JP2013028908A

JP2013028908A - Fender

Info

Publication number: JP2013028908A
Application number: JP2011164124A
Authority: JP
Inventors: Kohei Morita; 耕平森田; Koji Marui; 浩司丸井
Original assignee: Sumitomo Rubber Industries Ltd
Current assignee: Sumitomo Rubber Industries Ltd
Priority date: 2011-07-27
Filing date: 2011-07-27
Publication date: 2013-02-07
Anticipated expiration: 2031-07-27
Also published as: JP5453359B2

Abstract

PROBLEM TO BE SOLVED: To provide a fender with a simpler structure which can regulate the folding in the middle of an axial direction, of connected buffer members and which can prevent the individual buffer member from being compressed excessively in the axial direction, surely as much as possible.SOLUTION: In a fender, a first buffer member 5 fixed to a face 2 to be contacted by the side of a ship such as a pier and a second buffer member 6 softer than the first buffer member fixed to an impact receiving plate 3 to which a ship and others are contacted are connected through a spacer 7 in an axial direction, and the spacer 7 is provided with a stopper 24 which prevents the second buffer member from being compressed excessively in the axial direction by regulating the compressive deformation amount in the axial direction of the second buffer member.

Description

本発明は、岸壁や桟橋などの被接舷面への、船舶や艀など（以下「船舶等」と総称する場合がある。）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、当該船舶等を前記衝撃から保護するための防舷材に関するものである。 The present invention absorbs energy at the time of contact of a ship, a dredger, etc. (hereinafter sometimes referred to as “vessel etc.”) on a surface to be welded such as a quay or a pier, thereby reducing the impact. The present invention relates to a fender for protecting the ship or the like from the impact.

前記岸壁や桟橋などの被接舷面には、船舶等を接岸したり係留したりする接舷時に発生するエネルギーを吸収して衝撃を緩和することで、当該船舶等を前記衝撃から保護するための防舷材を設置するのが一般的である。
前記防舷材としては、前記被接舷面に固定され、船舶等の接舷によって圧縮変形されて前記エネルギーを吸収する、例えばゴム等の弾性材料からなる緩衝部材を備えたものが広く用いられる（例えば特許文献１等参照）。 In order to protect the said ship etc. from the said impact by absorbing the energy which generate | occur | produces at the time of the mooring of berthing or mooring a ship etc. on the to-be-joined surface of the said quay or pier etc. It is common to install fenders.
As the fender, a material provided with a buffer member made of an elastic material such as rubber, which is fixed to the surface to be contacted and is compressed and deformed by the contact of a ship or the like to absorb the energy, is widely used. (See, for example, Patent Document 1).

前記防舷材には、前記エネルギーを吸収する性能に優れる上、圧縮変形によって生じる緩衝部材の反発を低く抑えて、前記反発力によって船舶等が損傷するのを防止することが求められる。
かかる要求を満足するため、圧縮変形時に緩衝部材が座屈変形する位置の付近に、前記座屈変形を規制する硬質材を埋設する等の工夫がされている（例えば特許文献２等参照）。 The fender is required to have excellent performance for absorbing the energy, and to suppress the repulsion of the buffer member caused by the compression deformation to prevent the ship from being damaged by the repulsive force.
In order to satisfy such a requirement, a contrivance has been made such as embedding a hard material that restricts the buckling deformation in the vicinity of the position where the buffer member buckles and deforms during compression deformation (see, for example, Patent Document 2).

しかし特許文献１、２に記載されているように緩衝部材を一つだけ備えた防舷材では、前記の要求に十分に対応することができないのが現状である。
そこで２つ以上の緩衝部材を、船舶等の接舷による主たる圧縮変形方向、すなわち被接舷面の面方向と直交方向（以下「軸方向」と記載する場合がある。）に直列的に連結した複合構造を有する防舷材が採用される。 However, as described in Patent Documents 1 and 2, the present situation is that a fender having only one buffer member cannot sufficiently meet the above requirements.
Therefore, two or more buffer members are connected in series in the main compression deformation direction due to the contact of a ship or the like, that is, in the direction orthogonal to the surface direction of the contacted surface (hereinafter sometimes referred to as “axial direction”). A fender having a composite structure is employed.

特開２０００−３０９９１４号公報JP 2000-309914 A 特開２００１−７３３４６号公報JP 2001-73346 A

防舷材には、前記軸方向だけでなく、前記軸方向と交差する被接舷面の面方向（以下「交差方向」と記載する場合がある。）へのせん断力も複合的に作用し、それらは複合して不均一な負荷を発生する。そのため従来の防舷材では、緩衝部材の変形が不安定化して十分な性能が発揮されない場合がある。
例えば、前記複合構造を有する防舷材を構成する、軸方向に連結した緩衝部材のいずれかが、前記軸方向の途中の位置で異常な座屈（中折れ）を生じたり、個々の緩衝部材が、設定された圧縮量を超えて軸方向に過圧縮されたりしやすく、これらの問題が発生すると、船舶等の接舷のエネルギーを十分に吸収できなかったり、反発力が大きくなって船舶等が損傷したりするおそれが生じる。 In the fender, not only the axial direction but also the shearing force in the surface direction of the surface to be contacted intersecting the axial direction (hereinafter sometimes referred to as “crossing direction”) acts in a complex manner, They combine to generate uneven loads. Therefore, in the conventional fender, the deformation of the buffer member may become unstable and sufficient performance may not be exhibited.
For example, any of the buffer members connected in the axial direction constituting the fender having the composite structure may cause abnormal buckling (breaking) at an intermediate position in the axial direction, or individual buffer members However, it is easy to over-compress in the axial direction beyond the set compression amount, and when these problems occur, the energy of the vessel and the like can not be sufficiently absorbed or the repulsive force increases and the vessel etc. May be damaged.

そこで、
(1) 緩衝部材の外周を囲むように、前記被接舷面から軸方向に複数本のガイド棒を突設し、前記ガイド棒によって緩衝部材の変形をガイドして、前記中折れが生じるのを規制したり、
(2) 連結した緩衝部材が、あらかじめ許容される軸方向の最大変形量まで圧縮変形した際に、前記ガイド棒の先端が、連結した緩衝部材の先端に固定される、船舶等に接触する受衝板の裏面に当接するように、前記ガイド棒の突出高さを設定することで、緩衝部材が軸方向に過圧縮されるのを防止したり、
することが検討されている。 there,
(1) A plurality of guide bars are projected in the axial direction from the surface to be contacted so as to surround the outer periphery of the buffer member, and the deformation of the buffer member is guided by the guide bar, so that the middle folding occurs. Or regulate
(2) When the connected buffer member is compressed and deformed to the maximum allowable axial deformation amount, the tip of the guide bar is fixed to the tip of the connected buffer member and contacts the ship or the like. By setting the protruding height of the guide rod so as to contact the back surface of the impact plate, the buffer member can be prevented from being overcompressed in the axial direction,
To be considered.

しかし前記ガイド棒を設ける必要があること、緩衝部材側に、前記ガイド棒によってガイドされる被ガイド部を設ける必要があること等から、前記防舷材は、構成部品が多く構造が複雑で、しかもガイド棒設置のために通常よりも広い設置面積が必要になるという問題がある。
緩衝部材を略筒状に形成し、連結した複数の緩衝部材の筒内を貫通させてガイド棒を設けることも考えられ、その場合はガイド棒の本数を減らすとともに設置面積を小さく抑えることができる。 However, since it is necessary to provide the guide rod, and it is necessary to provide a guided portion guided by the guide rod on the buffer member side, the fender has many components and the structure is complicated. Moreover, there is a problem that a larger installation area than usual is required for installing the guide rod.
It is conceivable that the buffer member is formed in a substantially cylindrical shape and the guide rods are provided by penetrating through the cylinders of the plurality of coupled buffer members. In this case, the number of guide rods can be reduced and the installation area can be reduced. .

しかし、前記のようにガイド棒には、軸方向に連結した緩衝部材に加わる交差方向のせん断力に抗して前記緩衝部材が中折れするのを確実に防止できることが求められる上、前記ガイド棒を、軸方向に連結した複数の緩衝部材全体の、軸方向の最大変形量と略一致するように、被接舷面から軸方向に大きく突出させる必要がある。
そのため本数を減らすほど、個々のガイド棒を、途中で変形したり折れたりしないようにできるだけ頑丈に構成するとともに、根元から倒れこんだりしないようにしっかりと被接舷面に設置する必要がある。 However, as described above, the guide bar is required to be able to reliably prevent the buffer member from being bent against the shearing force in the cross direction applied to the buffer member connected in the axial direction. Needs to be protruded greatly in the axial direction from the surface to be contacted so as to substantially coincide with the maximum amount of axial deformation of the entire plurality of buffer members connected in the axial direction.
Therefore, as the number is reduced, it is necessary to construct each guide bar as firmly as possible so that it does not deform or break along the way, and to firmly install it on the surface of the contact so as not to fall down from the root.

本発明の目的は、より簡易な構造で、しかもできるだけ確実に、連結した緩衝部材が軸方向の途中で中折れするのを規制したり、個々の緩衝部材が軸方向に過圧縮されるのを防止したりできる防舷材を提供することにある。 An object of the present invention is to prevent the connected buffer members from being bent in the middle of the axial direction with a simpler structure and as reliably as possible, and to prevent individual buffer members from being overcompressed in the axial direction. The object is to provide a fender that can be prevented.

本発明は、被接舷面に設置され、前記被接舷面への船舶等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、当該船舶等を前記衝撃から保護するための防舷材であって、前記防舷材は、
前記被接舷面に対して略平行に配設され、船舶等に接触する受衝板、および前記受衝板と被接舷面との間に介在される緩衝部材を備え、前記緩衝部材は、
全体がゴム等の弾性材料からなり、前記被接舷面に固定され、前記受衝板への船舶等の接舷によって圧縮変形されて前記エネルギーを吸収する第一緩衝部材、
前記第一緩衝部材より軟質の弾性材料からなり、前記受衝板に固定され、前記受衝板への船舶等の接舷によって圧縮変形されて前記エネルギーを吸収する第二緩衝部材、および
前記第一、第二緩衝部材間に介在されて前記両緩衝部材を連結する、剛性体からなるスペーサを備えているとともに、
前記スペーサおよび受衝板のうちの少なくとも一方は、前記第二緩衝部材の、前記受衝板の面方向と直交方向（軸方向）の圧縮変形量を規制して、前記第二緩衝部材の、同方向への過圧縮を防止するためのストッパを備えていることを特徴とするものである。 The present invention is installed on a contact surface and absorbs energy at the time of contact of the ship or the like with the contact surface to mitigate the impact, thereby protecting the ship or the like from the impact. A fender, wherein the fender is
An impact plate disposed substantially parallel to the surface to be contacted and contacting a ship or the like, and a buffer member interposed between the impact plate and the surface to be contacted; ,
A first buffer member that is entirely made of an elastic material such as rubber, is fixed to the surface to be contacted, and is compressed and deformed by contact with the receiving plate such as a ship to absorb the energy;
A second buffer member made of an elastic material softer than the first buffer member, fixed to the receiving plate, and compressed and deformed by contact of the ship with the receiving plate to absorb the energy; and And a spacer made of a rigid body, which is interposed between the first and second buffer members and connects the two buffer members.
At least one of the spacer and the receiving plate regulates the amount of compressive deformation of the second buffer member in a direction orthogonal to the surface direction of the receiving plate (axial direction), and the second buffer member A stopper for preventing over-compression in the same direction is provided.

本発明によれば、スペーサを介して軸方向に連結する第一および第二緩衝部材のうち受衝板側の第二緩衝部材を、被接舷面側の第一緩衝部材より軟質の弾性材料で形成しているため、前記受衝板に船舶等が接舷する際には、必ず前記第二緩衝部材を、第一緩衝部材の変形に先立って変形させることができる。つまり船舶等の接舷時に先行して圧縮される緩衝部材を、第二緩衝部材に特定することができる。 According to the present invention, the second buffer member on the side of the receiving plate among the first and second buffer members coupled in the axial direction via the spacer is made of an elastic material that is softer than the first buffer member on the contact surface side. Therefore, when a ship or the like touches the receiving plate, the second buffer member can always be deformed prior to the deformation of the first buffer member. That is, the buffer member that is compressed in advance when the ship or the like is in contact can be specified as the second buffer member.

そのため前記第二緩衝部材側にのみ、軸方向の過圧縮を防止するためのストッパを設けるだけで、前記過圧縮によって反発力が大きくなって船舶等が損傷したりするのを防止することができる。またストッパ自体も、前記第二緩衝部材の過圧縮のみを防止するだけでよいため、従来のガイド棒に比べて小さくすることができる。
また、応力が集中して中折れを生じやすい被接舷面側の第一緩衝部材を、前記のように第二緩衝部材より硬質の弾性材料で形成することで、前記中折れが発生するのを抑制することもできる。 Therefore, only by providing a stopper for preventing over-compression in the axial direction only on the second buffer member side, it is possible to prevent the over-compression from increasing the repulsive force and damaging a ship or the like. . Further, the stopper itself can be made smaller than a conventional guide bar because it only needs to prevent over-compression of the second buffer member.
In addition, since the first buffer member on the side of the contact surface that is likely to be bent due to concentration of stress is formed of an elastic material harder than the second buffer member as described above, the above-described middle break occurs. Can also be suppressed.

したがって本発明によれば、より簡易な構造で、しかもできるだけ確実に、連結した緩衝部材が軸方向の途中で中折れするのを規制したり、個々の緩衝部材が軸方向に過圧縮されるのを防止したりできる防舷材を提供することができる。
前記第二緩衝部材は、その両端が開口された略筒状に形成され、前記両端がそれぞれ受衝板、およびスペーサに当接されて前記両開口が塞がれているとともに、前記スペーサおよび受衝板のうちの一方の、前記開口に臨み、前記第二緩衝部材によって囲まれた領域内にストッパが設けられており、スペーサおよび受衝板のうちの他方の、前記開口に臨み、前記第二緩衝部材によって囲まれた領域が、前記第二緩衝部材の圧縮変形によって前記ストッパが当接される被当接面とされているのが好ましい。 Therefore, according to the present invention, with a simpler structure and as reliably as possible, it is possible to restrict the connected buffer members from being bent halfway in the axial direction, or individual buffer members are over-compressed in the axial direction. It is possible to provide a fender that can prevent the above.
The second buffer member is formed in a substantially cylindrical shape having both ends opened, and both the ends are in contact with an impact plate and a spacer so that both the openings are closed, and the spacer and the receiver are also closed. A stopper is provided in an area of one of the impact plates facing the opening and surrounded by the second buffer member, and faces the opening of the other of the spacer and the impact plate, and the first It is preferable that a region surrounded by the two buffer members is a contacted surface on which the stopper comes into contact with the second buffer member by compressive deformation.

これにより、第二緩衝部材をスペーサおよび受衝板に固定するための面積以外に、ストッパの設置のための余計な面積を必要とせずに前記ストッパを設けることができ、防舷材の構造をより一層簡略化することができる。
前記第一緩衝部材、スペーサ、および第二緩衝部材は、それぞれ受衝板の面方向に複数個ずつ設けられているとともに、前記複数のスペーサは、剛性体からなる連結部材を介して互いに一体に連結されているのが好ましい。 Thus, in addition to the area for fixing the second buffer member to the spacer and the receiving plate, the stopper can be provided without requiring an extra area for installing the stopper, and the structure of the fender is It can be further simplified.
A plurality of the first buffer members, spacers, and second buffer members are provided in the surface direction of the receiving plate, respectively, and the plurality of spacers are integrated with each other via a connecting member made of a rigid body. Preferably they are linked.

これにより、隣り合う緩衝部材のせん断抵抗力を、前記スペーサおよび連結部材を介して連結して発揮させることができるため、交差方向のせん断力によって個々の緩衝部材に不均一な負荷が加わるのを防止して、前記中折れや過圧縮が発生するのをさらに確実に防止することができる。 Thereby, since the shear resistance force of the adjacent buffer member can be exerted by being connected via the spacer and the connecting member, it is possible to apply an uneven load to the individual buffer members due to the shearing force in the crossing direction. It is possible to prevent the occurrence of the middle break and over-compression more reliably.

本発明によれば、より簡易な構造で、しかもできるだけ確実に、連結した緩衝部材が軸方向の途中で中折れするのを規制したり、個々の緩衝部材が軸方向に過圧縮されるのを防止したりできる防舷材を提供することができる。 According to the present invention, it is possible to restrict the connected buffer members from being bent in the middle in the axial direction with a simpler structure and as reliably as possible, and to prevent individual buffer members from being overcompressed in the axial direction. It is possible to provide a fender that can be prevented.

本発明の防舷材の、実施の形態の一例を示す断面図である。It is sectional drawing which shows an example of embodiment of the fender of this invention. 図１の例の防舷材を構成する第一および第二緩衝部材の外観を示す斜視図である。It is a perspective view which shows the external appearance of the 1st and 2nd buffer member which comprises the fender of the example of FIG. 図１の例の防舷材を構成するスペーサ、およびストッパの外観を示す斜視図である。It is a perspective view which shows the external appearance of the spacer which comprises the fender of the example of FIG. 1, and a stopper. 本発明の防舷材の、実施の形態の他の例を示す斜視図である。It is a perspective view which shows the other example of embodiment of the fender of this invention. スペーサの接続構造の他の例を示す平面図である。It is a top view which shows the other example of the connection structure of a spacer. 図５の一部を拡大した平面図である。It is the top view which expanded a part of FIG.

図１は、本発明の防舷材の、実施の形態の一例を示す断面図である。図２は、図１の例の防舷材を構成する第一および第二緩衝部材の外観を示す斜視図である。図３は、図１の例の防舷材を構成するスペーサ、およびストッパの外観を示す斜視図である。
図１を参照して、この例の防舷材１は、岸壁等の被接舷面２に対して略平行に配設され、図示しない船舶等に接触する受衝板３、および前記受衝板３と被接舷面２との間に介在される緩衝部材４を備えている。 FIG. 1 is a cross-sectional view showing an example of an embodiment of the fender according to the present invention. FIG. 2 is a perspective view showing the outer appearance of the first and second cushioning members constituting the fender of the example of FIG. FIG. 3 is a perspective view showing the appearance of the spacers and stoppers constituting the fender of the example of FIG.
Referring to FIG. 1, a fender 1 of this example is disposed substantially parallel to a surface 2 to be contacted such as a quay, and receives an impact plate 3 that contacts a ship (not shown) and the like. A buffer member 4 is provided between the plate 3 and the contact surface 2.

また緩衝部材４は、
全体がゴム等の弾性材料からなり、前記被接舷面２に固定され、前記受衝板３への船舶等の接舷によって、被接舷面２の面方向と直交方向、つまり図中に二点鎖線で示す軸Ｌ０の方向（軸方向）に圧縮変形されて前記エネルギーを吸収する第一緩衝部材５、
前記第一緩衝部材５より軟質の弾性材料からなり、前記受衝板３に固定され、前記受衝板３への船舶等の接舷によって前記軸方向に圧縮変形されて前記エネルギーを吸収する第二緩衝部材６、および
前記第一、第二緩衝部材５、６間に介在されて前記両緩衝部材５、６を連結する、剛性体からなるスペーサ７を備えている。 The buffer member 4 is
The whole is made of an elastic material such as rubber, and is fixed to the contacted surface 2. By contact of the receiving plate 3 with a ship or the like, the direction orthogonal to the surface direction of the contacted surface 2, that is, in the figure. A first buffer member 5 that is compressed and deformed in the direction of the axis L0 indicated by a two-dot chain line (axial direction) to absorb the energy;
The first buffer member 5 is made of an elastic material softer than the first buffer member 5, is fixed to the impact plate 3, and is compressed and deformed in the axial direction by a ship or the like contacting the impact plate 3 to absorb the energy. Two buffer members 6, and a spacer 7 made of a rigid body that is interposed between the first and second buffer members 5, 6 and connects the buffer members 5, 6.

前記両緩衝部材５、６、およびスペーサ７は、それぞれの中心軸Ｌ１、Ｌ２（図２、図３参照）を互いに一致させるとともに、前記中心軸Ｌ１、Ｌ２の方向を前記軸Ｌ０の方向に一致させた状態で一体に連結されて、前記受衝板３と被接舷面２との間に介在されている。
図１、図２を参照して、前記のうち第一、第二緩衝部材５、６は、それぞれ、外径が一定の略円筒状に形成され、その一端面がスペーサ７への連結面８とされた連結部９、前記連結部９の他端側から被接舷面２へ向けて、その外径がテーパー状に拡がる中空円錐状の支衝部１０、および前記支衝部１０の、被接舷面２側の端部から径方向外方へ延設された、前記被接舷面２への固定部となる円形鍔状のフランジ１１を備えている。 The buffer members 5 and 6 and the spacer 7 have their central axes L1 and L2 (see FIGS. 2 and 3) aligned with each other, and the directions of the central axes L1 and L2 are aligned with the direction of the axis L0. In this state, they are integrally connected and are interposed between the receiving plate 3 and the contacted surface 2.
1 and 2, the first and second buffer members 5 and 6 are each formed in a substantially cylindrical shape having a constant outer diameter, and one end surface thereof is a connection surface 8 to the spacer 7. The connecting portion 9, the hollow conical support portion 10 whose outer diameter expands in a tapered shape from the other end side of the connecting portion 9 toward the contact surface 2, and the support portion 10. A circular flange-shaped flange 11 is provided that extends radially outward from an end of the contacted flange surface 2 and serves as a fixed portion to the contacted flange surface 2.

前記連結部９、支衝部１０、およびフランジ１１は、それぞれの中心軸Ｌ１を互いに一致させた状態で、前記のようにゴム等の弾性材料によって一体に形成されている。
連結面８は円形とされ、その中央には、中心軸Ｌ１を中心として前記連結面８と同心状に円形の通孔１２が形成されている。また支衝部１０は、フランジ１１側でも開口されている。これにより第一、第二緩衝部材５、６は、それぞれ両端が開口された略筒状に形成されている。 The connecting portion 9, the abutting portion 10, and the flange 11 are integrally formed of an elastic material such as rubber as described above in a state where the central axes L1 coincide with each other.
The connecting surface 8 has a circular shape, and a circular through hole 12 is formed in the center of the connecting surface 8 so as to be concentric with the connecting surface 8 with the central axis L1 as the center. Further, the support portion 10 is also opened on the flange 11 side. Thereby, the 1st, 2nd buffer members 5 and 6 are each formed in the substantially cylindrical shape by which both ends were opened.

前記通孔１２の周囲には、前記連結面８にスペーサ７を連結して固定するためのボルト（図１中に破線で示す）が螺合される複数のネジ孔１３が形成されている。各ネジ孔１３は、中心軸Ｌ１を中心として同心状で、かつ周方向に互いに等間隔に配列されている。
図１を参照して、支衝部１０の内周面１４のうち、軸方向の略中央には、前記内周面１４から径方向内方へ突出させて、前記内周面１４の全周に亘る環状の凸部１５が一体に形成されている。 Around the through hole 12, a plurality of screw holes 13 are formed into which bolts (shown by broken lines in FIG. 1) for connecting and fixing the spacer 7 to the connecting surface 8 are screwed. The screw holes 13 are concentric about the central axis L1 and are arranged at equal intervals in the circumferential direction.
Referring to FIG. 1, in the inner peripheral surface 14 of the support portion 10, a substantially central portion in the axial direction is protruded radially inward from the inner peripheral surface 14, and the entire circumference of the inner peripheral surface 14. An annular convex portion 15 is integrally formed.

また図１、図２を参照して、支衝部１０の外周面１６のうち、前記軸方向の、フランジ１１寄りの位置には、前記外周面１６から径方向外方へ突出させて、凸部１７が一体に形成されている。
フランジ１１には、第一、第二緩衝部材５、６をそれぞれ被接舷面２、受衝板３に固定するためのボルト（図１中に破線で示す）が挿通される複数の通孔１８が形成されている。各通孔１８は、中心軸Ｌ１を中心として同心状で、かつ周方向に互いに等間隔に設けられている。 1 and 2, the outer peripheral surface 16 of the abutting portion 10 is protruded radially outward from the outer peripheral surface 16 at a position near the flange 11 in the axial direction. The part 17 is integrally formed.
A plurality of through holes through which bolts (shown by broken lines in FIG. 1) for fixing the first and second buffer members 5 and 6 to the contact surface 2 and the receiving plate 3 are inserted in the flange 11. 18 is formed. The respective through holes 18 are concentric with respect to the central axis L1 and are provided at equal intervals in the circumferential direction.

凸部１７は、支衝部１０の外周面１６に、周方向に複数に別けて、前記複数の通孔１８と交互に配設されている。
支衝部１０の内外周面１４、１６に前記凸部１５、１７を設けることにより、第一、第二緩衝部材５、６に軸方向の圧縮力が加わった際に、前記支衝部１０を、常に一定の形状に圧縮変形させることができる。そのため前記両緩衝部材５、６の圧縮変形形状と、前記圧縮変形によって吸収できるエネルギー量とを安定化させることができる。 The convex portions 17 are alternately arranged with the plurality of through holes 18 on the outer peripheral surface 16 of the support portion 10 in a plurality in the circumferential direction.
By providing the convex portions 15 and 17 on the inner and outer peripheral surfaces 14 and 16 of the support portion 10, when an axial compressive force is applied to the first and second buffer members 5 and 6, the support portion 10. Can always be compressed and deformed into a constant shape. Therefore, the compression deformation shape of both the buffer members 5 and 6 and the amount of energy that can be absorbed by the compression deformation can be stabilized.

前記のように第一緩衝部材５は、全体がゴム等の弾性材料によって一体に形成され、第二緩衝部材６は、前記第一緩衝部材５より軟質の弾性材料によって一体に形成される。
両緩衝部材５、６を、それぞれどの程度の硬さを有する弾性材料によって形成するかは特に限定されないが、例えば第一緩衝部材５は、ＪＩＳＡ型硬さで表して７０〜７５°程度の弾性材料によって形成するのが好ましい。 As described above, the entire first buffer member 5 is integrally formed of an elastic material such as rubber, and the second buffer member 6 is integrally formed of an elastic material softer than the first buffer member 5.
There is no particular limitation on how hard each of the shock-absorbing members 5 and 6 is formed of an elastic material. For example, the first shock-absorbing member 5 has a JIS A-type hardness of about 70 to 75 °. It is preferably formed of an elastic material.

ＪＩＳＡ型硬さが前記範囲未満では、第一緩衝部材５を圧縮変形させることによって吸収できるエネルギー量が不足し、逆に前記範囲を超える場合には反発力が強くなりすぎるため、いずれの場合にも、船舶等を衝撃から保護する効果が十分に得られないおそれがある。
また第二緩衝部材６は、前記第一緩衝部材５よりもＪＩＳＡ型硬さが小さく、かつその差が１°以上、好ましくは２°以上である弾性材料によって形成するのが、先に説明した、船舶等の接舷時に先行して圧縮される緩衝部材を前記第二緩衝部材６に特定する効果を、より一層良好に発現させる上で好ましい。 If the JIS A-type hardness is less than the above range, the amount of energy that can be absorbed by compressing and deforming the first buffer member 5 is insufficient, and conversely, if it exceeds the above range, the repulsive force becomes too strong. In addition, there is a risk that the effect of protecting the ship or the like from impacts may not be sufficiently obtained.
The second buffer member 6 is formed of an elastic material having a JIS A-type hardness smaller than that of the first buffer member 5 and a difference of 1 ° or more, preferably 2 ° or more. The effect of specifying the second buffer member 6 as the buffer member to be compressed in advance at the time of the contact of a ship or the like is preferable in further expressing the effect.

ただし第二緩衝部材６が軟らかすぎると、当該第二緩衝部材６によって吸収できるエネルギー量が不足して、船舶等を衝撃から保護する効果が十分に得られないおそれがある。そのため前記第二緩衝部材６は、第一緩衝部材５よりもＪＩＳＡ型硬さが小さく、かつその差が、５°以下、特に３°以下である弾性材料によって形成するのが好ましい。
図１、図３を参照して、スペーサ７は、外径が一定の略円柱状に形成された本体１９と、前記本体１９の両端部から径方向外方へ延設された、一対の円形鍔状のフランジ２０、２０とを備えている。前記本体１９、およびフランジ２０、２０は、それぞれの中心軸Ｌ２を互いに一致させた状態で、例えば鋼材等の剛性体によって一体に形成されている。 However, if the second buffer member 6 is too soft, the amount of energy that can be absorbed by the second buffer member 6 is insufficient, and the effect of protecting the ship or the like from impact may not be sufficiently obtained. Therefore, the second buffer member 6 is preferably formed of an elastic material having a JIS A type hardness smaller than that of the first buffer member 5 and a difference of 5 ° or less, particularly 3 ° or less.
Referring to FIGS. 1 and 3, the spacer 7 includes a main body 19 formed in a substantially cylindrical shape with a constant outer diameter, and a pair of circular shapes extending radially outward from both ends of the main body 19. The flanges 20 and 20 are provided. The main body 19 and the flanges 20 and 20 are integrally formed of a rigid body such as a steel material in a state where the respective central axes L2 coincide with each other.

前記本体１９の両端面は、それぞれフランジ２０、２０の外側面と同一平面に形成されて、前記第一、第二緩衝部材５、６の連結部９への連結面２１とされている。
フランジ２０、２０にはそれぞれ、前記連結面２１を連結部９の連結面８に当接させた状態で互いに固定することで、第一、第二緩衝部材５、６を、スペーサ７を介して連結するためのボルト（図１中に破線で示す）が挿通される複数の通孔２２が形成されている。各通孔２２は、連結面８に形成された隣り合う２つのネジ孔１３に対応する円弧状の長孔とされている。各通孔２２の円弧は、中心軸Ｌ２を中心として同心状に形成されている。また各通孔２２は、中心軸Ｌ２を中心として同心状で、かつ周方向に互いに等間隔に設けられている。 Both end surfaces of the main body 19 are formed in the same plane as the outer surfaces of the flanges 20 and 20, respectively, and serve as connecting surfaces 21 to the connecting portions 9 of the first and second buffer members 5 and 6.
The flanges 20 and 20 are fixed to each other in a state in which the connecting surface 21 is in contact with the connecting surface 8 of the connecting portion 9 so that the first and second buffer members 5 and 6 are interposed via the spacer 7. A plurality of through holes 22 are formed through which bolts (indicated by broken lines in FIG. 1) for connection are inserted. Each through hole 22 is a long arc-shaped hole corresponding to two adjacent screw holes 13 formed in the connecting surface 8. The circular arc of each through hole 22 is formed concentrically about the central axis L2. The through holes 22 are concentric with respect to the central axis L2 and are provided at equal intervals in the circumferential direction.

前記本体１９の外周面の複数箇所には、一対のフランジ２０、２０間を繋いで、前記外周面から径方向外方へ延設された平板状の補強材２３が設けられている。各補強材２３は、中心軸Ｌ２から放射状に設けられている。前記補強材２３もまた、例えば鋼材等の剛性体によって、前記本体１９、およびフランジ２０、２０と一体に形成されている。
スペーサ７の、第二緩衝部材６側の連結面２１には、前記第二緩衝部材６の、軸方向への圧縮変形量を規制して、その過圧縮を防止するためのストッパ２４が設けられる。 At a plurality of locations on the outer peripheral surface of the main body 19, flat reinforcing members 23 extending from the outer peripheral surface radially outward are provided so as to connect the pair of flanges 20, 20. Each reinforcing member 23 is provided radially from the central axis L2. The reinforcing member 23 is also formed integrally with the main body 19 and the flanges 20 and 20 by a rigid body such as steel.
The connecting surface 21 of the spacer 7 on the second buffer member 6 side is provided with a stopper 24 for restricting the amount of compressive deformation of the second buffer member 6 in the axial direction and preventing its over compression. .

ストッパ２４は、この例では、外径が一定の略円柱体からなる。前記ストッパ２４は、例えば鋼材等の剛性体によって形成されている。前記外径は、第二緩衝部材６の連結面８の通孔１２の内径よりも小径とされており、それによってスペーサ７の連結面２１に設けられたストッパ２４が、前記通孔１２を通して第二緩衝部材６の筒内に突出させて配設される。 In this example, the stopper 24 is formed of a substantially cylindrical body having a constant outer diameter. The stopper 24 is formed of a rigid body such as a steel material. The outer diameter is smaller than the inner diameter of the through-hole 12 of the connecting surface 8 of the second buffer member 6, so that a stopper 24 provided on the connecting surface 21 of the spacer 7 passes through the through-hole 12. The two buffer members 6 are disposed so as to protrude into the cylinder.

ストッパ２４の一端面は、前記連結面２１への連結面２５とされ、他端面は、次に説明するように第二緩衝部材６が軸方向に圧縮変形された際に、受衝板３の裏面に当接する当接面２６とされている。
図１を参照して、ストッパ２４は、軸方向の高さＨ１が、第二緩衝部材６の無負荷時の高さＨ２から、前記第二緩衝部材６に設定された圧縮変形時の高さＨ３を差し引いた値に設定される。そのため、受衝板３への船舶等の接舷によって、第二緩衝部材６が軸方向に前記高さＨ３まで圧縮変形されると、ストッパ２４の当接面２６が受衝板３の裏面に当接してそれ以上の圧縮変形を規制することで、前記第二緩衝部材６の過圧縮が防止される。 One end face of the stopper 24 is a connecting face 25 to the connecting face 21, and the other end face of the impact receiving plate 3 when the second buffer member 6 is compressed and deformed in the axial direction as will be described below. The contact surface 26 is in contact with the back surface.
Referring to FIG. 1, the stopper 24 has an axial height H <b> 1 at the time of compressive deformation set in the second buffer member 6 from a height H <b> 2 when the second buffer member 6 is unloaded. It is set to a value obtained by subtracting H3. For this reason, when the second buffer member 6 is compressed and deformed in the axial direction to the height H3 by the contact of the ship or the like with the impact plate 3, the contact surface 26 of the stopper 24 is placed on the back surface of the impact plate 3. The second buffer member 6 is prevented from being overcompressed by abutting and restricting further compression deformation.

ストッパ２４の高さＨ１をどの程度とするかは、第二緩衝部材６の高さＨ２、Ｈ３によって任意に変更できるが、通常は、前記無負荷時の第二緩衝部材６の高さＨ２の２０〜４０％程度であるのが好ましい。
上記のようにこの例によれば、ストッパ２４の高さＨ１を、第二緩衝部材６の無負荷時の高さＨ２よりも大幅に小さくすることができる。そのためストッパ２４は、従来のガイド棒よりも大幅に小型化および簡略化した構造とすることができる。 The level of the height H1 of the stopper 24 can be arbitrarily changed according to the heights H2 and H3 of the second buffer member 6. Normally, however, the height H2 of the second buffer member 6 when no load is applied. It is preferably about 20 to 40%.
As described above, according to this example, the height H1 of the stopper 24 can be made significantly smaller than the height H2 of the second buffer member 6 when no load is applied. Therefore, the stopper 24 can have a structure that is significantly smaller and simplified than the conventional guide rod.

なおストッパ２４は、スペーサ７の連結面２１ではなく、受衝板３の裏面に設けてもよい。また合計の高さが前記Ｈ１となる２つのスペーサを、前記スペーサ７の連結面２１と、受衝板３の裏面にそれぞれ設けてもよい。
図４は、本発明の防舷材の、実施の形態の他の例を示す斜視図である。なお図４では、スペーサおよび連結部材の接続構造がわかり易いように、第二緩衝部材６、および受衝板３を取り付ける前の状態を示している。 The stopper 24 may be provided not on the connecting surface 21 of the spacer 7 but on the back surface of the impact receiving plate 3. Further, two spacers having a total height of H1 may be provided on the connection surface 21 of the spacer 7 and the back surface of the impact receiving plate 3, respectively.
FIG. 4 is a perspective view showing another example of the embodiment of the fender according to the present invention. FIG. 4 shows a state before the second buffer member 6 and the impact plate 3 are attached so that the connection structure of the spacer and the connecting member can be easily understood.

図４を参照して、この例の防舷材１は、緩衝部材４を構成する第一緩衝部材５、スペーサ７、および前記第二緩衝部材６（図示せず）を、同じく図示していないが受衝板３の面方向に複数個（この例では４個）ずつ設けるとともに、前記複数個の緩衝部材４のスペーサ７を、連結部材２７を介して互いに一体に連結した点が、先の例と相違している。
個々の第一緩衝部材５、スペーサ７、およびストッパ２４は先の例と同一であるので、同一箇所に同一符号を付して説明を省略する。 Referring to FIG. 4, the fender 1 of this example does not show the first buffer member 5, the spacer 7, and the second buffer member 6 (not shown) constituting the buffer member 4. Are provided in the surface direction of the receiving plate 3 (four in this example), and the spacers 7 of the plurality of buffer members 4 are integrally connected to each other via a connecting member 27. It is different from the example.
The individual first buffer members 5, the spacers 7, and the stoppers 24 are the same as those in the previous example, and thus the same portions are denoted by the same reference numerals and description thereof is omitted.

連結部材２７は、例えば鋼材等の剛性体によって形成される。
図の例の場合、４個の緩衝部材４が、前記受衝板３の面方向の上下左右４箇所に正方形状に配列されている。連結部材２７は、前記４個の緩衝部材４のスペーサ７のうち、上下に配列された２個ずつ、および左右に配列された２個ずつを繋いでいる。
これにより、隣り合う緩衝部材４のせん断抵抗力を、前記スペーサ７および連結部材２７を介して連結して発揮させることができるため、交差方向のせん断力によって個々の緩衝部材４を構成する第一、第二緩衝部材５、６に不均一な負荷が加わるのを防止して、前記中折れや過圧縮が発生するのをさらに確実に防止することができる。 The connecting member 27 is formed of a rigid body such as a steel material.
In the case of the example in the figure, four buffer members 4 are arranged in a square shape at four locations in the upper, lower, left and right directions of the receiving plate 3. The connecting member 27 connects two spacers 7 of the four buffer members 4 arranged one above the other and two arranged right and left.
Thereby, since the shear resistance force of the adjacent buffer member 4 can be connected and exhibited via the spacer 7 and the connecting member 27, the first buffer member 4 is configured by the shear force in the cross direction. Further, it is possible to prevent the second buffer members 5 and 6 from being applied with a non-uniform load, and to more reliably prevent the intermediate folding and over-compression from occurring.

なお緩衝部材４の個数、およびスペーサ７を連結部材２７によってどのように連結するかは任意に設定できる。
図５は、スペーサ７および連結部材２７の接続構造の他の例を示す平面図である。
図５を参照して、この例では、４個の緩衝部材４が受衝板３の面方向の上下左右４箇所に長方形状に配列されるとともに、前記長方形の対角線の交点上にも１個の緩衝部材４が配列されている。 The number of the buffer members 4 and how the spacers 7 are connected by the connecting members 27 can be arbitrarily set.
FIG. 5 is a plan view showing another example of the connection structure of the spacer 7 and the connecting member 27.
Referring to FIG. 5, in this example, four buffer members 4 are arranged in a rectangular shape at four positions in the vertical and horizontal directions in the surface direction of the receiving plate 3, and one is also on the intersection of the diagonal lines of the rectangle. The buffer members 4 are arranged.

連結部材２７は、前記長方形の四隅に配列された４個のスペーサ７のうち、上下に配列された２個ずつ、左右に配列された２個ずつ、および各四隅と中央の２個ずつを繋いでいる。
このように、連結部材２７によるスペーサ７の接続構造は、緩衝部材４の個数に応じて任意に設定することができる。 Of the four spacers 7 arranged at the four corners of the rectangle, the connecting member 27 connects two arranged vertically, two arranged left and right, and two each of the four corners and the center. It is out.
Thus, the connection structure of the spacer 7 by the connecting member 27 can be arbitrarily set according to the number of the buffer members 4.

本発明の防舷材の構成は、以上で説明した各図のものには限定されず、本発明の要旨を逸脱しない範囲で適宜設計変更を施すことができる。 The structure of the fender according to the present invention is not limited to that shown in the drawings described above, and can be appropriately changed in design without departing from the gist of the present invention.

（第一緩衝部材５）
第一緩衝部材５のモデルとして、ＪＩＳＡ型硬さが７３°であるゴムからなり、図１、図２に示す立体形状を有するとともに、無負荷時の軸方向の高さが１００ｍｍであるものを５個用意した。
（第二緩衝部材６）
第二緩衝部材６のモデルとして、ＪＩＳＡ型硬さが７１°であるゴムからなり、図１、図２に示す立体形状を有するとともに、無負荷時の軸方向の高さＨ２が１００ｍｍであるものを５個用意した。 (First buffer member 5)
As a model of the first buffer member 5, it is made of rubber having a JIS A type hardness of 73 °, has a three-dimensional shape shown in FIGS. 1 and 2, and has an axial height of 100 mm when no load is applied. 5 were prepared.
(Second shock absorbing member 6)
As a model of the second buffer member 6, it is made of rubber having a JIS A-type hardness of 71 °, has the three-dimensional shape shown in FIGS. 1 and 2, and has an axial height H2 of 100 mm when no load is applied. Five things were prepared.

（ストッパ２４）
ストッパ２４のモデルとして、鋼材からなり、図１、図３に示す立体形状を有するとともに、軸方向の高さＨ１が３０ｍｍ、直径が２２ｍｍであるものを５個用意した。前記ストッパ２４によって設定される、第二緩衝部材６の圧縮変形時の軸方向の高さＨ３は７０ｍｍ、無負荷時の高さＨ２の７０％とした。 (Stopper 24)
As the model of the stopper 24, five were prepared which are made of steel and have the three-dimensional shape shown in FIGS. 1 and 3, the height H1 in the axial direction is 30 mm, and the diameter is 22 mm. The height H3 in the axial direction at the time of compressive deformation of the second buffer member 6 set by the stopper 24 was 70 mm, and 70% of the height H2 at the time of no load.

（スペーサ７、および連結部材２７）
スペーサ７のモデルとして、鋼材からなり、図１、図３に示す立体形状を有するとともに、軸方向の高さが４９ｍｍ、フランジ２０の直径が８５ｍｍであるものを５個用意した。そして各スペーサ７を、図５に示すように、鋼材からなる軸方向の厚み１９ｍｍ、前記軸方向、および長さ方向と直交方向の幅３３ｍｍの連結部材２７によって連結（溶接）した。 (Spacer 7 and connecting member 27)
As a model of the spacer 7, five pieces made of steel, having the three-dimensional shape shown in FIGS. 1 and 3, an axial height of 49 mm, and a flange 20 having a diameter of 85 mm were prepared. Then, as shown in FIG. 5, each spacer 7 was connected (welded) by a connecting member 27 having an axial thickness of 19 mm made of steel, a width of 33 mm in the direction perpendicular to the axial direction and the length direction.

（防舷材１の組み立て）
圧縮試験機の可動盤上に取り付けた、被接舷面２のモデルとしての鋼板上に、前記第一緩衝部材５、スペーサ７を連結部材２７によって連結したもの、ストッパ２４、および第二緩衝部材６を順に取り付け、最後に圧縮試験機の固定盤と第二緩衝部材６とを、受衝板３のモデルとしての鋼板を介して取り付けて、図１に示す緩衝部材４が５個、図５に示す配列で配列された防舷材１のモデルを組み立てた。 (Assembly of fender 1)
A structure in which the first buffer member 5 and the spacer 7 are connected to each other by a connecting member 27 on a steel plate as a model of the contact surface 2 attached on the movable platen of the compression tester, a stopper 24, and a second buffer member. 6 are attached in order, and finally the stationary platen of the compression tester and the second buffer member 6 are attached via a steel plate as a model of the impact plate 3, and five buffer members 4 shown in FIG. A model of the fender 1 arranged in the arrangement shown in FIG.

長方形の四隅に配設された４個の緩衝部材４のうち、前記長方形の長辺側の２個ずつの緩衝部材４間の中心間距離は２９２．３ｍｍ、短辺側の２個ずつの緩衝部材４間の中心間距離は１８０．８ｍｍ、前記四隅の４個と中央の１個の緩衝部材４間の中心間距離は、いずれも１７１．８ｍｍであった。
前記防舷材１のモデルのうち連結部材２７の、図６に示す(1)〜(8)の８箇所の上下両面（計１６箇所）には、それぞれ歪みゲージを貼り付けた。歪みゲージは、各連結部材２７の長さ方向をｘ、前記長さ方向と直交方向をｙに設定した。図中の数字は歪みゲージの取り付け位置間の寸法を示す。単位はｍｍである。各歪みゲージには、連結部材２７の(1)の位置の上側（第二緩衝部材６側）のものを(1-1)、下側（第一緩衝部材５側）のものを(1-2)、(2)の位置の上側のものを(2-1)、下側のものを(2-2)と順に(8-2)まで番号を付した。 Of the four cushioning members 4 arranged at the four corners of the rectangle, the center-to-center distance between the two cushioning members 4 on the long side of the rectangle is 292.3 mm, and two cushions on the short side The center-to-center distance between the members 4 was 180.8 mm, and the center-to-center distance between the four corners and one central buffer member 4 was 171.8 mm.
In the model of the fender 1, strain gauges were respectively attached to the upper and lower surfaces (total of 16 locations) of (1) to (8) shown in FIG. In the strain gauge, the length direction of each connecting member 27 is set to x, and the direction orthogonal to the length direction is set to y. The numbers in the figure indicate the dimensions between the strain gauge mounting positions. The unit is mm. For each strain gauge, the one on the upper side (second buffer member 6 side) of the position (1) of the connecting member 27 is (1-1), and the one on the lower side (first buffer member 5 side) is (1- The numbers above (2) and (2) are numbered in the order (2-1), the number on the bottom (2-2), and so on (8-2).

（正規圧縮試験）
前記圧縮試験機の固定盤と可動盤の平行を維持しながら、前記防舷材１のモデルを軸方向に試験速度３３ｍｍ／分、圧縮量１４０ｍｍ（両緩衝部材５、６の合計の高さの７０％）で３回予備圧縮した後、２０分経過後に４回目（評価用）の圧縮をした。圧縮量は１４７ｍｍ（両緩衝部材５、６の合計の高さの７３．５％）を目標とした。 (Normal compression test)
The model of the fender 1 is tested in the axial direction at a test speed of 33 mm / min and a compression amount of 140 mm (the total height of both buffer members 5 and 6 while maintaining the parallel of the fixed plate and the movable plate of the compression tester. 70%) and pre-compressed three times, and after the lapse of 20 minutes, a fourth compression (for evaluation) was performed. The target of compression was 147 mm (73.5% of the total height of both buffer members 5 and 6).

前記４回目の圧縮時の各部の挙動を確認したところ、まず圧縮初期に、第二緩衝部材６が第一緩衝部材５に先立って変形を開始し、その圧縮変形時の高さが、ストッパ２４の高さＨ１によって規定された、第二緩衝部材６の無負荷時の高さＨ２の７０％に達した時点で第一緩衝部材５が変形を開始すること、そのためいずれの緩衝部材５、６も、前記圧縮量までの間に過圧縮を生じないことが判った。 When the behavior of each part at the time of the fourth compression was confirmed, first, at the initial stage of compression, the second buffer member 6 started to be deformed prior to the first buffer member 5, and the height at the time of the compressive deformation was determined by the stopper 24. The first buffer member 5 starts to be deformed when it reaches 70% of the unloaded height H2 of the second buffer member 6, which is defined by the height H1 of the first buffer member 6. It was also found that no over-compression occurs before the compression amount.

前記正規圧縮試験後の防舷材１のモデルの各部を観察したところ、いずれの部材にも破損やひび割れは観察されなかった。
また前記４回目の圧縮時に、各歪みゲージで測定されたｘ方向の歪み量εｘの最大値、最小値、およびｙ方向の歪み量εｙの最大値、最小値から、それぞれ式(1)： When each part of the model of the fender 1 after the regular compression test was observed, no damage or cracking was observed in any of the members.
Further, from the maximum value and the minimum value of the strain amount εx in the x direction and the maximum value and the minimum value of the strain amount εy in the y direction measured by each strain gauge at the time of the fourth compression, respectively, the equations (1):

によりｘ方向の発生応力σｘの最大値、および最小値を求めるとともに、式(2)： To obtain the maximum value and the minimum value of the generated stress σx in the x direction, and the equation (2):

によりｙ方向の発生応力σｙの最大値、および最小値を求めた。なお両式中のＥ＝２０５８００Ｎ／ｍｍ^２、ν＝０．３、εｘ＝１０^−６（με）、εｙ＝１０^−６（με）とした。結果を表１に示す。 Thus, the maximum value and the minimum value of the generated stress σy in the y direction were obtained. In both formulas, E = 205800 N / mm ² , ν = 0.3, εx = 10 ⁻⁶ (με), and εy = 10 ⁻⁶ (με). The results are shown in Table 1.

（１０°傾斜圧縮試験）
前記正規圧縮試験から２０分以上経過後に、可動盤を固定盤に対して傾斜させた状態として、試験速度２２ｍｍ／分で圧縮をした。最大傾斜角度は１０°、その傾斜方向は長方形の長辺と一致させた。圧縮量は、傾斜前方側の最大値１４６ｍｍを目標とした。
前記圧縮時の各部の挙動を確認したところ、まず圧縮初期に、傾斜前方側の緩衝部材４の第二緩衝部材６が第一緩衝部材５に先立って変形を開始し、その圧縮変形時の高さが、ストッパ２４の高さＨ１によって規定された、第二緩衝部材６の無負荷時の高さＨ２の７０％に達した時点で第一緩衝部材５が変形を開始すること、次いで準じ傾斜後方側の緩衝部材４についても同様の変形挙動をすすること、そのためいずれの緩衝部材５、６も、前記圧縮量までの間に過圧縮を生じないことが判った。 (10 ° inclined compression test)
After 20 minutes or more from the regular compression test, the movable platen was inclined with respect to the fixed platen and compressed at a test speed of 22 mm / min. The maximum inclination angle was 10 °, and the inclination direction was matched with the long side of the rectangle. The amount of compression targeted a maximum value of 146 mm on the front side of the slope.
When the behavior of each part at the time of compression was confirmed, first, at the initial stage of compression, the second buffer member 6 of the buffer member 4 on the inclined front side started to be deformed prior to the first buffer member 5, and the height at the time of the compression deformation was high. When the first buffer member 5 starts to be deformed when it reaches 70% of the unloaded height H2 of the second buffer member 6 defined by the height H1 of the stopper 24, then the inclination It has been found that the rear-side buffer member 4 exhibits the same deformation behavior, and therefore neither of the buffer members 5 and 6 is over-compressed before the compression amount.

前記１０°傾斜圧縮試験後の防舷材１のモデルの各部を観察したところ、いずれの部材にも破損やひび割れは観察されなかった。
また前記圧縮時に、各歪みゲージで測定されたｘ方向の歪み量εｘの最大値、最小値、およびｙ方向の歪み量εｙの最大値、最小値から、それぞれ前記式(1)によりｘ方向の発生応力σｘの最大値、および最小値を求めるとともに、式(2)によりｙ方向の発生応力σｙの最大値、および最小値を求めた。結果を表２に示す。 When each part of the model of the fender 1 after the 10 ° inclination compression test was observed, no damage or cracking was observed in any member.
Further, at the time of compression, the maximum value and the minimum value of the strain amount εx in the x direction measured by each strain gauge, and the maximum value and the minimum value of the strain amount εy in the y direction, respectively, The maximum value and the minimum value of the generated stress σx were obtained, and the maximum value and the minimum value of the generated stress σy in the y direction were obtained from Equation (2). The results are shown in Table 2.

（１５°傾斜圧縮試験）
前記１０°傾斜圧縮試験から２０分以上経過後に、可動盤を固定盤に対してさらに傾斜させた状態として、試験速度５０ｍｍ／分で圧縮をした。最大傾斜角度は１５°、その傾斜方向は長方形の長辺と一致させた。圧縮量は、傾斜前方側の最大値１４６ｍｍを目標とした。 (15 ° inclined compression test)
After 20 minutes or more from the 10 ° inclined compression test, the movable platen was further inclined with respect to the fixed platen, and compression was performed at a test speed of 50 mm / min. The maximum inclination angle was 15 °, and the inclination direction was matched with the long side of the rectangle. The amount of compression targeted a maximum value of 146 mm on the front side of the slope.

前記圧縮時の各部の挙動を確認したところ、まず圧縮初期に、傾斜前方側の緩衝部材４の第二緩衝部材６が第一緩衝部材５に先立って変形を開始し、その圧縮変形時の高さが、ストッパ２４の高さＨ１によって規定された、第二緩衝部材６の無負荷時の高さＨ２の７０％に達した時点で第一緩衝部材５が変形を開始すること、次いで準じ傾斜後方側の緩衝部材４についても同様の変形挙動をすすること、そのためいずれの緩衝部材５、６も、前記圧縮量までの間に過圧縮を生じないことが判った。 When the behavior of each part at the time of compression was confirmed, first, at the initial stage of compression, the second buffer member 6 of the buffer member 4 on the inclined front side started to be deformed prior to the first buffer member 5, and the When the first buffer member 5 starts to be deformed when it reaches 70% of the unloaded height H2 of the second buffer member 6 defined by the height H1 of the stopper 24, then the inclination It has been found that the rear-side buffer member 4 exhibits the same deformation behavior, and therefore neither of the buffer members 5 and 6 is over-compressed before the compression amount.

前記１５°傾斜圧縮試験後の防舷材１のモデルの各部を観察したところ、いずれの部材にも破損やひび割れは観察されなかった。
また前記圧縮時に、各歪みゲージで測定されたｘ方向の歪み量εｘの最大値、最小値、およびｙ方向の歪み量εｙの最大値、最小値から、それぞれ前記式(1)によりｘ方向の発生応力σｘの最大値、および最小値を求めるとともに、式(2)によりｙ方向の発生応力σｙの最大値、および最小値を求めた。結果を表３に示す。 When each part of the model of the fender 1 after the 15 ° inclined compression test was observed, no damage or cracking was observed in any of the members.
Further, at the time of compression, the maximum value and the minimum value of the strain amount εx in the x direction measured by each strain gauge, and the maximum value and the minimum value of the strain amount εy in the y direction, respectively, The maximum value and the minimum value of the generated stress σx were obtained, and the maximum value and the minimum value of the generated stress σy in the y direction were obtained from Equation (2). The results are shown in Table 3.

１防舷材
２被接舷面
３受衝板
４緩衝部材
５第一緩衝部材
６第二緩衝部材
７スペーサ
８連結面
９連結部
１０支衝部
１１フランジ
１２通孔
１３ネジ孔
１４内周面
１５凸部
１６外周面
１７凸部
１８通孔
１９本体
２０フランジ
２１連結面
２２通孔
２３補強材
２４ストッパ
２５連結面
２６当接面
２７連結部材 DESCRIPTION OF SYMBOLS 1 Fouling material 2 Contact surface 3 Receiving plate 4 Buffer member 5 First buffer member 6 Second buffer member 7 Spacer 8 Connection surface 9 Connection portion 10 Support portion 11 Flange 12 Through-hole 13 Screw hole 14 Inner peripheral surface 15 convex portion 16 outer peripheral surface 17 convex portion 18 through hole 19 main body 20 flange 21 connecting surface 22 through hole 23 reinforcing material 24 stopper 25 connecting surface 26 abutting surface 27 connecting member

Claims

It is a fender for protecting a ship from the impact by absorbing energy when the ship is in contact with the surface to be touched and absorbing the impact. The fender is
An impact plate disposed substantially parallel to the surface to be contacted and contacting a ship or the like, and a buffer member interposed between the impact plate and the surface to be contacted; ,
A first buffer member that is entirely made of an elastic material such as rubber, is fixed to the surface to be contacted, and is compressed and deformed by contact with the receiving plate such as a ship to absorb the energy;
A second buffer member made of an elastic material softer than the first buffer member, fixed to the receiving plate, and compressed and deformed by contact of the ship with the receiving plate to absorb the energy; and And a spacer made of a rigid body, which is interposed between the first and second buffer members and connects the two buffer members.
At least one of the spacer and the receiving plate regulates the amount of compressive deformation of the second buffer member in the direction orthogonal to the surface direction of the receiving plate, and the second buffer member moves in the same direction. A fender having a stopper for preventing overcompression.

The second buffer member is formed in a substantially cylindrical shape having both ends opened, and both the ends are in contact with an impact plate and a spacer so that both the openings are closed, and the spacer and the receiver are also closed. A stopper is provided in an area of one of the impact plates facing the opening and surrounded by the second buffer member, and faces the opening of the other of the spacer and the impact plate, and the first The fender according to claim 1, wherein a region surrounded by the two buffer members is a contacted surface on which the stopper is contacted by compression deformation of the second buffer member.

A plurality of the first buffer members, spacers, and second buffer members are provided in the surface direction of the receiving plate, respectively, and the plurality of spacers are integrated with each other via a connecting member made of a rigid body. The fender according to claim 1 or 2, which is connected.