance; then the first non-woven fabric layer, the first hot-melt adhesive film layer, the foam honeycomb core, The second hot-melt adhesive film layer and the second non-woven fabric layer are placed in the first mold for thermal compression bonding to form the middle core, and then the middle core is placed between two fiber-reinforced thermoplastic panels and passed through the second mold Carry out hot pressing lamination, and then carry out injection molding wrapping; there is a non-woven fabric layer between the fiber-reinforced thermoplastic panel and the foam honeycomb core. Due to the good toughness of the non-woven fabric itself, the mechanical properties of the entire structural part are enhanced; and the fiber-reinforced The thermoplastic panel and the foam honeycomb core are bonded through a non-woven fabric layer, which increases the bonding area of the two, and the injection molding edging strengthens the stability of the structural part. The second mold is hot-pressed by means of rapid heating and rapid cooling , cooling rapidly after the hot pressing is stable, which makes the bonding more stable, thus making the structural part less likely to be degummed and delaminated, and improving its service life.

实施例Example

在本实施例中,所述的蜂窝夹芯结构件的制备方法,其包括如下步骤:In this embodiment, the preparation method of the honeycomb sandwich structure comprises the following steps:

S1、选取蜂窝芯,蜂窝芯具有多个孔,在蜂窝芯的孔内填充泡沫,形成泡沫蜂窝芯。在本实施例中,蜂窝芯的厚度为6mm。蜂窝芯的材料为PC蜂窝芯,填充PVC泡沫,得到泡沫蜂窝芯。S1. A honeycomb core is selected. The honeycomb core has a plurality of holes, and the pores of the honeycomb core are filled with foam to form a foam honeycomb core. In this embodiment, the thickness of the honeycomb core is 6 mm. The material of the honeycomb core is a PC honeycomb core, which is filled with PVC foam to obtain a foam honeycomb core.

S2、选取第一无纺布层、第二无纺布层与第一热熔胶膜层、第二热熔胶膜层,并提供第一模具,将第一无纺布层、第二无纺布层与第一热熔胶膜层、第二热熔胶膜层与泡沫蜂窝芯裁切成相同尺寸,以保证制作的结构件周部整齐,第一热熔胶膜层与第二热熔胶膜层均为0.05mm的TPU热熔胶膜层,第一无纺布层与第二无纺布层均为PET无纺布层,规格为30g/m2;然后加热第一模具到大于第一热熔胶膜层与第二热熔胶膜层的熔点温度120℃,依次将第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层以及第二无纺布层置于第一模具中,整理至各个层对齐,合模热压,调整第一模具的压力为0.5MPa,保温保压60s,使得第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层以及第二无纺布层热压结合,脱模后得到中间芯。S2, select the first non-woven fabric layer, the second non-woven fabric layer, the first hot-melt adhesive film layer, and the second hot-melt adhesive film layer, and provide the first mold, the first non-woven fabric layer, the second non-woven fabric layer The woven fabric layer and the first hot-melt adhesive film layer, the second hot-melt adhesive film layer and the foam honeycomb core are cut to the same size to ensure that the circumference of the manufactured structural parts is neat, and the first hot-melt adhesive film layer and the second hot-melt adhesive film layer are Melt adhesive film layer is the TPU hot-melt adhesive film layer of 0.05mm, and the first non-woven fabric layer and the second non-woven fabric layer are PET non-woven fabric layers, and the specification is 30g/m 2 ; Then heat the first mold to Greater than the melting point temperature of the first hot-melt adhesive film layer and the second hot-melt adhesive film layer is 120°C, and the first non-woven fabric layer, the first hot-melt adhesive film layer, the foam honeycomb core, and the second hot-melt adhesive film layer are sequentially And the second non-woven fabric layer is placed in the first mold, arranged until each layer is aligned, the mold is closed and hot-pressed, the pressure of the first mold is adjusted to 0.5MPa, and the heat preservation and pressure are maintained for 60s, so that the first non-woven fabric layer, the first The hot-melt adhesive film layer, the foam honeycomb core, the second hot-melt adhesive film layer and the second non-woven fabric layer are combined by heat and pressure, and the intermediate core is obtained after demoulding.

S3、选取纤维增强热塑性面板并提供第二模具,纤维增强热塑性面板为TPU和玻璃纤维复合的热塑性面板,即采用玻璃纤维增强TPU面板,纤维的体积含量为45%,厚度为0.5mm,加热第二模具到170℃,将中间芯置于相同的两片纤维增强热塑性面板之间,并置于第二模具中,合模,调整第二模具的压力为1.5MPa,保温保压30s,使得纤维增强热塑性面板与中间芯热压结合在一起,在30s内迅速冷却后脱模,得到蜂窝夹芯中间板。纤维增强热塑性面板由树脂基体与增强相组成,不同种类纤维增强热塑性面板成型温度不同,例如选用树脂基体,玻璃纤维增强与碳纤维增强形成的面板成型温度不同。S3. Select a fiber-reinforced thermoplastic panel and provide a second mold. The fiber-reinforced thermoplastic panel is a composite thermoplastic panel of TPU and glass fiber, that is, a glass fiber-reinforced TPU panel with a fiber volume content of 45% and a thickness of 0.5mm. The second mold is at 170°C, place the middle core between the same two fiber-reinforced thermoplastic panels, and place it in the second mold, close the mold, adjust the pressure of the second mold to 1.5MPa, keep the heat and pressure for 30s, so that the fiber The reinforced thermoplastic panel and the middle core are hot-pressed together, cooled rapidly within 30s and demolded to obtain the honeycomb sandwich middle board. Fiber-reinforced thermoplastic panels are composed of a resin matrix and a reinforcement phase. Different types of fiber-reinforced thermoplastic panels have different molding temperatures. For example, if the resin matrix is selected, the molding temperatures of glass fiber-reinforced and carbon-fiber-reinforced panels are different.

S31、去除蜂窝夹芯中间板周部的飞边,以便使其表面光滑,更方便注塑。S31. Remove flashings around the middle plate of the honeycomb sandwich to make the surface smooth and more convenient for injection molding.

S4、将蜂窝夹芯中间板嵌入注塑模具内,采用重量含量为20%的玻纤TPU对蜂窝夹芯中间板进行注塑,注塑压力为500N,注塑温度为190℃,注塑模具的温度为80℃,注塑时间为4s。在蜂窝夹芯中间板的周部形成包边,得到蜂窝夹芯结构件。S4. Embed the honeycomb sandwich panel into the injection mold, inject the honeycomb sandwich panel with glass fiber TPU with a weight content of 20%, the injection pressure is 500N, the injection temperature is 190°C, and the temperature of the injection mold is 80°C , The injection time is 4s. A wrapping is formed on the periphery of the honeycomb sandwich middle plate to obtain a honeycomb sandwich structure.

以上所述实施例仅表达了本发明的几种实施方式,其描述较为具体和详细,但并不能因此而理解为对本发明专利范围的限制。应当指出的是,对于本领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干变形和改进,这些都属于本发明的保护范围。因此,本发明专利的保护范围应以所附权利要求为准。The above-mentioned embodiments only express several implementation modes of the present invention, and the description thereof is relatively specific and detailed, but should not be construed as limiting the patent scope of the present invention. It should be pointed out that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention, and these all belong to the protection scope of the present invention. Therefore, the protection scope of the patent for the present invention should be based on the appended claims.

Claims (8)

1.一种蜂窝夹芯结构件的制备方法,其特征在于,包括如下步骤:1. a preparation method of honeycomb sandwich structure, is characterized in that, comprises the steps: S1、选取蜂窝芯,在所述蜂窝芯的孔内填充泡沫,形成泡沫蜂窝芯;S1, selecting a honeycomb core, filling foam in the pores of the honeycomb core to form a foam honeycomb core; S2、选取第一无纺布层、第二无纺布层、第一热熔胶膜层、第二热熔胶膜层,并提供第一模具,然后加热第一模具到大于第一热熔胶膜层与第二热熔胶膜层的熔点温度1℃-100℃,依次将第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层以及第二无纺布层置于第一模具中,合模,调整第一模具的压力为0.1MPa-1MPa,保温保压3s-120s,使得第一无纺布层、第一热熔胶膜层、泡沫蜂窝芯、第二热熔胶膜层以及第二无纺布层热压结合,脱模后得到中间芯;S2. Select the first non-woven fabric layer, the second non-woven fabric layer, the first hot-melt adhesive film layer, and the second hot-melt adhesive film layer, and provide the first mold, and then heat the first mold to a temperature larger than the first hot-melt adhesive film layer. The melting point temperature of the adhesive film layer and the second hot-melt adhesive film layer is 1°C-100°C, and the first non-woven fabric layer, the first hot-melt adhesive film layer, the foam honeycomb core, the second hot-melt adhesive film layer and the second The second non-woven fabric layer is placed in the first mold, the mold is closed, the pressure of the first mold is adjusted to 0.1MPa-1MPa, and the heat preservation and pressure are maintained for 3s-120s, so that the first non-woven fabric layer, the first hot-melt adhesive film layer, The foam honeycomb core, the second hot-melt adhesive film layer and the second non-woven fabric layer are combined by heat and pressure, and the intermediate core is obtained after demoulding; S3、选取纤维增强热塑性面板并提供第二模具,加热第二模具到纤维增强热塑性面板的成型温度,将所述中间芯置于两片纤维增强热塑性面板之间,并置于所述第二模具中,合模,调整第二模具的压力为0.2MPa-5MPa,保温保压15s-150s,使得纤维增强热塑性面板与中间芯热压结合在一起,在30s-90s内迅速冷却后脱模,得到蜂窝夹芯中间板;S3. Select a fiber-reinforced thermoplastic panel and provide a second mold, heat the second mold to the molding temperature of the fiber-reinforced thermoplastic panel, place the intermediate core between two fiber-reinforced thermoplastic panels, and place it in the second mold In the process of closing the mold, adjust the pressure of the second mold to 0.2MPa-5MPa, and keep the heat and pressure for 15s-150s, so that the fiber-reinforced thermoplastic panel and the middle core are hot-compressed together, and they are demoulded after rapid cooling within 30s-90s to obtain Honeycomb sandwich panel; S4、将蜂窝夹芯中间板嵌入注塑模具内,对蜂窝夹芯中间板进行注塑,在所述蜂窝夹芯中间板的周部形成包边,得到蜂窝夹芯结构件。S4. Embedding the honeycomb sandwich middle plate into the injection mold, injecting the honeycomb sandwich middle plate, forming hemming on the periphery of the honeycomb sandwich middle plate, and obtaining the honeycomb sandwich structure. 2.根据权利要求1所述的蜂窝夹芯结构件的制备方法,其特征在于:所述步骤S3与步骤S4之间,还具有步骤S31:去除所述蜂窝夹芯中间板周部的飞边。2. The preparation method of the honeycomb sandwich structure according to claim 1, characterized in that: between the step S3 and the step S4, there is also a step S31: removing the flash on the periphery of the honeycomb sandwich middle plate . 3.根据权利要求1所述的蜂窝夹芯结构件的制备方法,其特征在于:所述步骤S1中蜂窝芯为PE蜂窝芯、PP蜂窝芯、PVC蜂窝芯、PC蜂窝芯、PET蜂窝芯、纸蜂窝芯、Nomex蜂窝芯以及铝蜂窝芯其中的一种,厚度为3mm-30mm。3. The preparation method of the honeycomb sandwich structure according to claim 1, characterized in that: the honeycomb core in the step S1 is a PE honeycomb core, a PP honeycomb core, a PVC honeycomb core, a PC honeycomb core, a PET honeycomb core, One of paper honeycomb core, Nomex honeycomb core and aluminum honeycomb core, the thickness is 3mm-30mm. 4.根据权利要求1所述的蜂窝夹芯结构件的制备方法,其特征在于:所述步骤S1中泡沫为PVC泡沫、PS泡沫、PU泡沫、PUR泡沫、PEI泡沫、PI泡沫、PMI泡沫、PPSU泡沫以及SAN泡沫其中的一种或几种的组合,所述泡沫的密度为40-200kg/m34. The preparation method of the honeycomb sandwich structure according to claim 1, characterized in that: in the step S1, the foam is PVC foam, PS foam, PU foam, PUR foam, PEI foam, PI foam, PMI foam, A combination of one or more of PPSU foam and SAN foam, the density of the foam is 40-200kg/m 3 . 5.根据权利要求1所述的蜂窝夹芯结构件的制备方法,其特征在于:所述步骤S2中第一无纺布层与第二无纺布层均选自丙纶、涤纶、锦纶、腈纶、乙纶、氯纶中的一种,平方克重为10g/m2-100g/m25. The preparation method of the honeycomb sandwich structure according to claim 1, characterized in that: in the step S2, the first non-woven layer and the second non-woven layer are all selected from polypropylene, polyester, nylon, acrylic , polyethylene, polyvinyl chloride, the square grammage is 10g/m 2 -100g/m 2 . 6.根据权利要求1所述的蜂窝夹芯结构件的制备方法,其特征在于:所述步骤S2中第一热熔胶膜层与第二热熔胶膜层选用同种热熔胶膜层,且均选自PO热熔胶膜、TPU热熔胶膜、PA热熔胶膜、EVA热熔胶膜以及PES热熔胶膜其中的一种,厚度为0.05mm-0.3mm。6. The method for preparing a honeycomb sandwich structure according to claim 1, characterized in that: the first hot-melt adhesive film layer and the second hot-melt adhesive film layer in the step S2 are selected from the same hot-melt adhesive film layer , and are all selected from one of PO hot melt adhesive film, TPU hot melt adhesive film, PA hot melt adhesive film, EVA hot melt adhesive film and PES hot melt adhesive film, with a thickness of 0.05mm-0.3mm. 7.根据权利要求1所述的蜂窝夹芯结构件的制备方法,其特征在于:所述步骤S3中纤维增强热塑性面板的厚度为0.2mm-3mm,纤维的体积含量为35%-65%,所述纤维增强热塑性面板由树脂基体与增强相组成,所述树脂基体为HDPE、LDPE、PP、PC、PC/ABS合金、TPU、PA6、PA66、PA11、PA12、PPS、PEK、PEEK、PI、PEI、PMMA、PLA、POM、PET和PBT中的一种,所述增强相为连续玻璃纤维、碳纤维、芳纶纤维、玄武岩纤维、PBO纤维、UHMWPE纤维、PET纤维、氧化铝纤维、碳化硅纤维编织布、单向布、编织布与单向布的混合布中的一种或多种。7. The method for preparing a honeycomb sandwich structure according to claim 1, characterized in that: in the step S3, the thickness of the fiber-reinforced thermoplastic panel is 0.2mm-3mm, and the volume content of the fiber is 35%-65%, The fiber-reinforced thermoplastic panel is composed of a resin matrix and a reinforcing phase, and the resin matrix is HDPE, LDPE, PP, PC, PC/ABS alloy, TPU, PA6, PA66, PA11, PA12, PPS, PEK, PEEK, PI, One of PEI, PMMA, PLA, POM, PET and PBT, the reinforcing phase is continuous glass fiber, carbon fiber, aramid fiber, basalt fiber, PBO fiber, UHMWPE fiber, PET fiber, alumina fiber, silicon carbide fiber One or more of woven fabrics, unidirectional fabrics, and mixed fabrics of woven fabrics and unidirectional fabrics. 8.根据权利要求1所述的蜂窝夹芯结构件的制备方法,其特征在于:所述步骤S4中注塑用塑料为玻璃纤维或碳纤维增强塑料,纤维的重量含量为5%-65%,所述玻璃纤维或碳纤维增强塑料中的塑料基体为HDPE、LDPE、PP、PC、PC/ABS合金、TPU、PA6、PA66、PA11、PA12、PPS、PEK、PEEK、PI、PEI、PMMA、PLA、POM、PET和PBT中的一种。8. The method for preparing a honeycomb sandwich structure according to claim 1, characterized in that: in the step S4, the plastic used for injection molding is glass fiber or carbon fiber reinforced plastic, and the weight content of the fiber is 5%-65%. The plastic matrix in the glass fiber or carbon fiber reinforced plastic is HDPE, LDPE, PP, PC, PC/ABS alloy, TPU, PA6, PA66, PA11, PA12, PPS, PEK, PEEK, PI, PEI, PMMA, PLA, POM One of , PET and PBT.
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