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JPS6021060B2 - lightweight structures - Google Patents
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JPS6021060B2 - lightweight structures - Google Patents

lightweight structures

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Publication number
JPS6021060B2
JPS6021060B2 JP11701877A JP11701877A JPS6021060B2 JP S6021060 B2 JPS6021060 B2 JP S6021060B2 JP 11701877 A JP11701877 A JP 11701877A JP 11701877 A JP11701877 A JP 11701877A JP S6021060 B2 JPS6021060 B2 JP S6021060B2
Authority
JP
Japan
Prior art keywords
crimping
pressure
pressure fluid
agent
coated
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
Application number
JP11701877A
Other languages
Japanese (ja)
Other versions
JPS5450584A (en
Inventor
一郎 和田
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.)
Toshiba Corp
Original Assignee
Tokyo Shibaura Electric 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 Tokyo Shibaura Electric Co Ltd filed Critical Tokyo Shibaura Electric Co Ltd
Priority to JP11701877A priority Critical patent/JPS6021060B2/en
Publication of JPS5450584A publication Critical patent/JPS5450584A/en
Publication of JPS6021060B2 publication Critical patent/JPS6021060B2/en
Expired legal-status Critical Current

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Description

【発明の詳細な説明】 本発明は例えば浮上式車両等に使用して好適な軽量機造
物に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a lightweight aircraft structure suitable for use in, for example, floating vehicles.

浮上式車両の超電導コイルは液体He等を充填した巨大
なデューァ・ベッセル(比warVessel)に収納
している。
The superconducting coil of the levitation vehicle is housed in a huge dewar vessel filled with liquid He, etc.

このデューア・ベッセルの壁は第1図に示すようにクリ
抜きのアルミニュム1にSUSステンレス2を補強した
ものであり、従って、製造工数が莫大にかかり、また全
体の外形が非常に大きなものとなる。通常、浮上式車両
は航空機と同様に可能な限り軽量化しなければならない
As shown in Figure 1, the walls of this duer vessel are made of hollow aluminum 1 reinforced with SUS stainless steel 2, and therefore require a huge amount of manufacturing man-hours and the overall external size is very large. . Typically, levitated vehicles, like aircraft, must be as light as possible.

しかし、浮上式車両に搭載するデューア・ベッセルは上
述したようにクリ抜き部分の占有スペースが多くなって
全体の形状が大きくなり、外壁部および内壁部に大気圧
が加わるためにアルミニウム1の肉圧を厚くしたり、強
度の点から非クリ抜き部分の骨の数を多くするために、
結果として大きな重量物となってしまう問題がある。そ
こで、近年、航空機で採用されているアルミ・ハネカム
構造や紙ハネカム強イ餌RP(Fi戊rReiMorc
edPlastics)等について研究しているが、価
格的に高価でかつ量産性に不向きであり、さらに2次加
工が難しい等の欠点がある。
However, as mentioned above, the dewar vessel installed on a floating vehicle occupies more space in the cutout part, making the overall shape larger, and because atmospheric pressure is applied to the outer and inner walls, the wall pressure of aluminum 1 increases. In order to increase the thickness of the bone or increase the number of bones in the non-criteria part from the point of view of strength,
As a result, there is a problem that it becomes a large and heavy object. Therefore, in recent years, aluminum honeycomb structure and paper honeycomb strong bait RP (Fi Rei Mor) have been adopted in aircraft.
edPlastics), etc., but they have drawbacks such as being expensive, unsuitable for mass production, and difficult to perform secondary processing.

本発明は上記実情にかんがみてなされたもので、金属板
に、所定の形状で圧着防止剤を塗布させた可塑性部村の
非圧着防止剤塗布部分を圧袋ボンド法などによって圧着
させた後、その非圧着部分で骨組を形成させて所定形状
の構造物を作るようにし、これにより曲げ加工が容易で
機械的強度が強く、かつ溶接等の2次加工も容易である
軽量構造物を提供するものである。
The present invention has been made in view of the above-mentioned circumstances, and after crimping the non-crimping preventive agent-applied portion of the plastic part coated with the anti-crimping agent in a predetermined shape to a metal plate using a pressure bag bonding method or the like, The non-crimped part forms a framework to create a structure of a predetermined shape, thereby providing a lightweight structure that is easy to bend, has strong mechanical strength, and is easy to perform secondary processing such as welding. It is something.

以下、図面を参照して本発明の実施例を説明する。Embodiments of the present invention will be described below with reference to the drawings.

第2図は浮上式車両に搭載する超電導コイルに適用した
例を示し、例えばL字状をなすステンレス容器10の内
部に2体の超電導コイル11a,11bが収納されてい
る。さらに、ステンレス容器10の外側をローラーボン
ド法で作られたローラボンド材12で覆うことにより、
第2図aに示すような超電導コイルの構造物が作られる
。そして、このローラボンド材12の内部に圧縮空気、
高圧ガス、高圧水等の高圧流体を注入することにより、
第2図bのようにローラボンド材12をふくらまして所
定形状の軽量構造物を完成させる。そして、以上のよう
な構造物の完成後、ステンレス容器10の内部に液体H
e(極低高液化ガス)等を充填し、またステンレス容器
10とローラボンド材12との間を真空ポンプ等を用い
て真空にして密閉するものである。
FIG. 2 shows an example in which the superconducting coil is applied to a superconducting coil mounted on a floating vehicle. For example, two superconducting coils 11a and 11b are housed inside an L-shaped stainless steel container 10. Furthermore, by covering the outside of the stainless steel container 10 with a roller bond material 12 made by a roller bond method,
A superconducting coil structure as shown in FIG. 2a is produced. Then, compressed air is placed inside this roller bond material 12.
By injecting high pressure fluid such as high pressure gas or high pressure water,
As shown in FIG. 2b, the roller bond material 12 is inflated to complete a lightweight structure of a predetermined shape. After the structure as described above is completed, liquid H is filled inside the stainless steel container 10.
e (extremely low and high liquefied gas), etc., and the space between the stainless steel container 10 and the roller bond material 12 is evacuated and sealed using a vacuum pump or the like.

なお、この場合第2図cのように構造物の角部が膨出し
ないこともあるが、この角部は大気圧に押されても変形
することがないので問題はない。ここでローラボンド法
を用いてローラボンド材12を作る例についてについて
第3図を参照して説明する。例えば同図aのように薄い
金属板12a,12a(例えばアルミ板)の間に、カー
ボン塗料やセラミック粉塗料等の圧着防止剤12bを予
め所定の形状に塗布してなる可塑性部材12cを挿入し
た後、外側からローラなどを用いて押圧することにより
、2枚の金属板12a,12a間に介在する可塑性部材
12cの非圧着防止塗布部分を該2枚の金属板12a,
12aの内壁部に圧着させる(第3図b参照)。しかる
後、ステンレス容器10の外側に以上のようにして作ら
れたローラボンド材12で覆うものである。次に、外側
の金属板12aを圧接する(第3図b参照)。
In this case, the corners of the structure may not bulge out as shown in FIG. 2c, but this is not a problem because the corners will not deform even when pressed by atmospheric pressure. Here, an example of making the roller bond material 12 using the roller bond method will be described with reference to FIG. 3. For example, as shown in Figure a, a plastic member 12c is inserted between thin metal plates 12a, 12a (for example, aluminum plates), which is made by applying an anti-crimping agent 12b such as carbon paint or ceramic powder paint in a predetermined shape. After that, by pressing from the outside using a roller or the like, the non-pressure prevention coated portion of the plastic member 12c interposed between the two metal plates 12a, 12a is pressed against the two metal plates 12a,
12a (see FIG. 3b). Thereafter, the outside of the stainless steel container 10 is covered with the roller bond material 12 made as described above. Next, the outer metal plate 12a is pressed (see FIG. 3b).

次に、金属板12aに吹込みパイプ13を取り付け(第
3図c参照)、圧着防止剤12cの塗布してある部分に
前述したような高圧流体を注入して膨出させることによ
り、圧着防止剤塗布部分の位置に相応する可塑性部材1
2cでローラボンド材12の骨組を作る。
Next, the blow pipe 13 is attached to the metal plate 12a (see Fig. 3c), and the above-mentioned high-pressure fluid is injected into the area where the anti-crimping agent 12c is applied to swell it, thereby preventing the anti-crimping agent. Plastic member 1 corresponding to the position of the agent application part
A frame of the roller bond material 12 is made using 2c.

従って、以上のようにして完成したローラボンド材12
は第3図dのような断面構造になっている。ところで、
第3図は2枚の金属板12a,12aを使用した例であ
るが、第4図a,bのように1枚の金属板12aに可塑
性部材12cの非圧着防止剤塗布部分を圧着させてもよ
く、また第5図4のように多数の金属板12a・・・を
重ねて作ってもよい。
Therefore, the roller bond material 12 completed as described above
has a cross-sectional structure as shown in Figure 3d. by the way,
Fig. 3 shows an example in which two metal plates 12a and 12a are used, but as shown in Figs. Alternatively, a large number of metal plates 12a may be stacked on top of each other as shown in FIG. 5.

従って、以上のようなローラボンド法を用いて第3図d
〜第5図のような軽量構造物が作られるが、この軽量構
造物はローラポンド材12に高圧流体を注入した状態で
使用してもよいし、あるいはローラボンド材12に高圧
流体を注入して永久変形させ、しかる後高圧流体を抜き
取って内部を真空にし断熱を兼ねた状態で使用すること
もできる。
Therefore, using the roller bonding method as described above, FIG.
~ A lightweight structure as shown in Fig. 5 is made, but this lightweight structure may be used with high pressure fluid injected into the roller bond material 12, or by injecting high pressure fluid into the roller bond material 12. It can also be used in a state where it is permanently deformed and then the high-pressure fluid is removed to create a vacuum inside and also serve as insulation.

また、高圧流体の代りに樹脂や油を注入して使用するこ
とも可能である。また、第2図のような超電導コイルの
軽量機造物は例えば第6図に示すように外側を平坦とす
る2次加工が必要である。
It is also possible to inject resin or oil instead of high-pressure fluid. Furthermore, a lightweight superconducting coil structure as shown in FIG. 2 requires secondary processing to flatten the outside as shown in FIG. 6, for example.

しかし、これの2次加工は成型体に入れて膨出させると
か或し、は圧着防止剤12bの塗布間隔を変えることに
よって比較的容易に行なうことができ、またローラボン
ド材12を膨出させる前に予め発泡合成樹脂断熱材等を
貼着して2次加工してもよい。このとき、第6図のよう
に内側角部につぶれ@が発生することがあるが、上述し
たように角部は外圧による抵抗力が強いので、外圧に対
してはよい結果が縛られる。
However, the secondary processing of this can be relatively easily carried out by putting it into a molded body and making it bulge out, or by changing the application interval of the anti-adhesive agent 12b, or by making the roller bond material 12 bulge out. A foamed synthetic resin heat insulating material or the like may be applied in advance for secondary processing. At this time, collapse @ may occur at the inner corner as shown in FIG. 6, but as described above, the corner has a strong resistance against external pressure, so good results are limited against external pressure.

外圧に対して強くするために、予めいまり(打ち出し)
等を行なった後に膨出させることも可能である。
In order to make it strong against external pressure, it is pre-hammered (launched).
It is also possible to bulge out after doing the above.

なお、上記実施例では圧薮ボンド法のうち特にローラボ
ンド法について説明したが、爆発ボンド法やプレスボン
ド法、摩擦圧鞍ボンド法等を用いて金属板12aに可塑
性部材12cを圧着させてもよい。
Note that in the above embodiment, the roller bonding method among pressure bonding methods was particularly explained, but the plastic member 12c may be crimped to the metal plate 12a using an explosive bonding method, a press bonding method, a friction saddle bonding method, etc. good.

また、上記実施例は超電導コイルについて適用したが、
例えば浮上式車両の車体壁や床、あるいは航空機、人工
衛星、宇宙船等の材料にも使用できることは言うまでも
ない。
In addition, although the above embodiment was applied to a superconducting coil,
It goes without saying that it can be used, for example, for the body walls and floors of floating vehicles, as well as for materials such as aircraft, artificial satellites, and spacecraft.

以上詳記したように本発明によれば、薄い金属板に圧着
防止剤の塗布された可塑性部村を圧着し、圧着防止剤を
塗布した非圧着部分を膨出させて軽量構造物を作るので
、軽量化の点で非常にすぐれており、例えば浮上式車両
等に使用して最適なものである。
As detailed above, according to the present invention, a lightweight structure is produced by crimping a plastic part coated with an anti-crimping agent on a thin metal plate and bulging the non-crimped part coated with an anti-crimping agent. It is extremely lightweight and is ideal for use in, for example, floating vehicles.

また、従来のようにハネカム構造のものでは製造工数や
2次加工の点で量産に不向きであるが、本構造物は膨出
前後何れでも曲げ加工が容易であり、2次加工も簡単に
行なえるなど量産性に適し、ひいてはコストの低減化に
も貢献させることができる。
In addition, conventional honeycomb structures are not suitable for mass production due to manufacturing man-hours and secondary processing, but this structure is easy to bend before and after expansion, and secondary processing can be easily performed. It is suitable for mass production, and can also contribute to cost reduction.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は従来の軽量構造物の断面図、第2図は本発明に
係る軽量構造物を適用した浮上式車両の超電導コイルを
示し、同図aは膨出前の断面図、同図bは膨出後の断面
図、同図cは同図bの■部を拡大して示した図、第3図
a〜cはローラボンド法による製造工程図で、同図dは
同図cのA−A矢視断面図、第4図a,bおよび第5図
は他の例を示すローラボンド材の断面図、第6図は2次
加工を説明するための一部欠切断面図である。 10・・・・・・ステンレス容器、11a,11b・・
・・・・超電導コイル、12・・・・・・ローラボンド
材、12a・・・・・・金属板、12b・・・・・・圧
着防止剤(塗料)、12c・・・・・・膨出部材。 第1図 第2図 第3図 第4図 第5図 第6図
Figure 1 is a sectional view of a conventional lightweight structure, and Figure 2 is a superconducting coil for a levitation vehicle to which the lightweight structure of the present invention is applied. Figure 3c is a cross-sectional view after swelling; Figure 3c is an enlarged view of part ■ in Figure 3b; Figures 3a to 3c are manufacturing process diagrams using the roller bonding method; Figure 3d is A of Figure 3c. -A cross-sectional view, FIGS. 4a, b, and 5 are cross-sectional views of roller bond materials showing other examples. FIG. 6 is a partially cutaway cross-sectional view for explaining secondary processing. . 10... Stainless steel container, 11a, 11b...
...Superconducting coil, 12... Roller bond material, 12a... Metal plate, 12b... Anti-crimping agent (paint), 12c... Swelling Extrusion parts. Figure 1 Figure 2 Figure 3 Figure 4 Figure 5 Figure 6

Claims (1)

【特許請求の範囲】 1 金属板体と、この金属板体に添着され、カーボン塗
料、セラミツク粉塗料等の圧着防止剤の一種を所定の形
状で塗布させた可塑性部材と、この金属部材および圧着
防止剤を塗布させた可塑性部材を圧接ボンド法により圧
接して前記金属部材に圧着防止剤塗布部分以外の部分を
圧着せしめる圧着手段とを備え、この手段によつて形成
された非圧着部分に圧縮空気、高圧ガスおよび高圧水等
の高圧流体の一種または樹脂、油等の非高圧流体の一種
を注入して膨出させて所定の骨組構造の構造物としたこ
とを特徴とする軽量構造物。 2 流体注入手段は、高圧流体を注入して非圧着部分を
膨出させて永久変形させた後、前記高圧流体を抜き取る
ものである特許請求の範囲第1項記載の軽量構造物。
[Scope of Claims] 1. A metal plate, a plastic member attached to the metal plate and coated with a type of anti-crimping agent such as carbon paint or ceramic powder paint in a predetermined shape, and the metal member and the crimping member. crimping means for pressing a plastic member coated with an anti-crimping agent using a pressure bonding method to crimping a portion other than the portion coated with the anti-crimping agent to the metal member, and compressing the non-crimped portion formed by this means. A lightweight structure characterized by being made into a structure with a predetermined frame structure by injecting and expanding a type of high-pressure fluid such as air, high-pressure gas, and high-pressure water, or a type of non-high-pressure fluid such as resin or oil. 2. The lightweight structure according to claim 1, wherein the fluid injection means injects high-pressure fluid to bulge and permanently deform the non-crimped portion, and then extracts the high-pressure fluid.
JP11701877A 1977-09-29 1977-09-29 lightweight structures Expired JPS6021060B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11701877A JPS6021060B2 (en) 1977-09-29 1977-09-29 lightweight structures

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11701877A JPS6021060B2 (en) 1977-09-29 1977-09-29 lightweight structures

Publications (2)

Publication Number Publication Date
JPS5450584A JPS5450584A (en) 1979-04-20
JPS6021060B2 true JPS6021060B2 (en) 1985-05-25

Family

ID=14701399

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11701877A Expired JPS6021060B2 (en) 1977-09-29 1977-09-29 lightweight structures

Country Status (1)

Country Link
JP (1) JPS6021060B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4772745B2 (en) * 2007-05-22 2011-09-14 カナフレックスコーポレーション株式会社 Lightweight incombustible duct and duct forming sheet material

Also Published As

Publication number Publication date
JPS5450584A (en) 1979-04-20

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