JPH041129B2 - - Google Patents
Info
- Publication number
- JPH041129B2 JPH041129B2 JP58003315A JP331583A JPH041129B2 JP H041129 B2 JPH041129 B2 JP H041129B2 JP 58003315 A JP58003315 A JP 58003315A JP 331583 A JP331583 A JP 331583A JP H041129 B2 JPH041129 B2 JP H041129B2
- Authority
- JP
- Japan
- Prior art keywords
- impact receiving
- impact
- cylindrical body
- buckling
- fender
- 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
Links
Classifications
-
- E—FIXED CONSTRUCTIONS
- E02—HYDRAULIC ENGINEERING; FOUNDATIONS; SOIL SHIFTING
- E02B—HYDRAULIC ENGINEERING
- E02B3/00—Engineering works in connection with control or use of streams, rivers, coasts, or other marine sites; Sealings or joints for engineering works in general
- E02B3/20—Equipment for shipping on coasts, in harbours or on other fixed marine structures, e.g. bollards
- E02B3/26—Fenders
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A30/00—Adapting or protecting infrastructure or their operation
- Y02A30/30—Adapting or protecting infrastructure or their operation in transportation, e.g. on roads, waterways or railways
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Ocean & Marine Engineering (AREA)
- Environmental & Geological Engineering (AREA)
- Mechanical Engineering (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
Description
【発明の詳細な説明】
本発明は港湾ないしは海洋における船舶や浮遊
構造物の衝撃を緩衝するための防舷装置に関する
ものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a fender device for cushioning the impact of ships and floating structures in ports or oceans.
第1図ないし第4図に図示するように、従来の
防舷材aにおいては、受衝部bは中実の四角錐形
状で、支衝部cは中空の四角錐形状からなつてい
る。そして支衝部cは第2図に図示する如く、内
面、外面ともに略平行で、かつ一様な傾斜を有し
ている。 As shown in FIGS. 1 to 4, in the conventional fender a, the impact receiving part b has a solid square pyramid shape, and the supporting part c has a hollow square pyramid shape. As shown in FIG. 2, the support portion c has an inner and outer surface that are substantially parallel and have a uniform inclination.
したがつて、船舶の接舷時、圧縮力を受ける際
の力学的現象は次のようになる。 Therefore, the mechanical phenomenon when a ship receives compressive force when coming alongside is as follows.
第3図において、支衝部四側部dの厚さtd、四
隅角部eの厚さteとすると、支衝部四側部dの断
面二次モーメントIdは、td4すなわち板厚tdの四
乗に比例し、かつ四隅角部eの断面二次モーメン
トIeは、te4すなわち板厚さteの四乗に比例する。 In Fig. 3, assuming that the thickness of the four sides d of the support section is td and the thickness of the four corner sections e is te, the moment of inertia Id of the four side sections d of the support section is td 4 , that is, the thickness of the plate thickness td. It is proportional to the fourth power, and the moment of inertia Ie of the four corners e is proportional to te 4 , that is, the fourth power of the plate thickness te.
ところで、圧縮力Pが働いた場合、圧縮力Pが
比較的小さい間は受衝部bおよび支衝部cいずれ
も弾性変形をするが、圧縮力Pが大きくなると支
衝部cは座屈変形へと変わることになる。この場
合、座屈応力σαEIとなり、座屈応力は断面二次
モーメントId、Ieにそれぞれ比例する。そしてte
>tdゆえ、断面二次モーメントIe>>Idとなる。 By the way, when the compressive force P is applied, both the impact receiving part b and the supporting part c undergo elastic deformation while the compressive force P is relatively small, but as the compressive force P increases, the supporting part c undergoes buckling deformation. It will change to In this case, the buckling stress is σαEI, and the buckling stress is proportional to the moment of inertia of area Id and Ie, respectively. And te
>td Therefore, the second moment of area Ie>>Id.
したがつて支衝部四側部dに比較して四隅角部
eは、はるかに座屈変形を起こしにくくなる。そ
の結果、周囲を形成する四側部dのみが座屈変形
を起こすことになる。 Therefore, compared to the four side portions d of the support portion, the four corner portions e are far less susceptible to buckling deformation. As a result, only the four side parts d forming the periphery undergo buckling deformation.
そして、この座屈変形は四隅角部eが直角を保
つようにして変形を起こすことが最も四側部dの
四隅角部eの近傍の変位量が少なくなるため、第
4図に図示する如くそれぞれ相対向する部材は外
側へふくらみ、他方の相対向する部材は内側にへ
こむという様な変形状態が生じ易く、変位量の低
下の要因となつた。 This buckling deformation is best caused by keeping the four corners e at right angles because the amount of displacement in the vicinity of the four corners e of the four sides d is small, as shown in FIG. 4. A deformed state in which one opposing member bulges outward and the other opposing member dents inward tends to occur, which causes a decrease in the amount of displacement.
また、支衝部cの断面が一様であるため、座屈
変形をおこす際は、支衝部cは長柱の座屈とほぼ
同様の現象となり、座屈応力σはEI/l2に比例し
て、支衝部cの長さlの2乗に逆比例することに
なる。 In addition, since the cross section of the support part c is uniform, when buckling deformation occurs, the buckling stress σ of the support part c becomes almost the same as the buckling of a long column, and the buckling stress σ becomes EI/l 2 . Proportionally, it is inversely proportional to the square of the length l of the support portion c.
したがつて弾性変形領域から座屈変形領域へ遷
移する境界点における応力低下が顕著となつた。 Therefore, the stress drop at the transition point from the elastic deformation region to the buckling deformation region became significant.
本発明はこのような欠点を除去した防舷装置の
改良に係り、ゴム弾性体からなる中空テーパ筒状
体の小径側を受衝部となし、大径側を取付け端と
なした防舷装置において、前記筒状体の肉厚を取
付け端側より受衝端側に向かつて次第に肉厚とな
し、該筒状体外周の受衝端側所定位置に溝を形成
し、該筒状体の内面および外面のいずれか一方ま
たは両方を多角錐体となしたことを特徴とするも
ので、その目的とする処は、変位量が大きく、安
定した変位が得られる緩衝性に優れた防舷装置を
供する点にある。 The present invention relates to an improvement of a fender device that eliminates such drawbacks, and provides a fender device in which the small diameter side of a hollow tapered cylindrical body made of a rubber elastic body is used as an impact receiving part, and the large diameter side is used as a mounting end. In this step, the thickness of the cylindrical body is gradually increased from the mounting end side toward the impact receiving end side, and a groove is formed at a predetermined position on the impact receiving end side of the outer periphery of the cylindrical body. It is characterized by having one or both of its inner and outer surfaces in the form of a polygonal pyramid, and its purpose is to provide fenders with excellent cushioning properties that can provide a large amount of displacement and stable displacement. The point is that it provides
本発明においては、前記したようにゴム弾性体
からなる中空テーパ筒状体の小径側を受衝端とな
し、大径側を取付け端となした防舷装置におい
て、前記筒状体の肉厚を取付け端側より受衝端側
に向かつて次第に肉厚となしたため、中腹部より
受衝端までの断面積が比較的大きく、歪量の比較
的小さい領域(弾性変形領域)における圧縮反力
の増加が大きくなる。なお、圧縮反力とは圧縮力
に抗する力をいうものとする。 In the present invention, in the fender device in which the small diameter side of the hollow tapered cylindrical body made of a rubber elastic body is used as the impact receiving end and the large diameter side is used as the attachment end, as described above, the wall thickness of the cylindrical body is Since the wall thickness gradually increases from the mounting end to the impact-receiving end, the cross-sectional area from the midsection to the impact-receiving end is relatively large, and the compressive reaction force in the region where the amount of strain is relatively small (elastic deformation region) is reduced. increases. Note that the compression reaction force refers to a force that resists the compression force.
また本発明では、筒状体外周の受衝端側所定位
置に溝を形成したため、該溝部にて座屈変形を起
こし易く、座屈反力(座屈荷重に抗する力をいう
ものとする)は前記したように該溝より受衝端ま
での柱長lの2乗に逆比例することになり、取付
け端側より受衝端側に一様な形状で形成したもの
に比較して(一様な形状のものでは取付け端から
受衝端までが柱長lとなる)飛躍的に大きくする
ことができる。したがたて前記弾性変形領域での
圧縮反力の増加と相まつて座屈変形領域において
も座屈反力の増加をはかることができ、弾性変形
領域より座屈変形領域への遷移領域における反力
の増加をはかることができる。 In addition, in the present invention, since the groove is formed at a predetermined position on the impact-receiving end side of the outer periphery of the cylindrical body, buckling deformation is likely to occur in the groove, and buckling reaction force (force that resists buckling load) ) is inversely proportional to the square of the column length l from the groove to the receiving end, and compared to a case where the shape is uniform from the mounting end to the receiving end. For those with a uniform shape, the column length from the mounting end to the impact receiving end is l), and can be dramatically increased. Therefore, together with the increase in compression reaction force in the elastic deformation region, the buckling reaction force can also be increased in the buckling deformation region, and the reaction in the transition region from the elastic deformation region to the buckling deformation region increases. It is possible to measure the increase in force.
さらに本発明においては、筒状体の内面および
外面のいずれか一方または両方を多角錐体となし
たため、圧縮力を受けた場合、角錐面の全面が外
側へふくらむ変形をし、その結果大きな変位をさ
せることができるため、緩衝性が優れた防舷装置
となる。しかも前記したように角錐面の全面が外
側へふくらむ変形をし、安定した変形となり、各
部に均一に圧縮力を分散させることができるた
め、応力集中を避けることができる。 Furthermore, in the present invention, since one or both of the inner and outer surfaces of the cylindrical body is made into a polygonal pyramid, when compressive force is applied, the entire surface of the pyramidal surface is deformed to bulge outward, resulting in a large displacement. This makes it a fender with excellent cushioning properties. Moreover, as described above, the entire surface of the pyramidal surface is deformed to bulge outward, resulting in stable deformation, and the compressive force can be evenly distributed to each part, so that stress concentration can be avoided.
さらにまた本発明では、筒状体を多角錐体とし
たため、断面二次モーメントIの増加となり、座
屈応力の増加をはかることができる。 Furthermore, in the present invention, since the cylindrical body is a polygonal pyramid, the moment of inertia I of area increases, and buckling stress can be increased.
以下第5図ないし第7図に図示された本発明の
一実施例について説明する。 An embodiment of the present invention illustrated in FIGS. 5 to 7 will be described below.
ゴム製弾性体からなる防舷装置1は、受衝部2
と、それに平行な取付部3と、同取付部3から受
衝部2に向かつて内向きの傾斜をして立設された
支衝部4から構成され、同支衝部4は第5図ない
し第6図に図示されるように内部が中空でかつ内
外面いずれも八角錐の角錐面を有して形成されて
いる。 The fender 1 made of a rubber elastic body has an impact receiving part 2
, a mounting part 3 parallel to the mounting part 3, and a support part 4 which is erected with an inward slope from the mounting part 3 toward the impact receiving part 2, and the support part 4 is shown in FIG. As shown in FIGS. 6 to 6, the interior is hollow and both the inner and outer surfaces are formed with octagonal pyramidal surfaces.
前記防舷材1の外面は、取付部3の底面から受
衝部2の上面までの高さをHとすると、取付部3
より受衝部下部5に向かつて内方へ所定の一様な
傾斜θ1(鉛直線に対して9゜±2゜)有して形成され同
受衝部下部5より受衝部2上面へは垂直に形成さ
れている。なお受衝部下部5の位置は、受衝部2
上面より略0.1Hとなつている。また受衝部2上
面より略0.2Hの位置には、上溝6が全周に亘り
形成されており、同上溝6は半円孤状に形成さ
れ、その半径は0.01〜0.015Hの範囲内の所定の寸
法に設定されている。さらに取付部3底面より略
0.1Hの範囲内の位置に下溝7が全周に亘り形成
されており、同下溝7も前記上溝6と同様の形状
および寸法に設定されている。 The outer surface of the fender 1 is defined by the height of the mounting portion 3, assuming that the height from the bottom surface of the mounting portion 3 to the top surface of the impact receiving portion 2 is H.
It is formed with a predetermined uniform inclination θ 1 (9°±2° with respect to the vertical line) inward toward the lower part 5 of the impact receiving part, and from the lower part 5 of the impact receiving part to the upper surface of the upper surface of the impact receiving part 2. is formed vertically. Note that the position of the lower part 5 of the impact receiving part is the same as that of the impact receiving part 2.
Approximately 0.1H from the top surface. Further, an upper groove 6 is formed around the entire circumference at a position approximately 0.2H from the upper surface of the impact receiving part 2, and the upper groove 6 is formed in the shape of a semicircular arc, and its radius is within the range of 0.01 to 0.015H. It is set to a predetermined size. Furthermore, it is omitted from the bottom of the mounting part 3.
A lower groove 7 is formed around the entire circumference at a position within a range of 0.1H, and the lower groove 7 is also set to have the same shape and dimensions as the upper groove 6.
一方、防舷装置1の内面は、取付部3底面より
略0.3H付近の支衝部中腹部8まで内方へ所定の
一様な傾斜角θ2(鉛直線に対してθ1+3〜4゜)を
有して形成されており、さらに同支衝部中腹部8
より受衝部下端部9に向かつて前記傾斜角θ2より
さらに内方に傾斜した傾斜角θ3(鉛直線に対して
θ1+4〜5゜)を有して形成されている。そして前
記受衝部下端部9より受衝部2上面までは垂直に
形成されている。なお、第6図に図示するよう
に、耐久性に関しては内面にRをつけた方が好ま
しく、また圧縮性能に対しては四隅隅部の肉厚が
厚すぎても変形量が小さくなる。したがつて、R
の範囲としては小さすぎると耐久性が悪く、大き
すぎても前述のごとく変位量不足を生ずるため、
適正範囲は0.08H≦R≦0.12Hである。 On the other hand, the inner surface of the fender 1 has a predetermined uniform inclination angle θ 2 (with respect to the vertical line θ 1 +3 to 4゜゜), and the mid-abdominal part 8
It is formed to have an inclination angle θ 3 (θ 1 +4 to 5° with respect to the vertical line) that is inclined further inwardly than the above-mentioned inclination angle θ 2 toward the lower impact-receiving end portion 9 . The portion from the lower end portion 9 of the impact receiving portion to the upper surface of the impact receiving portion 2 is vertically formed. As shown in FIG. 6, it is preferable to add a radius to the inner surface in terms of durability, and in terms of compression performance, even if the wall thickness at the four corners is too thick, the amount of deformation will be small. Therefore, R
If the range is too small, the durability will be poor, and if it is too large, the displacement will be insufficient as mentioned above.
The appropriate range is 0.08H≦R≦0.12H.
したがつて防舷装置1は取付部3より受衝部2
に向かつて次第に肉厚に形成されることになる。 Therefore, the fender 1 has a higher impact receiving part 2 than an attachment part 3.
It will gradually become thicker as it approaches.
第5図ないし第6図に図示される実施例は前記
したように構成されているので、防舷装置1に船
舶等の衝撃荷重が加わると第7図に図示されるよ
うに、同防舷装置1は変形することになる。すな
わち第7図は防舷装置1の変形状態を図示したも
のであり、同防舷装置1の圧縮荷重を受けたとき
の変位量を△Hとし、歪εを百分率で表わすこと
にすれば、ε=△H/H×100(%)となり、A図は
ε=0、B図はε=10、C図はε=20、D図はε
=30、E図はε=40、F図はε=50、G図はε=
55の状態をそれぞれ表わす。第7図から明らかな
ように、歪が極めて小さい間(ε=10)は、上溝
6の処でつぶれて相互に密着することはないが、
所定の歪以上となると(C図に示すε=20以上)、
上溝6はつぶれて相互に密着することになる。こ
のとき支衝部8は外方へふくらむ変形をなす。 Since the embodiment shown in FIGS. 5 and 6 is constructed as described above, when an impact load from a ship or the like is applied to the fender 1, the fender 1 will be damaged as shown in FIG. The device 1 will be deformed. That is, FIG. 7 illustrates the deformed state of the fender 1. If the amount of displacement of the fender 1 when subjected to a compressive load is ΔH, and the strain ε is expressed as a percentage, then ε=△H/H×100(%), ε=0 for figure A, ε=10 for figure B, ε=20 for figure C, ε for figure D.
= 30, E diagram is ε = 40, F diagram is ε = 50, G diagram is ε =
Each represents 55 states. As is clear from FIG. 7, while the strain is extremely small (ε=10), the upper grooves 6 do not collapse and come into close contact with each other;
When the strain exceeds a predetermined value (ε=20 or more shown in diagram C),
The upper grooves 6 are crushed and come into close contact with each other. At this time, the support portion 8 is deformed to swell outward.
さらに歪を大きくすればE図、F図に示すよう
に、上溝6より取付部3側の支衝部4はさらに外
方へふくらむ変形をなし、一方上溝6より上方の
受衝部2は外方へふくらむ変形はしないため、上
溝6の処で次第に座屈を起こし始め、上溝6より
上方の受衝部2は次第に外方へ膨出した支衝部4
内に陥没していく変形をなす。そしてG図に示す
ように歪ε=55になると、支衝部4の外壁と受衝
部2が接触することになる。このとき上溝6より
受衝部下部5までが所定の傾斜角θ1にて形成され
ているので、前記した圧縮荷重に対して反力を大
きくする機能を果たしている。すなわち、受衝部
下部5と上溝6間の傾斜部Iが圧縮変形を受ける
過程で受衝部2に対し直角になる。このような強
制変形を与える過程で、その反作用として反力が
増大する。仮に傾斜部Iが垂直なら圧縮反力は受
衝部2の曲げのみによつて生ずるため圧縮反力の
低下はあるが、変形は安定する。 If the strain is further increased, as shown in Figures E and F, the supporting part 4 on the side of the mounting part 3 from the upper groove 6 will further bulge outward, while the receiving part 2 above the upper groove 6 will expand outward. Since the deformation does not bulge in the direction, buckling gradually begins to occur at the upper groove 6, and the impact receiving part 2 above the upper groove 6 gradually bulges outward as the supporting part 4.
It becomes deformed by sinking inwards. When the strain ε=55 as shown in Figure G, the outer wall of the support portion 4 and the impact receiving portion 2 come into contact. At this time, since the area from the upper groove 6 to the lower part 5 of the impact receiving part is formed at a predetermined inclination angle θ 1 , it functions to increase the reaction force against the above-mentioned compressive load. That is, the inclined portion I between the lower part 5 of the impact receiving part and the upper groove 6 becomes perpendicular to the impact receiving part 2 during the process of being compressively deformed. In the process of applying such forced deformation, the reaction force increases as a reaction. If the slope I is vertical, the compression reaction force will be generated only by the bending of the impact receiving part 2, so although the compression reaction force will decrease, the deformation will be stabilized.
このように本実施例においては、取付部3より
受衝部2に向かつて次第に支衝部4を肉厚に形成
したため、支衝部中腹部8近傍より受衝部2まで
の断面積が比較的大きく、歪量の比較的小さい領
域(弾性変形領域)における圧縮反力の増加が大
きくなる。 As described above, in this embodiment, since the support part 4 is formed to be gradually thicker from the attachment part 3 toward the impact receiving part 2, the cross-sectional area from the vicinity of the midsection 8 of the support part to the impact receiving part 2 is comparatively large. The compressive reaction force increases greatly in a region (elastic deformation region) where the amount of strain is large and the amount of strain is relatively small (elastic deformation region).
また本実施例では、防舷装置1の外周に上溝6
を形成し、同上溝6の処で座屈変形を起こすよう
にしたため、同上溝6より取付部3までが柱長l
となつて同柱長lを短くすることができ、座屈反
力を極わめて大きくすることができる。したがつ
て、前記した弾性変形領域での圧縮反力の増加と
ともに、座屈変形領域においても座屈反力の増加
をはかることができる。 In addition, in this embodiment, an upper groove 6 is provided on the outer periphery of the fender 1.
Since buckling deformation occurs at the groove 6, the column length from the groove 6 to the mounting portion 3 is reduced to l.
Therefore, the column length l can be shortened, and the buckling reaction force can be extremely increased. Therefore, it is possible to increase the buckling reaction force in the buckling deformation area as well as increasing the compression reaction force in the elastic deformation area described above.
さらに本実施例においては、支衝部4を八角錐
体としたため、第7図に図示するように角錐面全
面が外側へふくらむ変形をなし、変位量も大きく
安定した変形となり、緩衝性が極わめて優れた防
舷装置となる。しかもこの安定した変形により各
部に均一に圧縮力を分散させることができるた
め、応力集中を避けることができる。 Furthermore, in this embodiment, since the support portion 4 is made of an octagonal pyramid, the entire surface of the pyramid is deformed to bulge outward as shown in FIG. It is an excellent fender. Moreover, this stable deformation allows compressive force to be uniformly distributed to each part, thereby avoiding stress concentration.
さらにまた本実施例では、取付部3近傍の外周
に下溝7を設けたため、圧縮力を受けた際、同下
溝7の処でつぶれて相互に密着し、同下溝7近傍
における歪量は内面の歪量に比較して大きくな
り、支衝部4の内外面の歪量の差により同支衝部
4の外面が外側へ傾斜し、この点からも角錐面全
面を外側へふくらむ変形をさせることができる。 Furthermore, in this embodiment, since the lower groove 7 is provided on the outer periphery near the attachment part 3, when compressive force is applied, the lower groove 7 collapses and comes into close contact with each other, and the amount of strain near the lower groove 7 is reduced by the inner surface. The difference in the amount of strain between the inner and outer surfaces of the support portion 4 causes the outer surface of the support portion 4 to incline outward, and from this point as well, the entire pyramidal surface is deformed to bulge outward. I can do it.
第4図ないし第7図に図示した実施例において
は、角錐面の各内面を直線で結んだが、第8図な
いし第9図に図示されるように、角錐面の内面の
四側部10を内方へふくらませて円孤状としても
よい。このようにすればさらに圧縮反力の増加を
はかることができる。 In the embodiments shown in FIGS. 4 to 7, the inner surfaces of the pyramidal surfaces are connected by straight lines, but as shown in FIGS. 8 to 9, the four sides 10 of the inner surfaces of the pyramidal surfaces are connected by straight lines. It may also be swollen inward to form a circular arc shape. In this way, the compression reaction force can be further increased.
また第10図ないし第11図に図示するよう
に、支衝部4の外面をふくらませて円孤状として
もよい。このようにすれば中立軸Y−Yは、外方
へ彎曲することとなり、圧縮力が働いた場合、必
然的に外方へ変形することになる。 Alternatively, as shown in FIGS. 10 to 11, the outer surface of the support portion 4 may be swollen to form a circular arc shape. In this way, the neutral axis Y-Y will curve outward, and will inevitably deform outward when a compressive force is applied.
第4図ないし第11図に図示した実施例では、
支衝部2にフランジを一体に形成し、同フランジ
がゴム本体から外方に出ていたが、第12図に図
示するごとく、フランジを除いてもよい。この場
合、支衝部2に鉄板11を埋設し、同鉄板11は
受衝部2の外壁と同一面にしてもよいし、同受衝
部2内に完全に埋めこんでもよい。そして同鉄板
11に袋ナツト12を一体に固定するかボルトを
固着して受衝板(図示せず)を取りつけるように
する。 In the embodiments illustrated in FIGS. 4 to 11,
Although the flange was integrally formed on the support portion 2 and protruded outward from the rubber body, the flange may be omitted as shown in FIG. 12. In this case, the iron plate 11 may be embedded in the support part 2, and the iron plate 11 may be flush with the outer wall of the impact receiving part 2, or may be completely buried within the impact receiving part 2. Then, a cap nut 12 is integrally fixed to the iron plate 11, or a bolt is firmly fixed thereto, and an impact receiving plate (not shown) is attached thereto.
このように、第12図に図示した実施例におい
ては、フランジを除いたため、フランジが膨出し
たゴム本体に接触することがないため、圧縮反力
が急激に上昇することがなくなり、船舶の接舷時
等における緩衝性が向上する。 In this way, in the embodiment shown in Fig. 12, since the flange is removed, the flange does not come into contact with the bulging rubber body, so the compression reaction force does not increase suddenly, and the contact of the ship is prevented. Improves cushioning properties during porttime, etc.
第1図は従来の防舷装置を図示した平面図、第
2図はその横断側面図、第3図はその−線に
沿つて截断した断面図、第4図はその圧縮状態を
図示した平面図、第5図は本発明に係る一実施例
を図示した横断側面図、第6図はその−線に
沿つて截断した断面図、第7図はその圧縮状態を
図示した説明図、第8図は本発明に係る他の実施
例を図示した横断側面図、第9図はその−線
に沿つて截断した断面図、第10図はさらに他の
実施例における横断側面図、第11図はその−
線に沿つて截断した断面図、第12図はさらに
また他の実施例における横断側面図である。
1…防舷装置、2…受衝部、3…取付部、4…
支衝部、5…受衝部下部、6…上溝、7…下溝、
8…支衝部中復部、9…受衝部下端部、10…四
側部、11…鉄板、12…袋ナツト。
Fig. 1 is a plan view showing a conventional fender, Fig. 2 is a cross-sectional side view thereof, Fig. 3 is a cross-sectional view taken along the - line, and Fig. 4 is a plan view illustrating its compressed state. 5 is a cross-sectional side view illustrating one embodiment of the present invention, FIG. 6 is a sectional view taken along the - line, FIG. 7 is an explanatory diagram illustrating its compressed state, and FIG. The figure is a cross-sectional side view illustrating another embodiment according to the present invention, FIG. 9 is a cross-sectional view taken along the - line, FIG. 10 is a cross-sectional side view of still another embodiment, and FIG. That-
FIG. 12 is a cross-sectional view taken along a line, and FIG. 12 is a cross-sectional side view of yet another embodiment. 1... fender device, 2... impact receiving part, 3... mounting part, 4...
Support part, 5... lower part of impact receiving part, 6... upper groove, 7... lower groove,
8... Central restoration part of the support part, 9... Lower end of the impact receiving part, 10... Four side parts, 11... Iron plate, 12... Cap nut.
Claims (1)
側を受衝端となし、大径側を取付け端となした防
舷装置において、前記筒状体の肉厚を取付け端側
より受衝端側に向かつて次第に肉厚となし、該筒
状体外周の受衝端側所定位置に溝を形成し、該筒
状体の内面および外面のいずれか一方または両方
を多角錐体となしたことを特徴とする防舷装置。1. In a fender device in which the small diameter side of a hollow tapered cylindrical body made of a rubber elastic body is the impact receiving end and the large diameter side is the mounting end, the wall thickness of the cylindrical body is increased from the mounting end to the impact receiving end. The thickness gradually increases toward the side, a groove is formed at a predetermined position on the impact-receiving end side of the outer periphery of the cylindrical body, and one or both of the inner and outer surfaces of the cylindrical body are formed into a polygonal pyramid. A fender device featuring:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58003315A JPS59130907A (en) | 1983-01-14 | 1983-01-14 | Fender device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP58003315A JPS59130907A (en) | 1983-01-14 | 1983-01-14 | Fender device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS59130907A JPS59130907A (en) | 1984-07-27 |
| JPH041129B2 true JPH041129B2 (en) | 1992-01-10 |
Family
ID=11553919
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP58003315A Granted JPS59130907A (en) | 1983-01-14 | 1983-01-14 | Fender device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS59130907A (en) |
-
1983
- 1983-01-14 JP JP58003315A patent/JPS59130907A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS59130907A (en) | 1984-07-27 |
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