JP4585723B2 - Method for manufacturing perforated honeycomb panel - Google Patents

Method for manufacturing perforated honeycomb panel Download PDF

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Publication number
JP4585723B2
JP4585723B2 JP2001283888A JP2001283888A JP4585723B2 JP 4585723 B2 JP4585723 B2 JP 4585723B2 JP 2001283888 A JP2001283888 A JP 2001283888A JP 2001283888 A JP2001283888 A JP 2001283888A JP 4585723 B2 JP4585723 B2 JP 4585723B2
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Japan
Prior art keywords
plate
honeycomb
forming jig
honeycomb panel
manufacturing
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Expired - Fee Related
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JP2001283888A
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Japanese (ja)
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JP2003089161A (en
Inventor
若富 中根
智 阿部
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.)
Nikkiso Co Ltd
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Nikkiso Co Ltd
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Filing date
Publication date
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Priority to JP2001283888A priority Critical patent/JP4585723B2/en
Publication of JP2003089161A publication Critical patent/JP2003089161A/en
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Publication of JP4585723B2 publication Critical patent/JP4585723B2/en
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  • Soundproofing, Sound Blocking, And Sound Damping (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は、面状部材とハニカム部材とを積層した積層体を製造する方法に関し、特に板状部材が、多数の孔が明けられた孔明き部材である孔明きハニカムパネルの製造方法に関する。
【0002】
【従来の技術】
軽量、高強度な構造材としてハニカムパネルが知られている。ハニカムパネルは、蜂の巣状のハニカム部材を、2枚の板状部材で挟むようにして構成されている。また、本明細書においては、ハニカム部材を構成する面に直交する面における、ハニカム部材の断面は蜂の巣状の六角形に限らず、他の多角形も含む。このようなハニカムパネルに関し、吸音部材として用いられる場合は、吸音特性を向上させるために、板状部材の多数の孔を明けることが行われている。
【0003】
このようなハニカムパネルは、従来、孔の明いた板状材料を加圧成形して板状部材を得、その後板状部材とハニカム材料を結合させて製造されていた。
【0004】
【発明が解決しようとする課題】
前述のように、従来の孔明きハニカムパネルの製造方法は、板状材料の成形とハニカム材料と板状材料の一体化を別途加圧成形にて行ったり、板状材料に多数の孔を明けるために、機械加工を施したり、ピン式の治具による孔明けでは、治具の曲面からの脱型が困難だったりして、製造工程数が多くなりコスト高となっていた。
【0005】
本発明は前述の問題点を解決するためになされたものであり、孔明きハニカムパネルの安価な製造方法を提供することを目的とする。
【課題を解決するための手段】
前述の課題を解決するために、本発明にかかる孔明きハニカムパネルの製造方法は、可撓性シートに複数の突起を立設した成形治具に、前記突起が貫通する状態に硬化前の第1の板状材料を載置し、この第1の板状材料に、同じく硬化前のハニカム材料を積層し、さらにその上に第2の板状材料を載置して、これらの材料を前記成形治具と一体の状態で硬化、一体成形するものである。一体成形後、成形治具を取り外す。この際、成形治具のシートの可撓性により、この成形治具を成形後のハニカムパネルから容易に取り外すことができる。
【0006】
また、ハニカム材料を載置する前に、前記成形治具上に載置された第1の板状材料の表面を平滑化し、また前記成形治具の突起先端が突出しないようにするカバーシートを、第1の板状材料に重ねて載置し、これらを一体にして加圧するようにすることができる。
【0007】
【発明の実施の形態】
以下、本発明の実施の形態(以下実施形態という)を、図面に従って説明する。図1は、本実施形態の孔明きハニカムパネルの製造方法の概略工程を示す図である。成形治具10は、可撓性を有する板状のシート12に、金属などの硬質の材料からなるピン14が埋め込まれて形成されている(図1a)。ピン14はシート12の表面から突出し、成形治具の突起となっている。この成形治具10の突起が設けられた面に、ハニカムパネルの一方の板状部材となる、硬化前の樹脂材料である、板状材料16を載置する(図1b)。このとき、ピン14の板状材料16に埋まる部分は略円筒形であり、板状材料16より突出した部分は、略円錐状となっている。これにより、板状材料16の孔の径を、その長さにわたってほぼ一定とし、板状材料16に対する孔明けも行えるようにしている。
【0008】
さらに、板状材料16上に、カバーシート18を重ねて載置する(図1c)。カバーシート18は可撓性を有し、板状材料16の上面から突出したピン14の先端を覆うように配置される。成形治具10、板状材料16およびカバーシート18を積層した状態で、これらを真空バッグ20内に納め、加圧を行う(図1d)。この加圧によって板状材料の表面が平滑化される。
【0009】
板状材料16などを真空バッグ20から取り出した後、カバーシート18を取り外し、板状材料16上にハニカム材料22を載置する(図1e)。ハニカム材料22の断面形状は文字通り六角形の蜂の巣状となっている。しかし、断面形状については、これに限らず、他の多角形を組み合わせた形状とすることも可能である。
【0010】
このハニカム材料22の上にさらに重ねて第2の板状材料24を載置し、第1と第2の板状材料16,24にてハニカム材料22を挟んだ状態とする(図1f)。積層された状態で、真空バッグ26内に納め、加圧および加熱し、第1および第2の板状材料16,24を構成する樹脂を硬化させる(図1g)。そして、真空バッグ26より取り出し、成形治具10を引き剥がすようにして取り外すことにより、ハニカム部材28を、孔明き板状部材30と孔なしの板状部材32とで挟んだハニカムパネル34を得る(図1h)。前述のように成形治具10のシート12は可撓性を有しているために、硬化したハニカムパネル34より容易に取り外すことができる。
【0011】
以上の製造方法によれば、材料の成形硬化を行う工程が1工程で済み、製造コストを削減することができる。
【0012】
図2は、成形治具10の製作工程の一例を示す図である。枠36と、これの内側に立設したピン型38からなる、金属製または樹脂製の第1の型40を準備する(図2a)。この型40に、樹脂を流し込み、硬化させる(図2b)。この樹脂は、硬化後も可撓性を有する材料である。この可撓性を利用して、型40より取り外し、前述した可撓性のシート12を得る(図2c)。
【0013】
次に、シート12を、第2の型44内に配置する(図2d)。第2の型44には、ピン型38によって形成されたシート12の孔46に対応する位置に略円錐状の穴48が設けられている。よって、第2の型44内にシート12が配置されたときに、シートの穴46と型の穴48は、連続した一つの穴となる。そこへ、溶融した金属50を流し込む(図2d)。金属50は、シートの孔46と型の穴48を埋める程度の量を流し込むのが好ましい。金属50が硬化して、前述のピン14となり、第2の型44から外して成形治具10を得る(図2e)。
【図面の簡単な説明】
【図1】本実施形態にかかる孔明きハニカムパネルの製造工程を示す図である。
【図2】成形治具10の製造工程を示す図である。
【符号の説明】
10 成形治具、12 可撓性のシート、14 ピン(突起)、16 第1の板状材料、18 カバーシート、20 真空バッグ、22 ハニカム材料、24第2の板状材料、26 真空バッグ、28 ハニカム部材、30 孔明き板状部材、32 板状部材、34 ハニカムパネル。
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a method for manufacturing a laminate in which a planar member and a honeycomb member are laminated, and more particularly to a method for manufacturing a perforated honeycomb panel in which a plate-like member is a perforated member having a large number of holes.
[0002]
[Prior art]
Honeycomb panels are known as lightweight and high-strength structural materials. The honeycomb panel is configured such that a honeycomb-like honeycomb member is sandwiched between two plate-like members. Further, in the present specification, the cross section of the honeycomb member on the surface orthogonal to the surface constituting the honeycomb member is not limited to the honeycomb-shaped hexagon but also includes other polygons. When such a honeycomb panel is used as a sound absorbing member, a large number of holes in the plate-like member are drilled in order to improve sound absorbing characteristics.
[0003]
Conventionally, such a honeycomb panel has been manufactured by press-molding a plate-like material with a hole to obtain a plate-like member, and then bonding the plate-like member and the honeycomb material.
[0004]
[Problems to be solved by the invention]
As described above, in the conventional method for manufacturing a perforated honeycomb panel, the plate-shaped material is molded and the honeycomb material and the plate-shaped material are integrated separately by pressure molding, or a large number of holes are formed in the plate-shaped material. For this reason, when machining or drilling with a pin-type jig, it is difficult to remove from the curved surface of the jig, resulting in an increase in the number of manufacturing steps and high costs.
[0005]
The present invention has been made to solve the above-described problems, and an object thereof is to provide an inexpensive method for manufacturing a perforated honeycomb panel.
[Means for Solving the Problems]
In order to solve the above-described problem, a method for manufacturing a perforated honeycomb panel according to the present invention is the first before the curing in a state where the protrusion penetrates a forming jig in which a plurality of protrusions are erected on a flexible sheet. The first plate material is placed, the honeycomb material before being cured is laminated on the first plate material, and the second plate material is placed thereon. It is cured and integrally molded in a state integrated with the molding jig. After the integral molding, remove the molding jig. At this time, due to the flexibility of the sheet of the forming jig, the forming jig can be easily detached from the formed honeycomb panel.
[0006]
Further, before placing the honeycomb material, a cover sheet for smoothing the surface of the first plate-like material placed on the forming jig and preventing the protrusion tip of the forming jig from protruding is provided. The first plate-like material can be placed on top of each other and pressed together.
[0007]
DETAILED DESCRIPTION OF THE INVENTION
Hereinafter, embodiments of the present invention (hereinafter referred to as embodiments) will be described with reference to the drawings. FIG. 1 is a diagram showing a schematic process of a method for manufacturing a perforated honeycomb panel of the present embodiment. The forming jig 10 is formed by embedding pins 14 made of a hard material such as metal in a plate-like sheet 12 having flexibility (FIG. 1a). The pin 14 protrudes from the surface of the sheet 12 and is a protrusion of the forming jig. On the surface of the forming jig 10 on which the protrusions are provided, a plate-like material 16 which is one of the plate-like members of the honeycomb panel and is a resin material before curing is placed (FIG. 1b). At this time, the portion embedded in the plate-like material 16 of the pin 14 has a substantially cylindrical shape, and the portion protruding from the plate-like material 16 has a substantially conical shape. Thereby, the diameter of the hole of the plate-like material 16 is made almost constant over the length thereof, and the hole for the plate-like material 16 can be made.
[0008]
Further, the cover sheet 18 is placed on the plate material 16 (FIG. 1c). The cover sheet 18 has flexibility and is disposed so as to cover the tips of the pins 14 protruding from the upper surface of the plate-like material 16. In a state where the forming jig 10, the plate-like material 16 and the cover sheet 18 are laminated, these are placed in the vacuum bag 20 and pressurized (FIG. 1d). By this pressurization, the surface of the plate-like material is smoothed.
[0009]
After the plate-like material 16 and the like are taken out from the vacuum bag 20, the cover sheet 18 is removed, and the honeycomb material 22 is placed on the plate-like material 16 (FIG. 1e). The cross-sectional shape of the honeycomb material 22 is literally a hexagonal honeycomb. However, the cross-sectional shape is not limited to this, and may be a shape combining other polygons.
[0010]
The second plate-like material 24 is further stacked on the honeycomb material 22 so that the honeycomb material 22 is sandwiched between the first and second plate-like materials 16 and 24 (FIG. 1f). In the laminated state, it is placed in the vacuum bag 26, and pressurized and heated to cure the resin constituting the first and second plate-like materials 16 and 24 (FIG. 1g). Then, the honeycomb panel 34 is obtained by sandwiching the honeycomb member 28 between the perforated plate member 30 and the plate member 32 without holes by taking out the vacuum bag 26 and removing the forming jig 10 by peeling off. (FIG. 1h). As described above, since the sheet 12 of the forming jig 10 has flexibility, it can be easily removed from the cured honeycomb panel 34.
[0011]
According to the above manufacturing method, the process of molding and hardening the material is only one process, and the manufacturing cost can be reduced.
[0012]
FIG. 2 is a diagram illustrating an example of a manufacturing process of the forming jig 10. A first die 40 made of metal or resin, which is composed of a frame 36 and a pin die 38 erected on the inside thereof, is prepared (FIG. 2a). A resin is poured into the mold 40 and cured (FIG. 2b). This resin is a flexible material even after curing. Using this flexibility, the flexible sheet 12 is removed from the mold 40 to obtain the flexible sheet 12 described above (FIG. 2c).
[0013]
Next, the sheet 12 is placed in the second mold 44 (FIG. 2d). The second die 44 is provided with a substantially conical hole 48 at a position corresponding to the hole 46 of the sheet 12 formed by the pin die 38. Therefore, when the sheet 12 is disposed in the second mold 44, the sheet hole 46 and the mold hole 48 become one continuous hole. There, the molten metal 50 is poured (FIG. 2d). The metal 50 is preferably poured in an amount sufficient to fill the hole 46 in the sheet and the hole 48 in the mold. The metal 50 is cured to become the above-described pin 14 and is removed from the second mold 44 to obtain the forming jig 10 (FIG. 2e).
[Brief description of the drawings]
FIG. 1 is a diagram showing a manufacturing process of a perforated honeycomb panel according to the present embodiment.
FIG. 2 is a diagram showing a manufacturing process of the forming jig 10;
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 10 Forming jig, 12 Flexible sheet, 14 Pin (projection), 16 1st plate-shaped material, 18 Cover sheet, 20 Vacuum bag, 22 Honeycomb material, 24 2nd plate-shaped material, 26 Vacuum bag, 28 honeycomb member, 30 perforated plate member, 32 plate member, 34 honeycomb panel.

Claims (2)

可撓性シートに複数の突起を立設した成形治具に、前記突起が貫通する状態に板状材料を載置する工程と、
前記第1の板状材料を、前記成形治具と共に加圧する工程と、
前記第1の板状材料の上にハニカム材料を載置する工程と、
前記ハニカム材料の上にさらに第2の板状材料を載置する工程と、
前記第1および第2の板状材料ならびに前記ハニカム材料を、前記成形治具と一体の状態で、硬化させ、一体成形する工程と、
前記一体成形された第1および第2の板状材料およびハニカム材料から、前記成形治具を取り外し、孔明きハニカムパネルを得る工程と、
を有する、孔明きハニカムパネルの製造方法。
Placing a plate-like material in a state where the protrusion penetrates a forming jig in which a plurality of protrusions are erected on a flexible sheet; and
Pressurizing the first plate material together with the forming jig;
Placing a honeycomb material on the first plate-like material;
Placing a second plate-like material on the honeycomb material;
Curing and integrally molding the first and second plate-like materials and the honeycomb material in a state of being integrated with the forming jig;
Removing the forming jig from the integrally formed first and second plate-like materials and honeycomb material to obtain a perforated honeycomb panel;
A method for manufacturing a perforated honeycomb panel.
請求項1に記載の孔明きハニカムパネルの製造方法であって、前記成形治具に前記第1の板状材料を載置する工程の後に、さらに前記成形治具の突起の先端が突出しないように、前記第1の板状材料に重ねてカバーシートを載置する工程を有し、
前記第1の板状材料と成形治具を共に加圧する工程は、前記カバーシートも含めて加圧する工程である、
孔明きハニカムパネルの製造方法。
2. The method for manufacturing a perforated honeycomb panel according to claim 1, wherein a tip of a protrusion of the forming jig is not further protruded after the step of placing the first plate-like material on the forming jig. And a step of placing a cover sheet on the first plate-like material,
The step of pressurizing both the first plate-shaped material and the forming jig is a step of pressurizing including the cover sheet.
A method for manufacturing a perforated honeycomb panel.
JP2001283888A 2001-09-18 2001-09-18 Method for manufacturing perforated honeycomb panel Expired - Fee Related JP4585723B2 (en)

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Application Number Priority Date Filing Date Title
JP2001283888A JP4585723B2 (en) 2001-09-18 2001-09-18 Method for manufacturing perforated honeycomb panel

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JP4585723B2 true JP4585723B2 (en) 2010-11-24

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54144488A (en) * 1978-05-01 1979-11-10 Boeing Wichita Co Sound absorbing panel
JPS5538595A (en) * 1978-09-11 1980-03-18 Boeing Wichita Co Producing cellular core having internal partitions
JPH106417A (en) * 1996-03-28 1998-01-13 Boeing Co:The Improved panel structure and process for producing the same
JPH10245908A (en) * 1997-03-06 1998-09-14 Sekisui Chem Co Ltd Sound absorbing material

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54144488A (en) * 1978-05-01 1979-11-10 Boeing Wichita Co Sound absorbing panel
JPS5538595A (en) * 1978-09-11 1980-03-18 Boeing Wichita Co Producing cellular core having internal partitions
JPH106417A (en) * 1996-03-28 1998-01-13 Boeing Co:The Improved panel structure and process for producing the same
JPH10245908A (en) * 1997-03-06 1998-09-14 Sekisui Chem Co Ltd Sound absorbing material

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