JPH106416A - Production of honeycomb core - Google Patents

Production of honeycomb core

Info

Publication number
JPH106416A
JPH106416A JP8178430A JP17843096A JPH106416A JP H106416 A JPH106416 A JP H106416A JP 8178430 A JP8178430 A JP 8178430A JP 17843096 A JP17843096 A JP 17843096A JP H106416 A JPH106416 A JP H106416A
Authority
JP
Japan
Prior art keywords
corrugated
adhesive
honeycomb core
manufacturing
space
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP8178430A
Other languages
Japanese (ja)
Inventor
Takaya Komine
孝也 小峰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Showa Aircraft Industry Co Ltd
Original Assignee
Showa Aircraft Industry Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Showa Aircraft Industry Co Ltd filed Critical Showa Aircraft Industry Co Ltd
Priority to JP8178430A priority Critical patent/JPH106416A/en
Publication of JPH106416A publication Critical patent/JPH106416A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/40General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
    • B29C66/41Joining substantially flat articles ; Making flat seams in tubular or hollow articles
    • B29C66/43Joining a relatively small portion of the surface of said articles
    • B29C66/438Joining sheets for making hollow-walled, channelled structures or multi-tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/18Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/18Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • B29C65/24Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools characterised by the means for heating the tool
    • B29C65/30Electrical means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/48Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
    • B29C65/4805Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
    • B29C65/483Reactive adhesives, e.g. chemically curing adhesives
    • B29C65/4835Heat curing adhesives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/112Single lapped joints
    • B29C66/1122Single lap to lap joints, i.e. overlap joints

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Laminated Bodies (AREA)

Abstract

PROBLEM TO BE SOLVED: To apply sufficient pressure required for adhesion to enhance bonding strength to a large extent, making even material quality softened at the curing temp. of an adhesive or lower usable as a matrix, to simply and easily realize these characteristics and to shorten the heating curing time of an adhesive. SOLUTION: In the production of a honeycomb core, a matrix 6 is molded into a corrugated plate 2 and a plurality of the corrugated plates 2 are stacked through an adhesive 3 in positional relation wherein spaces A are present and bottom parts and top parts are matched with each other. Piece members 9 are inserted into the spaces A between the corrugated plates 2 and the whole is heated at the curing temp. of the adhesive 3 to be pressed to bond the corrugated plates to obtain a honeycomb core 1 having the corrugated plates 2 as cell walls and the spaces A as cells. It is considered that a current supply heating elements 10 is inserted in each piece member 9.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、ハニカムコアの製
造方法に関する。すなわち、波板を重積,接着すること
によりハニカムコアを得る、いわゆるコルゲート法によ
るハニカムコアの製造方法に関するものである。
[0001] The present invention relates to a method for manufacturing a honeycomb core. That is, the present invention relates to a method for manufacturing a honeycomb core by a so-called corrugation method, in which a honeycomb core is obtained by stacking and bonding corrugated sheets.

【0002】[0002]

【従来の技術】ハニカムコアは、従来より一般的に、次
の工程を辿って製造されている。すなわち、まず母材を
波板に成形した後、このような複数枚の波板を、底部と
頂部とを合わせる位置関係で接着剤を介装しつつ重積
し、それから、接着剤の硬化温度にて加熱すると共に加
圧することにより各波板間を接着し、もって、各波板を
セル壁として区画形成された中空柱状のセルの平面的集
合体である、ハニカムコアを得ていた。
2. Description of the Related Art A honeycomb core is generally manufactured by the following steps. That is, first, after the base material is formed into a corrugated sheet, such a plurality of corrugated sheets are stacked while interposing an adhesive in a positional relationship where the bottom and the top are aligned, and then the curing temperature of the adhesive is set. By heating and pressurizing, the corrugated plates are bonded to each other, thereby obtaining a honeycomb core, which is a planar aggregate of hollow columnar cells partitioned and formed with each corrugated plate as a cell wall.

【0003】[0003]

【発明が解決しようとする課題】ところで、このような
従来例にあっては、次の問題が指摘されていた。すなわ
ちハニカムコアの製造工程では、上述したように、波板
を接着剤を介装しつつ重積した後、加熱すると共に加圧
することにより、各波板間を接着していた。図3は、こ
のような従来例の説明に供する斜視図であり、(1)図
は重積された波板を、(2)図はその潰れた状態を示
し、(3)図は得られたハニカムコアを、(4)図はそ
の形状が崩れた状態を示す。
The following problems have been pointed out in such a conventional example. That is, in the manufacturing process of the honeycomb core, as described above, after corrugated sheets are stacked with an adhesive interposed therebetween, the corrugated sheets are bonded by heating and pressing. FIGS. 3A and 3B are perspective views for explaining such a conventional example, in which FIG. 1A shows a stacked corrugated sheet, FIG. 2B shows its collapsed state, and FIG. FIG. 4D shows the honeycomb core that has been broken.

【0004】ところで第1に、この種従来例のハニカム
コア1の製造方法では、図3の(1)図に示したよう
に、波板2を底部と頂部とを合わせる位置関係で接着剤
3を介装しつつ重積し、相互間に中空の空間Aが存した
状態で、接着のため加熱しつつ、重積方向に沿い(図面
上では上下から)加圧されていた。そして、このように
空間Aが存していたので、接着のために必要十分な圧力
を加えることができず、接着には不十分な弱い圧力しか
加えることができなかった。そして、もしも圧力を加え
過ぎると、図3の(1)図に示した状態から図3の
(2)図に示したように、重積された波板2が潰れ、も
って、このような波板2をセル壁4として形成されたセ
ル5(図3の(3)図や(4)図を参照)も潰れてしま
うことがある、という問題が指摘されていた。第2に、
この種従来例のハニカムコア1の製造方法では、このよ
うに波板2相互間の接着に必要十分な圧力を加えること
ができなかったので、製造されたハニカムコア1につい
て、波板2相互間つまりセル壁4間の接着強度に不安が
指摘されることが多々あり、その圧縮強度や剪断強度に
問題が生じることがあった。
[0004] First, in the method of manufacturing a honeycomb core 1 of this kind in the related art, as shown in FIG. 3A, the adhesive 3 is attached to the corrugated plate 2 so that the bottom and top are aligned. Were stacked and interposed between them, and in a state where there was a hollow space A therebetween, pressure was applied along the stacking direction (from above and below in the drawing) while heating for bonding. Then, since the space A was present, a necessary and sufficient pressure for bonding could not be applied, and only an insufficient weak pressure could be applied for bonding. If too much pressure is applied, the piled corrugated sheet 2 is crushed from the state shown in FIG. 3A to the state shown in FIG. It has been pointed out that the cell 5 formed with the plate 2 as the cell wall 4 (see FIG. 3 (3) and FIG. 4 (4)) may be crushed. Second,
In the conventional method of manufacturing the honeycomb core 1 of this type, it was not possible to apply a necessary and sufficient pressure for bonding between the corrugated sheets 2. That is, anxiety is often pointed out about the adhesive strength between the cell walls 4, and a problem may occur in the compressive strength and the shear strength.

【0005】第3に、この種従来例のハニカムコア1の
製造方法では、波板2つまりセル壁4の母材としては、
接着剤3の硬化温度以下で軟化する材質のものは、使用
不能とされていた。すなわち、もしも接着剤3の硬化温
度(例えば170℃)以下で軟化する母材、例えばプラ
スチックや繊維強化プラスチック等を用いると、接着剤
3の硬化温度による加熱と加圧による接着に際し、この
ような母材が軟化してしまう。そして、重積方向例えば
上下から加圧されることにより、重積された波板2そし
てセル壁4やセル5が、前述したように図3の(1)図
に示した状態から図3の(2)図のように潰れたり、図
3の(3)図に示した状態から図3の(4)図に示した
ように全体形状が崩れてしまう、という問題が指摘され
ていた。そこで従来、母材として樹脂等を使用する場合
は、必ず接着剤3の硬化温度以上(例えば240℃程
度)で軟化するものが、選択使用されており、母材の材
質が限定されるという難点があった。なお、このような
各波板2間に更に平板を介装,重積,接着したハニカム
コア1も開発,使用されていたが、その製造方法に関し
ても、上述した第1,第2,第3に準じた問題が指摘さ
れていた。
Thirdly, in the method of manufacturing the honeycomb core 1 of this type in the related art, as a base material of the corrugated plate 2, that is, the cell wall 4,
Materials that soften below the curing temperature of the adhesive 3 have been considered unusable. That is, if a base material that softens below the curing temperature (for example, 170 ° C.) of the adhesive 3, such as plastic or fiber-reinforced plastic, is used, the bonding by heating and pressurization at the curing temperature of the adhesive 3 is performed. The base material softens. Then, by applying pressure in the stacking direction, for example, from above and below, the stacked stack of corrugated sheets 2 and the cell walls 4 and cells 5 are moved from the state shown in FIG. (2) It has been pointed out that a problem such as crushing as shown in FIG. 3 or collapse of the entire shape from the state shown in FIG. 3 (3) as shown in FIG. 3 (4) is obtained. Conventionally, when a resin or the like is used as a base material, a material that softens at a temperature equal to or higher than the curing temperature of the adhesive 3 (for example, about 240 ° C.) is selectively used, and the material of the base material is limited. was there. The honeycomb core 1 in which a flat plate is further interposed, stacked, and bonded between the corrugated plates 2 has been developed and used, but the manufacturing method thereof is also described in the first, second, and third embodiments. The problem according to was pointed out.

【0006】本発明は、このような実情に鑑み、上記従
来例の課題を解決すべくなされたものであって、重積さ
れた各波板(請求項2では更に各平板)間の加熱,加圧
による接着に際し、コマ部材を空間に挿入しておくよう
にしたことにより、第1に、接着するのに必要十分な圧
力を加えることができ、第2に、もって接着強度が大幅
に向上し、第3に、更に請求項4のように、接着剤の硬
化温度以下で軟化する材質のものも使用可能となり、第
4に、しかもこれらが簡単容易に実現される、ハニカム
コアの製造方法を提案することを目的とする。更に請求
項3では、コマ部材に通電発熱体を内装しておくことに
より、第5に、接着剤の加熱硬化時間を短縮することが
できる、ハニカムコアの製造方法を提案することも目的
とする。
SUMMARY OF THE INVENTION The present invention has been made in view of the above circumstances, and has been made to solve the above-mentioned problems of the prior art. In the case of bonding by pressing, the top member is inserted into the space, so that firstly enough pressure necessary for bonding can be applied, and secondly, bonding strength is greatly improved. Thirdly, it is possible to use a material which softens below the curing temperature of the adhesive as described in claim 4, and fourthly, it is possible to realize these easily and easily. The purpose is to propose. A third object of the present invention is to provide a method of manufacturing a honeycomb core, in which a heating member is provided inside a frame member to shorten the time required for heating and curing the adhesive. .

【0007】[0007]

【課題を解決するための手段】このような課題を解決す
る本発明の技術的手段は、次のとおりである。請求項1
については次のとおり。すなわち、この請求項1のハニ
カムコアの製造方法では、まず母材をコルゲート成形装
置にて、波形の凹凸が連続的に折曲形成された波板に成
形した後、複数枚の該波板を、順次波形の半ピッチ分ず
つずらし底部と頂部とを合わせる位置関係で、接着剤を
介装しつつ重積する。これと共に、各該波板間に形成さ
れた空間に、該空間の断面形状に見合った断面形状のコ
マ部材を密に挿入してから、該接着剤の硬化温度にて加
熱すると共に加圧することにより、各該波板間を接着さ
せ、もって、各該波板をセル壁とすると共に各該空間を
セルとし、各該セル壁にて区画形成された中空柱状のセ
ルの平面的集合体よりなるハニカムコアを得ること、を
特徴とする。
The technical means of the present invention for solving such a problem is as follows. Claim 1
Is as follows. That is, in the method for manufacturing a honeycomb core according to claim 1, first, the base material is formed into a corrugated sheet in which corrugations are continuously bent by a corrugating apparatus, and then a plurality of corrugated sheets are formed. Then, they are sequentially shifted by a half pitch of the waveform, and are stacked while interposing an adhesive in a positional relationship where the bottom and the top are aligned. At the same time, a top member having a sectional shape corresponding to the sectional shape of the space is densely inserted into the space formed between the corrugated sheets, and then heated and pressed at the curing temperature of the adhesive. Thereby, the corrugated sheets are adhered to each other, so that each corrugated sheet is used as a cell wall and each space is used as a cell, and a planar aggregate of hollow columnar cells partitioned by the cell walls is used. To obtain a honeycomb core.

【0008】次に、請求項2については次のとおり。す
なわち、この請求項2のハニカムコアの製造方法では、
まず、母材をコルゲート成形装置にて、波形の凹凸が連
続的に折曲形成された波板に成形した後、複数枚の該波
板と平坦な平板とを、接着剤を介装しつつ順次重積する
と共に、その際、各該波板に関しては、順次波形の半ピ
ッチ分ずつずらし底部と頂部とを対向させる位置関係に
配する。かつ、各該波板と平板間に形成された空間に、
該空間の断面形状に見合った断面形状のコマ部材を密に
挿入してから、該接着剤の硬化温度にて加熱すると共に
加圧することにより、各該波板と平板間を接着させ、も
って、各該波板と平板をセル壁とすると共に各該空間を
セルとし、各該セル壁にて区画形成された中空柱状のセ
ルの平面的集合体よりなるハニカムコアを得ること、を
特徴とする。
Next, claim 2 is as follows. That is, in the method for manufacturing a honeycomb core according to claim 2,
First, after the base material is formed into a corrugated sheet in which corrugations are continuously bent by a corrugating apparatus, a plurality of corrugated sheets and a flat plate are interposed with an adhesive. At the same time, the corrugated sheets are sequentially shifted by a half pitch of the waveform, and are arranged in a positional relationship such that the bottom and the top face each other. And, in the space formed between each of the corrugated sheet and the flat plate,
After densely inserting a top member having a cross-sectional shape corresponding to the cross-sectional shape of the space, by heating and pressing at the curing temperature of the adhesive, each corrugated plate and the flat plate are bonded, Each corrugated plate and flat plate is used as a cell wall, and each space is used as a cell, to obtain a honeycomb core formed of a planar aggregate of hollow columnar cells defined by each cell wall. .

【0009】次に、請求項3については次のとおり。す
なわち、この請求項3のハニカムコアの製造方法では、
請求項1又は2記載のハニカムコアの製造方法におい
て、該コマ部材に通電発熱体が内装されていること、を
特徴とする。又、請求項4については次のとおり。すな
わち、この請求項4のハニカムコアの製造方法では、請
求項1又は2記載のハニカムコアの製造方法において、
該母材として、該接着剤の硬化温度以下で軟化する材質
のものが用いられていること、を特徴とする。
Next, claim 3 is as follows. That is, in the method for manufacturing a honeycomb core according to the third aspect,
3. The method for manufacturing a honeycomb core according to claim 1, wherein an electric heating element is provided inside the top member. Claim 4 is as follows. That is, in the method for manufacturing a honeycomb core according to claim 4, in the method for manufacturing a honeycomb core according to claim 1 or 2,
The base material is made of a material that softens below the curing temperature of the adhesive.

【0010】このように、このハニカムコアの製造方法
では、まず母材を波板に成形した後、このような複数枚
の波板を、空間が存すると共に底部と頂部とを合わせる
位置関係で、接着剤を介装しつつ重積し、それから、接
着剤の硬化温度にて加熱すると共に加圧することにより
各波板間を接着し、もって、各波板をセル壁とし各空間
をセルとしたハニカムコアが得られる。そして、重積さ
れた各波板間の上述した加熱,加圧による接着に際し、
コマ部材を波板間の空間に挿入して、各波板をサポート
するようになっている。なお請求項2では、このような
各波板間に、更にそれぞれ平板が介装,重積,接着さ
れ、もって、各波板と平板とで各空間,セル壁,セル等
を形成している。又、請求項3では、コマ部材に通電発
熱体が内装され、接着に際し、内部の空間のコマ部材側
からも各波板等を加熱するようになっている。更に請求
項4では、接着剤の硬化温度で軟化する材質のものを、
母材として用いるようになっている。
As described above, in this method for manufacturing a honeycomb core, first, a base material is formed into a corrugated sheet, and then a plurality of such corrugated sheets are placed in such a manner that a space exists and a bottom portion and a top portion are aligned. The stacking was performed with the adhesive interposed, and then each corrugated sheet was adhered by heating and pressing at the curing temperature of the adhesive, so that each corrugated sheet was a cell wall and each space was a cell. A honeycomb core is obtained. Then, upon bonding by heating and pressing as described above between the stacked corrugated sheets,
The top member is inserted into the space between the corrugated sheets to support each corrugated sheet. In the second aspect, a flat plate is further interposed, stacked, and bonded between the corrugated sheets, so that each corrugated sheet and the flat plate form each space, cell wall, cell, and the like. . According to a third aspect of the present invention, a current-carrying heating element is provided inside the top member, and upon bonding, each corrugated plate is heated also from the top member side of the internal space. Further, in the fourth aspect, the material which is softened at the curing temperature of the adhesive,
It is designed to be used as a base material.

【0011】[0011]

【発明の実施の形態】以下本発明を、図面に示すその発
明の実施の形態に基づいて、詳細に説明する。図1,図
2は、本発明の実施の形態の説明に供する斜視図であ
り、図1の(1)図は第1例の要部を示し、(2)図は
同第1例におけるコマ部材を示し、(3)図は第2例の
要部を示し、(4)図は同第2例におけるコマ部材を示
す。図2の(1)図は第3例におけるコマ部材を示し、
(2)図は第4例におけるコマ部材を示す。図4は、一
般的なハニカムコアの製造方法の説明に供する正面説明
図であり、(1)図は準備された母材を、(2)図は波
板の成形工程を、(3)図は成形された波板を、(4)
図は波板を重積,接合する工程を示す。図5は、ハニカ
ムコアの正面説明図であり、(1)図はその1例を、
(2)図は他の例を示す。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, the present invention will be described in detail based on embodiments of the invention shown in the drawings. 1 and 2 are perspective views for explaining an embodiment of the present invention. FIG. 1 (1) shows a main part of the first example, and FIG. 1 (2) shows a frame in the first example. FIG. 3C shows a main part of the second example, and FIG. 4D shows a top member in the second example. FIG. 2A shows the top member in the third example,
(2) The figure shows the top member in the fourth example. FIG. 4 is an explanatory front view for explaining a general method for manufacturing a honeycomb core. FIG. 4A is a diagram illustrating a prepared base material, FIG. (4)
The figure shows the process of stacking and joining corrugated sheets. FIG. 5 is an explanatory front view of a honeycomb core, and FIG.
(2) The figure shows another example.

【0012】まず図4により、本発明のハニカムコア1
の製造方法について、その前提となる一般例(一般的な
コルゲート法)を述べる。この製造方法では、まず図4
の(1)図に示したように、母材6が準備される。この
母材6としては、アルミニウム箔その他の金属箔、繊維
強化プラスチック(FRP)シート、各種のプラスチッ
クシート、パルプを含む複合シート、その他各種材質の
シートが用いられる。なお、繊維強化プラスチック(F
RP)シートは、ガラス繊維,ケブラー繊維,カーボン
繊維,セラミック繊維,金属繊維,樹脂繊維,その他の
織・不織の繊維と、エポキシ系の樹脂,ポリイミド系の
樹脂,その他の熱硬化性樹脂や熱可塑性樹脂とを、適宜
選択して、付着,含浸,混入等により組み合わせたもの
よりなる。そして、この繊維強化プラスチックシート
は、まだ完全硬化しない半硬化状態、つまり柔軟性・粘
性を備えたプリプレグ状として用いられ、図示例では、
平織のカーボン繊維にエポキシ樹脂を付着,含浸,混入
等したものが、母材6として用いられており、そのガラ
ス転移点は120℃程度となっている。
First, referring to FIG. 4, the honeycomb core 1 of the present invention
A description will be given of a general example (general corrugation method) which is a premise of the method of manufacturing. In this manufacturing method, first, FIG.
As shown in FIG. 1A, a base material 6 is prepared. As the base material 6, an aluminum foil or other metal foil, a fiber reinforced plastic (FRP) sheet, various plastic sheets, a composite sheet containing pulp, and sheets of other various materials are used. In addition, fiber reinforced plastic (F
RP) sheet is made of glass fiber, Kevlar fiber, carbon fiber, ceramic fiber, metal fiber, resin fiber, other woven or non-woven fiber, epoxy resin, polyimide resin, other thermosetting resin, A thermoplastic resin is appropriately selected and combined by adhesion, impregnation, mixing or the like. And this fiber reinforced plastic sheet is used as a semi-cured state that is not yet completely cured, that is, a prepreg having flexibility and viscosity.
A material obtained by adhering, impregnating, or mixing an epoxy resin to a plain-woven carbon fiber is used as the base material 6, and its glass transition point is about 120 ° C.

【0013】次に、この製造方法では図4の(2)図に
示したように、このような母材6をコルゲート成形装置
7にて、波形の凹凸が連続的に折曲形成された波板2に
成形する。これらについて更に詳述すると、コルゲート
成形装置7は、図4の(2)図の例では上下1対のラッ
ク8よりなるが、その他各種ギヤ,プレス装置,ベルト
式金型等を用いたものも可能であり、母材6は、このよ
うなコルゲート成形装置7に挿入され、表裏両側から挟
み込まれて加熱加圧されることにより、図4の(3)図
に示したように、波形の凹凸が連続的に折曲形成された
波板2に成形される。波板2は、図示の台形状のほか、
略三角形状,略四角形状,その他各種形状の波形の凹凸
が、短手方向に直線的で平行かつ長手方向に連続的に、
所定ピッチと高さで折曲形成されてなる。
Next, in this manufacturing method, as shown in FIG. 4 (2), such a base material 6 is corrugated by a corrugating apparatus 7 so that the corrugated irregularities are continuously bent. Formed into plate 2. More specifically, the corrugating device 7 is composed of a pair of upper and lower racks 8 in the example shown in FIG. 4B, but may also use other gears, press devices, belt-type dies, and the like. The base material 6 can be inserted into such a corrugating device 7 and sandwiched from both front and back sides and heated and pressed to form corrugated irregularities as shown in FIG. Is formed into a corrugated sheet 2 which is continuously bent. The corrugated sheet 2 has a trapezoidal shape as shown,
The substantially triangular, substantially quadrangular, and other various shapes of corrugations are straight and parallel in the short direction and continuously in the long direction.
It is bent at a predetermined pitch and height.

【0014】しかる後、この製造方法では図4の(4)
図に示したように、このように成形された複数枚の波板
2を、順次波形の半ピッチ分ずつずらし底部と頂部とを
合わせる位置関係で、接着剤3を介装しつつ重積する。
これらについて更に詳述すると、前述により成形された
波板2は、例えば、波の谷部下面や頂部上面等に条線状
にノードボンドつまり接着剤3が塗布されて乾燥される
と共に、所定長さ毎に切断される。このような接着剤3
としては熱硬化性のものが使用され、例えば、硬化温度
が170℃以上のナイロン変性フェノール樹脂が使用さ
れる。それから図4の(4)図に示したように、複数枚
の波板2が、上下で波の半ピッチ分ずつずらされ、隣接
する上下相互間で谷部と頂部とを合わせる位置関係のも
とに、全体的に空間Aが存した積層ブロック状に重積さ
れる。なお後述するように、このような波板2間に、平
板が更に介装される場合もある。
Thereafter, in this manufacturing method, FIG.
As shown in the figure, a plurality of corrugated sheets 2 formed in this manner are successively shifted by a half pitch of the waveform, and are stacked with an adhesive 3 interposed therebetween in a positional relationship where the bottom and top are aligned. .
More specifically, the corrugated sheet 2 formed as described above is coated with a node bond, that is, an adhesive 3 on the lower surface of the wave valley or the upper surface of the top of the corrugated line, and dried. Cut every time. Such an adhesive 3
A thermosetting resin is used, for example, a nylon-modified phenol resin having a curing temperature of 170 ° C. or more is used. Then, as shown in FIG. 4 (4), the plurality of corrugated sheets 2 are shifted vertically by half a pitch of the wave, and the positional relationship between the valley and the top between the adjacent upper and lower sides is also changed. At the same time, they are stacked in a laminated block shape having the space A as a whole. As described later, a flat plate may be further interposed between such corrugated plates 2 in some cases.

【0015】しかる後、この種製造方法では、通常はそ
のまま、接着剤3の硬化温度にて加熱すると共に加圧す
ることにより、このように重積された各波板2の底部と
頂部間が接着される。もって、例えば図5の(1)図に
示したように、各波板2をセル壁4とすると共に各空間
Aをセル5とし、各セル壁4にて区画形成された中空柱
状のセル5の平面的集合体よりなる、ハニカムコア1が
製造される。
Thereafter, in this type of manufacturing method, the bottom and the top of each of the stacked corrugated sheets 2 are bonded by heating and pressing at the curing temperature of the adhesive 3 as it is. Is done. For example, as shown in FIG. 5A, each corrugated plate 2 is a cell wall 4 and each space A is a cell 5, and a hollow columnar cell 5 defined by each cell wall 4 is formed. The honeycomb core 1 made of the planar assembly of the above is manufactured.

【0016】ハニカムコア1は、このように重積,接着
された波板2をセル壁4として、各々独立空間に区画形
成された中空柱状の多数のセル5の平面的集合体よりな
る。なお、セル壁4そしてセル5の断面形状は、図示の
正六角形状のものが代表的であるが、これによらず、台
形状,略三角形状,略四角形状,その他各種形状のもの
も可能である。そしてハニカムコア1は、重量比強度に
優れ、軽量であると共に高い剛性・強度を備え、又、整
流効果、平面精度、保温性,遮音性等にも優れ、単位容
積当たりの表面積が大である、等々の特性が知られ、広
く各種の構造材として使用されている。
The honeycomb core 1 is made up of a planar assembly of a large number of hollow column-shaped cells 5 partitioned into independent spaces, with the corrugated plates 2 stacked and bonded in this manner as cell walls 4. The cross-sectional shape of the cell wall 4 and the cell 5 is typically a regular hexagonal shape as shown in the figure, but is not limited thereto, and may be trapezoidal, substantially triangular, substantially square, or various other shapes. It is. The honeycomb core 1 has excellent weight ratio strength, is lightweight and has high rigidity and strength, and also has excellent rectifying effect, flatness accuracy, heat insulation, sound insulation, etc., and has a large surface area per unit volume. , Etc., and are widely used as various structural materials.

【0017】本発明のハニカムコア1の製造方法につい
て、その前提となる一般例では、このような工程を辿
り、もってハニカムコア1が製造される。さて、本発明
に係るハニカムコア1の製造方法については、次のとお
り。すなわち、本発明の製造方法では、前述したように
接着剤3を介装しつつ波板2を重積する工程と、加熱,
加圧により各波板2間を接着する工程との間に、次の工
程を備えてなる。
In the method of manufacturing the honeycomb core 1 according to the present invention, the honeycomb core 1 is manufactured by following such steps in a general example which is a premise thereof. Now, the method for manufacturing the honeycomb core 1 according to the present invention is as follows. That is, in the manufacturing method of the present invention, as described above, the step of stacking the corrugated sheet 2 while interposing the adhesive 3,
The following steps are provided between the steps of bonding between the corrugated plates 2 by pressing.

【0018】すなわち図1に示したように、重積された
各波板2間に形成された空間Aに、空間Aの断面形状に
見合った断面形状のコマ部材9が密に挿入され、それか
ら接着が実施されるようになっている。このようなコマ
部材9について、更に詳述すると、まず、中子たるコマ
部材9の断面形状は図示例では正六角形状をなすが、勿
論、空間Aそしてセル5の断面形状に見合った各種断面
形状のものが考えられ、全体的には角柱状や角筒状をな
す。そして、このようなコマ部材9は、各波板2間に形
成された各空間Aについて、その全部又は適宜選択され
た一部について、密に挿入される。なお、このように挿
入されたコマ部材9は、加熱,加圧による接着が終了し
た後、接着された波板2や平板11間の空間Aから、つ
まりセル5から適宜抜き出され、除去される。又、図1
の(3)図,(4)図に示したコマ部材9は、図1の
(1)図,(2)図に示したコマ部材9とは異なり、更
に、ニクロム線等の通電発熱体10がヒーターとして内
装され、通電により発熱可能となっている。
That is, as shown in FIG. 1, the top member 9 having a sectional shape corresponding to the sectional shape of the space A is densely inserted into the space A formed between the stacked corrugated plates 2, and The bonding is performed. More specifically, such a top member 9 will be described. First, the cross-sectional shape of the core top member 9 is a regular hexagon in the illustrated example, but, of course, various cross-sections corresponding to the cross-sectional shape of the space A and the cell 5. Shapes are conceivable, and are generally prismatic or prismatic. Then, such a top member 9 is densely inserted in all or a part appropriately selected in each space A formed between the corrugated sheets 2. After the bonding by heating and pressing is completed, the inserted frame member 9 is appropriately extracted from the space A between the bonded corrugated plates 2 and the flat plates 11, that is, from the cell 5, and removed. You. Also, FIG.
The top member 9 shown in FIGS. (3) and (4) is different from the top member 9 shown in FIGS. (1) and (2) of FIG. Is provided as a heater, and can generate heat when energized.

【0019】本発明に係るハニカムコア1の製造方法で
は、このようにコマ部材9が用いられ、重積された各波
板2間に形成された空間Aに、コマ部材9が挿入されて
から、加熱,加圧による接着が実施される。ところで、
以上説明した例においてハニカムコア1は、図1や図5
の(1)図に示したように、セル壁4が波板2のみから
構成されていたが、本発明は更に、図5の(2)図に示
したように、セル壁4が波板2と平板11とから構成さ
れたハニカムコア1の製造方法にも適用可能である。こ
のように、波板2間に平板11が介装,重積,接着され
たハニカムコア1の製造方法については、次のとおり。
In the method for manufacturing the honeycomb core 1 according to the present invention, the top member 9 is used as described above, and after the top member 9 is inserted into the space A formed between the stacked corrugated plates 2. Then, bonding by heating and pressing is performed. by the way,
In the example described above, the honeycomb core 1 is the same as FIG.
As shown in FIG. 1A, the cell wall 4 is composed of only the corrugated sheet 2. However, in the present invention, as shown in FIG. The present invention is also applicable to a method for manufacturing the honeycomb core 1 composed of the honeycomb core 2 and the flat plate 11. The method for manufacturing the honeycomb core 1 in which the flat plates 11 are interposed, stacked, and bonded between the corrugated plates 2 as described above is as follows.

【0020】すなわちこの製造方法では、まず母材6を
コルゲート成形装置7にて、波形の凹凸が連続的に折曲
形成された波板2に成形した後(図4の(1)図,
(2)図,(3)図を参照)、複数枚の波板2と平坦な
平板11とを、接着剤3を介装しつつ順次重積する。そ
の際、各波板2に関しては、順次波形の半ピッチ分ずつ
ずらし底部と頂部とを対向させる位置関係にて配する
(図5の(2)図を参照)。これと共に、各波板2と平
板11間に形成された空間Aに、図2に示したように、
空間Aの断面形状に見合った例えば断面台形状のコマ部
材9を、密に挿入してから、接着剤3の硬化温度にて加
熱すると共に加圧する。これにより、各波板2と平板1
1間を接着させる。
That is, in this manufacturing method, first, the base material 6 is formed into a corrugated sheet 2 in which corrugations are continuously bent by a corrugating apparatus 7 (FIG. 4A, FIG.
(See FIGS. 2 and 3), a plurality of corrugated sheets 2 and a flat plate 11 are sequentially stacked with the adhesive 3 interposed therebetween. At this time, the corrugated plates 2 are sequentially shifted by a half pitch of the waveform and arranged in a positional relationship in which the bottom and the top face each other (see FIG. 5 (2)). At the same time, in the space A formed between each corrugated plate 2 and the flat plate 11, as shown in FIG.
A top member 9 having, for example, a trapezoidal cross section corresponding to the cross sectional shape of the space A is densely inserted, and then heated and pressed at the curing temperature of the adhesive 3. Thereby, each corrugated plate 2 and flat plate 1
Adhere between the two.

【0021】もって、各波板2と平板11をセル壁4と
すると共に各空間Aをセル5とし、各セル壁4にて区画
形成された、例えば断面台形状の中空柱状のセル5の平
面的集合体よりなる、いわゆるバイセクトタイプのハニ
カムコアが得られる(図5の(2)図を参照)。なお、
図2の(2)図に示したコマ部材9は、図2の(1)図
に示したコマ部材9とは異なり、通電発熱体10が内装
されている。なお平板11としては、通常、平坦な母材
6がそのまま用いられる。又、この図5の(2)図に示
したハニカムコア1の製造方法について、その他の構成
等は、図5の(1)図に示したハニカムコア1の製造方
法について、前述したところに準じるので、その説明は
省略する。
Thus, each corrugated plate 2 and flat plate 11 are used as cell walls 4 and each space A is used as a cell 5, and the plane of a hollow columnar cell 5 having a trapezoidal cross section, for example, is defined by each cell wall 4. As a result, a so-called bisect-type honeycomb core composed of a target aggregate is obtained (see FIG. 5 (2)). In addition,
The top member 9 shown in FIG. 2 (2) differs from the top member 9 shown in FIG. 2 (1) in that an energizing heating element 10 is provided. The flat base material 6 is usually used as the flat plate 11 as it is. The method of manufacturing the honeycomb core 1 shown in FIG. 5B is the same as that of the method of manufacturing the honeycomb core 1 shown in FIG. 5A. Therefore, the description is omitted.

【0022】本発明は、以上説明したように構成されて
いる。そこで以下のようになる。このハニカムコア1の
製造方法では、まず母材6を波板2に成形した後、この
ような複数枚の波板2を、空間Aが存すると共に、底部
と頂部とを合わせる位置関係で、接着剤3を介装しつつ
重積する(図4を参照)。それから、接着剤3の硬化温
度にて加熱すると共に加圧することにより、各波板2間
を接着し、もって、各波板2をセル壁4とし各空間Aを
セル5とした、ハニカムコア1が得られる(図5の
(1)図を参照)。そして、重積された各波板2間の上
述した加熱,加圧による接着に際し、コマ部材9を波板
2間の空間Aに挿入して(図1を参照)、各波板2をサ
ポートするようになっている。
The present invention is configured as described above. Then, it becomes as follows. In the method for manufacturing the honeycomb core 1, first, the base material 6 is formed into the corrugated sheet 2, and then the plurality of corrugated sheets 2 are bonded in a positional relationship where the space A is present and the bottom and the top are aligned. The insemination is carried out with the agent 3 interposed (see FIG. 4). Then, by heating and pressing at the curing temperature of the adhesive 3, the corrugated plates 2 are adhered to each other, so that each corrugated plate 2 is a cell wall 4 and each space A is a cell 5, the honeycomb core 1 (See FIG. 5 (1)). At the time of bonding between the stacked corrugated sheets 2 by the above-described heating and pressurization, the top member 9 is inserted into the space A between the corrugated sheets 2 (see FIG. 1) to support each corrugated sheet 2. It is supposed to.

【0023】そして更に、このような各波板2間にそれ
ぞれ平板11を介装,重積,接着すると共に、その際も
コマ部材9を使用し(図2を参照)、もって各波板2と
平板11とで、各空間A,セル壁4,セル5等を形成す
ることも考えられる(図5の(2)図を参照)。又、コ
マ部材9に通電発熱体10を内装しておき、接着に際
し、内部の空間Aのコマ部材9側からも、各波板2更に
は平板11を加熱することも考えられる(図1の(3)
図,(4)図,図2の(2)図等を参照)。更に、母材
6として、接着剤3の硬化温度以下で軟化する材質のも
のを用いることも考えられる。すなわち、波板2等やセ
ル壁4の母材として、波板2等の接着用に用いられる接
着剤3の硬化温度(例えば170℃程度)より低い(例
えば130℃程度)で軟化する材質のものを、用いるよ
うにすることも可能となる。図示例では、カーボン繊維
にエポキシ樹脂を付着,含浸,混入等し、ガラス転移点
が120℃程度の母材6が使用されている。
Further, the flat plates 11 are interposed, stacked, and bonded between the corrugated sheets 2 as described above, and at this time, the top members 9 are used (see FIG. 2). It is also conceivable to form each space A, cell wall 4, cell 5 and the like with the flat plate 11 (see FIG. 5 (2)). In addition, it is conceivable to heat the corrugated plates 2 and even the flat plate 11 from the side of the top member 9 in the internal space A when bonding the heating element 10 inside the top member 9 and bonding. (3)
, (4), and (2) of FIG. 2). Furthermore, it is also conceivable to use a material that softens below the curing temperature of the adhesive 3 as the base material 6. That is, the base material of the corrugated sheet 2 or the like or the cell wall 4 is made of a material which is softened at a temperature lower than the curing temperature (for example, about 170 ° C.) (for example, about 130 ° C.) of the adhesive 3 used for bonding the corrugated sheet 2 or the like. It is also possible to use one. In the illustrated example, a base material 6 having a glass transition point of about 120 ° C., in which an epoxy resin is attached to, impregnated with, or mixed with carbon fibers, is used.

【0024】さてそこで、このハニカムコア1の製造方
法にあっては、次の第1,第2,第3,第4,第5のよ
うになる。まず第1に、前述により重積されていた各波
板2や平板11間は、加熱,加圧されることにより接着
されるが、その際、空間Aにはコマ部材9が挿入されて
いる。このように、コマ部材9にて各波板2や平板11
がサポートされているので、接着に必要十分な圧力を加
えることができるようになる。
Now, in the method of manufacturing the honeycomb core 1, the following first, second, third, fourth and fifth steps are performed. First, the corrugated plates 2 and the flat plates 11 stacked as described above are bonded by heating and pressing. At this time, the top member 9 is inserted into the space A. . Thus, each corrugated plate 2 and flat plate 11 are
Is supported, so that necessary and sufficient pressure for bonding can be applied.

【0025】第2に、このように接着に際し、必要十分
な圧力を加えることができるので、各波板2相互間や各
波板2と平板11間つまりセル壁4間は、このような加
熱,加圧により、確実に接着されるようになる。つま
り、加熱により溶融硬化した接着剤3が確実に加圧され
ることにより、接着対象たる各波板2相互間や各波板2
と平板11間は、条線状に確実に接着される。
Second, since a necessary and sufficient pressure can be applied at the time of bonding as described above, the heating between the corrugated plates 2 and between the corrugated plates 2 and the flat plate 11, that is, between the cell walls 4. , By pressure, it can be surely adhered. In other words, the adhesive 3 that has been melt-cured by heating is reliably pressed, so that the corrugated sheets 2 to be bonded to each other and the corrugated sheets 2
And the flat plate 11 are securely bonded in a streak shape.

【0026】第3に、前述したように重積されていた各
波板2や平板11間は、接着剤3の硬化温度にて加熱、
そして加圧されることにより接着されるが、その際、空
間Aにはコマ部材9が挿入されている。このように、コ
マ部材9にて各波板2や平板11がサポートされるの
で、各波板2や平板11の母材6として、接着剤3の硬
化温度以下で軟化するプラスチックや繊維強化プラスチ
ック等を用いることも可能となる。すなわち、各波板2
や平板11は、接着剤3の硬化温度による加熱にて、若
干軟化するようなことがあっても、コマ部材9にてサポ
ートされているので、潰れ,変形,崩れ等の発生は回避
される。
Third, the corrugated plates 2 and the flat plates 11 stacked as described above are heated at the curing temperature of the adhesive 3.
At this time, the top member 9 is inserted into the space A. Since the corrugated sheet 2 and the flat plate 11 are supported by the top member 9 as described above, as the base material 6 of each corrugated sheet 2 or the flat plate 11, a plastic or a fiber-reinforced plastic that softens below the curing temperature of the adhesive 3 is used. Etc. can also be used. That is, each corrugated sheet 2
Even if the flat plate 11 is slightly softened by heating at the curing temperature of the adhesive 3, since it is supported by the top member 9, the occurrence of collapse, deformation, collapse, etc. is avoided. .

【0027】第4に、しかもこれら第1,第2,第3の
各点は、ハニカムコア1の製造方法において、コマ部材
9を採用したことにより、簡単容易に実現される。すな
わち、重積された各波板2間や各波板2と平板11間の
加熱,加圧による接着に際し、形成された空間Aにコマ
部材9を挿入するという、簡単な構成により、各点は容
易に実現される。
Fourth, these first, second and third points can be easily and easily realized by employing the top member 9 in the method of manufacturing the honeycomb core 1. That is, when bonding between the stacked corrugated sheets 2 or between the corrugated sheets 2 and the flat plate 11 by heating and pressing, the top member 9 is inserted into the formed space A, and each point is formed by a simple configuration. Is easily realized.

【0028】第5に、なおコマ部材9に、図1の(3)
図,(4)図や図2の(2)図に示したように、ニクロ
ム線等の通電発熱体10を内装した場合については、更
に次のようになる。すなわち、通電発熱体10を通電に
より発熱させることにより、内部の空間Aに挿入された
コマ部材9側からの加熱が、外部からの加熱に加えて実
施されるので、各波板2や平板11について、接着剤3
の硬化による接着に必要な、加熱用の昇温時間が短縮さ
れ、接着剤3の加熱硬化時間が短縮されるようになる。
Fifth, the top member 9 is provided with (3) in FIG.
As shown in the figures, (4) and (2) of FIG. 2, the case where the current-carrying heating element 10 such as a nichrome wire is internally provided is further as follows. That is, by heating the energizing heating element 10 by energizing, heating from the side of the top member 9 inserted into the internal space A is performed in addition to external heating. About adhesive 3
The time required for heating for heating, which is required for bonding by curing of the adhesive 3, is shortened, and the time for heating and curing the adhesive 3 is shortened.

【0029】[0029]

【発明の効果】本発明に係るハニカムコアの製造方法
は、以上説明したように、重積された各波板(請求項2
では更には各平板)間の加熱,加圧による接着に際し、
コマ部材を空間に挿入しておくようにしたことにより、
次の効果を発揮する。
According to the method for manufacturing a honeycomb core according to the present invention, as described above, each of the stacked corrugated sheets (Claim 2)
Then, when bonding by heating and pressing between each plate)
By inserting the top member into the space,
The following effects are exhibited.

【0030】第1に、接着するのに必要十分な圧力を加
えることができる。すなわち、このハニカムコアの製造
方法では、接着に際し、重積されていた各波板(請求項
2では更に各平板)間が加熱,加圧されるが、その際、
コマ部材が挿入されているので、コマ部材にて各波板
(更には各平板)がサポートされ、もって、接着に必要
十分な圧力を加えることができるようになる。つまり、
前述したこの種従来例のように、接着には不十分な弱い
圧力しか加えることができないような事態は回避される
と共に、もしも圧力を加え過ぎると重積された各波板
(更には各平板)そしてセル壁やセルが潰れてしまう、
という危険も回避される。
First, a necessary and sufficient pressure for bonding can be applied. That is, in the method for manufacturing the honeycomb core, the heating and pressurizing are performed between the stacked corrugated sheets (further, the respective flat plates in claim 2) at the time of bonding.
Since the top member is inserted, each corrugated sheet (and further each flat plate) is supported by the top member, so that a necessary and sufficient pressure for bonding can be applied. That is,
As in the above-described conventional example, a situation in which an insufficiently weak pressure can be applied to the bonding can be avoided, and if too much pressure is applied, the corrugated sheets (and even the flat ) And cell walls and cells will be crushed,
The danger of being avoided.

【0031】第2に、もって接着強度が大幅に向上す
る。すなわち、このハニカムコアの製造方法では、上述
した第1のように、接着に際し必要十分な圧力を加える
ことができるので、各波板相互間(請求項2では更に各
波板と平板間)つまりセル壁間が、確実に接着される。
もって、接着強度に優れたハニカムコアが得られ、前述
したこの種従来例のように、圧縮強度や剪断強度に不安
が指摘されるようなこともなくなる。
Second, the adhesive strength is greatly improved. That is, in the method for manufacturing the honeycomb core, as described above, since a necessary and sufficient pressure can be applied at the time of bonding, it can be applied between the corrugated sheets (further, between the corrugated sheets and the flat plate in claim 2). The cell walls are securely bonded.
As a result, a honeycomb core having excellent adhesive strength can be obtained, and there is no fear that the compressive strength or shear strength is pointed out as in the above-described conventional example.

【0032】第3に、接着剤の硬化温度以下で軟化する
材質のものも、使用可能となる。すなわち、このハニカ
ムコアの製造方法では、重積されていた各波板(請求項
2では更に各平板)間が、加熱,加圧されることにより
接着されるが、その際、コマ部材が挿入されているの
で、コマ部材にて各波板(更には各平板)がサポートさ
れている。そこで母材として、接着剤の硬化温度以下で
軟化する材質のものを用いた場合において、接着剤の硬
化温度による加熱にて若干軟化するようなことがあって
も、前述したこの種従来例のように、重積された各波板
(更には各平板)そしてセル壁やセルが、潰れたりする
ことはなく、全体形状が崩れてしまうこともない。もっ
て請求項4のように、接着剤の硬化温度以下で軟化する
材質の母材、つまり比較的低温で加熱成形可能な母材も
使用可能となり、母材の材質の選択幅が広がる。
Third, a material that softens below the curing temperature of the adhesive can be used. In other words, in this method for manufacturing a honeycomb core, the stacked corrugated plates (and the respective flat plates in claim 2) are bonded by heating and pressing, and at this time, the top member is inserted. Therefore, each corrugated sheet (and each flat sheet) is supported by the top member. Therefore, when a material that softens below the curing temperature of the adhesive is used as the base material, even if the material is slightly softened by heating at the curing temperature of the adhesive, the above-described conventional example of this type is used. As described above, the stacked corrugated plates (and each flat plate) and the cell walls and cells are not crushed and the entire shape is not collapsed. Thus, a base material of a material that softens below the curing temperature of the adhesive, that is, a base material that can be formed by heating at a relatively low temperature can be used, and the range of selection of the material of the base material is widened.

【0033】第4に、しかもこれらは簡単容易に実現さ
れる。すなわち、このハニカムコアの製造方法は、コマ
部材を採用した簡単な構成により、上述した第1,第
2,第3の点が容易に実現でき、コスト面にも優れてい
る。
Fourth, and they are easily and easily realized. That is, in the method for manufacturing the honeycomb core, the above-described first, second, and third points can be easily realized by a simple configuration employing the top member, and the cost is excellent.

【0034】更に請求項3では、コマ部材に通電発熱体
を内装したことにより、上述に加え次の効果を発揮す
る。すなわち第5に、接着剤の加熱硬化時間を短縮する
ことができる。つまり、このハニカムコアの製造方法で
は、重積されていた各波板(請求項2では各平板)間が
加熱,加圧により接着されるが、その際、各波板は内部
の空間に挿入されたコマ部材側からも、内装された通電
発熱体にて加熱される。もって、接着に必要な加熱用の
昇温時間が短縮され、接着剤の加熱硬化時間が短縮され
るので、その分、全体的な接着時間そしてハニカムコア
の製造時間も、短縮されるに至る。このように、この種
従来例に存した課題がすべて解決される等、本発明の発
揮する効果は、顕著にして大なるものがある。
In the third aspect, the following effects are exhibited in addition to the above-mentioned effects by providing the top member with the energized heating element. Fifth, it is possible to shorten the heating time of the adhesive. That is, in this method of manufacturing a honeycomb core, the stacked corrugated sheets (each flat plate in claim 2) are bonded by heating and pressing, and at this time, each corrugated sheet is inserted into the internal space. The heated top member is also heated by the built-in energizing heating element. Accordingly, the heating time required for heating required for bonding is shortened, and the heat curing time of the adhesive is shortened, so that the overall bonding time and the manufacturing time of the honeycomb core are also reduced accordingly. As described above, the effects exhibited by the present invention are remarkable and large, for example, all the problems existing in this type of conventional example are solved.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明に係るハニカムコアの製造方法につい
て、その発明の実施の形態の説明に供する斜視図であ
り、(1)図は第1例の要部を示し、(2)図は同第1
例におけるコマ部材を示し、(3)図は第2例の要部を
示し、(4)図は同第2例におけるコマ部材を示す。
FIG. 1 is a perspective view for explaining an embodiment of a method for manufacturing a honeycomb core according to the present invention, in which FIG. 1A shows a main part of a first example, and FIG. First
The top member in the example is shown, FIG. 3 (3) shows the main part of the second example, and FIG. 4 (4) shows the top member in the second example.

【図2】同発明の実施の形態の説明に供する斜視図であ
り、(1)図は第3例におけるコマ部材を示し、(2)
図は第4例におけるコマ部材を示す。
FIGS. 2A and 2B are perspective views for explaining the embodiment of the present invention, and FIG. 2A shows a top member in a third example, and FIG.
The figure shows the top member in the fourth example.

【図3】この種従来例のハニカムコアの製造方法の説明
に供する斜視図であり、(1)図は重積された波板を、
(2)図はその潰れた状態を示し、(3)図は得られた
ハニカムコアを、(4)図はその形状が崩れた状態を示
す。
FIG. 3 is a perspective view for explaining a method for manufacturing a honeycomb core of this type of conventional example, and FIG.
FIG. 2 (2) shows the collapsed state, FIG. 3 (3) shows the obtained honeycomb core, and FIG. 4 (4) shows the collapsed shape.

【図4】一般的なハニカムコアの製造方法の説明に供す
る正面説明図であり、(1)図は、準備された母材を、
(2)図は、波板の成形工程を、(3)図は、成形され
た波板を、(4)図は、波板を重積,接合する工程を示
す。
FIG. 4 is an explanatory front view for explaining a general method for manufacturing a honeycomb core, and FIG.
FIG. 2B shows a corrugated sheet forming step, FIG. 3C shows a formed corrugated sheet, and FIG. 4D shows a step of laminating and joining corrugated sheets.

【図5】ハニカムコアの正面説明図であり、(1)図は
その1例を、(2)図は他の例を示す。
FIGS. 5A and 5B are front explanatory views of a honeycomb core, in which FIG. 1A shows one example and FIG. 5B shows another example.

【符号の説明】[Explanation of symbols]

1 ハニカムコア 2 波板 3 接着剤 4 セル壁 5 セル 6 母材 7 コルゲート成形装置 8 ラック 9 コマ部材 10 通電発熱体 11 平板 A 空間 DESCRIPTION OF SYMBOLS 1 Honeycomb core 2 Corrugated sheet 3 Adhesive 4 Cell wall 5 Cell 6 Base material 7 Corrugating device 8 Rack 9 Top member 10 Electric heating element 11 Flat plate A space

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】 母材をコルゲート成形装置にて、波形の
凹凸が連続的に折曲形成された波板に成形した後、複数
枚の該波板を、順次波形の半ピッチ分ずつずらし底部と
頂部とを合わせる位置関係で、接着剤を介装しつつ重積
すると共に、 各該波板間に形成された空間に、該空間の断面形状に見
合った断面形状のコマ部材を密に挿入してから、該接着
剤の硬化温度にて加熱すると共に加圧することにより、
各該波板間を接着させ、もって、各該波板をセル壁とす
ると共に各該空間をセルとし、各該セル壁にて区画形成
された中空柱状のセルの平面的集合体よりなるハニカム
コアを得ること、を特徴とするハニカムコアの製造方
法。
After a base material is formed into a corrugated sheet in which corrugations are continuously bent by a corrugating apparatus, a plurality of corrugated sheets are sequentially shifted by a half pitch of a corrugated sheet to form a bottom portion. In the positional relationship where the top and the top are aligned, the stacking is performed while interposing the adhesive, and the top member having the cross-sectional shape corresponding to the cross-sectional shape of the space is densely inserted into the space formed between the corrugated plates. Then, by heating and pressing at the curing temperature of the adhesive,
A honeycomb formed of a planar aggregate of hollow columnar cells defined by the cell walls while adhering the corrugated sheets to each of the corrugated sheets as cell walls and each of the spaces as cells. A method for manufacturing a honeycomb core, comprising obtaining a core.
【請求項2】 母材をコルゲート成形装置にて、波形の
凹凸が連続的に折曲形成された波板に成形した後、複数
枚の該波板と平坦な平板とを、接着剤を介装しつつ順次
重積すると共に、その際、各該波板に関しては、順次波
形の半ピッチ分ずつずらし底部と頂部とを対向させる位
置関係に配し、 かつ、各該波板と平板間に形成された空間に、該空間の
断面形状に見合った断面形状のコマ部材を密に挿入して
から、該接着剤の硬化温度にて加熱すると共に加圧する
ことにより、各該波板と平板間を接着させ、もって、各
該波板と平板をセル壁とすると共に各該空間をセルと
し、各該セル壁にて区画形成された中空柱状のセルの平
面的集合体よりなるハニカムコアを得ること、を特徴と
するハニカムコアの製造方法。
2. A base material is formed into a corrugated sheet in which corrugations are continuously bent by a corrugating apparatus, and a plurality of the corrugated sheets and a flat plate are bonded with an adhesive. While stacking sequentially while mounting, with respect to each corrugated sheet, it is sequentially shifted by a half pitch of the waveform and arranged in a positional relationship in which the bottom and the top are opposed to each other, and between each corrugated sheet and the flat plate. After tightly inserting a top member having a cross-sectional shape corresponding to the cross-sectional shape of the space into the formed space, heating and pressurizing at the curing temperature of the adhesive, the gap between each corrugated plate and the flat plate is increased. To form a honeycomb core consisting of a planar aggregate of hollow columnar cells defined by the cell walls, with each of the corrugated plates and the flat plate being a cell wall and each of the spaces being a cell. And a method for manufacturing a honeycomb core.
【請求項3】 請求項1又は2記載のハニカムコアの製
造方法において、該コマ部材に通電発熱体が内装されて
いること、を特徴とするハニカムコアの製造方法。
3. The method for manufacturing a honeycomb core according to claim 1, wherein an electric heating element is provided inside the top member.
【請求項4】 請求項1又は2記載のハニカムコアの製
造方法において、該母材として、該接着剤の硬化温度以
下で軟化する材質のものが用いられていること、を特徴
とするハニカムコアの製造方法。
4. The method for manufacturing a honeycomb core according to claim 1, wherein the base material is made of a material that softens at a temperature lower than a curing temperature of the adhesive. Manufacturing method.
JP8178430A 1996-06-19 1996-06-19 Production of honeycomb core Pending JPH106416A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8178430A JPH106416A (en) 1996-06-19 1996-06-19 Production of honeycomb core

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8178430A JPH106416A (en) 1996-06-19 1996-06-19 Production of honeycomb core

Publications (1)

Publication Number Publication Date
JPH106416A true JPH106416A (en) 1998-01-13

Family

ID=16048380

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8178430A Pending JPH106416A (en) 1996-06-19 1996-06-19 Production of honeycomb core

Country Status (1)

Country Link
JP (1) JPH106416A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014008735A (en) * 2012-07-02 2014-01-20 Showa Aircraft Ind Co Ltd Production method of fiber-reinforced plastic honeycomb core
JP2014037101A (en) * 2012-08-17 2014-02-27 Showa Aircraft Ind Co Ltd Production method of fiber-reinforced plastic made honeycomb core
WO2022249260A1 (en) * 2021-05-25 2022-12-01 三菱電機株式会社 Ribbon laminate, honeycomb core precursor, honeycomb core, cylindrical structure, central cylinder for satellites, and method for producing ribbon laminate
CN117900347A (en) * 2024-03-15 2024-04-19 常州弘建新材料有限公司 Honeycomb aluminum plate corner profiling equipment

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014008735A (en) * 2012-07-02 2014-01-20 Showa Aircraft Ind Co Ltd Production method of fiber-reinforced plastic honeycomb core
JP2014037101A (en) * 2012-08-17 2014-02-27 Showa Aircraft Ind Co Ltd Production method of fiber-reinforced plastic made honeycomb core
WO2022249260A1 (en) * 2021-05-25 2022-12-01 三菱電機株式会社 Ribbon laminate, honeycomb core precursor, honeycomb core, cylindrical structure, central cylinder for satellites, and method for producing ribbon laminate
CN117900347A (en) * 2024-03-15 2024-04-19 常州弘建新材料有限公司 Honeycomb aluminum plate corner profiling equipment
CN117900347B (en) * 2024-03-15 2024-05-24 常州弘建新材料有限公司 Honeycomb aluminum plate corner profiling equipment

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