JPS5914125B2 - Hollow shell type fencing material and its manufacturing method - Google Patents

Hollow shell type fencing material and its manufacturing method

Info

Publication number
JPS5914125B2
JPS5914125B2 JP54156737A JP15673779A JPS5914125B2 JP S5914125 B2 JPS5914125 B2 JP S5914125B2 JP 54156737 A JP54156737 A JP 54156737A JP 15673779 A JP15673779 A JP 15673779A JP S5914125 B2 JPS5914125 B2 JP S5914125B2
Authority
JP
Japan
Prior art keywords
hollow shell
rubber
shell type
wing pieces
hollow
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
JP54156737A
Other languages
Japanese (ja)
Other versions
JPS5681704A (en
Inventor
久也 潤田
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.)
Bridgestone Corp
Original Assignee
Bridgestone Corp
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 Bridgestone Corp filed Critical Bridgestone Corp
Priority to JP54156737A priority Critical patent/JPS5914125B2/en
Publication of JPS5681704A publication Critical patent/JPS5681704A/en
Publication of JPS5914125B2 publication Critical patent/JPS5914125B2/en
Expired legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A30/00Adapting or protecting infrastructure or their operation
    • Y02A30/30Adapting or protecting infrastructure or their operation in transportation, e.g. on roads, waterways or railways

Description

【発明の詳細な説明】 この発明は、中空胴殻式防げん材とその製法に関し、と
くにこの種防げん材について船舶の接ケんに際して取付
は安定性を有効に改善すること、そして該性能のすぐれ
た防げん材の有利な製法を与えることを目的とする。
[Detailed Description of the Invention] The present invention relates to a hollow shell type fencing material and its manufacturing method, and in particular, to effectively improve the stability of this type of fencing material when it is attached to a ship, and to improve its performance. The object of the present invention is to provide an advantageous manufacturing method for a fencing material.

中空胴殻式防げん材は、従来恰も米俵のような外観形状
をなす中空円筒に成形をしたゴム袋からなり、その内部
を充気膨満させ、両端に設けた取付は金具に鎖などをつ
ないで、岸壁面に吊下げ保持することにより、船舶類の
接げん衝撃を、主として充気山王により緩和吸収するよ
うな使用に供されるところからしばし7ば空気式防げん
材とも呼ばれる。
Hollow shell type fencing consists of a rubber bag molded into a hollow cylinder with an appearance similar to a rice bag.The inside of the bag is inflated, and the attachments at both ends are connected to metal fittings such as chains. By hanging and holding it on a quay surface, it is often called a pneumatic protection material because it is mainly used to alleviate and absorb the impact of collisions with ships.

上記の鎖による吊下げ保持に代えて網にくるみ、この網
を保持するような係止も行われたが、げん側板との接触
状況の都合でゴム袋に生じる反発力により岸壁面の装着
位置から跳ね上って、所期した機能が害われるおそれが
あり、そのため第1図に示したように、広幅の抑止帯す
をもってゴム袋fのほぼ半周を取囲んで、この抑止帯す
も岸壁面qにねじ止めすることが多い。
Instead of suspending and holding the bag with a chain as described above, the net was wrapped in a net and locked to hold it, but due to the repulsive force generated in the rubber bag due to the contact situation with the side board of the ship, the mounting position on the quay surface was changed. Therefore, as shown in Figure 1, a wide restraining strap is used to surround approximately half of the rubber bag f, and this restraining strap is also placed on the quay. It is often screwed onto surface q.

しかしこの場合、ゴム袋fの横ずれを防ぐためになお鎖
などの係止具Cが省略できず、またその故に種々な向き
に働(接げん衝撃の下でゴム袋fを抑止する取付は金具
iに応力集中を生じ易く、しばしばゴム袋fの両端に損
傷を起して防げん性能が失われる欠点があったのである
However, in this case, in order to prevent the rubber bag f from shifting laterally, the locking device C such as a chain cannot be omitted, and therefore, the locking device C such as a chain works in various directions (the attachment to restrain the rubber bag f under contact impact requires the use of a metal fitting i). This has the drawback that stress concentration tends to occur in the rubber bag f, which often causes damage to both ends of the rubber bag f, resulting in a loss of fire prevention performance.

一方で上記米俵状の中空円筒にゴム袋fを成形するには
、一般に紙型などの芯材を用い、そのまわりに未加硫ゴ
ムシートなどを張り合わせて胴壁と片端壁を形成した上
で芯体を除去して他端壁の形成を行うなど、手間も時間
もかかる上に作業手順も面倒なので、工数が嵩み、高価
とならざるを得なかった上に、その成形の便宜のために
円形断面とされるので接げんの際や、波浪の衝突で岸壁
面にころがりを生じて鎖をねじったり、そこに接げん衝
撃を受けて鎖がねじ切れる不都合もあったのである。
On the other hand, in order to form the rubber bag f into the rice bag-shaped hollow cylinder, generally a core material such as a paper mold is used, and an unvulcanized rubber sheet is pasted around it to form a body wall and one end wall. The process of removing the core body and forming the other end wall takes time and effort, and the work procedure is troublesome, which increases the number of man-hours and increases the cost. Because of this, the chain had a circular cross section, which caused the chain to roll against the quay wall when it was hitched or hit by waves, causing the chain to twist, or the chain to become twisted due to the impact of the hitch.

なお鎖にかわる網は、その損傷でゴム袋fの流失を来す
うれいがある。
Note that if the net used instead of the chain is damaged, the rubber bag f may be washed away.

この発明は、上記のいわゆる従来型空気式防げん材にお
ける諸般の問題点を克服して、鎖や網を全く用いること
な(安定確実な岸壁面上における保持取付けが筒型かつ
容易に行え、しかもとくに製造工程における難点を除い
て単純な平プレスによる加圧成形をもって至極容易に、
また均整な品質の下での多量生産に適合させることの開
発成果を提案するものである。
This invention overcomes the various problems with the so-called conventional pneumatic fencing materials mentioned above, and can be stably and securely mounted on a quay surface using a cylindrical shape, without using chains or nets at all. In particular, it is extremely easy to pressurize with a simple flat press, excluding the difficulties in the manufacturing process.
It also proposes development results for adapting to mass production with uniform quality.

この発明は、両端をつぼめて閉ざした中空胴殻を主体と
し、該胴殻からその全長にわたり一体に張出す一対の翼
片をそなえ、これら中空胴殻および翼片が補強布を埋設
したゴムまたはゴム状弾性材料の単一成形体よりなる中
空胴殻式防げん材、ならびに補強布を添えたゴムまたは
ゴム状弾性材料シートをそれによって形成しようとする
両端をつぼめて閉ざした中空胴殻の内面相当域と、該胴
殻と一体をなすべき一対の翼片の張出し分離域とに非接
着処理を施して折重ねる積層成形段階と、この積層成形
体を平プレスの熱板相互間に挟んで加熱下に加圧する硬
化段階との結合になる中空胴殻式防げん材の製法である
This invention has a hollow fuselage whose main body is closed at both ends, and a pair of wing pieces that extend integrally over the entire length of the fuselage shell, and these hollow shell and wing pieces are made of rubber or rubber with a reinforcing cloth embedded therein. Hollow shell fencing consisting of a single molded body of rubber-like elastic material, as well as the inner surface of a hollow shell closed at both ends, from which a rubber or rubber-like elastic material sheet with reinforcing fabric is to be formed. a laminated molding step in which the area and the overhanging separation area of the pair of wing pieces that are to be integrated with the fuselage shell are subjected to non-adhesive treatment and folded, and this laminated molded product is sandwiched between hot plates of a flat press and heated. This is a manufacturing method for a hollow shell type fender that is combined with a curing stage that applies downward pressure.

ここに中空胴殻の両端は、この発明においてはとくに、
恰も練業磨きチューブの尾端におけるように一文字状に
つぼめて接着合体し、ここに接着強度を高めるために適
宜に必要な補強を施す場合があるのはいうまでもない。
In this invention, both ends of the hollow shell are, in particular,
Needless to say, there are cases where the parts are glued together in a straight shape like at the tail end of a training polishing tube, and the necessary reinforcement is applied as appropriate to increase the adhesive strength.

第2図にこの発明による中空胴殻防げん材の岸壁而qへ
の取付けのありさまを示し、図中1は中空胴殻、2は翼
片であり、3は翼片2の側縁を折曲げて形成した取付は
縁、4は取付は用ボルトを示し、5,6は中空胴殻1お
よび翼片2の内部補強、7は中空胴殻1の両端における
一文字状の閉止端である。
Fig. 2 shows how the hollow hull protection material according to the present invention is attached to a quay wall. The bent edges are attached, 4 indicates attachment bolts, 5 and 6 are internal reinforcements of the hollow shell 1 and the wing pieces 2, and 7 is a single-letter closed end at both ends of the hollow shell 1.

中空胴殻1および翼片2は以下のべるような平プレスに
よる加熱加圧操作の下に一体として成形する。
The hollow fuselage shell 1 and the wing pieces 2 are integrally molded by heating and pressing using a flat press as described below.

すなわち第3図a、第4図aにおいて8,9はプレス熱
板、10は枠型であり、この枠型10内に、内面補強1
1として各種有機繊維の糸またはコードあるいはスチー
ルコードなどのゴム引き布を、離型剤層12の挟在下に
重ね合わせ、こrLを挟んで上下に未加硫ゴムシー)1
3.14を添え、これらのまわりを、上面の少くとも一
部を残す離型剤層15の挟在下に、内部埋設補強16と
して上記と同様なゴム引き布を入れたサンドインチ構造
の未加硫ゴム積層シート17で包囲し、その向い合わせ
端縁にも離型剤層18を挟み、こうして熱板8,9間に
加圧して加熱、加硫を行う。
That is, in FIG. 3a and FIG. 4a, 8 and 9 are press hot plates, 10 is a frame mold, and inside this frame mold 10, the inner surface reinforcement 1 is
As 1, rubberized cloth such as threads or cords of various organic fibers or steel cords are layered with a release agent layer 12 sandwiched between them, and unvulcanized rubber sheets are placed on top and bottom with the layer 12 in between.
3.14, and surrounding these with a rubberized cloth similar to the above as the internal reinforcement 16 under the sandwiching of the mold release agent layer 15 leaving at least a part of the upper surface It is surrounded by a sulfur rubber laminated sheet 17, and a mold release agent layer 18 is also sandwiched between the opposite edges thereof, and then pressure is applied between hot plates 8 and 9 to heat and vulcanize.

内面補強11は、筒形に織成し、図のように圧扁し、要
すれば両端を折返すことが好ましいが、単に二枚重ねと
してもよい。
The inner reinforcement 11 is preferably woven into a cylindrical shape, pressed as shown in the figure, and folded back at both ends if necessary, but it may also be simply made of two layers.

上記の成形、強化工程を経て、離型剤層12゜15およ
び18での分離を行い、内部に充気したのちの要部断面
は、それぞれ第3図b、第4図すに示すとおりであり、
なお図中19は注気口金である。
After the molding and strengthening process described above, the mold release agent layers 12, 15 and 18 are separated and the inside is filled with air. can be,
Note that 19 in the figure is an air inlet.

上記のようにして得られるこの発明の空気式防げん材は
、船舶のげん側に面した受衝部20が、中空胴殻1と、
翼片2とにそれぞれ埋設した補強により2重に強化され
て、その耐久性が著しく増強され、かりに第5図に示し
たような、尖鋭突端の衝突の際にも補強の層間に充分に
厚いゴムを有することがら受衝部20の表面に圧縮応力
を生じて尖鋭突端によるカットにも有利に対抗し、耐カ
ット性についても耐久性の向上に有利である。
In the pneumatic shielding material of the present invention obtained as described above, the impact receiving part 20 facing the hull side of the ship is connected to the hollow hull 1,
It is doubly reinforced by the reinforcement embedded in each of the wing pieces 2, and its durability is significantly enhanced.In addition, the reinforcement layer is thick enough to withstand a collision with a sharp tip, as shown in Figure 5. The presence of rubber generates compressive stress on the surface of the impact-receiving portion 20, which advantageously resists cuts caused by sharp edges, and is advantageous in improving cut resistance and durability.

なお受衝部20における二重補強を必要としないとき、
第6図aのように、内面補強11′を添えたゴムシート
21に、内面補強11′の側で離型剤層12′をさらに
添えて、両側でそれぞれ一対の離型剤層22,23とた
ての離型剤層24を用いて三つ折りに折重ね、これを離
型剤層25の挟在下に内部埋設補強16′とのサンドイ
ンチ構造ゴムシート17′上に積層して、上側と同様に
して加熱下に加圧を施し、加硫硬化後に離型剤層12’
、24および25で分離形成される空胴に充気し、第6
図すのような角筒状の中空胴殻26を形成してもよい。
Note that when double reinforcement in the impact receiving part 20 is not required,
As shown in FIG. 6a, a release agent layer 12' is further added to the rubber sheet 21 provided with the inner surface reinforcement 11' on the side of the inner surface reinforcement 11', and a pair of release agent layers 22, 23 are formed on both sides, respectively. Using the freshly prepared mold release agent layer 24, fold it in three and laminate it on the sand-inch structure rubber sheet 17' with the internal embedded reinforcement 16' sandwiching the mold release agent layer 25 between them. Pressure is applied under heat in the same manner as above, and after vulcanization and curing, the mold release agent layer 12' is formed.
, 24 and 25 are filled, and the sixth
A hollow body shell 26 in the shape of a rectangular tube as shown in the figure may be formed.

図中7′は角筒両端で一文字状をなす閉止端で、ここに
は離型剤層12′ 。
In the figure, reference numeral 7' indicates a closed end formed in the shape of a letter at both ends of the rectangular tube, and there is a mold release agent layer 12' thereon.

24および25を施さないことにより形成される。It is formed by not applying 24 and 25.

上記のようにこの発明の中空胴殻式防げん材は、単なる
プレス加圧の如き簡単な成形手段によって容易につくる
ことができるだけでな(、受衝部として働く中空胴殻が
、それと一体の翼片の形で取付部をそなえるので、従来
のこの種防げん材のような吊下げ支持を必要とせず、接
げん衝撃に対して高い取付は安定性を呈して、吊下げ支
持手段またはそれに由来した防げん材の損傷の機会が減
少し、その耐久性を有利に増強することができる。
As mentioned above, the hollow shell type protection material of the present invention can be easily produced by a simple molding method such as pressurization (in addition, the hollow shell that acts as an impact receiving part is integrated with the wing). Since the mounting part is provided in the form of a piece, there is no need for suspension support like conventional protection materials of this type, and the installation exhibits high stability against contact impact, and the suspension support means or The chances of damage to the barrier material are reduced and its durability can be advantageously enhanced.

またこの発明によれば、中空胴殻式防げん材を、従来不
可欠であった石型やマンドレルなど、手間のかかる成形
手段を全く必要とせず、また大型の加硫缶を用いるまで
もな(、単純な平押しプレスによる加硫処理のみにより
、簡便に製造することができる。
Furthermore, according to the present invention, the hollow shell type fencing material does not require any time-consuming molding methods such as stone molds or mandrels, which were indispensable in the past, or even the use of large vulcanization cans. It can be manufactured simply by vulcanization treatment using a simple flat press.

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

第1図は従来の中空胴殻式防げん材の典型例を示す斜視
図、第2図はこの発明による中空胴殻式防げん材の取付
は姿勢を示す斜視図、第3図a。 bは、その加硫前後の各断面図、第4図a、bは、別な
実施例についての同様な各断面図であり、第5図は受衝
部の尖鋭突起による変形挙動説明図、第6図a、bはさ
らに別な実施例についての加硫前後にわたる各断面図で
ある。 1・・・中空胴殻、2・・・翼片。 22−
FIG. 1 is a perspective view showing a typical example of a conventional hollow shell type fencing material, FIG. 2 is a perspective view showing the installation attitude of the hollow shell fencing material according to the present invention, and FIG. 3a. 4b is a cross-sectional view before and after vulcanization, FIGS. 4a and 4b are similar cross-sectional views of another example, and FIG. 5 is an explanatory diagram of deformation behavior due to sharp projections of the impact receiving part FIGS. 6a and 6b are sectional views before and after vulcanization of yet another embodiment. 1...Hollow fuselage shell, 2...Wing piece. 22-

Claims (1)

【特許請求の範囲】 1 両端をつぼめて閉ざした中空胴殻を主体とし、該胴
殻の両側へ一体に張出す一対の翼片をそなえ、これら中
空胴殻および翼片が補強布を埋設したゴムまたはゴム状
弾性材料の単一成形体よりなる中空胴殻式防げん材。 2 補強布を添えたゴムまたはゴム状弾性材料シートを
、それによって形成しようとする両端をつぼめて閉ざし
た中空胴殻の内面相当域と、該胴殻と一体をなすべき一
対の翼片の張出し分離域とに非接着処理を施して折重な
る積層成形段階と、この積層成形体を平プレスの熱板相
互間に挟んで加熱下に加圧する硬化段階との結合になる
中空胴殻式防げん材の製法。
[Scope of Claims] 1 The main body is a hollow shell whose both ends are closed and is provided with a pair of wing pieces that extend integrally to both sides of the shell, and the hollow shell and the wing pieces have reinforcing fabric embedded therein. A hollow shell type protection material made of a single molded body of rubber or rubber-like elastic material. 2. An area corresponding to the inner surface of a hollow shell whose ends are closed by compressing a sheet of rubber or rubber-like elastic material with reinforcing cloth, and an overhang of a pair of wing pieces that are to be integrated with the shell. A hollow shell type fencing material that combines a laminated molding stage in which a non-adhesive treatment is applied to the separation area and folding, and a curing stage in which the laminated molded product is sandwiched between hot plates of a flat press and pressurized under heat. manufacturing method.
JP54156737A 1979-12-05 1979-12-05 Hollow shell type fencing material and its manufacturing method Expired JPS5914125B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP54156737A JPS5914125B2 (en) 1979-12-05 1979-12-05 Hollow shell type fencing material and its manufacturing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP54156737A JPS5914125B2 (en) 1979-12-05 1979-12-05 Hollow shell type fencing material and its manufacturing method

Publications (2)

Publication Number Publication Date
JPS5681704A JPS5681704A (en) 1981-07-04
JPS5914125B2 true JPS5914125B2 (en) 1984-04-03

Family

ID=15634211

Family Applications (1)

Application Number Title Priority Date Filing Date
JP54156737A Expired JPS5914125B2 (en) 1979-12-05 1979-12-05 Hollow shell type fencing material and its manufacturing method

Country Status (1)

Country Link
JP (1) JPS5914125B2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10184220B1 (en) * 2015-12-08 2019-01-22 James R McGilvery Boat fender holder
JP7239971B2 (en) * 2017-11-13 2023-03-15 シバタ工業株式会社 fender structure
KR20210102242A (en) * 2018-12-13 2021-08-19 시바타 코교 가부시키가이샤 fender structure

Also Published As

Publication number Publication date
JPS5681704A (en) 1981-07-04

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