JP2011088515A - Frictional resistance reducing ship - Google Patents
Frictional resistance reducing ship Download PDFInfo
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- JP2011088515A JP2011088515A JP2009242313A JP2009242313A JP2011088515A JP 2011088515 A JP2011088515 A JP 2011088515A JP 2009242313 A JP2009242313 A JP 2009242313A JP 2009242313 A JP2009242313 A JP 2009242313A JP 2011088515 A JP2011088515 A JP 2011088515A
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- 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
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
- Y02T70/10—Measures concerning design or construction of watercraft hulls
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Abstract
Description
本発明は、微細気泡(マイクロバブル)を船体の外表面に供給して、船体と水との間の摩擦抵抗を低減した摩擦抵抗低減船およびその運転方法に関する。 The present invention relates to a frictional resistance-reducing ship in which fine bubbles (microbubbles) are supplied to the outer surface of a hull to reduce the frictional resistance between the hull and water and a method for operating the same.
航行中の船体の表面に気泡を供給することで、水に対する船体の摩擦抵抗が小さくなることが従来から知られている。 Conventionally, it is known that the frictional resistance of a hull against water is reduced by supplying bubbles to the surface of the hull during navigation.
特に船の航行に伴って負圧を発生せしめ、この負圧によって空気を引き出して微細気泡とする技術が特許文献1に開示されている。 In particular, Patent Document 1 discloses a technique in which a negative pressure is generated as a ship sails and air is drawn out by the negative pressure to form fine bubbles.
この特許文献1には、船体に形成した開口部に取り付ける微細気泡発生部材として、前記開口部に嵌め付けられるプレートと、このプレートに取り付けられる負圧発生用のウィングとからなる構造が提案されている。 This Patent Document 1 proposes a structure comprising a plate fitted into the opening and a negative pressure generating wing attached to the opening as a fine bubble generating member attached to the opening formed in the hull. Yes.
特許文献1にあっては、ウィングの取り付け角度を船体に対して斜め、具体的にはウィングの前端縁と船体との隙間よりもウィングの後端縁と船体との隙間の方が大きくなるようにすることで、船の航行に伴ってウィングの船体との対向面側に負圧領域を形成し、この負圧領域に向かって船体に形成した開口から空気が引き込まれ、その際の空気と海水との界面において微細気泡を発生させるようにしたものである。 In Patent Document 1, the wing attachment angle is oblique to the hull, specifically, the gap between the wing rear edge and the hull is larger than the gap between the wing front edge and the hull. By forming a negative pressure area on the side of the wing facing the hull as the ship navigates, air is drawn from the opening formed in the hull toward this negative pressure area, and the air at that time Fine bubbles are generated at the interface with seawater.
特許文献1に開示される構造では、負圧領域と船体に形成した空気の供給口との距離が大きいため、負圧領域が形成されてもこの負圧領域に廻りの海水が瞬時に入り込んでしまい、空気の供給口から空気を十分に引き出すことができず、微細気泡の発生が不十分となっている。 In the structure disclosed in Patent Document 1, since the distance between the negative pressure region and the air supply port formed in the hull is large, even when the negative pressure region is formed, seawater around the negative pressure region immediately enters the negative pressure region. Therefore, the air cannot be sufficiently drawn out from the air supply port, and the generation of fine bubbles is insufficient.
上記課題を解決するため本発明に係る摩擦抵抗低減船は、船体に形成した開口部に微細気泡発生部材が取り付けられ、この微細気泡発生部材は前記開口部に嵌め付けられるプレートと、このプレートに脚部を介して取り付けられる負圧発生用のウィングとからなり、前記脚部には大気若しくは圧気源に連通する空気供給通路が形成され、前記ウィングは船体との対向面が航行時に負圧形成面となるようにウィングの前端縁と船体との隙間よりもウィングの後端縁と船体との隙間の方が大きくされ、また前記ウィングは内部に中空部が形成され、この中空部は前記脚部に形成した空気供給通路と連通し、更に前記ウィングの船体との対向面には負圧によって中空部内の空気を微細気泡として噴出する孔が形成されている。 In order to solve the above problems, a frictional resistance reducing ship according to the present invention has a fine bubble generating member attached to an opening formed in a hull, the fine bubble generating member being attached to the opening, and a plate attached to the plate. It consists of a wing for generating negative pressure attached via a leg, and an air supply passage communicating with the atmosphere or a pressure air source is formed in the leg, and the wing forms a negative pressure when navigating the hull. The gap between the rear edge of the wing and the hull is made larger than the gap between the front edge of the wing and the hull so as to be a plane, and the wing has a hollow portion formed therein, A hole for communicating air in the hollow portion as fine bubbles by negative pressure is formed on the surface of the wing facing the hull and communicating with the air supply passage formed in the portion.
船の走行速度に応じて発生する負圧の大きさも左右される。そこで、前記脚部に形成した空気供給通路に接続される空気供給用配管に、切替えバルブを設け、空気源として大気または圧気源のいずれかを選択することを可能にすることが好ましい。尚、本発明は空気供給用配管が大気のみに開放される場合および圧気源のみに接続される場合を含む。 The magnitude of the negative pressure generated according to the traveling speed of the ship is also affected. Therefore, it is preferable to provide a switching valve in the air supply pipe connected to the air supply passage formed in the leg portion so that either the atmospheric air or the pressurized air source can be selected as the air source. In addition, this invention includes the case where the piping for air supply is open | released only to air | atmosphere and the case where it connects only to a pressurized air source.
また、発生した微細気泡を船体側面に貼り付かせるために、ウィングの後方の船体表面に凸部を設けるようにしてもよい。 Further, a convex portion may be provided on the surface of the hull behind the wing in order to cause the generated fine bubbles to stick to the side surface of the hull.
本発明に係る摩擦抵抗低減船によれば、船体の底面および側面を微小気泡(マイクロバブル)で覆うことができるので、摩擦抵抗が更に低減され、燃費が向上する。 According to the frictional resistance reduction ship according to the present invention, the bottom and side surfaces of the hull can be covered with microbubbles, so that the frictional resistance is further reduced and fuel efficiency is improved.
特に本発明によれば、微細気泡発生部材自身が船の走行に伴って負圧を発生し、その負圧を無駄なく有効に利用しているため、十分な量の微細気泡を発生させることができる。 In particular, according to the present invention, the fine bubble generating member itself generates a negative pressure as the ship travels and effectively uses the negative pressure without waste, so that a sufficient amount of fine bubbles can be generated. it can.
以下に本発明の実施例を添付図面を参照しつつ説明する。図1に示すように、本発明に係る摩擦抵抗低減船は喫水面(L.W.L.)よりも下方の船体の外側面1から船底2に沿って複数の微細気泡発生部材10を取り付けている。複数の微細気泡発生部材10の配列は図示例では側方から見て直線状をなすように配列しているが、千鳥状や斜めでもよい。 Embodiments of the present invention will be described below with reference to the accompanying drawings. As shown in FIG. 1, the frictional resistance reduction ship according to the present invention has a plurality of fine bubble generating members 10 attached along the ship bottom 2 from the outer surface 1 of the hull below the draft surface (LWL). ing. In the illustrated example, the plurality of fine bubble generating members 10 are arranged so as to form a straight line when viewed from the side, but they may be staggered or slanted.
本実施例では喫水面(L.W.L.)よりも下方となる領域を喫水面に近い上方領域(R1)と船底に近い下方領域(R2)に分け、上方領域(R1)と下方領域(R2)に配置される微細気泡発生部材10への空気の供給形態を異ならせている。 In the present embodiment, the region below the draft surface (L.W.L.) is divided into an upper region (R1) near the draft surface and a lower region (R2) near the ship bottom, and the upper region (R1) and the lower region. The supply form of air to the fine bubble generating member 10 arranged in (R2) is different.
即ち、上方領域(R1)に配置される微細気泡発生部材10への空気の供給は先端が大気に開放される空気供給配管3を介して行われ、下方領域(R2)に配置される微細気泡発生部材10への空気の供給は、アシストコンプレッサ4からバッファタンク5にエアが送り込まれ、バッファタンク5からの分岐管6を介して行われる。 That is, the supply of air to the fine bubble generating member 10 disposed in the upper region (R1) is performed via the air supply pipe 3 whose tip is opened to the atmosphere, and the fine bubbles disposed in the lower region (R2). Air is supplied to the generating member 10 from the assist compressor 4 to the buffer tank 5 through the branch pipe 6 from the buffer tank 5.
つまり、下方領域(R2)に配置される微細気泡発生部材10への空気の供給は大気開放ではなく閉鎖系の配管を介して行われる。尚、説明を簡単にするため、図示例では上方領域(R1)に配置される微細気泡発生部材10の数を1つにしているが複数でもよい。 That is, the supply of air to the fine bubble generating member 10 disposed in the lower region (R2) is performed not through the atmosphere but through a closed piping. In addition, in order to simplify the description, in the illustrated example, the number of fine bubble generating members 10 arranged in the upper region (R1) is one, but a plurality of fine bubble generating members 10 may be provided.
前記各分岐管6には減圧弁V1〜V4が設けられ、下方領域(R2)に配置される微細気泡発生部材10への空気の供給圧を異ならせている。この実施例では上方に位置する減圧弁ほど絞り量を大きくして、下方の微細気泡発生部材10ほど高圧の空気が供給されるようにしている。分岐管6内の気液界面から微細気泡発生部材10までの距離は下方の微細気泡発生部材10ほど大きくなるので、減圧弁を設けてバッファタンク5から空気が均等に供給されるようにする。 Each branch pipe 6 is provided with pressure reducing valves V1 to V4, and the supply pressure of air to the fine bubble generating member 10 arranged in the lower region (R2) is varied. In this embodiment, the throttle amount is increased as the pressure reducing valve is located at the upper side, and the high pressure air is supplied to the fine bubble generating member 10 at the lower side. Since the distance from the gas-liquid interface in the branch pipe 6 to the fine bubble generating member 10 becomes larger as the fine bubble generating member 10 below, a pressure reducing valve is provided so that air is supplied uniformly from the buffer tank 5.
尚、最も下方に位置する微細気泡発生部材10への分岐管には、減圧弁V4を設けなくてもよい。更に、航行速度に応じてバッファタンク5から供給される空気圧を全体的に調整するようにしてもよい。 The pressure reducing valve V4 may not be provided in the branch pipe to the fine bubble generating member 10 located at the lowest position. Furthermore, the air pressure supplied from the buffer tank 5 may be adjusted as a whole in accordance with the navigation speed.
次に、微細気泡発生部材10の構造を図4〜図7に基づいて説明する。微細気泡発生部材10は船体に形成した開口1aに嵌め付けられるプレート11と、このプレート11に脚部12を介して取り付けられる負圧発生用のウィング13とからなる。 Next, the structure of the fine bubble generating member 10 will be described with reference to FIGS. The fine bubble generating member 10 includes a plate 11 fitted in an opening 1a formed in the hull, and a wing 13 for generating negative pressure attached to the plate 11 via a leg 12.
開口1aの内側部はプレート11を支持するバックアッププレート14にて塞がれ、前記脚部12には大気若しくは圧気源に連通する通路15が形成され、更に前記ウィング13は船体との対向面が航行時に負圧形成面となるようにウィング13の前端縁と船体との隙間g1よりもウィング13の後端縁と船体との隙間g2の方が大きくされている。 The inner side of the opening 1a is closed by a backup plate 14 that supports the plate 11, a passage 15 communicating with the atmosphere or a pressure source is formed in the leg 12, and the wing 13 has a surface facing the hull. The gap g2 between the rear end edge of the wing 13 and the hull is made larger than the gap g1 between the front end edge of the wing 13 and the hull so as to form a negative pressure forming surface during navigation.
前記ウィング13は内側板16と外側板17を合わせて結合することで構成され、内側板16と外側板17を合わせた状態でウィング13内部に前記通路15に連通する中空部18が形成される。 The wing 13 is configured by combining the inner plate 16 and the outer plate 17 together, and a hollow portion 18 communicating with the passage 15 is formed inside the wing 13 in a state where the inner plate 16 and the outer plate 17 are combined. .
前記内側板16の表面は航行時に負圧形成面となり、この内側板16には多数の微細な孔19が形成されている。 The surface of the inner plate 16 becomes a negative pressure forming surface during navigation, and a number of fine holes 19 are formed in the inner plate 16.
以上において、船が航行を開始した直後は速度が遅いためウィング13によって発生する負圧も小さく、上方領域(R1)に配置される微細気泡発生部材10へ空気の供給を行う空気供給配管3内の気液界面の引き下げ効果は十分でないため上方領域(R1)の微細気泡発生部材10からの微細気泡の発生はない。 In the above, since the speed is low immediately after the ship starts to sail, the negative pressure generated by the wing 13 is also small, and the inside of the air supply pipe 3 that supplies air to the fine bubble generating member 10 disposed in the upper region (R1). Since the effect of lowering the gas-liquid interface is not sufficient, fine bubbles are not generated from the fine bubble generating member 10 in the upper region (R1).
しかしながら、下方領域(R2)に配置される微細気泡発生部材10にはバッファタンク5から高圧空気が供給されているので、中空部18に供給された空気は内側板16に形成した孔19から噴出する。 However, since the high-pressure air is supplied from the buffer tank 5 to the fine bubble generating member 10 disposed in the lower region (R2), the air supplied to the hollow portion 18 is ejected from the hole 19 formed in the inner plate 16. To do.
一方、航行速度が速くなるとウィング13の内側板16の外側表面近傍に負圧領域が形成される。その結果、当該負圧によってウィング13の中空部18内の空気が孔19から噴出する。 On the other hand, when the navigation speed increases, a negative pressure region is formed near the outer surface of the inner plate 16 of the wing 13. As a result, the air in the hollow portion 18 of the wing 13 is ejected from the hole 19 by the negative pressure.
噴出した微細気泡は船体後方に移動するが、ウィング13の下流側には流線型の凸部20が船体1若しくはプレート11に設けられているので、噴出した微細気泡は船体に貼り付くように後方に移動する。この状態を図8で示している。 Although the ejected fine bubbles move to the rear of the hull, the streamlined convex portion 20 is provided on the hull 1 or the plate 11 on the downstream side of the wing 13, so that the ejected fine bubbles are attached to the rear so that the fine bubbles stick to the hull. Moving. This state is shown in FIG.
図9は微細気泡発生部材の別実施例を示す図であり、この実施例にあってはプレート11のウィング13に対向する面にスリット状開口22を設け、このスリット状開口22に分岐管6を介して空気が供給される構造になっている。尚、プレート11に形成する開口の形状は、スリット状に限定されない。 FIG. 9 is a view showing another embodiment of the fine bubble generating member. In this embodiment, a slit-shaped opening 22 is provided on the surface of the plate 11 facing the wing 13, and the branch pipe 6 is formed in the slit-shaped opening 22. It is the structure where air is supplied through. In addition, the shape of the opening formed in the plate 11 is not limited to the slit shape.
図10及び図11は別実施例を示す図3と同様の図であり、図10に示す別実施例にあっては、喫水面に近い上方領域R1に設ける微細気泡発生部材10につながる空気供給配管3に、切替弁21を介してバッファタンク5からの分岐管6を接続し、巡航速度に至らない極低速の場合でも、切替弁21を操作することで、バッファタンク5の空気が供給されるようにしている。この場合、分岐管6に設ける減圧弁V0は他の減圧弁V1〜V4よりも絞り度を大きく設定する。 FIGS. 10 and 11 are views similar to FIG. 3 showing another embodiment. In the other embodiment shown in FIG. 10, the air supply connected to the fine bubble generating member 10 provided in the upper region R1 close to the draft surface. Even if the branch pipe 6 from the buffer tank 5 is connected to the pipe 3 via the switching valve 21, and the switching valve 21 is operated even at an extremely low speed that does not reach the cruising speed, the air in the buffer tank 5 is supplied. I try to do it. In this case, the pressure reducing valve V0 provided in the branch pipe 6 is set to have a higher degree of throttle than the other pressure reducing valves V1 to V4.
図11に示す別実施例は、上方領域R1と下方領域R2の間に中間領域R3を設け、この中間領域R3に配置する微細気泡発生部材10について、大気開放兼バッファタンク5からの空気が供給されるようにしている。 In another embodiment shown in FIG. 11, an intermediate region R3 is provided between the upper region R1 and the lower region R2, and air from the atmosphere opening and buffer tank 5 is supplied to the fine bubble generating member 10 disposed in the intermediate region R3. To be.
1…船体の外側面、1a…船体の開口、2…船底、4…アシストコンプレッサ、5…バッファタンク、6…分岐管、10…微細気泡発生部材、11…プレート、12…脚部、13…ウィング、14…バックアッププレート、15…通路、16…内側板、17…外側板、18…中空部、19…微細な孔、20…凸部、21…切替弁、22…スリット状開口、R1…上方領域、R2…下方領域、R3…中間領域、g1…ウィングの前端縁とプレートとの間隔、g2…ウィングの後端縁とプレートとの間隔。
DESCRIPTION OF SYMBOLS 1 ... Outer surface of a hull, 1a ... Opening of a hull, 2 ... Ship bottom, 4 ... Assist compressor, 5 ... Buffer tank, 6 ... Branch pipe, 10 ... Fine bubble generating member, 11 ... Plate, 12 ... Leg part, 13 ... Wing, 14 ... backup plate, 15 ... passage, 16 ... inner plate, 17 ... outer plate, 18 ... hollow portion, 19 ... fine hole, 20 ... convex portion, 21 ... switching valve, 22 ... slit-like opening, R1 ... Upper region, R2 ... lower region, R3 ... intermediate region, g1 ... interval between the front edge of the wing and the plate, g2 ... interval between the rear edge of the wing and the plate.
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5132828B1 (en) * | 2012-06-01 | 2013-01-30 | 株式会社 ドットコム・リレーションズ | Friction resistance reduction ship |
CN105730607A (en) * | 2016-02-02 | 2016-07-06 | 南京航空航天大学 | Bubble damping device used for water navigation body |
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2009
- 2009-10-21 JP JP2009242313A patent/JP2011088515A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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JP5132828B1 (en) * | 2012-06-01 | 2013-01-30 | 株式会社 ドットコム・リレーションズ | Friction resistance reduction ship |
CN105730607A (en) * | 2016-02-02 | 2016-07-06 | 南京航空航天大学 | Bubble damping device used for water navigation body |
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