JP3723659B2 - Method for forming honeycomb core material - Google Patents

Method for forming honeycomb core material Download PDF

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Publication number
JP3723659B2
JP3723659B2 JP11099497A JP11099497A JP3723659B2 JP 3723659 B2 JP3723659 B2 JP 3723659B2 JP 11099497 A JP11099497 A JP 11099497A JP 11099497 A JP11099497 A JP 11099497A JP 3723659 B2 JP3723659 B2 JP 3723659B2
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Japan
Prior art keywords
forming
core material
honeycomb core
prepreg
press
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JP11099497A
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Japanese (ja)
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JPH10296763A (en
Inventor
哲也 中村
誠 中条
勝男 斎藤
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Sakura Rubber Co Ltd
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Sakura Rubber Co Ltd
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  • Laminated Bodies (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Shaping Of Tube Ends By Bending Or Straightening (AREA)

Description

【0001】
【発明の属する技術分野】
この発明は、プリプレグを波状(凹凸)に成形してコア材を成形するハニカムコア用材料の成形方法に関する。
【0002】
【従来の技術】
近年、軽量化並びに高強度化などの要請で、エポキシ樹脂や不飽和ポリエステル等の熱硬化性樹脂をマトリックスとしカーボン繊維やアラミド繊維或いはガラス繊維等の強化材を加えたプリプレグの開発がめざましく、これらプリプレグを用いた各種製品のニーズが非常に高まって来ている。
【0003】
これに加えて、最近では、ナイロンやポリエーテルエーテルケトン(PEEK)などの熱可塑性樹脂をマトリックスとした複合材製品のニーズも高まって来ている。
【0004】
特に、この種のプリプレグは軽量で高強度の構造体製品を製作できる優れた特性を持つ素材であるから、航空宇宙分野等の極限的条件で用いられる各種部材としては複合材が大きな力を発揮すると考えられる。
【0005】
複合材構造体で用いられるハニカム構造のコアとして熱硬化性樹脂または熱可塑性樹脂をマトリクスとし、補強繊維として長繊維の炭素繊維強化プラスチック(CFRP)を用いる場合、従来は台形状の凹凸のある型にプリプレグを積層してオートクレーブまたはプレス機などで硬化させる必要があった。
【0006】
【発明が解決しようとする課題】
しかしながら、補強繊維として長繊維の炭素繊維強化プラスチック(CFRP)をコア材とすれば、強度、剛性の高いハニカム板ができることは既知のことであるが、このコア材を作るための波板の成形における型への仕込みまたは積層作業に手間がかかるという問題があった。
【0007】
この発明は、前記事情に着目してなされたもので、その目的とするところは、剛性の高い繊維を含むプリプレグであっても、簡単に任意の形状のハニカムコア用材料を成形できるハニカムコア用材料の成形方法を提供することにある。
【0008】
【課題を解決するための手段】
この発明は、前記目的を達成するために、請求項1は、複数本の角棒材の長手方向の両端部相互を連結部材によって回動自在に連結した2枚の簾状の成形治具の間に、補強繊維からなるシートに熱硬化性樹脂または熱可塑性樹脂をマトリックスとして含浸させたプリプレグを挟み込んでサンドイッチ構造体とし、このサンドイッチ構造体を前記成形治具とともにプレス型によって加熱、加圧した後、前記プリプレグを硬化させ、前記成形治具の形状に倣ったハニカムコア用材料を成形することを特徴とする。
【0009】
請求項2は、請求項1の前記成形治具は、断面形状が異なる第1の部材と第2の部材を平行状態に交互に配置し、その長手方向の両端部相互を連結部材によって回動自在に連結したことを特徴とする。
請求項3は、請求項1の前記プリプレグは、炭素繊維強化プラスチックであることを特徴とする。
【0010】
【発明の実施の形態】
以下、この発明の実施の形態を図面に基づいて説明する。
図1〜図4は第1の実施形態を示す。図1は成形治具1を示し、この成形治具1は複数本の角棒材2と、これら角棒材2の長手方向の両端部相互を連結する連結部材3とによって簾状に形成されている。すなわち、角棒材2は、例えば断面が矩形状の平板状の第1の部材2aと断面が三角形状の第2の部材2bとが交互に平行に配置されている。
【0011】
第1の部材2aと第2の部材2bは同一幅で、同一長さに形成された金属またはセラミック材料によって形成されている。また、前記連結部材3は薄肉板状で、一端部が枢支ピン4によって第1の部材2aの端面に回動自在に連結され、他端部が枢支ピン4によって第2の部材2bの端面に回動自在に連結されている。
【0012】
したがって、成形治具1は、連結部材3が枢支ピン4を支点として回動自在であることから折り畳み可能であり、また巻回することも可能である。このように構成された成形治具1は、複数枚用意され、2枚の成形治具1を重ねて結合することも可能であり、第1の部材2aおよび第2の部材2bの端面にはコ字状の結合部材5の両端部が係合される係合穴6が設けられている。
【0013】
また、図2に示す、7はハニカムコア材として使用するプリプレグであり、シートとしてのカーボン繊維、アラミド繊維、ガラス繊維、炭素繊維等の補強繊維からなる基布に熱可塑性樹脂をマトリックスとして成形した平板状であるか、または熱可塑性樹脂を繊維状にして基布に織り込んだものであるか、もしくは熱硬化性樹脂をマトリックスとして含浸させて半硬化したもの、のいずれかである。このプリプレグ7を前記2枚の成形治具1によって挟み込み、サンドイッチ状態とする。そして、図1に示すように、2枚の成形治具1の第1の部材2aと第2の部材2bとを互いに対向させた状態で、連結部材5の両端部を第1の部材2aおよび第2の部材2bの係合穴6に係合し、2枚の成形治具1を結合する。
【0014】
図3はプレス型8を示し、プレス上型9とプレス下型10とから構成されている。プレス上型9とプレス下型10には断面が三角形状の凹部11と台形状の凸部12とが交互に連続して設けられ、凹部11は前記第2の部材2bの頂部における角度と略同一に形成され、凸部12の頂部は第1の部材2aと略同一幅に形成されている。そして、プレス上型9とプレス下型10は凹部11と凸部12とが互いに対向するように設置され、プレス上型9は可動型としてプレス下型10は固定型として形成されている。
【0015】
次に、ハニカムコア用材料の成形方法について説明する。
平板状のプリプレグ7を2枚の成形治具1によって挟み込み、サンドイッチ状態とする。このとき、2枚の成形治具1の第1の部材2aと第2の部材2bとを互いに対向させた状態で、結合部材5の両端部を第1の部材2aおよび第2の部材2bの係合穴6に係合し、2枚の成形治具1を結合してサンドイッチ構造体13とする。
【0016】
次に、サンドイッチ構造体13をプレス型8のプレス上型9とプレス下型10との間に挿入する。そして、サンドイッチ構造体13の下側に位置する成形治具1の第1の部材2aをプレス下型10の凸部12に、第2の部材2bをプレス下型10の凹部11に位置すると、第1の部材2aと第2の部材2bが連結部材3によって回動自在に連結されていることから、第1の部材2aは凸部12に載置され、第2の部材2bは凹部11の内部に落ち込み、サンドイッチ構造体13が波状に屈曲した状態となる。そして、サンドイッチ構造体13の上側に位置する成形治具1の第1の部材2aをプレス上型9の凸部12に、第2の部材2bをプレス上型9の凹部11が対向する。
【0017】
この状態で、サンドイッチ構造体13を加熱するとともに、プレス上型9を下降してプレス下型10との間でサンドイッチ構造体13をプレス成形すると、サンドイッチ構造体13はプレス上型9とプレス下型10の形状に倣って成形される。ここで、熱可塑性樹脂の場合にはサンドイッチ構造体13を冷却してプリプレグ7を硬化し、熱硬化性樹脂の場合には高温下で反応が促進されて硬化する。
【0018】
次に、硬化したサンドイッチ構造体13をプレス型8から取り外し、結合部材5を取り外すと、プリプレグ7は2枚の成形治具1から分離され、図4に示すように、山部14aと谷部14bとが交互に形成されたハニカムコア用材料14が成形される。
【0019】
図5および図6は第2の実施形態を示す。本実施形態の成形治具15は、図5に示すように、複数本の角棒材16と、これら角棒材16の長手方向の両端部相互を連結する連結部材17とによって簾状に形成されている。すなわち、角棒材16は断面が大形台形状の第1の部材16aと断面が小形台形状の第2の部材16bとが交互に平行に配置されている。そして、第1の部材16aの台形状の傾斜角と第2の部材16bの台形状の傾斜角は同一角度に形成され、第1の部材16aに第2の部材16bを載置したとき1つの台形が形成されるようになっている。
【0020】
第1の部材16aと第2の部材16bは、同一長さに形成された金属またはセラミック材料によって形成されている。また、前記連結部材17は薄肉板状で、一端部が枢支ピン19によって第1の部材16aの端面に回動自在に連結され、他端部が枢支ピン19によって第2の部材16bの端面に回動自在に連結されている。
【0021】
したがって、成形治具15は、連結部材17が枢支ピン19を支点として回動自在であることから折り畳み可能であり、また巻回することも可能である。このように構成された成形治具15は、複数枚用意され、2枚の成形治具15を重ねて結合することも可能であり、第1の部材16aおよび第2の部材16bの端面にはコ字状の結合部材20の両端部が係合される係合穴21が設けられている。
【0022】
図6はプレス型22を示し、プレス上型23とプレス下型24とから構成されている。プレス上型23とプレス下型24はプレス面が平坦面23a,24aに形成され、プレス上型23は可動型としてプレス下型24は固定型として形成されている。
【0023】
次に、ハニカムコア用材料の成形方法について説明する。
平板状のプリプレグ7を2枚の成形治具15によって挟み込み、サンドイッチ状態とする。このとき、2枚の成形治具15の第1の部材16aと第2の部材16bとを互いに対向させた状態で、結合部材20の両端部を第1の部材16aおよび第2の部材16bの係合穴21に係合し、2枚の成形治具15を結合してサンドイッチ構造体25とすると、第1の部材16aと第2の部材16bが連結部材18によって回動自在に連結されていることから、第1の部材16aと第2の部材16bとによってサンドイッチ構造体2が波状に屈曲した状態となる。
【0024】
次に、サンドイッチ構造体25をプレス型22のプレス上型23とプレス下型24との間に挿入し、サンドイッチ構造体25をプレス下型24の平坦面24aに載置する。この状態で、サンドイッチ構造体25を加熱するとともに、プレス上型22を下降してプレス下型23との間でサンドイッチ構造体25をプレス成形すると、サンドイッチ構造体25は第1の部材16aと第2の部材16bの形状に倣って成形される。そして、サンドイッチ構造体25を冷却してプリプレグ7を硬化したのち、サンドイッチ構造体25をプレス型22から取り外し、結合部材22を取り外すと、プリプレグ7は2枚の成形治具15から分離され、ハニカムコア用材料が成形される。
【0025】
なお、前記各実施形態においては、成形治具として平板形状、三角形状あるいは台形状の角柱棒の部材を組み合わせて簾形状としたが、部材の形状は前記実施形態に限定されるものではなく、適宜変更可能である。
【0026】
また、補強繊維からなるシートとして基布を用いて、この基布に熱可塑性樹脂をマトリックスとしてプリプレグを形成したが、補強繊維を引きそろえたテープに熱可塑性樹脂をマトリックスとしてプリプレグを形成してもよい。
【0027】
【発明の効果】
この発明は以上説明したように、2枚の簾状の成形治具の間に、補強繊維からなるシートに熱硬化性樹脂または熱可塑性樹脂をマトリックスとして含浸させたプリプレグを挟み込み、プリプレグを成形治具とともにプレス型によって加熱、加圧した後、プリプレグを硬化させ、成形治具の形状に倣ったハニカムコア用材料を成形することにより、剛性の高い補強繊維を使用しても成形治具とプレス型によって容易に所望の波状(凹凸)に成形でき、ハニカムコア用材料の成形作業の能率向上を図ることができるという効果がある。
【図面の簡単な説明】
【図1】この発明の第1の実施形態のハニカムコア用材料の成形する成形治具を示し、(a)は斜視図、(b)はA−A線に沿う断面図、(c)はB部を拡大した斜視図。
【図2】同実施形態の2枚の成形治具とプリプレグのサンドイッチ構造体の側面図。
【図3】同実施形態のプレス型によってサンドイッチ構造体をプレスする様子を示す縦断側面図。
【図4】同実施形態によって得られたハニカムコア用材料の斜視図。
【図5】この発明の第2の実施形態のハニカムコア用材料の成形する成形治具を示し、(a)は斜視図、(b)はC−C線に沿う断面図、(c)はD部を拡大した斜視図。
【図6】同実施形態のプレス型によってサンドイッチ構造体をプレスする様子を示す縦断側面図。
【符号の説明】
1…成形治具
2a…第1の部材
2b…第2の部材
7…プリプレグ
8…プレス型
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a method for forming a honeycomb core material, in which a core material is formed by forming a prepreg into a wave shape (unevenness).
[0002]
[Prior art]
In recent years, due to demands for weight reduction and higher strength, the development of prepregs with a thermosetting resin such as epoxy resin and unsaturated polyester as a matrix and addition of reinforcing materials such as carbon fiber, aramid fiber or glass fiber has been remarkable. The need for various products using prepreg has been greatly increased.
[0003]
In addition to this, recently, there is an increasing need for composite products using a thermoplastic resin matrix such as nylon or polyetheretherketone (PEEK).
[0004]
In particular, this type of prepreg is a material with excellent properties that can produce lightweight, high-strength structural products. Therefore, composite materials exert great power as various members used in extreme conditions such as the aerospace field. I think that.
[0005]
When a thermosetting resin or thermoplastic resin is used as a matrix as a core of a honeycomb structure used in a composite structure, and a long fiber carbon fiber reinforced plastic (CFRP) is used as a reinforcing fiber, a trapezoidal uneven mold is conventionally used. It was necessary to laminate a prepreg on the substrate and cure it with an autoclave or a press.
[0006]
[Problems to be solved by the invention]
However, it is known that if a long fiber carbon fiber reinforced plastic (CFRP) is used as a reinforcing fiber, a honeycomb plate having high strength and rigidity can be formed. There has been a problem that it takes time to prepare or laminate the mold.
[0007]
The present invention has been made paying attention to the above circumstances, and the object of the present invention is for a honeycomb core that can easily form a honeycomb core material having an arbitrary shape even for a prepreg containing highly rigid fibers. The object is to provide a method of forming a material.
[0008]
[Means for Solving the Problems]
In order to achieve the above object, according to the present invention, there is provided a pair of bowl-shaped forming jigs in which both end portions in the longitudinal direction of a plurality of square bar members are rotatably connected by a connecting member. A sandwich structure is formed by sandwiching a prepreg impregnated with a thermosetting resin or a thermoplastic resin as a matrix between sheets of reinforcing fibers, and this sandwich structure is heated and pressed by a press die together with the molding jig. Thereafter, the prepreg is cured, and a honeycomb core material is formed following the shape of the forming jig.
[0009]
According to a second aspect of the present invention, in the molding jig according to the first aspect, first members and second members having different cross-sectional shapes are alternately arranged in parallel, and both end portions in the longitudinal direction are rotated by a connecting member. It is characterized by being connected freely.
A third aspect of the present invention is characterized in that the prepreg of the first aspect is a carbon fiber reinforced plastic.
[0010]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, embodiments of the present invention will be described with reference to the drawings.
1 to 4 show a first embodiment. FIG. 1 shows a forming jig 1, which is formed in a bowl shape by a plurality of square bar members 2 and a connecting member 3 that connects both ends in the longitudinal direction of the square bar members 2. ing. That is, in the square bar member 2, for example, flat plate-like first members 2 a having a rectangular cross section and second members 2 b having a triangular cross section are alternately arranged in parallel.
[0011]
The first member 2a and the second member 2b are made of a metal or ceramic material having the same width and the same length. The connecting member 3 has a thin plate shape, one end of which is pivotally connected to the end surface of the first member 2 a by a pivot pin 4, and the other end of the second member 2 b by a pivot pin 4. It is rotatably connected to the end face.
[0012]
Therefore, the forming jig 1 can be folded and wound because the connecting member 3 is rotatable about the pivot pin 4 as a fulcrum. A plurality of the forming jigs 1 configured in this way are prepared, and two forming jigs 1 can be overlapped and joined together. The end surfaces of the first member 2a and the second member 2b An engagement hole 6 is provided in which both ends of the U-shaped coupling member 5 are engaged.
[0013]
Also, 7 shown in FIG. 2 is a prepreg used as a honeycomb core material, in which a thermoplastic resin is formed as a matrix on a base fabric made of reinforcing fibers such as carbon fibers, aramid fibers, glass fibers, and carbon fibers as a sheet. Either a flat plate, a thermoplastic resin woven into a base fabric, or a semi-cured material impregnated with a thermosetting resin as a matrix. The prepreg 7 is sandwiched between the two forming jigs 1 to form a sandwich. Then, as shown in FIG. 1, in a state where the first member 2a and the second member 2b of the two forming jigs 1 are opposed to each other, both ends of the connecting member 5 are connected to the first member 2a and The two forming jigs 1 are joined by engaging with the engaging holes 6 of the second member 2b.
[0014]
FIG. 3 shows a press die 8, which is composed of an upper press die 9 and a lower press die 10. The press upper mold 9 and the press lower mold 10 are provided with recesses 11 having a triangular cross section and trapezoidal protrusions 12 alternately and continuously, and the recesses 11 are substantially the same as the angle at the top of the second member 2b. It is formed in the same way, and the top part of the convex part 12 is formed in the substantially same width as the 1st member 2a. The press upper die 9 and the press lower die 10 are installed so that the concave portion 11 and the convex portion 12 face each other, the press upper die 9 is formed as a movable die, and the press lower die 10 is formed as a fixed die.
[0015]
Next, a method for forming the honeycomb core material will be described.
A flat prepreg 7 is sandwiched between two molding jigs 1 to form a sandwich. At this time, in a state where the first member 2a and the second member 2b of the two forming jigs 1 are opposed to each other, both ends of the coupling member 5 are connected to the first member 2a and the second member 2b. The sandwiched structure 13 is formed by engaging the engagement holes 6 and joining the two forming jigs 1 together.
[0016]
Next, the sandwich structure 13 is inserted between the upper press die 9 and the lower press die 10 of the press die 8. Then, when the first member 2a of the forming jig 1 located on the lower side of the sandwich structure 13 is positioned on the convex portion 12 of the press lower mold 10 and the second member 2b is positioned on the concave portion 11 of the press lower mold 10, Since the first member 2 a and the second member 2 b are rotatably connected by the connecting member 3, the first member 2 a is placed on the convex portion 12, and the second member 2 b is the concave portion 11. It falls into the inside and the sandwich structure 13 is bent into a wave shape. Then, the first member 2a of the forming jig 1 positioned above the sandwich structure 13 is opposed to the convex portion 12 of the upper press mold 9, and the second member 2b is opposed to the concave portion 11 of the upper press mold 9.
[0017]
In this state, the sandwich structure 13 is heated and the press upper die 9 is lowered to press the sandwich structure 13 between the press lower die 10 and the sandwich structure 13 is pressed between the press upper die 9 and the press lower die 10. Molded according to the shape of the mold 10. Here, in the case of a thermoplastic resin, the sandwich structure 13 is cooled to cure the prepreg 7, and in the case of a thermosetting resin, the reaction is accelerated and cured at a high temperature.
[0018]
Next, when the cured sandwich structure 13 is removed from the press die 8 and the coupling member 5 is removed, the prepreg 7 is separated from the two molding jigs 1 and, as shown in FIG. The honeycomb core material 14 formed alternately with 14b is formed.
[0019]
5 and 6 show a second embodiment. As shown in FIG. 5, the forming jig 15 of the present embodiment is formed in a bowl shape by a plurality of square bar members 16 and a connecting member 17 that connects both ends of the square bar members 16 in the longitudinal direction. Has been. That is, in the square bar member 16, the first member 16 a having a large trapezoidal cross section and the second member 16 b having a small trapezoidal cross section are alternately arranged in parallel. The trapezoidal inclination angle of the first member 16a and the trapezoidal inclination angle of the second member 16b are formed at the same angle, and one is provided when the second member 16b is placed on the first member 16a. A trapezoid is formed.
[0020]
The 1st member 16a and the 2nd member 16b are formed with the metal or ceramic material formed in the same length. The connecting member 17 has a thin plate shape, one end of which is pivotally connected to the end surface of the first member 16a by a pivot pin 19, and the other end of the second member 16b by a pivot pin 19. It is rotatably connected to the end face.
[0021]
Accordingly, the forming jig 15 can be folded and wound because the connecting member 17 is rotatable about the pivot pin 19 as a fulcrum. A plurality of the forming jigs 15 configured as described above are prepared, and two forming jigs 15 can be overlapped and joined. The end faces of the first member 16a and the second member 16b An engagement hole 21 is provided in which both ends of the U-shaped coupling member 20 are engaged.
[0022]
FIG. 6 shows a press die 22, which is composed of an upper press die 23 and a lower press die 24. The press upper mold 23 and the press lower mold 24 have press surfaces formed on flat surfaces 23a and 24a, the press upper mold 23 is formed as a movable mold, and the press lower mold 24 is formed as a fixed mold.
[0023]
Next, a method for forming the honeycomb core material will be described.
The flat prepreg 7 is sandwiched between two molding jigs 15 to form a sandwich. At this time, in a state where the first member 16a and the second member 16b of the two forming jigs 15 are opposed to each other, both ends of the coupling member 20 are connected to the first member 16a and the second member 16b. When the engaging structure 21 is engaged and the two forming jigs 15 are joined to form the sandwich structure 25, the first member 16a and the second member 16b are rotatably connected by the connecting member 18. Therefore, the sandwich structure 2 is bent in a wave shape by the first member 16a and the second member 16b.
[0024]
Next, the sandwich structure 25 is inserted between the upper press mold 23 and the lower press mold 24 of the press mold 22, and the sandwich structure 25 is placed on the flat surface 24 a of the lower press mold 24. In this state, when the sandwich structure 25 is heated and the press upper die 22 is lowered and the sandwich structure 25 is press-molded between the press lower die 23, the sandwich structure 25 has the first member 16a and the first member 16a. The second member 16b is shaped to follow the shape. Then, after the sandwich structure 25 is cooled and the prepreg 7 is cured, the sandwich structure 25 is removed from the press die 22 and the coupling member 22 is removed. Then, the prepreg 7 is separated from the two molding jigs 15, and the honeycomb structure 25 is removed. A core material is formed.
[0025]
In each of the above embodiments, a flat plate shape, a triangular shape, or a trapezoidal prismatic rod member is combined into a bowl shape as a forming jig, but the shape of the member is not limited to the above embodiment, It can be changed as appropriate.
[0026]
In addition, a base fabric was used as a sheet made of reinforcing fibers, and a prepreg was formed on the base fabric using a thermoplastic resin as a matrix. However, a prepreg may be formed using a thermoplastic resin as a matrix on a tape in which reinforcing fibers are aligned. Good.
[0027]
【The invention's effect】
As described above, according to the present invention, a prepreg impregnated with a thermosetting resin or a thermoplastic resin as a matrix is sandwiched between sheets of reinforcing fibers between two ridge-shaped forming jigs, and the prepreg is molded. After heating and pressurizing with a press die together with the tool, the prepreg is cured, and the honeycomb core material is molded according to the shape of the forming jig. The mold can be easily formed into a desired wave shape (unevenness), and the efficiency of the forming operation of the honeycomb core material can be improved.
[Brief description of the drawings]
1A and 1B show a forming jig for forming a honeycomb core material according to a first embodiment of the present invention, wherein FIG. 1A is a perspective view, FIG. 1B is a cross-sectional view taken along line AA, and FIG. The perspective view which expanded the B section.
FIG. 2 is a side view of a sandwich structure of two forming jigs and a prepreg according to the embodiment.
FIG. 3 is a longitudinal side view showing a state in which the sandwich structure is pressed by the press die according to the embodiment.
Fig. 4 is a perspective view of a honeycomb core material obtained by the same embodiment.
5A and 5B show a forming jig for forming a honeycomb core material according to a second embodiment of the present invention, wherein FIG. 5A is a perspective view, FIG. 5B is a cross-sectional view taken along the line CC, and FIG. The perspective view which expanded D section.
FIG. 6 is a longitudinal side view showing a state in which the sandwich structure is pressed by the press die according to the embodiment.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 ... Molding jig 2a ... 1st member 2b ... 2nd member 7 ... Prepreg 8 ... Press die

Claims (3)

複数本の角棒材の長手方向の両端部相互を連結部材によって回動自在に連結した2枚の簾状の成形治具の間に、補強繊維からなるシートに熱硬化性樹脂または熱可塑性樹脂をマトリックスとして含浸させたプリプレグを挟み込んでサンドイッチ構造体とし、このサンドイッチ構造体を前記成形治具とともにプレス型によって加熱、加圧した後、前記プリプレグを硬化させ、前記成形治具の形状に倣ったハニカムコア用材料を成形することを特徴とするハニカムコア用材料の成形方法。A thermosetting resin or a thermoplastic resin is formed on a sheet made of reinforcing fibers between two hook-shaped forming jigs in which both ends in the longitudinal direction of a plurality of square bar members are rotatably connected by a connecting member. A sandwich structure is formed by sandwiching a prepreg impregnated as a matrix, and the sandwich structure is heated and pressed by a press die together with the molding jig, and then the prepreg is cured to follow the shape of the molding jig. A method for forming a honeycomb core material, comprising forming the honeycomb core material. 前記成形治具は、断面形状が異なる第1の部材と第2の部材を平行状態に交互に配置し、その長手方向の両端部相互を連結部材によって回動自在に連結したことを特徴とする請求項1記載のハニカムコア用材料の成形方法。The forming jig is characterized in that first members and second members having different cross-sectional shapes are alternately arranged in a parallel state, and both ends in the longitudinal direction thereof are rotatably connected by a connecting member. The method for forming a honeycomb core material according to claim 1. 前記プリプレグは、炭素繊維強化プラスチックであることを特徴とする請求項1記載のハニカムコア用材料の成形方法。The method for molding a honeycomb core material according to claim 1, wherein the prepreg is a carbon fiber reinforced plastic.
JP11099497A 1997-04-28 1997-04-28 Method for forming honeycomb core material Expired - Lifetime JP3723659B2 (en)

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