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CN108045002A - A kind of honeycomb sandwich construction and preparation method thereof - Google Patents

A kind of honeycomb sandwich construction and preparation method thereof Download PDF

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Publication number
CN108045002A
CN108045002A CN201810002556.2A CN201810002556A CN108045002A CN 108045002 A CN108045002 A CN 108045002A CN 201810002556 A CN201810002556 A CN 201810002556A CN 108045002 A CN108045002 A CN 108045002A
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China
Prior art keywords
core material
honeycomb core
honeycomb
coated
preparation
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CN201810002556.2A
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Chinese (zh)
Inventor
熊美蓉
丛晶洁
陈凯
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Commercial Aircraft Corp of China Ltd
Beijing Aeronautic Science and Technology Research Institute of COMAC
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Commercial Aircraft Corp of China Ltd
Beijing Aeronautic Science and Technology Research Institute of COMAC
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Priority to CN201810002556.2A priority Critical patent/CN108045002A/en
Publication of CN108045002A publication Critical patent/CN108045002A/en
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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
    • 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
    • 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
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/146Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers whereby one or more of the layers is 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
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/18Handling of layers or the laminate
    • 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
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/18Handling of layers or the laminate
    • B32B38/1858Handling of layers or the laminate using vacuum
    • 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
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of 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
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04Impregnation, embedding, or binder material
    • B32B2260/046Synthetic resin
    • 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
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02Synthetic macromolecular fibres
    • B32B2262/0261Polyamide fibres
    • 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
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/101Glass fibres
    • 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
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/106Carbon fibres, e.g. graphite fibres

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  • Laminated Bodies (AREA)

Abstract

The invention discloses a kind of honeycomb sandwich construction and preparation method thereof, which includes:One layer of sticky object is coated with respectively in honeycomb core material upper and lower surface;One layer of prepreg is coated with respectively in the honeycomb core material upper and lower surface for being coated with sticky object;Vacuum Package is carried out to the honeycomb core material for being coated with prepreg, and is cured at one atm, obtains pretreated honeycomb core material;Vacuum Package is carried out to pretreated honeycomb core material, and carries out curing molding, obtains honeycomb sandwich construction.The present invention is of low cost, and can avoid collapsing for cellular material.

Description

一种蜂窝夹层结构及其制备方法A kind of honeycomb sandwich structure and preparation method thereof

技术领域technical field

本发明属于材料成型技术领域,尤其涉及一种蜂窝夹层结构的制备方法和利用该制备方法制备的蜂窝夹层结构。The invention belongs to the technical field of material forming, and in particular relates to a preparation method of a honeycomb sandwich structure and a honeycomb sandwich structure prepared by the preparation method.

背景技术Background technique

蜂窝夹层结构是一种蒙皮与蜂窝芯材组成的层状结构,具有轻质、强度刚度好、抗冲击、耐疲劳等优点,同时也是飞机结构中结构效率最高的结构形式之一。常见的蜂窝芯材包含铝蜂窝、Nomex蜂窝等。蜂窝夹层结构在飞机机翼前缘、方向舵、襟翼、副翼等部分应用广泛。The honeycomb sandwich structure is a layered structure composed of a skin and a honeycomb core material. It has the advantages of light weight, good strength and rigidity, impact resistance, and fatigue resistance. It is also one of the structural forms with the highest structural efficiency in aircraft structures. Common honeycomb core materials include aluminum honeycomb, Nomex honeycomb, etc. Honeycomb sandwich structure is widely used in aircraft wing leading edge, rudder, flap, aileron and other parts.

目前在航空领域,蜂窝夹层结构的制备方法主要是在模具上将预浸料铺叠在已预先加工好的蜂窝结构上下,并由胶膜实现粘接,封装好真空袋后于热压罐中固化成型。At present, in the field of aviation, the preparation method of the honeycomb sandwich structure is mainly to lay the prepreg on the pre-processed honeycomb structure on the mold, and use the adhesive film to realize the bonding, and then seal the vacuum bag and place it in the autoclave. Curing and forming.

复合材料液体成型技术中真空灌注成型工艺常用于制备层合板和泡沫夹层结构,其优异在于仅在一个大气压下成型且质量优越。但蜂窝为多开孔材料,采用常规工艺方法,在树脂注入时会流入蜂窝孔格中,且蜂窝孔中的大量气体难以在抽真空条件下完成排除,气体易进入蒙皮面板中形成孔隙。The vacuum infusion molding process in the liquid molding technology of composite materials is often used to prepare laminated boards and foam sandwich structures. However, the honeycomb is a multi-porous material, and the conventional process method will flow into the honeycomb cells when the resin is injected, and it is difficult to remove a large amount of gas in the honeycomb cells under vacuum conditions, and the gas easily enters the skin panel to form pores.

发明内容Contents of the invention

(一)发明目的(1) Purpose of the invention

本发明的目的是提供一种能够避免制成的蜂窝材料塌陷的蜂窝夹层结构的制备方法及其采用该制备方法制备的蜂窝夹层结构。The object of the present invention is to provide a method for preparing a honeycomb sandwich structure capable of avoiding the collapse of the manufactured honeycomb material and the honeycomb sandwich structure prepared by the preparation method.

(二)技术方案(2) Technical solutions

为解决上述问题,本发明的第一方面提供了一种蜂窝夹层结构的制备方法,包括:在蜂窝芯材上表面、下表面和四周分别铺覆一层粘接物;在铺覆了粘接物的蜂窝芯材上表面、下表面和四周分别铺覆一层预浸料;对铺覆了预浸料的蜂窝芯材进行真空封装,并在一个大气压下进行固化,得到预处理后的蜂窝芯材;对预处理后的蜂窝芯材进行真空封装,并进行固化成型,得到蜂窝夹层结构。In order to solve the above problems, the first aspect of the present invention provides a method for preparing a honeycomb sandwich structure, comprising: covering the upper surface, lower surface and surroundings of the honeycomb core material with a layer of adhesive; The upper surface, the lower surface and the surrounding of the honeycomb core material of the object are respectively covered with a layer of prepreg material; the honeycomb core material coated with prepreg material is vacuum packaged and cured under an atmospheric pressure to obtain the pretreated honeycomb Core material: vacuum-encapsulate the pretreated honeycomb core material, and perform curing molding to obtain a honeycomb sandwich structure.

进一步地,在铺覆预浸料之后以及进行真空封装之前,制备方法还包括:在铺覆了预浸料的蜂窝芯材上表面和下表面分别铺覆一表面粗糙的粗糙层;对铺覆了粗糙层的蜂窝芯材进行真空封装,并进行固化,得到预处理后的蜂窝芯材。Further, after laying the prepreg and before vacuum encapsulation, the preparation method further includes: laying a rough layer on the upper and lower surfaces of the honeycomb core covered with the prepreg; The honeycomb core material with the rough layer is vacuum-packed and cured to obtain the pretreated honeycomb core material.

进一步地,在铺覆了预浸料的蜂窝芯材上表面和下表面分别铺覆一表面粗糙的粗糙层的步骤包括:在铺覆了预浸料的蜂窝芯材上表面和下表面分别铺覆一脱模层;在铺覆了脱模层的蜂窝芯材上表面和下表面分别铺覆一透气层。Further, the step of paving a rough layer on the upper surface and the lower surface of the prepreg-coated honeycomb core material respectively includes: paving the upper surface and the lower surface of the prepreg-coated honeycomb core material respectively. A release layer is covered; a breathable layer is respectively laid on the upper surface and the lower surface of the honeycomb core material covered with the release layer.

进一步地,粘接物与蒙皮面板材料为同一种类树脂体系。Further, the adhesive is the same type of resin system as the skin panel material.

进一步地,预浸料与蒙皮面板材料为同一种类树脂体系。Further, the prepreg and the skin panel material are the same kind of resin system.

进一步地,制备方法还包括:当预处理后的蜂窝芯材存在裸露孔格时,在裸露孔格的位置添加预浸料并进行二次固化。Further, the preparation method further includes: when there are bare cells in the pretreated honeycomb core material, adding a prepreg at the position of the exposed cells and performing secondary curing.

进一步地,对预处理后的蜂窝芯材按照真空灌注或真空导入工艺进行封装的步骤包括:在预处理后的蜂窝芯材的上、下表面分别铺放一增强纤维;在铺放了增强纤维的蜂窝芯材的上、下表面分别铺放一脱模物质层;在铺放了脱模物质层的蜂窝芯材的上、下表面分别铺放一抗粘物质层;在铺放了抗粘物质层的蜂窝芯材的上、下表面分别铺放一导流装置;将铺放了导流装置的蜂窝芯材采用两层真空袋进行真空封装,且在内层真空袋上设置注胶口和出胶口。Further, the step of encapsulating the pretreated honeycomb core material according to the vacuum infusion or vacuum introduction process includes: respectively laying a reinforcing fiber on the upper and lower surfaces of the pretreated honeycomb core material; A release material layer is laid on the upper and lower surfaces of the honeycomb core material respectively; an anti-adhesive material layer is respectively laid on the upper and lower surfaces of the honeycomb core material with the release material layer laid; A diversion device is placed on the upper and lower surfaces of the honeycomb core material of the substance layer; the honeycomb core material with the diversion device is vacuum-packed with two layers of vacuum bags, and a glue injection port is set on the inner vacuum bag and glue outlet.

进一步地,在进行真空封装之后,还包括:对两层真空袋进行抽真空,保持预定时间;通过注胶口向导流装置注胶;当出胶口处出现树脂时,停止注胶,对外真空袋继续抽真空;在基于材料体系设定的固化温度和升温、降温速率,对真空封装的蜂窝芯材进行固化;对固化处理后的蜂窝芯材进行冷却,对冷却后的蜂窝芯材进行脱模,得到蜂窝芯材。Further, after the vacuum encapsulation, it also includes: vacuuming the two-layer vacuum bag and keeping it for a predetermined time; injecting glue through the glue injection port to the guide device; when resin appears at the glue outlet, stop the glue injection, and vacuum Continue vacuuming the bag; solidify the vacuum-encapsulated honeycomb core material at the solidification temperature and heating and cooling rate set based on the material system; cool the honeycomb core material after solidification treatment, and detach the cooled honeycomb core material mold to obtain a honeycomb core material.

进一步地,粘接物、预浸料和蒙皮面板为相同固化温度水平的材料。Further, the adhesive, prepreg and skin panel are materials at the same curing temperature level.

根据本发明的另一个方面,提供一种根据一种蜂窝夹层结构的制备方法制备的蜂窝夹层结构。According to another aspect of the present invention, a honeycomb sandwich structure prepared according to a method for preparing a honeycomb sandwich structure is provided.

(三)有益效果(3) Beneficial effects

本发明的上述技术方案具有如下有益的技术效果:The technical solution of the present invention has the following beneficial technical effects:

1.采用液体成型工艺制备蜂窝夹层结构,降低了制造成本,且由于其在一个大气压下成型,因此避免了蜂窝材料的塌陷;1. The honeycomb sandwich structure is prepared by liquid forming technology, which reduces the manufacturing cost, and because it is formed under an atmospheric pressure, the collapse of the honeycomb material is avoided;

2.解决了传统真空导入工艺过程中树脂易流胶充填进蜂窝孔格,蒙皮面板易出现孔隙的问题。通过采用预浸料对蜂窝芯材进行处理,将蜂窝芯材的孔堵住,从而避免在真空导入时树脂进入蜂窝孔格,经过预处理的蜂窝在真空导入时会使得树脂沿着干纤维的方向流动,而不会流入蜂窝孔格中,形成蒙皮面板与芯材的强粘接界面。2. It solves the problem that the resin is easy to flow and the glue is filled into the honeycomb cells in the traditional vacuum introduction process, and the skin panel is easy to have pores. Prepreg is used to process the honeycomb core material to block the pores of the honeycomb core material, so as to prevent the resin from entering the honeycomb cells when the vacuum is introduced. The pretreated honeycomb will make the resin along the dry fiber when the vacuum is introduced. Flow in the same direction without flowing into the honeycomb cells, forming a strong bonding interface between the skin panel and the core material.

3.由于采用商用的预浸料和胶膜材料(粘接物),使得预处理后的蜂窝质量稳定可靠。3. Due to the use of commercial prepreg and adhesive film materials (adhesives), the quality of the pretreated honeycomb is stable and reliable.

4.采用湿可剥布和透气毡,使固化后的蜂窝上下表面能够形成易粘接的粗糙界面,进而使得导入的树脂与处理后的蜂窝上下表面形成良好的粘接界面。4. Wet peelable cloth and air felt are used to make the upper and lower surfaces of the cured honeycomb form a rough interface that is easy to bond, so that the introduced resin forms a good bonding interface with the treated upper and lower surfaces of the honeycomb.

5.预浸料与胶膜的使用实现了蒙皮面板与蜂窝芯材的良好粘接界面。5. The use of prepreg and adhesive film achieves a good bonding interface between the skin panel and the honeycomb core material.

附图说明Description of drawings

图1是本发明实施例一的一种蜂窝夹层结构的制备方法的流程图;Fig. 1 is the flow chart of the preparation method of a kind of honeycomb sandwich structure of the embodiment of the present invention;

图2是本发明实施例二的一种蜂窝夹层结构的制备方法的流程图;Fig. 2 is the flowchart of the preparation method of a kind of honeycomb sandwich structure of the embodiment of the present invention;

图3是本发明实施例三的一种蜂窝夹层结构的制备方法的流程图;Fig. 3 is the flowchart of the preparation method of a kind of honeycomb sandwich structure of embodiment three of the present invention;

图4是本发明实施例四的一种蜂窝夹层结构的制备方法的流程图;Fig. 4 is the flowchart of the preparation method of a kind of honeycomb sandwich structure of embodiment four of the present invention;

图5是本发明实施例五的一种蜂窝夹层结构的制备方法的流程图;Fig. 5 is the flowchart of the preparation method of a kind of honeycomb sandwich structure of embodiment five of the present invention;

图6是本发明实施例六的一种蜂窝夹层结构的制备方法的流程图;6 is a flowchart of a method for preparing a honeycomb sandwich structure according to Embodiment 6 of the present invention;

图7是蜂窝芯材预处理过程的示意图;Fig. 7 is the schematic diagram of honeycomb core material pretreatment process;

图8是经过固化处理后得到的蜂窝芯材的示意图;Fig. 8 is the schematic diagram of the honeycomb core material obtained after curing;

图9是采用液体成型工艺制备蜂窝夹层结构的过程的示意图。Fig. 9 is a schematic diagram of the process of preparing a honeycomb sandwich structure using a liquid forming process.

附图标记:Reference signs:

1.蜂窝芯材,1-0.预处理后的蜂窝芯材,2.胶膜,3.预浸料,4.湿可剥布,5.透气毡,6.模具,7.真空袋,8.增强纤维,9.脱模布,10.四氟布,11.导流网。1. Honeycomb core material, 1-0. Honeycomb core material after pretreatment, 2. Adhesive film, 3. Prepreg, 4. Wet peelable cloth, 5. Air felt, 6. Mold, 7. Vacuum bag, 8. Reinforcing fiber, 9. Release cloth, 10. Tetrafluoro cloth, 11. Drainage net.

具体实施方式Detailed ways

为使本发明的目的、技术方案和优点更加清楚明了,下面结合具体实施方式并参照附图,对本发明进一步详细说明。应该理解,这些描述只是示例性的,而并非要限制本发明的范围。此外,在以下说明中,省略了对公知结构和技术的描述,以避免不必要地混淆本发明的概念。In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in combination with specific embodiments and with reference to the accompanying drawings. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the present invention. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concept of the present invention.

本发明是采用复合材料液体成型工艺来制备蜂窝夹层结构,其中,在制备蜂窝夹层结构之前,需要预先准备蜂窝芯材,由于本发明所选取的蜂窝芯材的蒙皮面板材料主要由树脂和增强纤维组成,其中树脂包含环氧树脂、双马树脂、苯并噁嗪树脂等,增强纤维包含碳纤维、玻璃纤维、芳纶纤维等。因此蜂窝芯材可以选取铝蜂窝、Nomax蜂窝、Kevlar蜂窝等,例如:Hexcel公司的HRH-10、CR-PAA Core等蜂窝芯材。The present invention adopts the composite material liquid molding process to prepare the honeycomb sandwich structure, wherein, before preparing the honeycomb sandwich structure, it is necessary to prepare the honeycomb core material in advance, because the skin panel material of the honeycomb core material selected in the present invention is mainly composed of resin and reinforced Composed of fibers, the resins include epoxy resin, double horse resin, benzoxazine resin, etc., and the reinforcing fibers include carbon fiber, glass fiber, aramid fiber, etc. Therefore, the honeycomb core material can choose aluminum honeycomb, Nomax honeycomb, Kevlar honeycomb, etc., for example: HRH-10, CR-PAA Core and other honeycomb core materials of Hexcel Company.

图1是本发明实施例一的一种蜂窝夹层结构的制备方法的流程图。Fig. 1 is a flowchart of a method for preparing a honeycomb sandwich structure according to Embodiment 1 of the present invention.

如图1所示,该制备方法包括如下步骤S101-S104:As shown in Figure 1, the preparation method includes the following steps S101-S104:

S101,在蜂窝芯材1的上表面、下表面和四周铺覆一层粘接物2;S101, laying a layer of adhesive 2 on the upper surface, lower surface and surroundings of the honeycomb core material 1;

具体地,粘接物可以是胶膜,由于蜂窝芯材的蒙皮面板材料和胶膜的材料均为树脂,因此为了确保树脂间的相容性,粘接物的材料应选择与蜂窝芯材蒙皮面板的树脂材料同种树脂体系的胶膜和预浸料,以及选择相同固化温度水平的材料,如低温固化材料、中温固化材料或高温固化材料;可选地,胶膜材料可以选用Henkel公司的HYSOL EA 9628、PL7000、METLBOND 1515等。Specifically, the adhesive can be an adhesive film. Since both the skin panel material of the honeycomb core material and the adhesive film are made of resin, in order to ensure the compatibility between the resins, the material of the adhesive should be selected to be compatible with the honeycomb core material. The resin material of the skin panel is the adhesive film and prepreg of the same resin system, and the material with the same curing temperature level is selected, such as low temperature curing material, medium temperature curing material or high temperature curing material; optionally, the adhesive film material can be Henkel The company's HYSOL EA 9628, PL7000, METLBOND 1515, etc.

S102,在铺覆了粘接物的蜂窝芯材上表面、下表面和四周铺覆一层预浸料3;S102, laying a layer of prepreg 3 on the upper surface, lower surface and surroundings of the honeycomb core material covered with the adhesive;

具体地,是在铺覆了粘接物之后的蜂窝芯材的上、下表面和四周再铺覆一层预浸料,粘接物和预浸料的顺序是由内至外。Specifically, a layer of prepreg is laid on the upper, lower and surrounding surfaces of the honeycomb core material after the adhesive is applied, and the order of the adhesive and the prepreg is from the inside to the outside.

可选地,预浸料可以是采用商用CYCOM 970、CYCOM977、CYCOM 7701或Loctite BZ9704等。Optionally, the prepreg can be commercial CYCOM 970, CYCOM977, CYCOM 7701 or Loctite BZ9704, etc.

S103,对铺覆了预浸料3的蜂窝芯材进行真空封装,并在一个大气压下进行固化,得到预处理后的蜂窝芯材;S103, vacuum-encapsulating the honeycomb core material coated with the prepreg 3, and curing it under an atmospheric pressure to obtain a pretreated honeycomb core material;

其中,真空封装主要是采用真空袋来实现。Among them, vacuum packaging is mainly realized by vacuum bags.

S104,对预处理后的蜂窝芯材进行真空封装,并进行固化成型,得到蜂窝夹层结构。S104, vacuum-encapsulate the pretreated honeycomb core material, and perform curing molding to obtain a honeycomb sandwich structure.

具体地,是对预处理后的蜂窝芯材按照复合材料液体成型工艺进行真空封装;优选地,液体成型工艺可以采用真空灌注工艺。Specifically, the pretreated honeycomb core material is vacuum-packaged according to a composite material liquid forming process; preferably, the liquid forming process can adopt a vacuum infusion process.

本发明实施例一通过对蜂窝芯材进行预处理(即步骤S101和S102),从而使得预处理后的蜂窝芯材能够和上、下表面铺覆的预浸料实现良好粘接。预浸料和粘接物分别采用商用的预浸料和胶膜材料,由于蜂窝预处理过程和真空导入工艺过程具有较强的可操作性,使得预处理后的蜂窝质量稳定可靠。预浸料与胶膜的使用实现了蒙皮面板与蜂窝的良好粘接界面。在本发明中,蒙皮面板是指真空导入后在蜂窝芯材上、下表面所形成的层状结构。In Embodiment 1 of the present invention, pretreatment is performed on the honeycomb core material (ie steps S101 and S102 ), so that the pretreated honeycomb core material can be well bonded to the prepreg covering the upper and lower surfaces. Prepregs and adhesives are commercially available prepregs and adhesive film materials respectively. Due to the strong operability of the honeycomb pretreatment process and the vacuum introduction process, the quality of the pretreated honeycomb is stable and reliable. The use of prepreg and adhesive film achieves a good bonding interface between the skin panel and the honeycomb. In the present invention, the skin panel refers to the layered structure formed on the upper and lower surfaces of the honeycomb core material after vacuum introduction.

图2是本发明实施例二的一种蜂窝夹层结构的制备方法的流程图。Fig. 2 is a flowchart of a method for preparing a honeycomb sandwich structure according to Embodiment 2 of the present invention.

如图2所示,本发明实施例二是在本发明实施例一的步骤S102之后增加了步骤S201-步骤S202,其包括:As shown in Figure 2, the second embodiment of the present invention adds step S201-step S202 after step S102 of the first embodiment of the present invention, which includes:

S201,在铺覆了预浸料3的蜂窝芯材上表面、下表面和四周分别铺覆一表面粗糙的粗糙层;S201, laying a rough layer with a rough surface on the upper surface, the lower surface and the periphery of the honeycomb core material covered with the prepreg 3;

粗糙层的目的一方面是为了便于脱模和透气,另一方面也是为了使其上下表面形成粗糙表面,有利于与蒙皮面板的粘接。On the one hand, the purpose of the rough layer is to facilitate demoulding and ventilation, and on the other hand, it is also to form a rough surface on the upper and lower surfaces, which is conducive to bonding with the skin panel.

S202,对铺覆了粗糙层的蜂窝芯材进行真空封装,并进行固化,得到预处理后的蜂窝芯材。S202, vacuum-encapsulating and curing the honeycomb core material coated with the rough layer to obtain a pretreated honeycomb core material.

具体地,在真空封装后,是将铺覆完成的蜂窝芯材放入固化炉中进行固化,在固化结束后还包括对固化的蜂窝芯材进行冷却脱模的步骤。如果在固化结束后,蜂窝芯材周围存在溢出树脂,可以通过手工修整的方式对固化后的蜂窝芯材进行处理。Specifically, after vacuum encapsulation, the paved honeycomb core material is put into a curing furnace for curing, and the solidified honeycomb core material is cooled and demolded after curing. If resin overflows around the honeycomb core material after curing, the cured honeycomb core material can be processed by manual trimming.

本发明实施例一通过对蜂窝芯材进行进一步预处理,从而使得预处理后的蜂窝芯材能够和上、下表面铺覆的预浸料实现进一步的良好粘接。In Embodiment 1 of the present invention, further pretreatment is performed on the honeycomb core material, so that the pretreated honeycomb core material can achieve further good bonding with the prepreg material covered on the upper and lower surfaces.

图3是本发明实施例三的一种蜂窝夹层结构的制备方法的流程图。Fig. 3 is a flowchart of a method for preparing a honeycomb sandwich structure according to Embodiment 3 of the present invention.

如图3所示,本发明实施例三是实施例二中步骤S201的子步骤,其包括:As shown in Figure 3, Embodiment 3 of the present invention is a sub-step of step S201 in Embodiment 2, which includes:

S2011,在铺覆了预浸料的蜂窝芯材上表面和下表面分别铺覆一脱模层4;S2011, laying a release layer 4 on the upper and lower surfaces of the prepreg-coated honeycomb core material;

S2012,在铺覆了脱模层4的蜂窝芯材上表面和下表面分别铺覆一透气层5。S2012, respectively laying a breathable layer 5 on the upper surface and the lower surface of the honeycomb core material covered with the release layer 4 .

脱模层4可以是湿可剥布,透气层可以是透气毡,当脱模层是湿可剥布,透气层是透气毡时,步骤S2021具体是:在铺覆了预浸料的蜂窝芯材上表面和下表面分别铺覆一层湿可剥布;The release layer 4 can be a wet-peelable cloth, and the air-permeable layer can be an air-felt. When the release layer is a wet-peelable cloth and the air-permeable layer is an air-felt, step S2021 is specifically: The upper surface and the lower surface of the material are respectively covered with a layer of wet peelable cloth;

步骤S2022具体是:在铺覆了湿可剥布的蜂窝芯材上表面和下表面分别铺覆一层透气毡。Step S2022 is specifically: spreading a layer of air felt on the upper surface and the lower surface of the honeycomb core material covered with wet peelable cloth.

其中,铺覆湿可剥布和透气毡的目的一方面是为了便于脱模和透气,另一方面也是为了使其上下表面形成粗糙表面,有利于与蒙皮面板的粘接。可选的,湿可剥布可选用商用,商用的湿可剥布材料可以选用Airtech公司的Release Ply系列可剥布,Hexcel公司的湿可剥布 M21/48%/F08111和 F161/43%/F08111,Henkel公司的EA9895WPP(高温)和EA9896(中温),以及Cytec公司的CYCOM7701/52006等;湿可剥布和透气毡的使用,使固化后的蜂窝芯材上下表面能够形成易粘接的粗糙界面,从而使得导入的树脂与处理后的蜂窝上下表面形成良好的粘接界面。Among them, the purpose of covering wet peelable cloth and air felt is to facilitate demoulding and ventilation on the one hand, and on the other hand to form a rough surface on the upper and lower surfaces, which is conducive to bonding with the skin panel. Optionally, commercial wet-peelable cloth can be used, and commercial wet-peelable cloth materials can be selected from Airtech’s Release Ply series of peelable cloth, Hexcel’s wet-peelable cloth M21/48%/F08111 and F161/43%/F08111, Henkel's EA9895WPP (high temperature) and EA9896 (medium temperature), and Cytec's CYCOM7701/52006, etc.; the use of wet peelable cloth and air felt enables the upper and lower surfaces of the cured honeycomb core material to form Easy-to-adhesive rough interface, so that the imported resin forms a good bonding interface with the upper and lower surfaces of the processed honeycomb.

图4是本发明实施例四的一种蜂窝夹层结构的制备方法的流程图。Fig. 4 is a flowchart of a method for preparing a honeycomb sandwich structure according to Embodiment 4 of the present invention.

如图4所示,本发明实施例四是在实施例一的基础上,还包括如下步骤S105:As shown in Figure 4, Embodiment 4 of the present invention is based on Embodiment 1, and further includes the following step S105:

S105,当预处理后的蜂窝芯材存在裸露孔格时,在裸露孔格的位置添加预浸料并进行二次固化。S105, when there are bare cells in the pretreated honeycomb core material, adding prepreg at the positions of the exposed cells and performing secondary curing.

具体地,二次固化也是在一个大气压下进行,且在固化结束后仍需冷却脱模。Specifically, the secondary curing is also carried out under one atmospheric pressure, and after the curing is completed, it still needs to be cooled and demolded.

图5是本发明实施例五的一种蜂窝夹层结构的制备方法的流程图。Fig. 5 is a flowchart of a method for preparing a honeycomb sandwich structure according to Embodiment 5 of the present invention.

具体地,是将固化结束后脱模的蜂窝芯材进行封闭,并放在模具上,然后通过手工铺覆或自动铺放的方式在其上、下表面铺放干纤维,如碳纤维、玻璃纤维、芳纶纤维等。按照真空灌注或真空导入的工艺进行封装后,完成抽真空、注胶、固化和成型等过程。Specifically, the honeycomb core material that has been released from the mold after curing is sealed and placed on the mold, and then dry fibers, such as carbon fibers and glass fibers, are laid on the upper and lower surfaces by manual or automatic laying. , Aramid fiber, etc. After packaging according to the process of vacuum infusion or vacuum introduction, the processes of vacuuming, glue injection, curing and molding are completed.

如图5所示,本发明实施例五是在实施例四的步骤S105之后实施,包括如下步骤S501-S505:As shown in Figure 5, the fifth embodiment of the present invention is implemented after step S105 of the fourth embodiment, including the following steps S501-S505:

S501,在固化后获得的蜂窝芯材的上、下表面分别铺放一增强纤维;S501, respectively laying a reinforcing fiber on the upper and lower surfaces of the honeycomb core material obtained after curing;

S502,在铺放了增强纤维的蜂窝芯材的上、下表面分别铺放一脱模物质层;S502, respectively laying a release material layer on the upper and lower surfaces of the honeycomb core material laid with reinforcing fibers;

其中,脱模物质层可以采用脱模布。Wherein, the release material layer can adopt a release cloth.

S503,在铺放了脱模物质层的蜂窝芯材的上、下表面分别铺放一抗粘物质层;S503, laying an anti-adhesive substance layer on the upper and lower surfaces of the honeycomb core material on which the release substance layer is laid;

抗粘物质层可以采用四氟布。The anti-adhesive substance layer can adopt tetrafluorocloth.

S504,在铺放了抗粘物质层的蜂窝芯材的上、下表面分别铺放一导流装置;S504, respectively laying a diversion device on the upper and lower surfaces of the honeycomb core material on which the anti-adhesive material layer is laid;

其中,导流装置可以采用导流网。Wherein, the diversion device may adopt a diversion net.

S505,将铺放了导流装置的蜂窝芯材采用两层真空袋进行真空封装,且在内层真空袋上设置注胶口和出胶口,出胶口应当在内层真空袋的下方,真空封装可以是采用真空袋将其密封在模具上。S505, vacuum-encapsulate the honeycomb core material with the diversion device in two layers of vacuum bags, and set the glue injection port and the glue outlet on the inner vacuum bag, the glue outlet should be below the inner vacuum bag, Vacuum packaging can be done by using a vacuum bag to seal it on the mold.

如图6所示,本发明实施例六是在实施例五的真空封装步骤之后实施,包括如下步骤S601-S606:As shown in Figure 6, the sixth embodiment of the present invention is implemented after the vacuum packaging step of the fifth embodiment, including the following steps S601-S606:

S601,对两层真空袋之间的密闭空间进行抽真空,保持预定时间;S601, vacuumize the airtight space between the two layers of vacuum bags for a predetermined time;

具体地,是对两层真空袋之间的空间进行抽真空操作,保持12小时,以确保真空封装无漏气。Specifically, vacuumize the space between the two layers of vacuum bags and keep it for 12 hours to ensure that there is no air leakage in the vacuum packaging.

S602,通过注胶口向导流网注胶;S602, injecting glue into the guide net through the glue injection port;

具体地,注胶口和注胶管连接,注胶管与树脂罐连接,以通过注胶管向注胶口输入流体,进而从蜂窝芯材上表面沿着导流网、四氟布、脱模布逐层渗透直至下表面的导流网。Specifically, the glue injection port is connected with the glue injection pipe, and the glue injection pipe is connected with the resin tank, so that the fluid can be input to the glue injection port through the glue injection pipe, and then from the upper surface of the honeycomb core material along the flow guide net, PTFE cloth, and mold release cloth. The layer penetrates down to the deflector mesh on the lower surface.

S603,当出胶口处出现树脂时,停止注胶,对两层真空袋之间的密闭空间继续抽真空;S603, when the resin appears at the glue outlet, stop the glue injection, and continue to evacuate the airtight space between the two layers of vacuum bags;

S604,在基于材料体系设定的固化温度和升温、降温速率,对真空封装的蜂窝芯材进行固化;S604, curing the vacuum-encapsulated honeycomb core material at the curing temperature and the heating and cooling rates set based on the material system;

S605,对固化处理后的蜂窝芯材进行冷却;S605, cooling the solidified honeycomb core material;

具体地,是随炉冷却。Specifically, it is cooled with the furnace.

S606,对冷却后的蜂窝芯材进行脱模,得到蜂窝芯材。本发明通过采用预浸料和粘接物对蜂窝芯材进行预处理,并在蜂窝芯材处理过程中增加湿可剥布和透气毡使其形成易胶接的粗糙表面,之后采用液体成型工艺制备蜂窝夹层结构。液体成型工艺不仅能够降低制备成本,并且由于其在一个大气压下成型,因此避免了蜂窝材料的塌陷。对蜂窝芯材进行预处理堵住了孔格,因此避免了因树脂流入造成的蒙皮面板缺胶。同时解决了传统真空导入工艺过程中树脂易流胶充填进蜂窝孔格,蒙皮面板易出现孔隙的问题。S606, demoulding the cooled honeycomb core material to obtain the honeycomb core material. The present invention pretreats the honeycomb core material by using prepreg and adhesives, and adds wet peelable cloth and air felt during the honeycomb core material treatment process to form a rough surface that is easy to bond, and then adopts a liquid forming process Prepare the honeycomb sandwich structure. The liquid forming process can not only reduce the manufacturing cost, but also avoid the collapse of the honeycomb material because it is formed under one atmospheric pressure. Pre-treatment of the honeycomb core blocks the cells, thus avoiding starvation of the skin panels due to resin inflow. At the same time, it solves the problem that the resin is easy to flow and the glue is filled into the honeycomb cells in the traditional vacuum introduction process, and the skin panel is easy to have pores.

下面通过举例对本发明上述实施例的方式进行详细说明,其工艺过程可分为三个大步骤:The mode of the above-mentioned embodiment of the present invention is described in detail below by giving examples, and its technical process can be divided into three major steps:

步骤一:如图7所示,首先在蜂窝芯材1的上下表面由内至外依次铺覆胶膜2、预浸料3、湿可剥布4和透气毡5,至此完成预处理,然后将预处理后的蜂窝芯材1-0放置于模具6上,再采用真空袋7罩在上面进行密封。Step 1: As shown in Figure 7, firstly, the upper and lower surfaces of the honeycomb core material 1 are sequentially covered with adhesive film 2, prepreg 3, wet peelable cloth 4 and air felt 5, and the pretreatment is completed so far, and then Place the pretreated honeycomb core material 1-0 on the mold 6, and then cover it with a vacuum bag 7 for sealing.

步骤二:密封后将其放入固化炉进行固化,固化后进行冷却脱模,得到如图8所示的蜂窝芯材1-0。Step 2: After sealing, put it into a curing furnace for curing, and then cool and demould after curing to obtain a honeycomb core material 1-0 as shown in FIG. 8 .

步骤三:如图9所示,在脱模后的蜂窝芯材1-0的上、下表面分别由内至外依次铺覆增强纤维8、脱模布9、四氟布10和导流网11,然后再采用真空袋5将其密封在模具上。Step 3: As shown in Figure 9, the upper and lower surfaces of the demoulded honeycomb core material 1-0 are respectively covered with reinforcing fibers 8, release cloth 9, tetrafluoro cloth 10 and flow guide net from the inside to the outside. 11, and then adopt vacuum bag 5 to seal it on the mould.

通过本发明的制备方法制备的蜂窝夹层结构可以与复合材料胶结,也可以与金属胶结,形成强粘接界面。The honeycomb sandwich structure prepared by the preparation method of the present invention can be cemented with composite materials, and can also be cemented with metals to form a strong bonding interface.

应当理解的是,本发明的上述具体实施方式仅仅用于示例性说明或解释本发明的原理,而不构成对本发明的限制。因此,在不偏离本发明的精神和范围的情况下所做的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。此外,本发明所附权利要求旨在涵盖落入所附权利要求范围和边界、或者这种范围和边界的等同形式内的全部变化和修改例。It should be understood that the above specific embodiments of the present invention are only used to illustrate or explain the principles of the present invention, and not to limit the present invention. Therefore, any modification, equivalent replacement, improvement, etc. made without departing from the spirit and scope of the present invention shall fall within the protection scope of the present invention. Furthermore, it is intended that the appended claims of the present invention cover all changes and modifications that come within the scope and metespan of the appended claims, or equivalents of such scope and metesight.

Claims (10)

1. a kind of preparation method of honeycomb sandwich construction, which is characterized in that including:
One layer of sticky object is coated in honeycomb core material upper surface, lower surface and surrounding;
One layer of prepreg is coated with respectively in the honeycomb core material upper surface, lower surface and the surrounding for being coated with the sticky object;
Vacuum Package is carried out to the honeycomb core material for being coated with the prepreg, and is cured at one atm, is obtained To pretreated honeycomb core material;
Vacuum Package is carried out to the pretreated honeycomb core material, and carries out curing molding, obtains honeycomb sandwich construction.
2. the preparation method of a kind of honeycomb sandwich construction according to claim 1, which is characterized in that be coated with the preimpregnation After material and before progress Vacuum Package, the preparation method further includes:
A shaggy rough layer is coated with respectively in the honeycomb core material upper and lower surface for being coated with the prepreg;
Vacuum Package is carried out to the honeycomb core material for being coated with the rough layer, and is cured, obtains pretreated bee Nest core.
3. the preparation method of a kind of honeycomb sandwich construction according to claim 2, which is characterized in that described pre- being coated with The step of honeycomb core material upper and lower surface of leaching material is coated with a shaggy rough layer respectively includes:
A release layer is coated with respectively in the honeycomb core material upper and lower surface for being coated with the prepreg;
An air-permeable layer is coated with respectively in the honeycomb core material upper and lower surface for being coated with the release layer.
4. the preparation method of a kind of honeycomb sandwich construction according to claim 1, which is characterized in that the sticky object is with covering Surface plate material is one species resin system.
5. the preparation method of a kind of honeycomb sandwich construction according to claim 1, which is characterized in that the prepreg is with covering Surface plate material is one species resin system.
A kind of 6. preparation method of honeycomb sandwich construction according to claim 4 or 5, which is characterized in that the preparation side Method further includes:
When the pretreated honeycomb core material is there are during exposed cell, in the position of the exposed cell, addition prepreg is gone forward side by side Row secondary curing.
7. the preparation method of a kind of honeycomb sandwich construction according to claim 1, which is characterized in that after the pretreatment Honeycomb core material the step of being packaged according to priming by vacuum or vacuum introducing technology include:
Upper and lower surface difference one reinforcing fiber of placed of the honeycomb core material obtained after hardening;
In placed, the upper and lower surface difference placed one of the honeycomb core material of the reinforcing fiber demoulds material layer;
The upper and lower surface difference placed primary antibody adhesive material layer of the honeycomb core material of the demoulding material layer in placed;
Upper and lower surface difference placed one guiding device of the honeycomb core material of the anti-stick material layer in placed;
By placed, the honeycomb core material of the guiding device carries out Vacuum Package using two layers of vacuum bag, and in internal layer vacuum Gum-injecting port and gum outlet are set on bag.
8. the preparation method of a kind of honeycomb sandwich construction according to claim 7, which is characterized in that carrying out Vacuum Package Afterwards, further include:
Confined space between two layers of vacuum bag is vacuumized, is kept for the predetermined time;
By gum-injecting port to the guiding device injecting glue;
When occurring resin at gum outlet, stop injecting glue, the confined space between two layers of vacuum bag is continued to vacuumize;
In the solidification temperature and heating, cooling rate set based on material system, the honeycomb core material of Vacuum Package is cured;
The honeycomb core material after curing process is cooled down;
The honeycomb core material after cooling is demoulded, obtains honeycomb core material.
9. the preparation method of a kind of honeycomb sandwich construction according to claim 1, which is characterized in that the sticky object, institute State the material of prepreg and skin panel for identical solidification temperature level.
10. honeycomb prepared by a kind of a kind of preparation method of honeycomb sandwich construction according to any one of claim 1-9 Sandwich.
CN201810002556.2A 2018-01-02 2018-01-02 A kind of honeycomb sandwich construction and preparation method thereof Pending CN108045002A (en)

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CN109001219A (en) * 2018-09-11 2018-12-14 山东大学 Composite material honeycomb sandwich board low-velocity impact damage on-line monitoring system and method
CN109916767A (en) * 2019-03-12 2019-06-21 西北核技术研究所 A method for evaluating the debonding of honeycomb sandwich structures at high temperature
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CN112743874A (en) * 2020-12-11 2021-05-04 哈尔滨飞机工业集团有限责任公司 Laying method of composite material honeycomb sandwich piece adhesive film
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CN114179396A (en) * 2021-12-17 2022-03-15 江西洪都航空工业集团有限责任公司 Forming method and die suitable for irregular U-shaped composite material foam sandwich structural member
CN116278063A (en) * 2021-12-20 2023-06-23 中国石油化工股份有限公司 Honeycomb sandwich structure preform and honeycomb sandwich structure composite material molding method
EP4395987A4 (en) * 2021-09-03 2025-07-30 Carbon Ocean Yachts FILM-BOUND INFUSION

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109001219A (en) * 2018-09-11 2018-12-14 山东大学 Composite material honeycomb sandwich board low-velocity impact damage on-line monitoring system and method
CN109001219B (en) * 2018-09-11 2019-06-28 山东大学 Composite material honeycomb sandwich board low-velocity impact damage on-line monitoring system and method
CN109916767A (en) * 2019-03-12 2019-06-21 西北核技术研究所 A method for evaluating the debonding of honeycomb sandwich structures at high temperature
CN109916767B (en) * 2019-03-12 2021-11-05 西北核技术研究所 A method for evaluating the debonding of honeycomb sandwich structures at high temperature
CN110183976A (en) * 2019-06-03 2019-08-30 中航复合材料有限责任公司 A kind of surface treatment method improving adhesive bonding of composites performance
CN112743874A (en) * 2020-12-11 2021-05-04 哈尔滨飞机工业集团有限责任公司 Laying method of composite material honeycomb sandwich piece adhesive film
CN113178694A (en) * 2021-03-30 2021-07-27 中国航空制造技术研究院 Self-adhesive prepreg-containing broadband radome and preparation method thereof
CN113178694B (en) * 2021-03-30 2022-12-16 中国航空制造技术研究院 Self-adhesive prepreg-containing broadband radome and preparation method thereof
EP4395987A4 (en) * 2021-09-03 2025-07-30 Carbon Ocean Yachts FILM-BOUND INFUSION
CN114179396A (en) * 2021-12-17 2022-03-15 江西洪都航空工业集团有限责任公司 Forming method and die suitable for irregular U-shaped composite material foam sandwich structural member
CN116278063A (en) * 2021-12-20 2023-06-23 中国石油化工股份有限公司 Honeycomb sandwich structure preform and honeycomb sandwich structure composite material molding method

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Application publication date: 20180518