JPH0688363B2 - Method for manufacturing hollow structure - Google Patents

Method for manufacturing hollow structure

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Publication number
JPH0688363B2
JPH0688363B2 JP1161156A JP16115689A JPH0688363B2 JP H0688363 B2 JPH0688363 B2 JP H0688363B2 JP 1161156 A JP1161156 A JP 1161156A JP 16115689 A JP16115689 A JP 16115689A JP H0688363 B2 JPH0688363 B2 JP H0688363B2
Authority
JP
Japan
Prior art keywords
honeycomb material
honeycomb
hollow structure
wound
winding
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.)
Expired - Lifetime
Application number
JP1161156A
Other languages
Japanese (ja)
Other versions
JPH0324941A (en
Inventor
昭 春原
Original Assignee
日産車体株式会社
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 日産車体株式会社 filed Critical 日産車体株式会社
Priority to JP1161156A priority Critical patent/JPH0688363B2/en
Publication of JPH0324941A publication Critical patent/JPH0324941A/en
Publication of JPH0688363B2 publication Critical patent/JPH0688363B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
空構造体の製造方法に関する。
Description: TECHNICAL FIELD The present invention relates to a method for manufacturing a hollow structure used for a vehicle body and an air conditioning duct of a cargo loading portion such as a refrigerating vehicle and a cold storage vehicle, and a skeleton of a container.

(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。
(Prior Art) Conventionally, for example, as a peripheral wall of a load-carrying portion such as a refrigerating car and a refrigerating car, a foam member such as urethane foam is used as a core.
It had a structure in which both front and back sides were sandwiched between aluminum panels.

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, a gap is apt to be formed between the walls, and a member or the like that constitutes a metal frame is required at that portion to connect the walls to each other. There is a problem in heat retention due to the heat transfer of the above, and it took time and effort to bring the walls into close contact with each other so that there is no gap therebetween.

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 a problem, it is conceivable to form the hollow structure as a peripheral wall having a seamless integrated structure.

このような中空構造体としては、例えば、工業材料198
7,VOL.35、NO.7(昭和62年5月20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。
Examples of such a hollow structure include industrial materials 198.
7, VOL.35, NO.7 (May 20, 1987, 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ィング法により成形され
るものであり、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 winding a resin-attached glass fiber around a mandrel and curing it, and then molding it by a filament winding method in which the mandrel is demolded, and its peripheral wall is glass fiber reinforced plastic (FRP). Are formed integrally.

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。
However, in the conventional hollow structure described above,
High specific gravity due to high glass fiber ratio (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, if the wall thickness of the peripheral wall is increased in order to ensure the required rigidity, there is a problem that the weight is increased accordingly.

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 that it has an excellent heat insulating effect, and there is a problem that it is not suitable for a heat insulating application.

そこで、軽量で断熱性を高めるために、ハニカム材を利
用することが考えられる。
Therefore, it is conceivable to use a honeycomb material in order to reduce the weight and improve the heat insulating property.

このようなハニカム材を利用した中空構造体としては、
特開昭61−54927号公報に記載されたものが知られてい
る。この中空構造体は、小径の内側筒状体の外側にハニ
カム構造体を巻き付けて接着し、その外側に大径の外側
筒状体を滑り嵌め合わせて接着させて製造されている。
As a hollow structure using such a honeycomb material,
The one described in JP-A-61-54927 is known. This hollow structure is manufactured by winding and adhering a honeycomb structure on the outside of a small-diameter inner tubular body, and slidingly fitting and adhering a large-diameter outer tubular body on the outside thereof.

(発明が解決しようとする課題) しかしながら、上述のような製造方法では、外側筒状体
がハニカム構造体の外側に滑り嵌め合わせることのでき
る形状に限られてしまい、中空構造体の形状に制約を受
けて造形自由度が低いものであり、特に、冷凍車及び保
冷車の冷凍・冷蔵庫部分のように大型の部分には適用す
ることができなかった。
(Problems to be Solved by the Invention) However, in the manufacturing method as described above, the outer tubular body is limited to a shape that can be slidably fitted to the outside of the honeycomb structure, and the shape of the hollow structure is restricted. As a result, the degree of freedom in molding is low, and in particular, it cannot be applied to large-sized parts such as the freezer / refrigerator part of a refrigerated vehicle and a refrigerated vehicle.

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つとい
う特徴を有したハニカム材を用いた中空構造体を製造す
るにあたり、造形自由度が高く仕上がりも良い製造方法
を提供することを目的としている。
The present invention was made in view of the above conventional problems, in manufacturing a hollow structure using a honeycomb material having a feature of being lightweight and highly rigid and having an excellent heat insulating effect. The object of the present invention is to provide a manufacturing method having a high degree of freedom in molding and a good finish.

(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の製造
方法では、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。
(Means for Solving the Problem) In order to achieve the above-mentioned object, in the method for manufacturing a hollow structure of the present invention, an inner surface member is wound around a mandrel, and then an adhesive layer is formed between the inner surface member and the inner surface member. The honeycomb material is wound and adhered from above the inner side surface material with the interposition of, and then the outer side surface material is wound and adhered from above the honeycomb material with an adhesive layer interposed between the inner surface material and the surface of the honeycomb material. Then, finally, after curing the adhesive layer, the honeycomb material and the inner and outer surface materials in the laminated state are released 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を介在させた状態で
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。
(Operation) In the present invention, first, the inner side material is wrapped around the mandrel,
Next, the honeycomb material is wound and adhered on the inner surface material with the adhesive layer interposed. The adhesive layer may be formed in advance before winding the inner surface material, or may be formed on the outer surface of the inner surface material or the back surface of the honeycomb material after winding the inner surface material. 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。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。
Next, the outer surface material is wound and adhered on the honeycomb material with the adhesive layer interposed. Also in this case, the adhesive layer may be formed on the surface of the honeycomb material before winding the honeycomb material, or may be formed on the surface of the honeycomb material or the back surface of the outer surface material after winding the honeycomb material. Good. Then, finally, after the adhesive layer is cured, the honeycomb material and the inner and outer surface materials in the laminated state are released 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。
In this manner, the hollow structure is formed by the inner and outer surface materials having the honeycomb material as the core, but the honeycomb material and the inner and outer surface materials are first laminated to form a hollow body, and while being wound around the mandrel. In order to stack, even if there is a circumferential difference between the inside and outside of the honeycomb material, there is no deviation in the bonding surface between the honeycomb material and the double-sided material, and the stacking is performed while minimizing the internal and external deformation of the honeycomb material. You can

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。
In addition, since the honeycomb material and the double-sided material are laminated while being wound in this manner, no joint is 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 excellent heat insulating property because the air layer is formed of the honeycomb material.

(実施例) 以下、本発明の実施例を図面により詳述する。(Examples) Hereinafter, examples of the present invention will be described in detail with reference to the drawings.

第1図は本発明実施例製造方法によりの製造した中空構
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
形の中空部10が形成されている。
FIG. 1 is a cross-sectional view showing a hollow structure A manufactured by a manufacturing method according to an embodiment of the present invention. The hollow structure A is used, for example, as a cold room of a cold vehicle and has a substantially rectangular hollow inside. The part 10 is formed.

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。
In the figure, 1 indicates a peripheral wall, and FIG. 2 shows a partially enlarged view thereof.

この周壁1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。
The peripheral wall 1 is formed by using the honeycomb material 2 as a core and adhering the inner side surface material 5 and the outer side surface material 6 to the inner and outer surfaces thereof with the inner adhesive member 3 and the 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 continuously arranged vertically and horizontally, and is formed of a plate material such as an aluminum plate, a paper, a plate, and 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/m2)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3:1
〜6:1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。
The inner and outer adhesive members 3 and 4 are those in which a base material having permeability is impregnated with a resin, and as the base material, for example,
Paper or non-woven fabric (polyester resin, vinylon resin, etc., with a basis weight of 30 to 60 g / m 2 ) is used. As the resin, unsaturated polyester is used as a hard urethane foam system material in a 3: 1 ratio.
Mixtures of up to 6: 1 (weight ratio) are used. Both adhesive members 3 and 4 are for adhering the inner and outer double-sided materials 5 and 6 to the honeycomb material 2. Instead of both adhesive members 3 and 4, simply apply an adhesive material to this portion. You may make it form an adhesive layer.

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 double-sided materials 5 and 6 are formed of FRP plates formed by impregnating reinforcing fibers with a resin. For example, as the reinforcing fibers, a fiber material such as glass, carbon, aramid, or polyacrylate is used. As the material, a thermosetting resin such as unsaturated polyester or epoxy is used.

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 described 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)、外側接着部材4の巻付工
程、外側面材6の巻付工程、硬化工程、脱堅工程の順に
行なわれる。
This manufacturing method includes a step of winding the inner surface material 5 (FIG. 3), a step of winding the inner adhesive member 3 (FIG. 4), a step of winding the honeycomb material 2 (FIGS. 6 to 9), The winding process of the outer adhesive member 4, the winding process of the outer side material 6, the hardening process, and the defastening process 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51又は糸材52を
繰り出しながら樹脂槽53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 step of winding the inner side surface material 5, as shown in FIG. 3, the tape material 50, the sheet material 51, or the thread material 52 of the reinforced fiber is fed through the resin tank 53 and impregnated with the resin 54. Is wrapped around the mandrel M so as to form a face.

次に、内側接着部材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
31に通して樹脂32を含浸させ、これを前記内側面材5の
上から巻き付ける。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
時に行なっても良い。
Next, in the step of winding the inner adhesive member 3, as shown in FIG.
The resin 32 is impregnated through the material 31 and is wound on the inner surface member 5. The step of winding the inner adhesive member 3 may be performed simultaneously with the step of winding the inner surface 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 winding the honeycomb material 2, the honeycomb material 2 is wound on 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, the honeycomb material 2 formed in a tape shape is expanded and wound in a spiral shape.

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
るものである。
In the method shown in FIG. 7, the wide honeycomb material 2 corresponding to the length of the mandrel M is spread and the whole is wound.

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。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。
In the case of the method shown in FIGS. 6 and 7, as shown in FIG. 8, a sheet material such as paper or nonwoven fabric is provided on one side of the honeycomb material 2.
20 is pre-bonded and wound so that this sheet material 20 is on the inside. This is a deformation preventing means for restricting the cells of the honeycomb material 2 so as not to be opened due to winding.

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 the method of FIG. 9, the unexpanded honeycomb block 2 shown in (a) is formed into a tubular shape by adhering the end faces in the expanding direction to each other as shown in (b), and then as shown in (c). Then, the inner surface member 5 and the inner adhesive member 3 are wound on the inner surface member 5 so as to cover the mandrel M from one end side thereof in advance, and in this wound state, it is in a stretched 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 expansion 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、(ロ)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。
As shown in FIG. 10, the honeycomb material 2 can be subjected to various processing before expansion. In the figure, (a) part is an example in which the groove 21 is cut, and (b) part is radiused. twenty two
Is an example in which is cut, and (C) is an example in which another member 23 is insert-processed.

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。
In the next step of winding the outer adhesive member 4, the outer adhesive member 4 is wound from above the honeycomb material 2 in the same manner as the step of winding 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。
Further, in the subsequent step of winding the outer surface material 6, the outer surface material 6 is wound from above the outer adhesive member 4 in the same manner as the step of winding 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
温で硬化させてもよい。
Next, in the curing step, the resin used in each step described above is cured, which 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10が形成
された中空構造体Aが成形される。
The demolding step is the final step, and by demolding the mandrel M after the curing step, the hollow structure A having the 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1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1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。
And, the hollow structure A molded as described above,
Since the peripheral wall 1 has a honeycomb material 2 as a core, and this is sandwiched between the inner and outer double-sided materials 5 and 6 by FRP,
It is lightweight and has high rigidity, and an excellent heat insulating effect is obtained by the air layer of the honeycomb material 2. Furthermore, the honeycomb material 2
Also, since the double-sided materials 5 and 6 are wound, no seam is formed in the middle of the peripheral wall 1, which also improves the heat insulating property.

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
ハニカム材30の端面の周辺部分に樹脂32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。
In addition, since the adhesive members 3 and 4 in which the base material 30 is impregnated with the resin 32 are interposed between the double-sided materials 5 and 6 and the honeycomb material 2, the honeycomb material 2 is formed in the winding step of the honeycomb material 2. Material
When pressed against 30, the resin 32 oozes from the base material 30 to the peripheral portion of the end surface of the honeycomb material 30, as shown in FIG.
A stronger adhesive force can be obtained compared to the case where only the end faces are bonded.

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、保冷車・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 embodiment of the present invention has been described in detail above with reference to the drawings, the specific structure is not limited to this embodiment. For example, the hollow structure is used in a luggage compartment of an automobile such as a cold storage vehicle and a freezing vehicle. Not limited to this, it can be used for air-conditioning ducts for vehicles, bumper amateurs, 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 square 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、本発明では、軽量かつ高剛性
であり、しかも、優れた断熱性能を有し加工応用性にも
優れた、コアにハニカム材を用いた中空構造体を製造す
るにあたり、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付けながら積層
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。
(Effects of the Invention) As described above, according to the present invention, a hollow structure using a honeycomb material for the core, which is lightweight and highly rigid, has excellent heat insulating performance and is excellent in processing applicability. In manufacturing, since the inner and outer surface materials and the honeycomb material are molding methods in which the mandrel is wound in order, even if there is a circumferential difference between the inside and the outside of the honeycomb material, a deviation occurs in the bonding surface between the honeycomb material and the double-sided material. In addition, the honeycomb material can be laminated while minimizing the deformation inside and outside, and the effect that a clean finish can be obtained is obtained.
Since the honeycomb material and the double-sided material are laminated while being wound in this manner, it is possible to provide an effect that a hollow structure having a seamless peripheral wall can be provided.

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 portion can be changed simply by changing the shape of the mandrel, and the effect that the degree of freedom in molding is high can be obtained.

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

第1図は本発明実施例の製造方法により製造した中空構
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10図はそれぞれ本発明実施例の
製造方法を示す説明図である。 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
FIG. 1 is a cross-sectional view showing a hollow structure manufactured by a manufacturing method according to an embodiment of the present invention, FIG. 2 is a partially enlarged view showing a peripheral wall of the hollow structure, and FIGS. It is explanatory drawing which shows the manufacturing method of an example. A ... Hollow structure 1 ... Peripheral wall 2 ... Honeycomb material 3 ... Inner adhesive member (adhesive layer) 4 ... Outer adhesive member (adhesive layer) 5 ... Inner surface material 6 ... Outer surface material 10 ... Hollow part M ... Mandrel

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】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。
1. A mandrel is wound with an inner surface material, and an adhesive layer is interposed between the mandrel and the inner surface material so that a honeycomb material is wound from above the inner surface material so as to be adhered. The outer surface material is wound and adhered from above the honeycomb material by interposing an adhesive layer between the honeycomb material and the surface of the material, and finally, after curing of the adhesive layer, the honeycomb material and the inner and outer surface materials in a laminated state are removed from the mandrel. A method for producing a hollow structure, which comprises demolding.
JP1161156A 1989-06-23 1989-06-23 Method for manufacturing hollow structure Expired - Lifetime JPH0688363B2 (en)

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 JPH0324941A (en) 1991-02-01
JPH0688363B2 true 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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130213562A1 (en) * 2012-02-16 2013-08-22 Mohammad R. Ehsani Continuous onsite-manufactured pipe

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DK0564741T3 (en) * 1992-04-07 1999-07-19 Ashimori Ind Co Ltd Method and apparatus for repairing a pipeline and suitable repair material

Family Cites Families (1)

* Cited by examiner, † Cited by third party
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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130213562A1 (en) * 2012-02-16 2013-08-22 Mohammad R. Ehsani Continuous onsite-manufactured pipe

Also Published As

Publication number Publication date
JPH0324941A (en) 1991-02-01

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