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JP3429720B2 - Fender - Google Patents
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JP3429720B2 - Fender - Google Patents

Fender

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Publication number
JP3429720B2
JP3429720B2 JP36135899A JP36135899A JP3429720B2 JP 3429720 B2 JP3429720 B2 JP 3429720B2 JP 36135899 A JP36135899 A JP 36135899A JP 36135899 A JP36135899 A JP 36135899A JP 3429720 B2 JP3429720 B2 JP 3429720B2
Authority
JP
Japan
Prior art keywords
support
fender
thickness
reaction force
support portion
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 - Fee Related
Application number
JP36135899A
Other languages
Japanese (ja)
Other versions
JP2001172939A (en
Inventor
啓 田島
泰史 小園
明 神頃
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.)
Sumitomo Rubber Industries Ltd
Original Assignee
Sumitomo Rubber Industries 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
Priority to JP36135899A priority Critical patent/JP3429720B2/en
Application filed by Sumitomo Rubber Industries Ltd filed Critical Sumitomo Rubber Industries Ltd
Priority to SE0004704A priority patent/SE522901C2/en
Priority to KR1020000078462A priority patent/KR100640030B1/en
Priority to SG200007523A priority patent/SG96592A1/en
Priority to MYPI20005956A priority patent/MY126856A/en
Priority to AU72441/00A priority patent/AU780181B2/en
Priority to US09/739,804 priority patent/US6572307B2/en
Publication of JP2001172939A publication Critical patent/JP2001172939A/en
Application granted granted Critical
Publication of JP3429720B2 publication Critical patent/JP3429720B2/en
Priority to AU2005200291A priority patent/AU2005200291B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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

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  • Body Structure For Vehicles (AREA)

Description

【発明の詳細な説明】 【0001】 【発明の属する技術分野】本発明は、防舷材に関するも
のである。 【0002】 【従来の技術】船舶の、岸壁などへの接舷時のエネルギ
ーを吸収して衝撃を緩和することで、当該船舶の船体を
保護するいわゆる防舷材9として、たとえば図8(a)に
その断面形状を示すように、図示していないが、その先
端に受衝板などの受衝部材が取り付けられる、外径およ
び厚みの一定な円筒状の第1支衝部91と、この第1支
衝部の基端側から岸壁などの取付面Qへ向けてテーパー
状に広がる、厚みの一定な中空円錐状の第2支衝部92
とを、ゴムなどの弾性材料により一体に形成した、いわ
ゆるサークル型と呼ばれるものが広く一般に使用されて
いる。 【0003】かかるサークル型の防舷材9は、船舶の接
舷によって圧縮力を受けるとまず、上記圧縮力に対して
反力を生じながら、第1支衝部91と第2支衝部92と
の境界部分、および第2支衝部92の途中の、高さ方向
のほぼ中心位置で屈曲を開始して、最終的に圧縮力に抗
し切れなくなった段階で座屈する。ついで、図8(b)に
示すようにその全体がほぼ隙間なく折り畳まれるまで変
形したのち、さらに1つのゴムの塊となって圧縮変形さ
れる。 【0004】この経過を、圧縮による防舷材9の歪み量
と、その際に防舷材9に生じる反力とを示す歪み−反力
特性曲線で表すと図9に示す結果となる。すなわち図8
(a)の平常状態から、屈曲部分が座屈する直前までが、
図9で説明すると原点Oから極大点Aまでに相当し、こ
の間は、圧縮力を受けることによって屈曲された防舷材
9が元に戻ろうとする反力を生じるため、反力が上昇す
る。 【0005】ところが防舷材9は、座屈すると上記の反
力をほとんど失うために、その全体が押しつぶされて図
8(b)に示す折り畳まれた状態となるまでの間、防舷材
9の反力は低下する。すなわち極大点Aから極小点Cま
での経過をたどる。そして図8(b)の状態となると今度
は、防舷材9の全体が、前記のように1つのゴムの塊と
して挙動して再び大きな反力を生じるため、上記極小点
Cからあとは、点Bを経由して反力が一方的に上昇す
る。 【0006】 【発明が解決しようとする課題】このような特性曲線を
持つ防舷材を実際に使用できる範囲は通常、原点Oか
ら、C点以降、再び反力が増加に転じて、極大点Aと同
じ反力値を示すB点までの、歪み量で言えば原点Oから
歪み量Dまでの範囲に規制される。これは、歪み量D以
降では反力が高くなりすぎて、船体を損傷するなどの問
題を生じるおそれがあるからである。 【0007】そして上記防舷材が、許容された歪み量D
の範囲内で吸収できるエネルギー量は、上記の特性曲線
と、原点Oを通る横軸と、点Bを通る縦軸とで仕切られ
た領域の面積S1に相当する分となる。防舷材は、上記
面積S1に、特性曲線と、点A−B間を結ぶ横軸とで仕
切られた領域の面積S2を加えた分に相当する量のエネ
ルギーを吸収できるのが理想的であるが、実際には上記
面積S2分だけ、吸収できるエネルギー量が小さくな
り、エネルギー吸収の効率が低下するのである。 【0008】それゆえ防舷材の歪み−反力特性曲線は、
極大点A以降の部分ができるだけ水平に近い、つまり極
大点A以降の反力が、ほぼ一定に近い値を示すのが理想
的である。本発明の目的は、許容された歪み量の範囲内
での歪み−反力特性曲線をできるだけ理想形に近づける
ことができる、新規な防舷材を提供することにある。 【0009】 【課題を解決するための手段および発明の効果】上記課
題を解決するために発明者らは、サークル型の防舷材の
断面形状を種々、検討した。その結果、図8(a)に示し
た従来の防舷材9では、上記第1支衝部91と第2支衝
部92との境界部分の外周面がきれいに連続していたも
のを、第2支衝部92の外周面を第1支衝部91の外周
面より一段外方へ突出させるべく段差が設けられるよう
に断面形状を調整すると、極大点A以降の反力の落ち込
みを抑えて、特性曲線をできるだけ理想形に近づけると
ともに、防舷材が吸収できるエネルギー量を大きくし、
かつエネルギー吸収の効率を向上できることを見出し
た。 【0010】すなわち本発明の防舷材は、先端に受衝部
材が取り付けられる、外径および厚みの一定な円筒状の
第1支衝部と、この第1支衝部の基端側から岸壁などの
取付面へ向けてテーパー状に広がる、厚みの一定な中空
円錐状の第2支衝部とを弾性材料により一体に形成して
なり、上記第2支衝部の厚みを第1支衝部の厚みより大
きくすることで、両支衝部の境界部分の外周面に、第2
支衝部の外周面を第1支衝部の外周面より一段外方へ突
出させるべく段差が設けられたことを特徴とするもので
ある。 【0011】図8(a)に示した従来の、両支衝部91、
92の境界部分の外周面がきれいに連続した防舷材9
は、屈曲時に、両支衝部91、92の屈曲部に空隙Cを
生じ、この空隙Cが原因となって、極大点Aでの反力が
低下するとともに、極大点A以降の、座屈後の反力の落
ち込みが大きくなる。これに対し、たとえば図1(a)(b)
に示したように第1支衝部11と第2支衝部12との境
界部分の外周面に、第2支衝部12の外周面を第1支衝
部11の外周面より一段外方へ突出させるべく段差14
を設けた本発明の防舷材1では、上記屈曲部に生じる空
隙を小さくできるか、あるいは全くなくしてしまうこと
ができるために、極大点Aでの反力を向上できる上、極
大点A以降の反力の落ち込みを抑えることができる。 【0012】また従来の防舷材9は、座屈後に、両支衝
部91、92の外周面同士が接触するタイミングが早い
ために、反力が増加に転じて、極大点Aと同じ反力値を
示すB点に達するまでの歪み量Dが小さくなる。これに
対し、上記本発明の防舷材においては、座屈後に、両支
衝部の外周面同士が接触するタイミングを遅らせること
ができるために、反力が増加に転じて、極大点Aと同じ
反力値を示すB点に達するまでの歪み量Dを大きくする
ことができる。 【0013】それゆえ本発明の防舷材によれば、これら
の相乗効果によって、特性曲線をできるだけ理想形に近
づけるとともに、防舷材が吸収できるエネルギー量を大
きくし、かつエネルギー吸収の効率を向上することが可
能となる。 【0014】 【発明の実施の形態】以下に本発明の防舷材を、その実
施の形態の一例を示す図1(a)(b)を参照しつつ説明す
る。これらの図に見るようにこの例の防舷材1は、図示
していないが、その先端に受衝板などの受衝部材が取り
付けられる、外径および厚みの一定な円筒状の第1支衝
部11と、この第1支衝部11の基端側から岸壁などの
取付面Qへ向けてテーパー状に広がる、厚みの一定な中
空円錐状の第2支衝部12と、この第2支衝部12の最
も広がった基端部から外方へ延設された、上記取付面Q
への取付部となる円形鍔状のフランジ13とを、ゴムな
どの弾性材料により一体に形成したものである。 【0015】そして本発明では、上記各部のうち第1支
衝部11と第2支衝部12との境界部分の外周面に、第
2支衝部12の外周面を第1支衝部11の外周面より一
段外方へ突出させるべく段差14を設けている。段差1
4の大きさは特に限定されないが、図の例のように両支
衝部11、12の境界部分の内周面をきれいに連続させ
ている場合は、両支衝部11、12の厚みT1、T2の比
によって、段差14の大きさを規定することができる。
具体的には、第1支衝部11の厚みT1が、第2支衝部
12の厚みT2の0.8〜0.9倍となるように、段差
14の大きさを設定するのが好ましい。 【0016】第1支衝部11の厚みT1が上記の範囲未
満では段差14が大きくなりすぎるとともに、相対的
に、第2支衝部12の厚みが大きくなりすぎて、座屈後
に、当該第2支衝部12の、高さ方向のほぼ中心位置で
屈曲した上下の部分の内周面同士が接触するタイミング
が早くなるために却って、反力が増加に転じて、極大点
Aと同じ反力値を示すB点に達するまでの歪み量Dが小
さくなってしまうという問題を生じるおそれがある。 【0017】また逆に、第1支衝部11の厚みT1が上
記の範囲を超えた場合には段差14の大きさが十分に得
られないために、当該段差14による、前述した、屈曲
部に生じる空隙を小さくするかまたは全くなくしてしま
って、極大点Aでの反力を向上し、かつ極大点A以降の
反力の落ち込みを抑える効果や、あるいは座屈後に、両
支衝部11、12の外周面同士が接触するタイミングを
遅らせることで、反力が増加に転じて、極大点Aと同じ
反力値を示すB点に達するまでの歪み量Dを大きくする
効果が得られないという問題を生じるおそれがある。 【0018】なおこれらの特性を考慮すると、第1支衝
部11の厚みT1は前記の範囲内でも小さいほど、つま
り第2支衝部12の厚みT2の0.8倍に近いほど好ま
しい。前記図において符号13a…は、防舷材1を取付
面Qに固定するボルト(図示せず)などを挿通するため
に、前記フランジ13に形成された通孔である。フラン
ジ13内には、図示していないが、たとえば鋼板など
の、補強のための剛体部材を埋設してもよい。また第1
支衝部11の先端部(図において上端部)には、やはり
補強のためと、そして受衝板などの受衝部材取付のため
に、たとえば鋼板などの、補強のための剛体部材を埋設
してもよい。 【0019】本発明の防舷材1の、上記以外の形状や寸
法についてはとくに限定されないが、第1支衝部11の
高さH1は、両支衝部11、12の高さの合計値であ
る、全体の高さH0の0.1〜0.3倍であるのが好ま
しい。また第2支衝部12のテーパーの、取付面Qに対
する角度θ1は、70〜80°であるのが好ましい。上
記高さH1と角度θ1は、全体の高さH0が一定で、かつ
取付面Qへの取付面積を規定するフランジ13の外径D
2が一定である場合、相関関係を示す。すなわち図4、
5に示したように第1支衝部11の高さH1の、全体の
高さH0に占める割合が大きくなるほど第2支衝部12
の角度θ1は小さくなり、逆に高さH1の割合が小さくな
るほど第2支衝部12の角度θ1は大きくなる。 【0020】そして第1支衝部11の高さH1が上記の
範囲未満であるか、または角度θ1が上記の範囲を超え
た場合には、相対的に第2支衝部12の占める割合が大
きくなるため、屈曲および座屈時の反力が大きくなると
ともに、第2支衝部12が屈曲を開始するタイミング
や、座屈するタイミング、そしてそれ以上、座屈しなく
なるタイミングが遅れるため、全体としての吸収エネル
ギーは増加するものの、特性上、第1支衝部11が担う
定荷重領域、つまり前記特性曲線において、極大点A以
降、B点までの、反力がほぼ一定である領域が小さくな
りすぎて、防舷材としての使用に適さなくなるおそれが
ある。 【0021】また逆に、第1支衝部11の高さH1が上
記の範囲を超えるか、または角度θ1が上記の範囲未満
であった場合には、相対的に第2支衝部12の占める割
合が小さくなるため、屈曲および座屈時の反力が小さく
なる上、第2支衝部12が屈曲を開始するタイミング
や、座屈するタイミング、そしてそれ以上、座屈しなく
なるタイミングが早まるため、全体としての吸収エネル
ギーが減少する傾向を示す。 【0022】なおこれらの特性のバランスを考慮する
と、第1支衝部11の高さH1は、全体の高さH0の0.
25倍前後であるのがさらに好ましく、また第2支衝部
12のテーパーの角度θ1は、72.5°前後であるの
がさらに好ましい。上記各部からなるこの例の防舷材1
は、たとえば未加硫のゴムコンパウンドと、必要に応じ
て第1支衝部11の先端部やフランジ13内に埋設され
る板状の剛体部材とを、防舷材1の形状に対応した型内
に仕込み、加熱、加圧してゴムを加硫することによって
製造される。 【0023】なお本発明の防舷材の構成は、以上で説明
した図の例のものには限定されず、本発明の要旨を変更
しない範囲で、種々の設計変更を施すことができる。 【0024】 【実施例】以下に本発明を、実施例、比較例に基づいて
説明する。 実施例1 天然ゴムとブタジエンゴムとの、重量比6:4の混合ゴ
ムを基材ゴムとするゴムコンパウンドと、厚み28m
m、外径650mm、内径270mmの1枚の円形鍔状
の鋼板(第1支衝部11の先端部に埋設する剛体部材)
と、厚み28mm、外径1470mm、内径710mm
の1枚の円形鍔状の鋼板(フランジ13に埋設する剛体
部材)とを型内に仕込み、加熱、加圧して基材ゴムを加
硫することにより、図2(a)に示す断面形状を有し、か
つ各部が下記の寸法および角度を有するサークル型の防
舷材1を製造した。 〈寸法および角度〉 第1支衝部11の厚みT1=220mm 第2支衝部12の厚みT2=244mm 厚みの比T1/T2=0.9 第1支衝部11の高さH1=250mm 全体の高さH0=1000mm 高さの比H1/H0=0.25 第2支衝部12の角度θ1=72.5° 第1支衝部11の外径D1=680mm フランジ13の外径D2=1500mm 実施例2 上記実施例1で使用したのと同じゴムコンパウンドと、
円形鍔状の鋼板2枚とを用いて、図3(a)に示す断面形
状を有し、かつ各部が下記の寸法および角度を有するサ
ークル型の防舷材1を製造した。 〈寸法および角度〉 第1支衝部11の厚みT1=220mm 第2支衝部12の厚みT2=275mm 厚みの比T1/T2=0.8 第1支衝部11の高さH1=250mm 全体の高さH0=1000mm 高さの比H1/H0=0.25 第2支衝部12の角度θ1=72.5° 第1支衝部11の外径D1=680mm フランジ13の外径D2=1500mm 実施例3 前記実施例1で使用したのと同じゴムコンパウンドと、
円形鍔状の鋼板2枚とを用いて、図4(a)に示す断面形
状を有し、かつ各部が下記の寸法および角度を有するサ
ークル型の防舷材1を製造した。 〈寸法および角度〉 第1支衝部11の厚みT1=220mm 第2支衝部12の厚みT2=244mm 厚みの比T1/T2=0.9 第1支衝部11の高さH1=300mm 全体の高さH0=1000mm 高さの比H1/H0=0.30 第2支衝部12の角度θ1=70.0° 第1支衝部11の外径D1=680mm フランジ13の外径D2=1500mm 実施例4 前記実施例1で使用したのと同じゴムコンパウンドと、
円形鍔状の鋼板2枚とを用いて、図5(a)に示す断面形
状を有し、かつ各部が下記の寸法および角度を有するサ
ークル型の防舷材1を製造した。 〈寸法および角度〉 第1支衝部11の厚みT1=220mm 第2支衝部12の厚みT2=244mm 厚みの比T1/T2=0.9 第1支衝部11の高さH1=100mm 全体の高さH0=1000mm 高さの比H1/H0=0.10 第2支衝部12の角度θ1=80.0° 第1支衝部11の外径D1=680mm フランジ13の外径D2=1500mm 比較例1 前記実施例1で使用したのと同じゴムコンパウンドと、
円形鍔状の鋼板2枚とを用いて、図8(a)に示す従来の
断面形状を有し、かつ各部が下記の寸法および角度を有
するサークル型の防舷材9を製造した。なお第1支衝部
91の先端部に埋設する鋼板としては、厚み28mm、
外径670mm、内径270mmのものを使用した。 〈寸法および角度〉 第1支衝部91の厚みT1=230mm 第2支衝部92の厚みT2=230mm 厚みの比T1/T2=1.0 第1支衝部91の高さH1=250mm 全体の高さH0=1000mm 高さの比H1/H0=0.25 第2支衝部92の角度θ1=72.5° 第1支衝部91の外径D1=700mm フランジ93の外径D2=1500mm 比較例2 前記実施例1で使用したのと同じゴムコンパウンドと、
円形鍔状の鋼板とを用いて、図6(a)に示す断面形状を
有し、かつ各部が下記の寸法および角度を有するサーク
ル型の防舷材7を製造した。なお第1支衝部71の先端
部に埋設する鋼板としては、厚み28mm、外径690
mm、内径270mmのものを使用した。 〈寸法および角度〉 第1支衝部71の先端側(図では上端側)の厚みT11
240mm 第1支衝部71の基端側(下端側)の厚みT12=216
mm 第2支衝部72の厚みT2=240mm 厚みの比T11/T2=1.0 厚みの比T12/T2=0.9 第1支衝部71の高さH1=250mm 全体の高さH0=1000mm 高さの比H1/H0=0.25 第2支衝部72の角度θ1=72.5° 第1支衝部71の外径D1=720mm フランジ73の外径D2=1500mm 上記各実施例、比較例の防舷材の主要寸法を表1にまと
めた。 【0025】 【表1】 【0026】圧縮試験 上記各実施例、比較例の防舷材を、第1支衝部の先端
に、受衝板に擬した、当該第1支衝部と同径でかつ厚み
が200mmのスペーサを取り付けた状態で、500ト
ン油圧プレスのヘッドに固定して圧縮した際の歪み(圧
縮率)−反力特性を測定した。なお圧縮率は、下記の式
によって求めた。 圧縮率(%)=(H0−H0′)/H0×100 〔ただしH0は初期形状における全体の高さ、H0′は圧
縮状態での全体の高さである。〕 結果を図7に示す。 【0027】図より、従来例である、第1支衝部91の
厚みT1と、第2支衝部92の厚みT2とを等しくして段
差を無くした比較例1の防舷材9は、屈曲時に、極大点
Aでの反力が低下するとともに、極大点A以降の、座屈
後の反力の落ち込みが大きくなることがわかった。そこ
で屈曲状態での断面形状を調べたところ、図8(b)に示
すように両支衝部91、92の屈曲部に大きな空隙Cを
生じているのが確認された。 【0028】また上記比較例1の防舷材9は、図8(b)
に示すように座屈後に、両支衝部91、92の外周面9
1a、92aが接触するタイミングが早いために、反力
が増加に転じて、極大点Aと同じ反力値を示すB点に達
するまでの歪み量Dに相当する圧縮率が60%と小さい
ことも確認された。また第1支衝部71を、その外周面
が、基端側(図では下端側)から先端側(上端側)へ向
けてテーパー状に広がっているとともに、上記先端側の
厚みT11が、テーパーの分だけ基端側の厚みT12より大
きい断面形状とした比較例2の防舷材7は、図6(b)に
示すように屈曲状態において、両支衝部71、72の屈
曲部に空隙Cを生じないため、座屈後の反力の落ち込み
は小さいものの、座屈後に、両支衝部71、72の外周
面71a、72aが接触するタイミングが早いために、
反力が増加に転じて、極大点Aと同じ反力値を示すB点
に達するまでの歪み量Dに相当する圧縮率が58%と小
さいことも確認された。 【0029】これに対し、実施例1〜4の防舷材1はい
ずれも、図2(b)〜図5(b)に示すように屈曲状態におい
て、両支衝部11、12の屈曲部に空隙Cを生じないた
め、座屈後の反力の落ち込みが小さいことが確認され
た。また各実施例の防舷材はいずれも、座屈後に、両支
衝部11、12の外周面同士や、第2支衝部12の、高
さ方向のほぼ中心位置で屈曲した上下の部分の内周面同
士が接触するタイミングを、比較例1〜3に比べて遅く
できるために、反力が増加に転じて、極大点Aと同じ反
力値を示すB点に達するまでの歪み量Dに相当する圧縮
率を62〜67%程度まで大きくできることも確認され
た。 【0030】また各実施例のうち、両支衝部11、12
の厚みの比T1/T2のみが異なる実施例1、2を比較す
ると、上記比が小さいほど、僅かではあるが吸収エネル
ギー量を増加できることがわかった。さらに上記比T1
/T2は同じで、第1支衝部11の高さの比H1/H
0と、第2支衝部12の角度θ1とが異なる実施例1、3
および4を比較すると、比H1/H 0が大きく、かつ角度
θ1が小さいほど、全体としての吸収エネルギーが減少
する傾向を示し、逆に比H1/H0が小さく、かつ角度θ
1が大きいほど、第1支衝部11が担う定荷重領域が小
さくなる傾向を示すことが確認された。
DETAILED DESCRIPTION OF THE INVENTION [0001] TECHNICAL FIELD The present invention relates to a fender.
It is. [0002] 2. Description of the Related Art Energy when a ship berths at a quay or the like
To absorb the shocks and reduce the impact, thereby reducing the hull of the ship.
As a so-called fender 9 for protection, for example, as shown in FIG.
It is not shown to show its cross-sectional shape,
At the end, a receiving member such as a receiving plate is attached.
Cylindrical first supporting portion 91 having a constant and constant thickness,
Taper from the base end side of the contact part to the mounting surface Q such as a quay
Hollow cone-shaped second support portion 92 having a constant thickness and spreading in a shape
Are integrally formed of an elastic material such as rubber.
What is called a loose circle type is widely used in general
I have. [0003] Such a circle-shaped fender 9 is used for connecting a ship.
When receiving the compressive force by the port, first,
While generating a reaction force, the first support unit 91 and the second support unit 92
In the height direction in the middle of the boundary portion of the second support portion 92
Begins bending at approximately the center of the
Buckles when it can no longer be done. Next, FIG. 8 (b)
As shown, change until the whole is folded almost without gaps.
After being shaped, it is further compressed into a single lump of rubber.
It is. [0004] This process is determined by the amount of distortion of the fender 9 due to compression.
-Reaction force indicating the reaction force generated in the fender 9 at that time
When represented by a characteristic curve, the result shown in FIG. 9 is obtained. That is, FIG.
From the normal state of (a) until immediately before the bent portion buckles,
Referring to FIG. 9, this corresponds to the range from the origin O to the maximum point A.
Fenders bent during compression
The reaction force rises because 9 produces a reaction force that tries to return
You. However, when the fender 9 buckles,
Figure crushed in its entirety to almost lose power
Until the folded state shown in Fig. 8 (b), the fenders
The reaction force of 9 decreases. That is, from the maximum point A to the minimum point C
Follow the course at. Then, when the state shown in FIG.
Means that the entire fender 9 is made up of one rubber lump as described above.
The minimum point
After C, the reaction force increases unilaterally via point B
You. [0006] SUMMARY OF THE INVENTION
The range in which the fenders can actually be used is usually the origin O
Then, after point C, the reaction force began to increase again, and was the same as the maximum point A.
From the origin O to the point B which shows the same reaction force value
It is restricted to the range up to the distortion amount D. This is the amount of distortion D
When descending, the reaction force becomes too high and damages the hull.
This may cause a problem. [0007] The above-mentioned fender has an allowable distortion D
The amount of energy that can be absorbed within the range of
And a horizontal axis passing through the origin O and a vertical axis passing through the point B.
Area S1Is equivalent to The fender is above
Area S1Next, the characteristic curve and the horizontal axis connecting points AB are specified.
Area S of cut areaTwoOf energy equivalent to the amount
Ideally, it should be able to absorb energy.
Area STwoThe amount of energy that can be absorbed is small
This reduces the efficiency of energy absorption. Therefore, the distortion-reaction characteristic curve of the fender is
The part after the maximum point A is as horizontal as possible.
Ideally, the reaction force after the point A should be almost constant
It is a target. An object of the present invention is to set the range of the allowable distortion amount.
The characteristic curve of strain-reaction force as close to the ideal as possible
And to provide a new fender. [0009] Means for Solving the Problems and Effects of the Invention
In order to solve the problem, the inventors have developed a circle-shaped fender.
Various cross-sectional shapes were studied. As a result, as shown in FIG.
In the conventional fender 9, the first support part 91 and the second support
The outer peripheral surface at the boundary with the portion 92 was clean and continuous
The outer peripheral surface of the second support portion 92 is
A step is provided so that it protrudes one step outward from the surface
When the cross-sectional shape is adjusted, the reaction force drops after the maximum point A
The characteristic curve as close to the ideal as possible
In both cases, the amount of energy that the fender can absorb is increased,
And improved energy absorption efficiency
Was. That is, the fender according to the present invention is provided with
Outside diameter to which the material is attachedAnd thicknessConstant cylindrical
A first support part and a quay or the like from the proximal end side of the first support part
Spreads in a tapered shape toward the mounting surface, Constant thicknessHollow
The conical second support part is formed integrally with an elastic material
And aboveThe thickness of the second support is larger than the thickness of the first support
The two supporting unitsThe outer peripheral surface at the boundary of
Project the outer peripheral surface of the support portion one step outward from the outer peripheral surface of the first support portion.
It is characterized by having a step to make it come out
is there. FIG. 8 (a) shows a conventional double support portion 91,
Fender 9 with a beautifully continuous outer peripheral surface at the boundary of 92
Creates a gap C in the bending portion of both supporting portions 91 and 92 when bending.
The reaction force at the maximum point A is generated due to the gap C.
As well as the reaction force after buckling after the maximum point A
Insertion becomes large. On the other hand, for example, FIG.
The boundary between the first support 11 and the second support 12 as shown in FIG.
The outer peripheral surface of the second support portion 12 is provided on the outer peripheral surface of the boundary portion by the first support.
A step 14 is formed to protrude outward from the outer peripheral surface of the portion 11 by one step.
In the fender 1 of the present invention provided with the air gap, the air gap generated in the bent portion is provided.
The gap can be reduced or eliminated entirely
The reaction force at the maximum point A can be improved,
A drop in the reaction force after the point A can be suppressed. In addition, the conventional fender 9 is configured such that, after buckling,
The timing at which the outer peripheral surfaces of the portions 91 and 92 come into contact with each other is early
Therefore, the reaction force starts to increase, and the same reaction force value as the maximum point A
The distortion amount D until reaching the point B shown in FIG. to this
On the other hand, in the fender of the present invention, after buckling,
Delay the timing of contact between the outer peripheral surfaces of the contact parts
, The reaction force starts to increase and is the same as the maximum point A
Increase the distortion amount D until the point B indicating the reaction force value is reached
be able to. Therefore, according to the fender of the present invention,
The characteristic curve as close to the ideal as possible
And increase the amount of energy that the fender can absorb
It is possible to improve the efficiency of energy absorption
It works. [0014] BEST MODE FOR CARRYING OUT THE INVENTION The fender of the present invention will be described in detail below.
This will be described with reference to FIGS. 1A and 1B showing an example of the embodiment.
You. As seen in these figures, the fender 1 of this example is illustrated
However, a receiving member such as a receiving plate is attached to the tip.
A cylindrical first support having a constant outer diameter and thickness to be attached
Part 11 and the quay from the base end side of the first support part 11
Spreads in a tapered shape toward the mounting surface Q, with a constant thickness
An empty cone-shaped second support portion 12 and the second support portion 12
Mounting surface Q extended outward from the base end where
The flange 13 having a circular flange shape,
It is integrally formed of any elastic material. According to the present invention, the first support of the above-mentioned respective parts is provided.
On the outer peripheral surface of the boundary between the collision portion 11 and the second support portion 12
2 The outer peripheral surface of the support portion 12 is
A step 14 is provided to protrude outward from the step. Step 1
Although the size of 4 is not particularly limited, as shown in FIG.
Make the inner peripheral surface of the boundary between the contact parts 11 and 12 clean and continuous
The thickness T of both support parts 11 and 121, TTwoRatio
Thus, the size of the step 14 can be defined.
Specifically, the thickness T of the first support 111But the second support unit
12 thickness TTwo0.8-0.9 times of
It is preferable to set the size of 14. The thickness T of the first support 111Is not in the above range
When full, the step 14 becomes too large,
In addition, the second support portion 12 becomes too thick,
At the substantially center position of the second support portion 12 in the height direction.
Timing at which the inner peripheral surfaces of the bent upper and lower parts contact each other
Instead, the reaction force started to increase and the maximum point
The amount of distortion D until the point B showing the same reaction force value as A is reached is small.
There is a possibility that a problem of becoming smaller may occur. Conversely, the thickness T of the first support 111Is on
If the value exceeds the above range, the size of the step 14 is sufficiently obtained.
As described above, due to the step 14, the bending
Reduce or eliminate voids in the part
Therefore, the reaction force at the maximum point A is improved, and
The effect of suppressing the reaction force drop or after buckling,
The timing at which the outer peripheral surfaces of the support portions 11 and 12 come into contact with each other
By delaying, the reaction force starts to increase and is the same as the maximum point A
Increase the distortion amount D until the point B indicating the reaction force value is reached
There is a possibility that a problem that the effect cannot be obtained may occur. Considering these characteristics, the first support
Thickness T of part 111Is smaller in the above range,
Thickness T of the second support portion 12Two0.8 times as large as
New In the above figures, reference numerals 13a ... attach the fender 1
To insert bolts (not shown) for fixing to surface Q
And a through hole formed in the flange 13. Franc
Although not shown, for example, a steel plate
However, a rigid member for reinforcement may be embedded. Also the first
The tip (upper end in the figure) of the support portion 11 also has
For reinforcement and mounting of receiving members such as receiving plates
Buried rigid members such as steel plates for reinforcement
May be. Shapes and dimensions of the fender 1 of the present invention other than those described above
The law is not particularly limited.
Height H1Is the sum of the heights of both support parts 11 and 12.
The total height H00.1 to 0.3 times of
New Also, the tapered mounting surface Q of the second support portion 12
Angle θ1Is preferably 70 to 80 °. Up
Notation height H1And angle θ1Is the total height H0Is constant, and
Outer diameter D of flange 13 that defines the mounting area on mounting surface Q
TwoIs constant, indicates a correlation. That is, FIG.
As shown in FIG. 5, the height H of the first support 111Of the whole
Height H0The larger the ratio of the second support unit 12
Angle θ1Becomes smaller and conversely the height H1Ratio is small
The angle θ of the second support portion 121Becomes larger. The height H of the first support 111Is above
Is less than the range or the angle θ1Exceeds the above range
The second support unit 12 occupies a relatively large
When the reaction force during bending and buckling increases,
In both cases, the timing at which the second support unit 12 starts bending
Or when to buckle, and more
The absorption energy as a whole
Although the energy increases, the first support unit 11 is responsible for the characteristics.
In the constant load area, that is, in the characteristic curve,
The area where the reaction force is almost constant up to the descent and point B is small.
May become unsuitable for use as fenders
is there. Conversely, the height H of the first support 111Is on
Above the range or the angle θ1Is less than the above range
, The relative share of the second support unit 12
Reaction force during bending and buckling is small
In addition, the timing at which the second support portion 12 starts bending
Or when to buckle, and more
As the timing becomes faster, the absorption energy as a whole
Energy tends to decrease. The balance between these characteristics is taken into consideration.
And the height H of the first support portion 111Is the total height H00.
More preferably, it is about 25 times.
12 taper angle θ1Is around 72.5 °
Is more preferred. Fender 1 of this example composed of the above parts
Is, for example, an unvulcanized rubber compound and
And is embedded in the tip of the first support portion 11 and the flange 13.
Plate-shaped rigid member in a mold corresponding to the shape of the fender 1
By heating, pressing and vulcanizing the rubber
Manufactured. The structure of the fender according to the present invention has been described above.
The gist of the present invention is not limited to
Various design changes can be made without departing from the scope. [0024] EXAMPLES The present invention will be described below based on Examples and Comparative Examples.
explain. Example 1 Mixture of natural rubber and butadiene rubber in a weight ratio of 6: 4
Rubber compound with rubber as base rubber and thickness 28m
m, one circular flange with an outer diameter of 650 mm and an inner diameter of 270 mm
Steel plate (a rigid member embedded at the tip of the first support portion 11)
And thickness 28mm, outer diameter 1470mm, inner diameter 710mm
One circular flanged steel plate (a rigid body embedded in the flange 13)
Components) in a mold, and heat and pressurize to apply base rubber.
By sulphating, it has the cross-sectional shape shown in FIG.
Each part has the following dimensions and angles.
Port material 1 was manufactured. <Dimensions and angles> Thickness T of first support 111= 220mm Thickness T of second support portion 12Two= 244mm Thickness ratio T1/ TTwo= 0.9 Height H of first support 111= 250mm Overall height H0= 1000mm Height ratio H1/ H0= 0.25 Angle θ of second support unit 121= 72.5 ° Outer diameter D of first support 111= 680mm Outer diameter D of flange 13Two= 1500mm Example 2 The same rubber compound as used in Example 1 above,
The cross-sectional shape shown in FIG.
And each part has the following dimensions and angles.
The vehicle-type fender 1 was manufactured. <Dimensions and angles> Thickness T of first support 111= 220mm Thickness T of second support portion 12Two= 275mm Thickness ratio T1/ TTwo= 0.8 Height H of first support 111= 250mm Overall height H0= 1000mm Height ratio H1/ H0= 0.25 Angle θ of second support unit 121= 72.5 ° Outer diameter D of first support 111= 680mm Outer diameter D of flange 13Two= 1500mm Example 3 The same rubber compound as used in Example 1;
The cross-sectional shape shown in FIG.
And each part has the following dimensions and angles.
The vehicle-type fender 1 was manufactured. <Dimensions and angles> Thickness T of first support 111= 220mm Thickness T of second support portion 12Two= 244mm Thickness ratio T1/ TTwo= 0.9 Height H of first support 111= 300mm Overall height H0= 1000mm Height ratio H1/ H0= 0.30 Angle θ of second support unit 121= 70.0 ° Outer diameter D of first support 111= 680mm Outer diameter D of flange 13Two= 1500mm Example 4 The same rubber compound as used in Example 1;
The cross-sectional shape shown in FIG.
And each part has the following dimensions and angles.
The vehicle-type fender 1 was manufactured. <Dimensions and angles> Thickness T of first support 111= 220mm Thickness T of second support portion 12Two= 244mm Thickness ratio T1/ TTwo= 0.9 Height H of first support 111= 100mm Overall height H0= 1000mm Height ratio H1/ H0= 0.10 Angle θ of second support unit 121= 80.0 ° Outer diameter D of first support 111= 680mm Outer diameter D of flange 13Two= 1500mm Comparative Example 1 The same rubber compound as used in Example 1;
Using two circular flange-shaped steel plates, a conventional steel plate shown in FIG.
It has a cross-sectional shape and each part has the following dimensions and angles.
A circle-shaped fender 9 was manufactured. The first support section
As a steel plate embedded at the tip of 91, a thickness of 28 mm,
Those having an outer diameter of 670 mm and an inner diameter of 270 mm were used. <Dimensions and angles> Thickness T of first supporting portion 911= 230mm Thickness T of second support portion 92Two= 230mm Thickness ratio T1/ TTwo= 1.0 Height H of first support 911= 250mm Overall height H0= 1000mm Height ratio H1/ H0= 0.25 Angle θ of second support 921= 72.5 ° Outer diameter D of first support portion 911= 700mm Outer diameter D of flange 93Two= 1500mm Comparative Example 2 The same rubber compound as used in Example 1;
Using a circular flange-shaped steel plate, the cross-sectional shape shown in FIG.
Sark having each of the following dimensions and angles
A fender 7 was manufactured. Note that the tip of the first support portion 71
The steel plate embedded in the part has a thickness of 28 mm and an outer diameter of 690
mm and an inner diameter of 270 mm were used. <Dimensions and angles> Thickness T of the tip end side (upper end side in the figure) of the first support portion 7111=
240mm Thickness T on the base end side (lower end side) of the first support portion 7112= 216
mm Thickness T of second support portion 72Two= 240mm Thickness ratio T11/ TTwo= 1.0 Thickness ratio T12/ TTwo= 0.9 Height H of first support 711= 250mm Overall height H0= 1000mm Height ratio H1/ H0= 0.25 Angle θ of second support portion 721= 72.5 ° Outer diameter D of first support 711= 720mm Outer diameter D of flange 73Two= 1500mm Table 1 summarizes the main dimensions of the fenders of the above examples and comparative examples.
I did. [0025] [Table 1] Compression test The fender of each of the above embodiments and the comparative example was attached to the tip of the first support portion.
The same diameter and thickness as the first support part, simulating a receiving plate
With a 200 mm spacer attached, 500 tons
Distortion when compressed and fixed to the head of a hydraulic press (pressure
Shrinkage) -Reaction force characteristics were measured. The compression ratio is given by the following equation
Asked by. Compression rate (%) = (H0-H0') / H0× 100 [However, H0Is the overall height in the initial shape, H0′ Is pressure
This is the overall height in the collapsed state. ] FIG. 7 shows the results. As shown in the figure, the first support portion 91 of the prior art
Thickness T1And the thickness T of the second support portion 92TwoEqual and
The fender 9 of Comparative Example 1 in which the difference is eliminated has a maximum point when bent.
The reaction force at A decreases and buckling occurs after the maximum point A
It turned out that the drop of the later reaction force became large. There
Fig. 8 (b) shows the cross-sectional shape in the bent state.
So that a large gap C is formed at the bent portion of both support portions 91 and 92.
It was confirmed that it had occurred. The fender 9 of Comparative Example 1 is shown in FIG.
After buckling, as shown in FIG.
Since the timing of contact between 1a and 92a is early, the reaction force
Turns to increase and reaches the point B which shows the same reaction force value as the maximum point A
The compression ratio corresponding to the distortion amount D before the compression is as small as 60%
It was also confirmed. Also, the first support portion 71 is provided on its outer peripheral surface.
From the base end (lower end in the figure) to the distal end (upper end)
At the tip end
Thickness T11Is the thickness T on the base side by the amount of the taper.12Greater than
FIG. 6B shows the fender 7 of Comparative Example 2 having a sharp cross-sectional shape.
As shown in FIG.
No reaction force after buckling due to no void C in the curved part
Is small, but after buckling, the outer periphery of both support portions 71 and 72
Because the timing of contact between the surfaces 71a and 72a is early,
Point B where the reaction force starts to increase and shows the same reaction value as the maximum point A
The compression rate corresponding to the distortion amount D until the compression reaches 58% is as small as 58%.
It was also confirmed. On the other hand, the fender 1 of the first to fourth embodiments has a
The displacement is also in the bent state as shown in FIGS. 2 (b) to 5 (b).
As a result, no gap C is formed in the bent portions of both the support portions 11 and 12.
It was confirmed that the drop of the reaction force after buckling was small.
Was. In addition, the fenders of each embodiment were both supported after buckling.
Between the outer peripheral surfaces of the collision portions 11 and 12 and the second support portion 12
The inner peripheral surface of the upper and lower parts bent at almost the center position in the vertical direction
The timing of the contact of the technician is later than in Comparative Examples 1 to 3.
In order to be able to do so, the reaction force starts to increase and
Compression equivalent to the amount of distortion D until the point B indicating the force value is reached
It has been confirmed that the rate can be increased to about 62-67%.
Was. In each of the embodiments, both the support units 11 and 12
Thickness ratio T1/ TTwoExample 1 and Example 2 differing only in
Therefore, the smaller the above ratio, the smaller the absorption energy
Energy can be increased. Further, the above ratio T1
/ TTwoAre the same, and the ratio H of the height of the first support 11 is1/ H
0And the angle θ of the second support portion 121Examples 1 and 3 differing from
And 4, the ratio H1/ H 0Is large and the angle
θ1Is smaller, the overall absorbed energy decreases
And the ratio H1/ H0Is small and the angle θ
1Is larger, the constant load area carried by the first support 11 is smaller.
It was confirmed that it had a tendency to decrease.

【図面の簡単な説明】 【図1】同図(a)は、本発明の防舷材の、実施の形態の
一例を示す縦方向断面図、同図(b)は、上記例の防舷材
の、部分切り欠き斜視図である。 【図2】同図(a)は、本発明の実施例1の防舷材の、圧
縮しない平常状態での断面形状を示す縦方向断面図、同
図(b)は、上記実施例1の防舷材の、圧縮して屈曲させ
た状態を拡大して示す縦方向断面図である。 【図3】同図(a)は、本発明の実施例2の防舷材の、圧
縮しない平常状態での断面形状を示す縦方向断面図、同
図(b)は、上記実施例2の防舷材の、圧縮して屈曲させ
た状態を拡大して示す縦方向断面図である。 【図4】同図(a)は、本発明の実施例3の防舷材の、圧
縮しない平常状態での断面形状を示す縦方向断面図、同
図(b)は、上記実施例3の防舷材の、圧縮して屈曲させ
た状態を拡大して示す縦方向断面図である。 【図5】同図(a)は、本発明の実施例4の防舷材の、圧
縮しない平常状態での断面形状を示す縦方向断面図、同
図(b)は、上記実施例4の防舷材の、圧縮して屈曲させ
た状態を拡大して示す縦方向断面図である。 【図6】同図(a)は、比較例2の防舷材の、圧縮しない
平常状態での断面形状を示す縦方向断面図、同図(b)
は、上記比較例2の防舷材の、圧縮して屈曲させた状態
を拡大して示す縦方向断面図である。 【図7】本発明の各実施例、比較例の防舷材における、
歪み量(圧縮率)−反力特性を示すグラフである。 【図8】同図(a)は、従来例である比較例1の防舷材
の、圧縮しない平常状態での断面形状を示す縦方向断面
図、同図(b)は、上記比較例1の防舷材の、圧縮して屈
曲させた状態を拡大して示す縦方向断面図である。 【図9】従来の防舷材の歪み量−反力特性と、そこから
求められる吸収エネルギー量とを説明するグラフであ
る。 【符号の説明】 1 防舷材 11 第1支衝部 12 第2支衝部 14 段差 Q 取付面(岸壁など)
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 (a) is a longitudinal sectional view showing an example of an embodiment of a fender according to the present invention, and FIG. 1 (b) is a fender of the above example. FIG. 2 is a partially cutaway perspective view of a material. FIG. 2 (a) is a longitudinal sectional view showing a cross-sectional shape of the fender according to the first embodiment of the present invention in a normal state without compression, and FIG. 2 (b) is a longitudinal sectional view of the first embodiment. It is a longitudinal cross-sectional view which expands and shows the state which compressed and bent the fender. FIG. 3 (a) is a longitudinal sectional view showing a cross-sectional shape of a fender according to a second embodiment of the present invention in a normal state without compression, and FIG. 3 (b) is a longitudinal sectional view of the second embodiment. It is a longitudinal cross-sectional view which expands and shows the state which compressed and bent the fender. FIG. 4A is a longitudinal sectional view showing a cross-sectional shape of a fender according to a third embodiment of the present invention in an uncompressed normal state; FIG. 4B is a longitudinal sectional view of the third embodiment; It is a longitudinal cross-sectional view which expands and shows the state which compressed and bent the fender. FIG. 5A is a longitudinal sectional view showing a cross-sectional shape of a fender according to a fourth embodiment of the present invention in an uncompressed normal state, and FIG. 5B is a longitudinal sectional view of the fourth embodiment. It is a longitudinal cross-sectional view which expands and shows the state which compressed and bent the fender. FIG. 6 (a) is a longitudinal sectional view showing a cross-sectional shape of the fender of Comparative Example 2 in a normal state without compression, and FIG. 6 (b).
FIG. 4 is an enlarged longitudinal sectional view showing a compressed and bent state of the fender of Comparative Example 2; FIG. 7 is a view illustrating a fender of each embodiment and a comparative example of the present invention.
It is a graph which shows the amount of distortion (compression rate)-reaction force characteristic. FIG. 8 (a) is a longitudinal sectional view showing a cross-sectional shape of a fender of Comparative Example 1 which is a conventional example in an uncompressed normal state, and FIG. 8 (b) is a longitudinal sectional view of Comparative Example 1; FIG. 4 is an enlarged longitudinal sectional view showing a state in which the fender is compressed and bent. FIG. 9 is a graph illustrating the relationship between the amount of strain and the reaction force of a conventional fender and the amount of absorbed energy obtained therefrom. [Description of Signs] 1 Fender 11 First support part 12 Second support part 14 Step Q Mounting surface (quay, etc.)

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平11−222833(JP,A) 特開 平10−1927(JP,A) 特開 平6−26022(JP,A) 特公 平4−1129(JP,B2) 欧州特許出願公開92893(EP,A1) (58)調査した分野(Int.Cl.7,DB名) E02B 3/26 ──────────────────────────────────────────────────続 き Continuation of the front page (56) References JP-A-11-222833 (JP, A) JP-A-10-1927 (JP, A) JP-A-6-26022 (JP, A) 1129 (JP, B2) EP 92893 (EP, A1) (58) Fields investigated (Int. Cl. 7 , DB name) E02B 3/26

Claims (1)

(57)【特許請求の範囲】 【請求項1】先端に受衝部材が取り付けられる、外径
よび厚みの一定な円筒状の第1支衝部と、この第1支衝
部の基端側から岸壁などの取付面へ向けてテーパー状に
広がる、厚みの一定な中空円錐状の第2支衝部とを弾性
材料により一体に形成してなり、上記第2支衝部の厚み
を第1支衝部の厚みより大きくすることで、両支衝部
境界部分の外周面に、第2支衝部の外周面を第1支衝部
の外周面より一段外方へ突出させるべく段差が設けられ
たことを特徴とする防舷材。
(57) [Claims] [Claim 1] An outer diameter or a diameter at which a receiving member is attached to the tip .
And a cylindrical first support part having a constant thickness and a second conical hollow support part having a constant thickness and extending in a tapered shape from a base end side of the first support part toward a mounting surface such as a quay. And the contact portion is integrally formed of an elastic material.
Is made larger than the thickness of the first supporting portion, so that the outer peripheral surface of the second supporting portion projects outward by one step from the outer peripheral surface of the first supporting portion on the outer peripheral surface at the boundary between the two supporting portions. A fender characterized by the provision of steps.
JP36135899A 1999-12-20 1999-12-20 Fender Expired - Fee Related JP3429720B2 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
JP36135899A JP3429720B2 (en) 1999-12-20 1999-12-20 Fender
KR1020000078462A KR100640030B1 (en) 1999-12-20 2000-12-19 Fender
SG200007523A SG96592A1 (en) 1999-12-20 2000-12-19 Fender
MYPI20005956A MY126856A (en) 1999-12-20 2000-12-19 Fender with step and/or projection
SE0004704A SE522901C2 (en) 1999-12-20 2000-12-19 Fender attached to a doll
AU72441/00A AU780181B2 (en) 1999-12-20 2000-12-20 Fender
US09/739,804 US6572307B2 (en) 1999-12-20 2000-12-20 Fender with step and/or projection
AU2005200291A AU2005200291B2 (en) 1999-12-20 2005-01-24 Fender

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP36135899A JP3429720B2 (en) 1999-12-20 1999-12-20 Fender

Publications (2)

Publication Number Publication Date
JP2001172939A JP2001172939A (en) 2001-06-26
JP3429720B2 true JP3429720B2 (en) 2003-07-22

Family

ID=18473261

Family Applications (1)

Application Number Title Priority Date Filing Date
JP36135899A Expired - Fee Related JP3429720B2 (en) 1999-12-20 1999-12-20 Fender

Country Status (1)

Country Link
JP (1) JP3429720B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4836708B2 (en) * 2006-08-22 2011-12-14 倉敷化工株式会社 Shock absorber

Also Published As

Publication number Publication date
JP2001172939A (en) 2001-06-26

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