WO2018185951A1

WO2018185951A1 - Ship

Info

Publication number: WO2018185951A1
Application number: PCT/JP2017/029634
Authority: WO
Inventors: 日向　泰彦
Original assignee: 三菱造船株式会社
Priority date: 2017-04-07
Filing date: 2017-08-18
Publication date: 2018-10-11
Also published as: KR20210035329A; JP2018176900A; KR102473787B1; CN110446655A; KR20190109771A; JP6575033B2

Abstract

This ship comprises: a hull (10); a bridge disposed on the upper part of the stern side of the hull; a main engine (40) provided inside the hull (10); a fuel tank (50) provided on the bow side of the bridge on the upper deck (13) of the hull (10), fuel for the main engine being stored therein, and the fuel tank having an outer peripheral surface extending along an axis line (O) inclined downward toward the bow; and a pump (70) having a suction opening disposed in a bow-side portion of the fuel tank (50), the pump (70) suctioning out fuel.

Description

Ship

The present invention relates to a ship. This application claims priority based on Japanese Patent Application No. 2017-077686 filed in Japan on April 7, 2017, the contents of which are incorporated herein by reference.

As a carrier ship as a kind of ship, a carrier ship in which a plurality of cargo tanks storing liquefied gas such as LNG are arranged in the fore-and-aft direction is known (see, for example, Patent Documents 1 and 2). The plurality of cargo tanks are spherical tanks. The spherical tank is provided so that the upper half protrudes from the upper deck on the bow side of the bridge provided on the stern side of the ship.

In the carrier ship of patent documents 1 and 2, the height of the spherical tank arranged on the bow side among a plurality of spherical tanks arranged in the bow-stern direction so as to ensure a view from the bridge to the front water surface. A configuration is disclosed in which the height is smaller than that of a spherical tank disposed on the stern side.

JP-A-9-24891 JP 61-241293 A

In the above carrier, the liquid gas in the cargo tank as cargo can be used as fuel for the main engine of the ship. However, there is a case where a fuel tank for storing fuel is installed separately from a cargo tank for storing liquefied gas because of a request to separate cargo and fuel.

It is desirable to increase the volume of such a fuel tank as much as possible in order to secure the cruising distance of the ship. Moreover, since it is necessary to install a fuel tank in a limited space in a ship, there are restrictions on the installation position of the fuel tank and the size of the fuel tank.

Especially, depending on where the fuel tank is installed, it may interfere with the view from the bridge to the water surface. On the other hand, in order to properly suck out the fuel in the fuel tank by the pump, it is necessary to pay attention to the posture of the fuel tank in order to secure the liquid level of the fuel at the pump installation position in the fuel tank. is there.

The present invention provides a ship capable of ensuring the size of the fuel tank and the fuel sucking property while securing the view from the bridge.

According to a first aspect of the present invention, a ship includes a hull, a bridge disposed at an upper portion on the stern side of the hull, a main engine provided in the hull, and the bridge on an upper deck of the hull. A fuel tank having an outer peripheral surface extending along an axis inclined downward toward the bow side and storing fuel of the main engine, and on the bow side in the fuel tank A suction port disposed in the portion, and a pump for sucking out the fuel.

According to the ship of the above aspect, the outer peripheral surface of the fuel tank installed on the upper deck extends along an axis that inclines downward toward the bow side. Therefore, the volume of the fuel tank can be increased within a range in which the visibility can be secured while securing the visibility from the bridge to the front of the bow.
Furthermore, because the pump sucks fuel from the bow side of the fuel tank, which is the lower part of the inclination of the fuel tank, even when the fuel in the fuel tank is relatively low, the pump at the time of suction The head can be secured. Therefore, it can be reduced that the fuel in the fuel tank remains without being used up to the end.

According to the second aspect of the present invention, it is preferable that the upper tank line and the lower tank line forming the outer peripheral surface of the fuel tank as viewed from the width direction of the ship are parallel to the axis.

Since the upper tank line is inclined downward toward the bow side, it is possible to avoid obstructing the view from the bridge to the front of the bow. Further, since the lower tank line is inclined downward toward the bow side, when the fuel in the fuel tank is reduced, the fuel is collected in front of the fuel tank. Therefore, the fuel collected forward can be sucked out by the pump provided on the bow side in the fuel tank.

According to the third aspect of the present invention, the upper tank line extends along a visibility request line connecting the bridge and the water surface in front of the bow as viewed from the width direction of the ship.

This makes it possible to secure the maximum volume of the fuel tank as long as the fuel tank does not obstruct the view from the bridge to the front of the bow, that is, within the range that does not violate the rules regarding the view of the ship.

According to the fourth aspect of the present invention, it is preferable that the outer peripheral surface of the fuel tank has a cylindrical surface shape around the axis.

This can reduce the cost of manufacturing the fuel tank. Moreover, the pressure | voltage resistant structure for storing a fuel in a high voltage | pressure state can be manufactured at low cost.

According to a fifth aspect of the present invention, a cargo hold is formed in the hull, and a cargo tank is disposed in the cargo hold and contains a liquefied gas.

Even when a cargo tank for storing liquefied gas and a fuel tank for storing fuel are provided separately, as described above, while ensuring the maximum volume of the fuel tank, visibility from the bridge, Fuel consumption can be ensured.

According to the above-mentioned ship, the size of the fuel tank and the fuel sucking property can be ensured while ensuring the view from the bridge.

It is a side view of the carrier ship concerning an embodiment. It is a principal part enlarged view of FIG. It is sectional drawing orthogonal to the axis line of the fuel tank of the carrier ship which concerns on embodiment. It is a figure for demonstrating a visual field request | requirement line. It is sectional drawing orthogonal to the axis line of the said fuel tank which shows the 1st modification of the fuel tank of a carrier ship. It is sectional drawing orthogonal to the axis line of the said fuel tank which shows the 2nd modification of the fuel tank of a carrier ship. It is sectional drawing orthogonal to the axis line of the said fuel tank which shows the 3rd modification of the fuel tank of a carrier ship.

Hereinafter, a ship 100 according to a first embodiment of the present invention will be described in detail with reference to the drawings. The ship 100 of this embodiment is a liquefied gas carrier ship that transports liquefied petroleum gas (LPG) as liquefied gas.
As shown in FIG. 1, the ship 100 includes a hull 10, a bridge 20, a cargo tank 30, a main engine 40, a fuel tank 50, and a pump 70.

The hull 10 has a side 11, a ship bottom 12 and an upper deck 13. The heel side 11 is composed of a pair of heel side outer plates that respectively constitute the left and right heel sides 11. The ship bottom 12 is composed of a ship bottom skin plate that connects the left and right ridges 11 at the bottom.

The upper deck 13 is connected to a pair of left and right sides 11 above the bottom 12 of the ship. The upper deck 13 is an exposed deck extending from the bow to the stern. The upper deck 13 extends in the horizontal direction. Depending on the navigation state of the ship 100, the upper deck 13 itself may be inclined downward on the stern side of the upper deck 13 itself.

The hull 10 has a cross-sectional shape orthogonal to the bow-stern direction formed in a substantially box shape that forms a space inside by the side 11, the ship bottom 12, and the upper deck 13. A portion on the stern side in the hull 10 is an engine room 14. A portion on the bow side of the engine room 14 in the hull 10 is a cargo hold 15 partitioned by the engine room 14 and a partition wall.

The bridge 20 is provided so as to extend upward from the upper part of the hull 10. The bridge 20 is provided on the stern side in the upper part of the hull 10 and is provided above the engine room 14. The bridge 20 has a plurality of hierarchies. A cockpit 21 for maneuvering the ship 100 is provided on the upper layer of the bridge 20. The cockpit 21 is configured so that the front of the ship 100 can be seen from a high place.

The cargo tanks 30 are provided in the cargo hold 15 of the hull 10 so that a plurality (three in this embodiment) are arranged in the bow-stern direction. A partition between adjacent cargo tanks 30 is provided with a partition separating the compartments in which the respective cargo tanks 30 are accommodated.

The cargo tank 30 of the present embodiment is a rectangular tank configured by joining flat tank wall portions to each other. In the cargo tank 30, LPG as cargo is stored in a normal pressure and low temperature state. The “normal pressure low temperature state” means a state in which the liquefied state of LPG is maintained only by lowering the LPG without increasing the pressure. LPG is liquefied at normal pressure by keeping it at about −46 ° C. or lower. Therefore, the ship 100 is provided with an evaporative gas processing device (not shown) for maintaining the LPG in a low-temperature liquefied state. A reliquefaction device is adopted as the evaporative gas treatment device.

The re-liquefaction device cools the vaporized gas discharged when the LPG is vaporized by external heat in the cargo tank 30 outside the cargo tank 30 and liquefies it again. The liquefied gas is returned to the cargo tank 30 as LPG. As a result, a low temperature state (for example, a temperature of −46 ° C. or lower) is maintained in the LPG.

The main engine 40 is disposed in the engine room 14 in the hull 10. The main engine 40 of this embodiment is driven using LPG as fuel. Here, the fuel of the main engine 40 is not limited to LPG, and may be a combination of LPG and another fuel (bi-fuel), mixing (dual fuel), or the like. By driving the main engine 40, the screw 41 provided below the stern of the hull 10 rotates.

Next, the fuel tank 50 will be described with reference to FIG. The fuel tank 50 according to the present embodiment stores LPG as fuel for the main engine 40. The fuel tank 50 is provided on the upper deck 13. In the present embodiment, for example, among the three cargo tanks 30 arranged in the bow-stern direction, the upper tank 13 is provided above the central cargo tank 30.

The fuel tank 50 can store LPG at high pressure and room temperature. Therefore, the fuel tank 50 is configured by a pressure vessel. The “high pressure normal temperature state” means a state in which the LPG liquefied state is maintained only by pressurizing the LPG without cooling it.

The fuel tank 50 has a cylindrical portion 51 and a pair of lid portions 52. The cylindrical portion 51 has a cylindrical shape with the axis O as the center. In this embodiment, as shown in FIG. 3, the cross-sectional shape orthogonal to the axis O of the cylinder part 51 is circular, that is, the cylinder part 51 has a cylindrical shape. The thickness of the wall constituting the cylindrical portion 51 is constant. The dimension of the cylinder part 51 in the axis O direction is larger than the diameter of the cylinder part 51. That is, the fuel tank 50 has the longitudinal direction in the axis O direction.

The pair of lid portions 52 are provided so as to close both ends of the cylindrical portion 51 in the axis O direction. For example, the cylindrical portion 51 has a curved surface shape protruding outward from both ends of the cylindrical portion 51, and preferably has a spherical shape. As described above, the fuel tank 50 is configured by the cylindrical portion 51 having a cylindrical shape and the pair of lid portions 52 having a curved shape, so that the pressure resistance is ensured by having a cylindrical shape as a whole. The outer peripheral surface centering on the axis of the fuel tank 50 is also cylindrical. The volume of the fuel tank 50 is sufficiently smaller than the volume of the cargo tank 30.

Such a fuel tank 50 is provided on the upper deck 13 so that the axis O is inclined downward as it goes to the bow side. That is, the fuel tank 50 extends along the axis O that goes downward as it goes to the bow side. The axis O coincides with the fore-and-aft direction in plan view of the ship 100. A pair of fuel tanks 50 may be arranged so that the axis lines O are parallel to each other in a plan view and spaced apart in the ship width direction.

The axis O arranged above the upper deck 13 is inclined with respect to the upper deck 13 so as to approach the upper deck 13 toward the bow side. The inclination angle of the axis O with respect to the upper deck 13 is downward as the axis O moves toward the bow with respect to the horizontal plane even when the ship 100 and the stern side of the upper deck 13 are lowered during the navigation of the ship 100. It is said that it can maintain that it is inclined.

As shown in FIG. 2, a line connected to the upper ends of the outer peripheral surfaces of the cylindrical portion 51 of the fuel tank 50 at each fore-and-aft position is defined as an upper tank line La. The upper tank line La forms an upper contour in a side view of the ship 100. A line connected to the lower ends of the outer peripheral surfaces of the cylinder portion 51 of the fuel tank 50 at each bow-tail direction position is defined as a lower tank line Lb. The lower tank line Lb forms a lower contour in a side view of the ship 100.

These upper tank line La and lower tank line Lb are inclined downward toward the bow side. In the present embodiment, the upper tank line La and the lower tank line Lb are parallel to the axis O. Since the thickness of the cylinder portion 51 constituting the fuel tank 50 is constant, the bottom tank line defining the space in the fuel tank 50 is inclined in the same manner as the lower tank line Lb because the lower tank line Lb is inclined. is doing.

The inclined posture of the fuel tank 50 as described above is, for example, made by a tank support portion 60 that supports the inclined tank. The tank support portion 60 supports the fuel tank 50 on the upper deck 13 so that the axis O of the fuel tank 50 is inclined as described above. For example, in the present embodiment, the fuel tank 50 is supported by the upper ends of the bow side support portion 61 and the stern side support portion 62. The bow side support part 61 and the stern side support part 62 are respectively fixed on the upper deck 13, and the upper end of the stern side support part 62 is located above the upper end of the bow side support part 61. Thus, the inclined posture of the fuel tank 50 is maintained by the difference in height between the stern side support portion 62 and the bow side support portion 61. The configuration of the tank support portion 60 is not limited to the above configuration, and may be another configuration as long as the fuel tank 50 can be supported on the upper deck 13 in an inclined posture.

Here, with reference to FIG. 4, the inclined posture of the fuel tank 50 will be described in more detail. The fuel tank 50 is arranged on the upper deck 13 so as to be below the visibility request line Lv shown in FIG. Here, the visibility request line Lv is an imaginary line that connects the cockpit 21 in the bridge 20 and the shorter position of twice the full length Loa of the ship 100 or 500 m from the bow on the front water surface of the bow.

That is, in the ship 100, a structure such as the fuel tank 50 on the upper deck 13 has a field of view from the cockpit 21 of the bridge 20 to the shorter position of twice the full length or 500 m from the bow on the front water surface of the bow. It is stipulated as a requirement not to disturb. More specifically, the base end of the visibility request line Lv on the bridge 20 side is defined as a position of 750 mm from the front wall surface in front of the cockpit 21 toward the stern side and a position of 1800 mm from the floor surface. If the fuel tank 50 is disposed below the visibility request line Lv, that is, if the upper tank line La of the fuel tank 50 is not located above the visibility requirement line Lv, the requirement according to the above rule is satisfied. .

In order to increase the volume of the fuel tank 50 as much as possible, it is preferable that the upper tank line La of the fuel tank 50 is arranged as close as possible to the visibility request line Lv. The upper tank line La of the fuel tank 50 may be parallel to the visibility request line Lv. The upper tank line La of the fuel tank 50 may extend so as to coincide with the visibility request line Lv. That is, the upper tank line La of the fuel tank 50 only needs to extend along the visibility request line Lv.

Next, the pump 70 will be described. As shown in FIG. 2, the pump 70 has a role of pumping LPG in the fuel tank 50 to the main unit 40. A drive unit such as an electric motor for driving the pump 70 may be provided in the fuel tank 50 or may be provided outside the fuel tank 50. In particular, since the LPG stored in the fuel tank 50 has an insulating property, there is no problem even if a drive unit is provided in the fuel tank 50.

The suction port of the pump 70 is provided in a portion on the bow side in the fuel tank 50. In particular, in the present embodiment, the suction port of the pump 70 is disposed near the boundary between the cylinder portion 51 and the bow side lid portion 52 in the space in the fuel tank 50. It is preferable that the suction port of the pump 70 is provided at a position located at the lowest position in the space in the fuel tank 50 or close to the position. The suction port of the pump 70 is preferably provided so as to correspond to a position where the lower tank line Lb of the fuel tank 50 is located at the lowest position. The fuel sucked out from the pump 70 is transferred to the main engine 40 via the pipe 71.

Next, the operation of this embodiment will be described.
In this embodiment, the outer peripheral surface of the fuel tank 50 installed on the upper deck 13 extends along the axis O that inclines downward toward the bow side. Therefore, it is possible to increase the volume of the fuel tank 50 within a range in which the visibility can be ensured while ensuring a large visibility from the cockpit 21 of the bridge 20 to the front of the bow.

That is, if the fuel tank 50 is tilted toward the bow side, it is possible to prevent the view of the bridge 20 from looking down from the cockpit 21 toward the bow side toward the water surface. Furthermore, since the stern side of the fuel tank 50 is positioned upward due to the inclined posture, the fuel tank 50 occupies a space that has not been used so far and does not obstruct the view. Therefore, the effective volume in which the fuel tank 50 can store fuel can be expanded.

Further, because the pump 70 sucks fuel from the bow side portion in the fuel tank 50 that is the lower part of the inclination of the fuel tank 50, even if the fuel in the fuel tank 50 becomes relatively small, The head of the pump 70 at the time of suction can be secured. That is, as shown in FIG. 2, when the remaining amount of LPG in the fuel tank 50 decreases, the LPG gathers on the bow side in the fuel tank 50 according to the inclination of the fuel tank 50. When the pump 70 sucks out the LPG collected in this way through the suction port, it is possible to reduce that the fuel in the fuel tank 50 remains without being used up to the end. That is, the fuel sucking property by the pump 70 can be secured.

Here, if the inclined posture of the fuel tank 50 is opposite to that of the present embodiment, that is, if the axis O of the fuel tank 50 is inclined downward toward the stern side, the bow side of the fuel tank 50 is upward. Will be located. In this case, the visibility of the bridge 20 from the cockpit 21 may be hindered. Moreover, in order to ensure visibility, the fuel tank 50 must be installed on the stern side, which impedes the freedom of installation. Further, if the fuel tank 50 is to be installed on the bow side so as not to obstruct the view from the bridge 20, it is necessary to make the fuel tank 50 itself small, and the effective volume is reduced.

On the other hand, if the fuel tank 50 is arranged so as to extend downward as the axis O of the fuel tank 50 extends toward the bow as in the present embodiment, the fuel tank 50 is placed on the upper deck 13 within a range that does not hinder the visibility. That is, the degree of freedom of the arrangement of the fuel tank 50 on the deck can be improved. Furthermore, the volume of the fuel tank 50 can be maximized within a range that does not obstruct the view from the bridge 20.

Further, particularly in the present embodiment, the upper tank line La and the lower tank line Lb of the fuel tank 50 are parallel to the inclined axis O. That is, since the upper tank line La inclines downward toward the bow side, it is possible to further avoid obstructing the view from the bridge 20 to the front of the bow. Further, since the lower tank line Lb is inclined downward toward the bow side, the bottom surface constituting the space inside the fuel tank 50 is similarly inclined. Therefore, when the LPG in the fuel tank 50 decreases, the fuel in the fuel tank 50 is guided to the bow side by the bottom surface, so that the LPG can be collected in the bow side portion in the fuel tank 50. it can. Therefore, the fuel collected in the front can be efficiently sucked out by the pump 70 provided on the bow side in the fuel tank 50.

Further, since the upper tank line La extends along the view requirement line Lv that connects the bridge 20 and the water surface in front of the bow as viewed from the width direction of the ship, the fuel tank 50 satisfies the required rules while satisfying the required rules. The volume of the fuel tank 50 can be maximized within a range that does not obstruct the view from the bridge 20 to the front of the bow.

In addition, since the fuel tank 50 has a cylindrical shape, the manufacturing cost of the fuel tank 50 can be suppressed. Furthermore, the pressure | voltage resistant structure for storing a fuel in a high voltage | pressure state can be manufactured at low cost.

Even if the cargo tank 30 for storing LPG as cargo and the fuel tank 50 for storing LPG as fuel are separately provided as in the present embodiment, the volume of the fuel tank 50 is increased as described above. While ensuring the maximum, the visibility from the bridge 20 and the ability to suck out the fuel in the fuel tank 50 can be ensured.

The embodiment of the present invention has been described above, but the present invention is not limited to this, and can be appropriately changed without departing from the technical idea of the present invention.

For example, as a first modification, a fuel tank 150 shown in FIG. 5A may be employed. The fuel tank 150 according to the first modification has a shape in which two cylindrical portions 151 extending in the direction of the axis O are arranged in parallel to each other and are combined in a part of the circumferential direction.

Further, as a second modification, a fuel tank 160 shown in FIG. 5B may be adopted. The fuel tank 160 of the second modified example includes an upper plate portion 161 and a lower plate portion 162 that extend along the axis O and face each other in the vertical direction. Both sides of the upper plate portion 161 and the lower plate portion 162 in the ship width direction are connected in an arc shape by a curved portion 163.

Furthermore, as a third modification, a fuel tank 170 shown in FIG. 5C may be adopted. The fuel tank 170 according to the third modified example includes a rectangular tube portion 171 having a quadrangular cross section extending along the axis O.
In any case of the first to third modifications, the

fuel tanks

150, 160, 170 are formed on the outer peripheral surface extending along the axis O inclined downward and extending toward the bow side, and on the outer peripheral surface. An upper tank line La and a lower tank line Lb are included. Therefore, there exists an effect similar to embodiment.

In the embodiment, the fuel stored in the fuel tank 50 is LPG, but another liquefied gas such as LNG may be used as the fuel. The cargo stored in the cargo tank 30 is not limited to LPG, and may be other liquefied gas. Furthermore, the cargo stored in the cargo tank 30 may be a liquid or a material other than the liquefied gas.

According to this ship, it is possible to ensure the size of the fuel tank and the fuel sucking property while securing the view from the bridge.

DESCRIPTION OF SYMBOLS 10 Hull 11 Anchor side 12 Ship bottom 13 Upper deck 14 Engine room 15 Cargo hold 20 Bridge 21 Control room 30 Cargo tank 40 Main engine 41 Screw 50 Fuel tank 51 Tube part 52 Lid part 60 Tank support part 61 Bow side support part 62 Stern side support part 70 Pump 71 Piping 100 Ship 150 Fuel tank 151 Cylindrical portion 160 Fuel tank 161 Upper plate portion 162 Lower plate portion 163 Curved portion 170 Fuel tank 171 Square tube portion O Axis line Lv Visibility requirement line La Upper tank line Lb Lower tank line

Claims

The hull,
A bridge arranged at the upper part of the stern side of the hull;
A main engine provided in the hull;
A fuel tank provided on the bow side of the bridge on the upper deck of the hull and having an outer circumferential surface extending along an axis inclined downward toward the bow side while storing fuel of the main engine; ,
A pump in which a suction port is arranged at a bow side portion in the fuel tank and sucks out the fuel;
Ship equipped with.
2. The ship according to claim 1, wherein an upper tank line and a lower tank line that form the outer peripheral surface of the fuel tank as viewed from the ship width direction are parallel to the axis.
The ship according to claim 2, wherein the upper tank line extends along a visibility request line connecting the bridge and a water surface in front of the bow as viewed from the width direction of the ship.
The ship according to claim 2 or 3, wherein an outer peripheral surface of the fuel tank has a cylindrical surface shape centered on the axis.
A cargo hold is formed in the hull,
The ship according to any one of claims 1 to 4, further comprising a cargo tank that is disposed in the cargo hold and stores liquefied gas.