JPH0324941A - Hollow structural body and preparation thereof - Google Patents
Hollow structural body and preparation thereofInfo
- Publication number
- JPH0324941A JPH0324941A JP16115689A JP16115689A JPH0324941A JP H0324941 A JPH0324941 A JP H0324941A JP 16115689 A JP16115689 A JP 16115689A JP 16115689 A JP16115689 A JP 16115689A JP H0324941 A JPH0324941 A JP H0324941A
- Authority
- JP
- Japan
- Prior art keywords
- honeycomb
- honeycomb material
- adhesive member
- wound around
- mandrel
- 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.)
- Granted
Links
- 239000000463 material Substances 0.000 claims abstract description 130
- 230000002093 peripheral effect Effects 0.000 claims abstract description 23
- 238000000034 method Methods 0.000 claims abstract description 18
- 239000012790 adhesive layer Substances 0.000 claims description 15
- 238000004519 manufacturing process Methods 0.000 claims description 8
- 239000000853 adhesive Substances 0.000 abstract description 29
- 230000001070 adhesive effect Effects 0.000 abstract description 29
- 229920005989 resin Polymers 0.000 abstract description 16
- 239000011347 resin Substances 0.000 abstract description 16
- 230000000694 effects Effects 0.000 abstract description 9
- 238000004804 winding Methods 0.000 abstract description 4
- 239000012783 reinforcing fiber Substances 0.000 abstract description 3
- 238000010438 heat treatment Methods 0.000 abstract description 2
- 239000004745 nonwoven fabric Substances 0.000 abstract description 2
- 239000011162 core material Substances 0.000 description 11
- 238000009413 insulation Methods 0.000 description 5
- 239000006260 foam Substances 0.000 description 3
- 239000010410 layer Substances 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 2
- 238000004378 air conditioning Methods 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000004760 aramid Substances 0.000 description 2
- 229920003235 aromatic polyamide Polymers 0.000 description 2
- 238000009730 filament winding Methods 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- 229920006305 unsaturated polyester Polymers 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 229920002978 Vinylon Polymers 0.000 description 1
- 239000002775 capsule Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000012770 industrial material Substances 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 229920000058 polyacrylate Polymers 0.000 description 1
- 229920001225 polyester resin Polymers 0.000 description 1
- 239000004645 polyester resin Substances 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229920001187 thermosetting polymer Polymers 0.000 description 1
Landscapes
- Making Paper Articles (AREA)
- Laminated Bodies (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野)
本発明は、冷凍車及び保冷車等の荷物積載部分の車体や
空調ダクト、そのほかコンテナの躯体等に用いられる中
空構造体に関する6
(従来の技術)
従来、例えば、冷凍車及び保冷車等の荷物積載部分の周
壁としては、発泡ウレタン等の発泡部材をコアとして、
その表裏両面をアルミパネルで挟んだ構造のものが用い
られていた。[Detailed Description of the Invention] (Industrial Application Field) The present invention relates to a hollow structure used for the body of a cargo loading section of a refrigerated truck or a refrigerated truck, an air conditioning duct, or the frame of a container. Technology) Conventionally, for example, the peripheral wall of the cargo loading part of a refrigerated truck or a refrigerated truck has been made of a foamed material such as urethane foam as a core.
A structure in which both the front and back sides were sandwiched between aluminum panels was used.
この場合,壁と壁との間には隙間が生じ易かったり、ま
た、壁と壁とを接続するためにその部分に金属性のフレ
ームを構成する部材等が必要となり、この部材を介して
外部の熱が伝達されたりして、保温性に問題があり,ま
た、壁と壁とを、その間に隙間が生じないように密着さ
せるのに手間を要していた。In this case, gaps are likely to occur between the walls, and in order to connect the walls, a member that constitutes a metal frame is required at that part, and the external There was a problem with heat retention due to the heat being transferred, and it also took a lot of effort to make sure the walls were in close contact with each other so that there were no gaps between them.
そこで、このような問題を解決するために、周壁を継ぎ
目のない一体構造として中空構造体を形成することが考
えられる。Therefore, in order to solve such problems, it is conceivable to form a hollow structure with a peripheral wall having a seamless integral structure.
このような中空構造体としては、例えば、工業材料19
87. VOL. 35、NO.7(昭和62年5月2
0日、日刊工業新聞社発行)の第191頁に記載されて
いるようなものが知られている。As such a hollow structure, for example, industrial material 19
87. VOL. 35, NO. 7 (May 2, 1986)
0, published by Nikkan Kogyo Shimbun), page 191, is known.
この従来の中空構造体は、樹脂が付着したガラス繊維を
マンドレルに巻き付けて硬化させた後、マンドレルを脱
型させるフィラメントワインデインク法により成形され
るちのであり、その周壁はガラス繊維強化プラスチック
(FRP)で一体に形成されている。This conventional hollow structure is formed by the filament winding ink method, in which resin-attached glass fiber is wound around a mandrel and cured, and then the mandrel is removed from the mold.The surrounding wall is made of glass fiber-reinforced plastic ( It is integrally formed from FRP.
(発明が解決しようとする課題)
しかしながら,上述した従来の中空構造体にあっては、
ガラス繊維の割合が高い(50%)ために、比重が重い
。(Problem to be solved by the invention) However, in the conventional hollow structure described above,
It has a high specific gravity due to the high proportion of glass fiber (50%).
従って,必要な剛性を確保するために周壁の肉厚を厚く
すると、それだけ重量が増える結果になるという問題が
あった。Therefore, there is a problem in that increasing the thickness of the peripheral wall in order to ensure the necessary rigidity results in an increase in weight.
又、周壁がFRPであるため、断熱効果に優れたものと
は言えず、断熱性を有する用途には不向きであるという
問題があった。Further, since the peripheral wall is made of FRP, it cannot be said to have an excellent heat insulating effect, and there is a problem in that it is unsuitable for use with heat insulating properties.
本発明は,上述のような従来の問題に着目して成された
もので、軽量かつ高剛性で、優れた断熱効果を持った中
空構造体とその製造方法を提供することを目的としてい
る。The present invention has been made in view of the above-mentioned conventional problems, and aims to provide a hollow structure that is lightweight, highly rigid, and has an excellent heat insulating effect, and a method for manufacturing the same.
(課題を解決するための手段)
上述の目的を達成する為に、本発明の中空構造体では、
周壁に囲まれて内部に中空部が形成され、前記周壁が、
コアを形成するハニカム材と、このハニカム材の内外両
面を覆う面材とにより形成されている手段とした。(Means for Solving the Problem) In order to achieve the above-mentioned object, the hollow structure of the present invention has the following features:
A hollow part is formed inside surrounded by a peripheral wall, and the peripheral wall is
The means is formed by a honeycomb material forming a core and face materials covering both the inner and outer surfaces of the honeycomb material.
また、本発明では、この中空構造体を製造するにあたり
、マンドレルに内側面材を巻き付け、次に、前記内側面
材との間に接着層を介在してこの内側面材の上からハニ
カム材を巻き付けて接着させ,次に、前記ハニカム材の
表面との間に接着層を介在してこのハニカム材の上から
外側面材を巻き付けて接着させ、最後に、前記接着層の
硬化後、積層状態のハニカム材及び内外面材をマンドレ
ルから脱型させることとした。Further, in the present invention, when manufacturing this hollow structure, the inner wall material is wound around a mandrel, and then an adhesive layer is interposed between the inner wall material and the honeycomb material is placed over the inner wall material. Next, an adhesive layer is interposed between the surface of the honeycomb material, and an outer surface material is wrapped and adhered from above the honeycomb material.Finally, after the adhesive layer is cured, the laminated state is obtained. It was decided to demold the honeycomb material and the inner and outer materials from the mandrel.
(作 用)
本発明では、まず、マンドレルに内側面材を巻き付け、
次に、この内側面材の上から接着層な介在させた状態で
ハニカム材を巻き付けて接着させる。尚、この接着層は
、内側面材を巻き付ける前に予め形成しておいてもよい
し、内側面材を巻き付けた後に、内側面材の外側面もし
くはハニカム材の裏面に形成するようにしてもよい。(Function) In the present invention, first, the inner surface material is wound around the mandrel,
Next, the honeycomb material is wrapped and bonded onto the inner wall material with an adhesive layer interposed therebetween. Note that this adhesive layer may be formed in advance before wrapping the inner wall material, or it may be formed on the outer surface of the inner wall material or the back surface of the honeycomb material after the inner wall material is wrapped. good.
次に、前記ハニカム材の上から接着層を介在させた状態
で外側面材を巻き付けて接着させる。この場合も、接着
層は、ハニカム材を巻き付ける前にハニカム材の表面に
形成してもよいし、ハニカム材を巻き付けた後に、ハニ
カム材の表面もしくは外側面材の裏面に形成するように
してもよい。Next, the outer surface material is wrapped and bonded onto the honeycomb material with an adhesive layer interposed therebetween. In this case as well, the adhesive layer may be formed on the surface of the honeycomb material before the honeycomb material is wrapped, or it may be formed on the surface of the honeycomb material or the back surface of the outer surface material after the honeycomb material is wrapped. good.
そして、最後に、前記接着層の硬化後、積層状態のハニ
カム材及び内外面材をマンドレルから脱型させて中空構
造体を形成する。Finally, after the adhesive layer is cured, the laminated honeycomb material and inner and outer materials are removed from the mandrel to form a hollow structure.
このようにして、ハニカム材をコアとした内外面材によ
り中空構造体を形成するが、先にハニカム材と内外面材
とを積層してそれから中空体を形成するのではなく、マ
ンドレルに巻き付けながら積層するために、ハニカム材
の内外で周差があっても、ハニカム材と両面材との間の
接着面でズレが生しることなく、また,ハニカム材の内
外の変形を最小としながら積層することができる。In this way, a hollow structure is formed using the inner and outer materials with the honeycomb material as the core, but instead of first laminating the honeycomb material and the inner and outer materials and then forming the hollow structure, the hollow structure is formed by winding it around a mandrel. Even if there is a circumference difference between the outside and the outside of the honeycomb material, there will be no slippage between the adhesive surfaces between the honeycomb material and the double-sided materials, and the material will be laminated while minimizing deformation of the inside and outside of the honeycomb material. can do.
また、このようにハニカム材及び両面材を巻き付けなが
ら積層するために、周壁に継ぎ目が生じない。Moreover, since the honeycomb material and the double-sided materials are laminated while being wrapped, no seams are formed on the peripheral wall.
また,本発明の中空構造体は、ハニカム材によって空気
層が形成されているため、断熱性に優れている。Further, the hollow structure of the present invention has an air layer formed of the honeycomb material, and therefore has excellent heat insulation properties.
(実施例) 以下、本発明の実施例を図面により詳述する。(Example) Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings.
第I図は本発明実施例の中空構造体Aを示す断面図であ
って、この中空構造体Aは、例えば、保冷自動車の保冷
室として用いられ、内部に略方Jfgの中空部10が形
成されている。FIG. I is a sectional view showing a hollow structure A according to an embodiment of the present invention. This hollow structure A is used, for example, as a refrigerated chamber of a refrigerated automobile, and a hollow portion 10 of approximately Jfg is formed inside. has been done.
図中1は周壁を示しており、第2図にその部分拡大図を
示している。Reference numeral 1 in the figure indicates a peripheral wall, and FIG. 2 shows a partially enlarged view of the peripheral wall.
この周壁lは、ハニカム材2をコアとすると共に,その
内外両面に接着層としての内側接着部材3及び外側接着
部材4を介して内側面材5と外側面材6を接着させて形
成されている。This peripheral wall 1 is formed by using the honeycomb material 2 as a core and adhering an inner wall material 5 and an outer wall material 6 to the inner and outer surfaces of the honeycomb material 2 through an inner adhesive member 3 and an outer adhesive member 4 as adhesive layers. There is.
前記ハニカム材2は、六角断面形状の多数のセルが縦横
に連続して配設された周知構造のもので、例えば、アル
ミ板,紙,板.アラミド樹脂板等の板材により形成され
ている。The honeycomb material 2 has a well-known structure in which a large number of cells each having a hexagonal cross-section are arranged in series vertically and horizontally, and is made of, for example, an aluminum plate, paper, plate, etc. It is formed from a plate material such as an aramid resin plate.
前記内外両接着部材3.4は、浸透性を有する基材に樹
脂が含浸されたものが用いられ、例えば、基材としては
、紙や不織布(ポリエステル樹脂やビニロン樹脂等で、
目付量30〜60g/m”)が用いられ、樹脂としては
、不飽和ポリエステルに硬質ウレタンフォーム用システ
ム材を3:l〜6:lの範囲(重量比)で混合したもの
が使用されている。尚、両接着部材3.4は、内外両面
材5.6をハニカム材2に接着するためのものであり、
この両接着部材3.4の代わりに、ただ単にこの部分に
接着材を塗って接着層を形成するようにしてもよい.
前記内外両面材5.6は、強化繊維に樹脂を含浸させて
形成したFRP板により形成され、例えば、強化繊維と
しては、ガラス.カーボン.アラミド.ポリアクレレー
ト等の繊維材が用いられ、樹脂としては、不飽和ポリエ
ステルやエポキシ等の熱硬化性樹脂が用いられる。The inner and outer adhesive members 3.4 are made of a permeable base material impregnated with resin. For example, the base material may be paper or nonwoven fabric (polyester resin, vinylon resin, etc.).
The resin used is a mixture of unsaturated polyester and rigid urethane foam system material in a range of 3:l to 6:l (weight ratio). Note that both adhesive members 3.4 are for bonding the inner and outer surfaces 5.6 to the honeycomb material 2,
Instead of both adhesive members 3.4, an adhesive layer may be formed by simply applying an adhesive to these parts. The inner and outer surfaces 5.6 are formed of FRP boards made by impregnating reinforcing fibers with resin. For example, the reinforcing fibers may include glass. carbon. Aramid. A fiber material such as polyacrylate is used, and a thermosetting resin such as unsaturated polyester or epoxy is used as the resin.
次に、前記中空構造体Aの製造方法について、順を追っ
て説明する。Next, a method for manufacturing the hollow structure A will be explained step by step.
この製造方法は、内側面材5の巻付工程(第3図)、内
側接着部材3の巻付工程(第4図)、ハニカム材2の巻
付工程(第6図〜第9図)、外測接着部材4の巻付工程
、外側面材6の巻付工程、硬化工程,脱型工程の順に行
なわれる。This manufacturing method includes a step of wrapping the inner side material 5 (FIG. 3), a step of wrapping the inner adhesive member 3 (FIG. 4), a step of wrapping the honeycomb material 2 (FIGS. 6 to 9), The steps of wrapping the external adhesive member 4, wrapping the outer surface material 6, curing, and demolding are performed in this order.
まず、内側面材5の巻付工程では、第3図に示すように
、強化繊維のテープ材50又はシート材5l又は糸材5
2を繰り出しながら樹脂153に通して樹脂54を含浸
させ、これをマンドレルMに面を成すように巻き付ける
。First, in the process of wrapping the inner side material 5, as shown in FIG.
2 is passed through the resin 153 while being fed out to be impregnated with the resin 54, and this is wound around the mandrel M so as to form a surface.
次に、内測接青部材3の巻付工程では、第4図に示すよ
うに、紙や不織布による基材30を繰り出しながら樹脂
槽3lに通して樹脂32を含浸させ、これを前記内測面
材5の上から巻き付ける。Next, in the step of winding the inner blue member 3, as shown in FIG. Wrap it around the top of the facing material 5.
尚、この内側接着部材3の巻付工程は第5図に示すよう
に、前記内側面材5の巻付工程と同時に行なっでも良い
。The process of wrapping the inner adhesive member 3 may be performed simultaneously with the process of wrapping the inner side member 5, as shown in FIG.
その後に行うハニカム材2の巻付工程では、前記内側接
着部材3上からハニカム材2を巻き付けるもので、例え
ば第6図〜第9図に示すような3通りの方法がある。In the subsequent step of wrapping the honeycomb material 2, the honeycomb material 2 is wound from above the inner adhesive member 3, and there are three methods as shown in FIGS. 6 to 9, for example.
第6図の方法は、テープ状に形成されたハニカム材2を
展張して、これを螺旋状に巻き付けていくものである。In the method shown in FIG. 6, a tape-shaped honeycomb material 2 is stretched and wound in a spiral manner.
又、第7図の方法は、マンドレルMの長さに対応した広
幅のハニカム材2を展張して、これを全体的に巻き付け
るちのである。Further, in the method shown in FIG. 7, a wide honeycomb material 2 corresponding to the length of the mandrel M is stretched and wrapped around the entire honeycomb material.
尚、前記第6図及び第7図の方法の場合、第8図に示す
ように、ハニカム材2の片面に紙や不織布等のシート材
20を予め接着して、このシート材20が内側になるよ
うにして巻き付けている。In the case of the method shown in FIGS. 6 and 7, as shown in FIG. I wrap it so that it looks like this.
これはハニカム材2のセルが巻き付けに伴って開かない
ように規制する為の変形防止手段である。This is a deformation prevention means to prevent the cells of the honeycomb material 2 from opening as the honeycomb material 2 is wound.
又、第9図の方法は、(a)に示す未展張のハニカムブ
ロック2を、(b)に示すように展張方向の端面同士で
接着して筒状に形成し、(c)に示すように、これをあ
らかじめ内側面材5及び内側接着部材3を巻き付けたマ
ンドレルMの一端側から被せるようにして内側面材5の
上に巻き付け、この巻付状態において展張状態となるよ
うになっている。この場合、未展張のハニカムブロック
2は展張時に170%近く伸びるので、この伸び率を計
算に入れてハニカムブロック2の長さを決定しておく。In addition, the method shown in FIG. 9 involves forming the unexpanded honeycomb block 2 shown in (a) into a cylindrical shape by bonding the end faces in the expanding direction as shown in (b), and then forming the unexpanded honeycomb block 2 shown in (c) Then, this is wrapped around the inner wall material 5 so as to cover it from one end side of the mandrel M on which the inner wall material 5 and the inner adhesive member 3 have been wound beforehand, and in this wrapped state, it is in an expanded state. . In this case, since the unexpanded honeycomb block 2 expands by nearly 170% when expanded, the length of the honeycomb block 2 is determined by taking this elongation rate into account.
尚、ハニカム材2については、第10図に示すように展
張前において種々の加工を施すことが可能であり、図中
(イ)部は溝21を切削加工した例、(口)部はアール
22を切削加工した例、(ハ)部は別部材23をインサ
ート加工した例である.
次に行う外側接着部材4の巻付工程では、前記内側接着
部材3の巻付工程と同様にして,ハニカム材2の上から
外側接着部材4を巻き付ける。The honeycomb material 2 can be processed in various ways before being expanded, as shown in Fig. 10. In the figure, the (A) part is an example where the grooves 21 are cut, and the (mouth) part is an example where the grooves 21 are cut. 22 is cut, and part (c) is an example in which another member 23 is inserted. In the next step of wrapping the outer adhesive member 4, the outer adhesive member 4 is wound over the honeycomb material 2 in the same manner as the wrapping step of the inner adhesive member 3.
さらに、この後に行う外側面材6の巻付工程では、前記
内側面材5の巻付工程と同様にして、外側接着部材4の
上から外側面材6を巻き付けるものである。Furthermore, in the subsequent step of wrapping the outer surface material 6, the outer surface material 6 is wound over the outer adhesive member 4 in the same manner as the step of wrapping the inner surface material 5.
次に硬化工程は、上述した各工程で使用した樹脂を硬化
させるもので、加熱炉等用いて硬化させてもよいし、常
温で硬化させてちよい。Next, in the curing step, the resin used in each step described above is cured, and may be cured using a heating furnace or the like, or may be cured at room temperature.
脱型工程は、最終工程となるもので、硬化工程の後にマ
ンドレルMから脱型することで、内部に中空部lOが形
成された中空構造体Aが成形される。The mold removal step is the final step, and by removing the mold from the mandrel M after the curing step, a hollow structure A having a hollow portion 10 formed therein is molded.
そして、上述のようにして成形された中空構造体Aは、
その周壁lがハニカム材2をコアとし、これをFRPに
よる内外両面材5.6で挟んだサンドイッチ構造となる
為、軽量で高剛性となり、また、ハニカム材2の空気層
によって優れた断熱効果が得られる。さらに、ハニカム
材2及び両面材5.6を巻き付けているため、周壁lの
途中に継ぎ目が生じず,これによっても、さらに断熱性
が向上する。The hollow structure A formed as described above is
The peripheral wall 1 has a sandwich structure with the honeycomb material 2 as a core sandwiched between inner and outer FRP materials 5.6, making it lightweight and highly rigid, and the air layer of the honeycomb material 2 provides excellent heat insulation effect. can get. Furthermore, since the honeycomb material 2 and the double-sided materials 5.6 are wrapped around each other, no seams occur in the middle of the peripheral wall 1, and this also further improves the heat insulation properties.
また、両面材5.6とハニカム材2との間に、基材30
に樹脂32を含浸させた接着部材3.4が介在している
ので、ハニカム材2の巻き付け工程においてハニカム材
2を基材30に圧接させた際に、第2図に示すように、
基材30からハニヵム材30の端面の周辺部分に樹脂3
2がにじみ出し、端面のみを接着するのに比べて強固な
接着力が得られる.
尚、第II図は本発明の応用により成形された構造体B
を示している。この構造体Bは、発泡体を芯材7とし、
この芯材7が周壁8によって囲まれた中空構造体であり
前記周壁8が前記中空構造体Aと同様にハニカム材81
の内外両面に内外接着部材82.83を介して内外面材
84.85を接着して形成されたものとなっている。In addition, between the double-sided material 5.6 and the honeycomb material 2, a base material 30
Since the adhesive member 3.4 impregnated with resin 32 is interposed in the adhesive member 3.4, when the honeycomb material 2 is pressed against the base material 30 in the wrapping process of the honeycomb material 2, as shown in FIG.
Resin 3 is applied from the base material 30 to the peripheral portion of the end face of the honeycomb material 30.
2 oozes out, and a stronger adhesive force is obtained compared to bonding only the end surfaces. Incidentally, FIG. II shows structure B formed by applying the present invention.
It shows. This structure B uses a foam as a core material 7,
This core material 7 is a hollow structure surrounded by a peripheral wall 8, and the peripheral wall 8 is a honeycomb material 81 similar to the hollow structure A.
It is formed by bonding inner and outer surface materials 84 and 85 to both the inner and outer surfaces of the inner and outer surfaces via inner and outer adhesive members 82 and 83.
又、その製造については、マンドレルMの代わりに芯材
7を用い、この芯材7に、内側面材84、内側接着部材
82、ハニカム材81.外側接着部材83.外側面材8
5を順に巻き付け、これを硬化させるもので、この場合
には脱型工程がなく、芯材7はそのまま残すので中空部
は存在しない構造体となる。Regarding its manufacture, a core material 7 is used instead of the mandrel M, and an inner surface material 84, an inner adhesive member 82, a honeycomb material 81 . Outer adhesive member 83. Outer side material 8
5 are wound one after the other and then cured. In this case, there is no demolding step and the core material 7 is left as is, resulting in a structure without any hollow parts.
従って、この構造体Bについても、軽量.高剛性.断熱
性が得られ、その特性を活かしたパネル等に使用できる
。Therefore, this structure B is also lightweight. High rigidity. It provides thermal insulation properties and can be used for panels etc. that take advantage of this property.
以上、本発明の実施例を図面により詳述してきたが、具
体的な構成はこの実施例に限られるものではなく、例え
ば、中空構造体は、保冷屯・冷凍車等の自動車の荷室に
限らず、車両用の空調ダクトやバンパアマチュア、その
他の産業機器や建築物(コンテナ、カプセルハウス)等
に使用できる。Although the embodiments of the present invention have been described above in detail with reference to the drawings, the specific configuration is not limited to these embodiments. It can also be used not only for vehicle air conditioning ducts, bumper armatures, but also for other industrial equipment and buildings (containers, capsule houses), etc.
又、中空部の形状も、方形に限らず、円形、多角形、等
任意であり、この場合、マンドレルの形状が中空部の形
状に対応する。Further, the shape of the hollow portion is not limited to a rectangular shape, but may be any shape such as a circle or a polygon. In this case, the shape of the mandrel corresponds to the shape of the hollow portion.
(発明の効果)
以上説明してきたように、本発明の中空構造体では、ハ
ニカム材をコアとしたため、従来のフィラメントワイン
ディング法による中空構造体に比べて、軽量としながら
高剛性とすることができるし、また、周壁に継ぎ目がな
く、かつ、空気層を有することで、優れた断熱性能が得
られるという効果を有する。(Effects of the Invention) As explained above, since the hollow structure of the present invention uses a honeycomb material as a core, it can be made lighter and more rigid than a hollow structure made by the conventional filament winding method. Furthermore, since the peripheral wall is seamless and has an air layer, it has the effect of providing excellent heat insulation performance.
さらに、上述のように周壁がハニカム材ヲコアとしてい
るため、ハニカム材を展張する前に、必要に応じてハニ
カム材に溝加工やR加工やインサート加工を行うことが
でき、加工応用性に優れているという効果も得られる。Furthermore, as mentioned above, since the peripheral wall is made of honeycomb material as the core, it is possible to perform groove machining, R machining, and insert machining on the honeycomb material as necessary before expanding the honeycomb material, which has excellent processing applicability. You can also get the effect of being there.
また,本発明の製造方法では、内外面材及びハニカム材
を、マンドレルに順に巻き付ける成形方法であるため、
ハニカム材の内外で周差があっても、ハニカム材と両面
材との間の接着面でズレが生じることなく、また、ハニ
カム材の内外の変形を最小としながら積層することがで
きるもので、きれいな仕上がりが得られるという効果が
得られ,加えて、このようにハニカム材及び両面材を巻
きイ4けながら積層するために、周壁に継ぎ目のない中
空構造体を提供することができるという効果が得られる
。In addition, since the manufacturing method of the present invention is a forming method in which the inner and outer surface materials and the honeycomb material are sequentially wound around a mandrel,
Even if there is a difference in circumference between the outside and outside of the honeycomb material, the adhesive surface between the honeycomb material and the double-sided material will not shift, and the honeycomb material can be laminated while minimizing deformation of the inside and outside of the material. This method has the effect that a beautiful finish can be obtained, and in addition, since the honeycomb material and double-sided materials are rolled and laminated in this way, it is possible to provide a hollow structure with no seams on the peripheral wall. can get.
加えて,マンドレルの形状を代えるだけで、中空部の形
状を変化させることができ、造形自由度が高いという効
果も得られる,In addition, the shape of the hollow part can be changed simply by changing the shape of the mandrel, giving the effect of a high degree of freedom in shaping.
【図面の簡単な説明】
第1図は本発明実施例の中空構造体を示す断面図、第2
図は該中空構造体の周壁を示す部分拡大図、第3図〜第
lO図はそれぞれ本発明実施例の製造方法を示す説明図
、第11図は本発明の応用例を示す断面図である。
A・・・中空構造体
1・・・周壁
2・・・ハニカム材
3・・・内側接着部材(接着層)
4・・・外側接着部材(接着層)
5・・・内側面材
6・・・外側面材
10・・・中空部
M・・・マンドレル[Brief Description of the Drawings] Fig. 1 is a sectional view showing a hollow structure according to an embodiment of the present invention;
The figure is a partially enlarged view showing the peripheral wall of the hollow structure, FIGS. 3 to 10 are explanatory views showing the manufacturing method of the embodiment of the present invention, and FIG. 11 is a sectional view showing an application example of the present invention. . A...Hollow structure 1...Peripheral wall 2...Honeycomb material 3...Inner adhesive member (adhesive layer) 4...Outer adhesive member (adhesive layer) 5...Inner side member 6...・Outer side material 10...Hollow part M...Mandrel
Claims (1)
が、コアを形成するハニカム材と、このハニカム材の内
外両面を覆う面材とにより形成されていることを特徴と
する中空構造体。 2)マンドレルに内側面材を巻き付け、 次に、前記内側面材との間に接着層を介在してこの内側
面材の上からハニカム材を巻き付けて接着させ、 次に、前記ハニカム材の表面との間に接着層を介在して
このハニカム材の上から外側面材を巻き付けて接着させ
、 最後に、前記接着層の硬化後、積層状態のハニカム材及
び内外面材をマンドレルから脱型させることを特徴とす
る中空構造体の製造方法。[Scope of Claims] 1) A hollow portion is formed inside surrounded by a peripheral wall, and the peripheral wall is formed of a honeycomb material forming a core and a face material covering both the inside and outside of this honeycomb material. A hollow structure characterized by 2) Wrap the inner wall material around the mandrel, then wrap and bond the honeycomb material over the inner wall material with an adhesive layer interposed between the inner wall material and the surface of the honeycomb material. An adhesive layer is interposed between the honeycomb material and the outer surface material is wrapped around and bonded to the honeycomb material.Finally, after the adhesive layer is cured, the laminated honeycomb material and inner and outer surface materials are removed from the mandrel. A method for manufacturing a hollow structure, characterized by:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1161156A JPH0688363B2 (en) | 1989-06-23 | 1989-06-23 | Method for manufacturing hollow structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1161156A JPH0688363B2 (en) | 1989-06-23 | 1989-06-23 | Method for manufacturing hollow structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0324941A true JPH0324941A (en) | 1991-02-01 |
| JPH0688363B2 JPH0688363B2 (en) | 1994-11-09 |
Family
ID=15729662
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1161156A Expired - Lifetime JPH0688363B2 (en) | 1989-06-23 | 1989-06-23 | Method for manufacturing hollow structure |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0688363B2 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0615736A (en) * | 1992-04-07 | 1994-01-25 | Ashimori Ind Co Ltd | Method, device and repair material for repairing pipeline |
| US20130213562A1 (en) * | 2012-02-16 | 2013-08-22 | Mohammad R. Ehsani | Continuous onsite-manufactured pipe |
| JP2023004234A (en) * | 2021-06-25 | 2023-01-17 | 株式会社Trine | boat deck |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6154927A (en) * | 1984-08-24 | 1986-03-19 | ヨハン・ヨセフ・マグダレ−ナ・エリザベス・ウエイツ | Double wall structure material and manufacture thereof |
-
1989
- 1989-06-23 JP JP1161156A patent/JPH0688363B2/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6154927A (en) * | 1984-08-24 | 1986-03-19 | ヨハン・ヨセフ・マグダレ−ナ・エリザベス・ウエイツ | Double wall structure material and manufacture thereof |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0615736A (en) * | 1992-04-07 | 1994-01-25 | Ashimori Ind Co Ltd | Method, device and repair material for repairing pipeline |
| US20130213562A1 (en) * | 2012-02-16 | 2013-08-22 | Mohammad R. Ehsani | Continuous onsite-manufactured pipe |
| JP2023004234A (en) * | 2021-06-25 | 2023-01-17 | 株式会社Trine | boat deck |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0688363B2 (en) | 1994-11-09 |
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