KR101531489B1 - Venting apparatus for ships - Google Patents

Abstract

The present invention provides a venting apparatus for ships. An embodiment of the present invention comprises: a gas venting line which includes a first gas venting line connected to a fuel gas supplying system which processes and supplies liquefied fuel stored in a storage tank of a ship in accordance with the requirements of an engine, and a second gas venting line connected to the engine; and an air supply line connected to an air injector which supplies air to an accelerator of a ship. The gas venting line and the air supply line can be extended towards the accelerator.

Description

[0001] VENTING APPARATUS FOR SHIPS [0002]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a gas discharge apparatus for a ship, and more particularly, to a gas discharge apparatus for a ship which discharges fuel gas remaining in an engine or a fuel gas supply system of a ship to a propeller side of a ship, ≪ / RTI >

In recent years, ships have been made larger and faster in order to quickly transport large quantities of cargo or personnel. As the propeller that propels such a ship is enlarged, the fluid pressure caused by the rotation of the propeller impinges the hull, so that the vibration of the hull is high.

The force that the fluid pressure impacts the hull causes the hull to vibrate is referred to as the vibration excitation force. Such vibratory excitation force is also transmitted to the residence of the ship, which reduces the comfort of the ship and affects various equipments and systems installed on the ship There is a need to reduce the vibratory excitement of the ship.

In the meantime, heavy oil and diesel oil have been mainly used as fuels for operating these propellers. However, as the IMO regulations on the emission of greenhouse gases and various air pollutants are strengthened, the shipbuilding and shipping industry Natural gas, which is a clean energy source, is often used as fuel for ships.

A ship using natural gas (hereinafter referred to as "NG") as a fuel includes a storage tank for storing LNG (Liquefied Natural Gas) in which NG is liquefied, and a boil off gas (BOG) or LNG stored in a storage tank And a fuel gas supply system for supplying the fuel to the engine (converting pressure, temperature, state, etc.) so as to be usable as fuel. Here, the storage tank may be an LNG fuel tank or an LNG cargo tank.

Recently, a high-pressure gas injection engine such as the ME-GI engine developed by MAN Diesel & Turbo has been spotlighted as being excellent in terms of efficiency. Such a high-pressure gas injection engine is characterized in that it supplies gas fuel at a high pressure close to 300 bar. Therefore, in the related industry, researches on a fuel gas supply system for supplying fuel gas to such a high-pressure gas injection engine are actively conducted.

When shutting down the high-pressure gas injection engine or shutting off the supply of the fuel gas in an emergency, high-pressure fuel gas remains in the high-pressure gas injection engine or the fuel gas supply system, The high-pressure gas injection engine or the fuel gas supply system may be affected, which may lead to damage or shortening of durability.

Therefore, in order to discharge the remaining high-pressure fuel gas, a method of connecting a pipe to a conventional vent mast and discharging it is used. However, since the vent mast is used to discharge low-pressure evaporation gas, there is a fear that the vent mast may be damaged Therefore, there is a risk of fire or explosion as high-pressure fuel gas is discharged, and thus there is a need for a method for safely treating residual high-pressure fuel gas.

Korean Registered Patent No. 10-1149505 (issued on May 25, 2012)

An embodiment of the present invention is to provide a gas discharging device for a ship capable of reducing vibration excitation force of a ship propeller by using fuel gas remaining in an engine and a fuel gas supplying system of a ship.

An embodiment of the present invention is to provide a gas discharging device for a ship capable of ensuring the comfort of the ship habitat by using the fuel gas remaining in the engine and the fuel gas supply system of the ship and achieving safe navigation conditions.

An embodiment of the present invention is to provide a gas discharge apparatus for a ship capable of safely disposing residual high-pressure fuel gas into water.

An embodiment of the present invention is to provide a gas discharging device for a ship capable of preventing a danger such as a fire or an explosion that may occur in a gas discharging process.

According to one aspect of the present invention, there is provided a method for controlling a liquefied fuel, comprising the steps of: providing a first gas discharge line connected to a fuel gas supply system for processing and supplying liquefied fuel stored in a storage tank of a ship to meet the requirements of an engine; A gas discharge line including a line; And an air supply line connected to an air injector for supplying gas toward the propeller of the ship, wherein the gas discharge line and the air supply line can be extended toward the propeller.

At least one of the fuel gas remaining in the engine, the fuel gas remaining in the fuel gas supply system, and the gas supplied from the air injector is jetted toward the propeller, thereby reducing the vibration excitation force generated by the propeller.

The gas discharge line and the air supply line may be connected to each other.

The first gas discharge line and the second gas discharge line may be joined to the air supply line and connected to each other in front of the propeller.

Wherein the engine includes a high-pressure gas injection engine that operates by receiving a high-pressure fuel gas, and a low-pressure gas injection engine that operates by receiving low-pressure fuel gas,

Wherein the fuel gas supply system includes a first fuel supply line for supplying a high-pressure fuel gas to the high-pressure gas injection engine, and a second fuel supply line for supplying a low-pressure fuel gas to the low-pressure gas injection engine,

Wherein the first gas discharge line includes a first high-pressure gas discharge line, one end of which is connected to the first fuel supply line, and a first low-pressure gas discharge line, one end of which is connected to the second fuel supply line, And the other end of the high-pressure gas discharge line and the other end of the first low-pressure gas discharge line may be joined to the other end of the air supply line.

The second gas discharge line includes a second high pressure gas discharge line having one end connected to the high pressure gas injection engine and a second low pressure gas discharge line having one end connected to the low pressure gas injection engine, And the other end of the discharge line and the other end of the second low-pressure gas discharge line may be joined to the other end of the air supply line.

The gas discharge line and the air supply line may be respectively provided with valves for regulating passage or interruption of the remaining fuel gas and gas.

The first high-pressure gas discharge line and the first low-pressure gas discharge line may be respectively provided with valves for controlling passage or interruption of the remaining fuel gas.

The second high-pressure gas discharge line and the second low-pressure gas discharge line may be respectively provided with valves for controlling passage or blocking of the remaining fuel gas.

The apparatus for discharging the gas according to the embodiment of the present invention has the effect of discharging the fuel gas remaining in the engine and the fuel gas supply system to the propeller of the ship to reduce the vibration excitation force of the ship propeller.

The gas discharge device for a ship according to the embodiment of the present invention has an effect of enabling the comfort of the ship habitat to be achieved by discharging the fuel gas remaining in the engine and the fuel gas supply system to the propeller of the ship, .

The apparatus for discharging the gas of the ship according to the embodiment of the present invention has the effect of discharging the high-pressure fuel gas remaining in the high-pressure gas injection engine or the fuel gas supply system to water and safely treating it.

The apparatus for evacuating a ship according to an embodiment of the present invention has an effect of minimizing the risk of fire or explosion which may occur in the process of discharging remaining fuel gas.

BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a schematic view showing a state in which a gas discharging device for a ship according to an embodiment of the present invention is installed on a ship; Fig.
2 is a view showing a gas discharge apparatus of a ship according to an embodiment of the present invention.

Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings. The embodiments described below are provided by way of example so that those skilled in the art will be able to fully understand the spirit of the present invention. The present invention is not limited to the embodiments described below, but may be embodied in other forms. In order to clearly explain the present invention, parts not related to the description are omitted from the drawings, and the width, length, thickness, etc. of the components may be exaggerated for convenience. Like reference numerals designate like elements throughout the specification.

FIG. 1 is a view schematically showing a state in which a gas exhausting apparatus 100 of a ship according to an embodiment of the present invention is installed on a ship. FIG. 2 is a schematic view of a gas exhausting apparatus 100 of a ship according to an embodiment of the present invention. Fig.

Referring to FIG. 1, the ship includes a propeller 4 provided at the stern and generating power by propelling the propeller 4 by rotation, an engine 20 providing power to the propeller 4, The fuel gas supply system 10 that processes and supplies the fuel gas and the gas exhaust apparatus 100 that discharges the fuel gas or gas remaining in the engine 20 or the fuel gas supply system 10 to the propeller 4 side have.

The engine 20 and the fuel gas supply system 10 described below are provided for the purpose of facilitating understanding of the present invention. For example, the gas discharge apparatus 100 of the present invention, as an example, The specific configuration of the engine 20 and the fuel gas supply system 10 may be configured differently from that described in the present embodiment.

The engine 20 includes a high-pressure gas injection engine 21 requiring a fuel gas supply at a pressure of approximately 150 to 300 bar, such as an ME-GI engine, and a low-pressure gas injection engine 21, And a low pressure gas injection engine 22 in which the supply of fuel gas at a pressure of ~ 7 bar is required. Here, the term high pressure means a pressure range for supplying the fuel gas to the high pressure gas injection engine 21, that is, a pressure of about 150 to 300 bar, and the term low pressure means that the low pressure gas injection engine 22 supplies the fuel gas Pressure range, i.e., a pressure of about 5 to 7 bar.

The high-pressure gas injection engine 21 and the low-pressure gas injection engine 22 may be provided as a dual fuel engine capable of using not only natural gas but also heavy fuel oil (HFO) The low pressure gas injection engine 22 may be a power generation engine that supplies power to various facilities in the ship such as the DFDE engine 20. [

Here, the liquefied fuel may be any one of LNG, LPG, and DME (Dimethylether) which can be stored in a liquefied state and can be used as a fuel, but the present invention is not limited thereto. However, in the following description, it is assumed that the liquefied fuel is LNG for convenience.

1 and 2, the fuel gas supply system 10 includes a storage tank 2 for storing an LNG, a first fuel supplying the LNG of the storage tank 2 as a fuel to the high-pressure gas injection engine 21, A high-pressure pump 40 for pressurizing and sending the LNG, and a high-pressure vaporizer 50 for vaporizing the pressurized LNG, and the evaporation gas generated in the storage tank 2 is supplied to the low-pressure gas injection engine 22, a second fuel supply line 12 for supplying the fuel as a fuel, an evaporative gas compressor 70 for compressing the evaporative gas, and a re-liquefier 80 for re-liquefaction of the evaporated gas.

Herein, the ship to which the fuel gas supply system 10 is applied is not limited to a ship such as an LNG carrier, an LNG carrier, a container ship, and a general merchant ship employing the high-pressure gas injection engine 21 but also a floating marine plant such as LNG FPSO, LNG FSRU .

The storage tank 2 may be an LNG fuel tank for storing the LNG as fuel or an LNG cargo tank provided for the LNG carrier. In LNG carrier, LNG stored in cargo tank can be used as fuel. This storage tank 2 can maintain the internal pressure at about 1 bar and the internal LNG can be maintained at about -163 degrees Celsius (liquefaction temperature at normal pressure).

The storage tank 2 is provided with a vent mast 3 for discharging the evaporation gas to the atmosphere to prevent the pressure inside the storage tank 2 from rising due to the accumulation of the evaporation gas generated by evaporation of the LNG stored in the storage tank 2 ). The vent mast 3 may be provided in the form of a chimney in the upper part of the storage tank 2 to reduce the possibility of ignition and explosion in the process of discharging the evaporative gas.

The high-pressure pump (40) is installed in the first fuel supply line (11). The high-pressure pump 40 extracts the LNG from the storage tank 2, raises the fuel gas supply pressure of the high-pressure gas injection engine 21 to 150 to 300 bar, and sends it to the high-pressure vaporizer 50. The high-pressure pump 40 may be a reciprocating pump that can easily raise the LNG of the storage tank 2 to a high pressure of 150 to 300 bar.

The high-pressure vaporizer 50 vaporizes the high-pressure LNG delivered from the high-pressure pump 40 and sends it to the high-pressure gas injection engine 21 side. At this time, the NG supplied from the high-pressure vaporizer 50 to the high-pressure gas injection engine 21 can be adjusted to match the fuel gas supply conditions (pressure, temperature) of the high-pressure gas injection engine 21. [ Although not shown in the drawing, the first fuel supply line 11 between the high-pressure vaporizer 50 and the high-pressure gas injection engine 21 is provided with a means capable of controlling the temperature through heating or the like and a pressure tank Adjustable means may be provided.

The evaporation gas compressor 70 of the second fuel supply line 12 compresses the evaporation gas of the storage tank 2 to a pressure of 5 to 7 bar which is the fuel gas supply pressure of the low pressure gas injection engine 22, (22) so that the evaporation gas of the storage tank (2) can be used as fuel.

In a state in which the low-pressure gas injection engine 22 is not operated, the evaporation gas may be compressed using the evaporative gas compressor 70, and then re-liquefied through the re-liquefier 80 to be stored again in the storage tank 2 . The re-liquefier 80 may include a refrigerator with a compressor, a condenser, an expansion device, and an evaporator using nitrogen gas as a refrigerant. When the pressure of the storage tank 2 is likely to rise excessively due to the evaporation gas in a state where the low pressure gas injection engine 22 is not operated, the evaporation gas 2 is supplied through the vent mast 3 provided in the storage tank 2, To the atmosphere.

On the other hand, when the high-pressure gas injection engine 21 or the low-pressure gas injection engine 22 is shut down or the supply of the fuel gas in an emergency is interrupted, the high-pressure pump 30 of the first fuel supply line 11, The high-pressure fuel gas remaining in the first fuel supply line 11 and the high-pressure gas injection engine 21 can exert a large load due to the difference in pressure with the atmospheric pressure because the LNG is raised at a high pressure of 150 to 300 bar. Further, even if the low-pressure gas injection engine 22 supplies the relatively low-pressure fuel gas, when the fuel gas remains in the second fuel supply line 12 and the low-pressure gas injection engine 22, Pressure gas injection engine 12 and the low-pressure gas injection engine 22 may be loaded. Therefore, there is a need to safely discharge the fuel gas remaining in the fuel gas supply system 10 and the engine 20 to the outside.

On the other hand, the propeller 4 of the ship rotates to provide the propulsion force to the ship. In the course of the rotation of the propeller 4, the fluid pressure impacts the hull 1 and causes the hull 1 to vibrate. In order to reduce the vibration excitation force of the hull 1, the force that causes the fluid pressure to impact the hull 1 and cause the vibration of the hull 1 is referred to as a vibration excitation force, And the vibration of the propeller 4 is reduced.

The high pressure fuel gas remaining in the fuel gas supply system 10 and the engine 20 is discharged into the water and safely treated and the remaining fuel gas is discharged from the front of the propeller 4 in consideration of the above two problems A gas exhaust device for reducing the vibration excitation force of the propeller (4) when the remaining fuel gas is not exhausted, (100).

The gas exhausting apparatus 100 includes a gas exhaust line having one end connected to the fuel gas supply system 10 or the engine 20 to discharge remaining fuel gas and an exhaust gas line connected to the air injector 131, And the other end of the gas discharge line and the other end of the air supply line 130 are joined and connected to each other in the water in front of the propeller 4 so as to be connected to the engine 20 or the fuel gas supply system 10. [ The fuel gas remaining in the fuel injector 131 or the gas injected from the air injector 131 may be injected toward the propeller 4 to reduce the vibration excitation force of the propeller 4. [

In the case of the air injector 131 connected to one end of the air supply line 130, the gas ejecting apparatus may be an inert gas such as nitrogen gas or argon gas which is chemically stable and difficult to react with other substances, As shown in Fig.

The gas discharge line includes a first gas discharge line 110, one end of which is connected to the fuel gas supply system, and a second gas discharge line 120, one end of which is connected to the engine. And the other end of the second gas discharge line 120 may be joined to the other end of the air supply line 130 to be connected to the water in front of the propeller 4.

The first gas discharge line 110 includes a first high-pressure gas discharge line 111 having one end connected to the first fuel supply line 11 and a second high-pressure gas discharge line 111 having one end connected to the second fuel supply line 12 And a low-pressure gas discharge line 112. The other end of the first high-pressure gas discharge line 111 and the other end of the first low-pressure gas discharge line 112 are arranged to join with the other end of the air supply line 130. The first gas discharge line 120 may be joined to the other end of the second gas discharge line 120 so as to form one passage and then join with the other end of the air supply line 130.

2 and the present embodiment, one end of the first high-pressure gas discharge line 111 is connected to the downstream of the high-pressure vaporizer 50 and one end of the first low-pressure gas discharge line 112 is connected to the downstream of the evaporative gas compressor 70 The first fuel supply line 11 and the second fuel supply line 12 may be provided in various configurations. In this case, the fuel gas is supplied to the fuel supply line in a compressed state, In case of residual fuel supply lines and other facilities can be connected to various points as long as the load can be applied to them.

The second gas discharge line 120 includes a second high-pressure gas discharge line 121, one end of which is connected to the high-pressure gas injection engine 21, and a second low-pressure gas discharge line 122, (Not shown). The other end of the second high-pressure gas discharge line 121 and the other end of the second low-pressure gas discharge line 122 are arranged to join with the other end of the air supply line 130 or to join with the other end of the first gas discharge line 110 And may be arranged to join with the other end of the air supply line 130 after forming one passage.

As described above, the first gas discharge line 110 including the first high-pressure gas discharge line 111 and the first low-pressure gas discharge line 112, and the second gas discharge line 110 including the second high-pressure gas discharge line 121, The other end of the second gas discharge line 120 including the first gas discharge line 122 may join independently or together to form one passage and then join with the other end of the air supply line 130 to be introduced into the water in front of the propeller 4 The risk of fire or explosion can be significantly reduced compared with the case where the fuel gas remaining in the atmosphere is discharged.

In particular, since the fuel gas remaining in the first fuel supply line 11 and the high-pressure gas injection engine 21 has a high pressure, there is a possibility that a safety accident may occur due to a large pressure difference when the fuel gas is released into the atmosphere. However, when the first high-pressure gas discharge line 111 and the second high-pressure gas discharge line 121 are connected to the first fuel supply line 11 and the high-pressure gas injection engine 21, respectively, It is possible to prevent safety accidents and prevent equipment damage.

The gas discharge lines 110 and 120 need to be closed for stable operation of the fuel gas supply system 10 and the engine 20 in the process of discharging the remaining fuel gas and the gas discharge lines 110 and 120 need to be closed, Since the pressure of the fuel gas discharged through the air injector 120 is higher than the pressure of the gas discharged from the air injector 131 through the air supply line 130, the fuel gas may flow back to the air supply line 130 side, The pressure of the fuel gas passing through the first high-pressure gas discharge line 111 and the second high-pressure gas discharge line 121 is lower than the pressure of the fuel passing through the first low-pressure gas discharge line 112 and the second low- There is a possibility that the fuel gas flows back to the first and second low-pressure gas discharge lines 112 and 122 in the process of discharging the fuel gas.

In order to prevent this, the gas discharge lines 110 and 120 and the air supply line 130 may be provided with valves 30 so as to respectively control passage or interruption of the remaining fuel gas and gas. The first gas discharge line 110 and the second gas discharge line 120 may be provided with valves 30 or the other end of the first gas discharge line 110 and the second gas discharge line 120 may be merged, The valve 30 may be provided after the point at which the first gas discharge line 110 and the second gas discharge line 120 merge. The valve 30 may be provided in the first high-pressure gas discharge line 111 and the first low-pressure gas discharge line 112. Similarly, the second high-pressure gas discharge line 121 and the second low- Line 122, respectively.

The valve 30 is provided with a sensor (not shown) for sensing the pressure of each of the gas discharge lines 110 and 120 for efficiency and rapid operation of the operation, although the operator can manually adjust the opening and closing. The opening and closing of each of the gas discharge lines 110 and 120 and the air supply line 130 may be automatically controlled.

In general, when the ship is driven using a propeller, the gas discharging device 100 of the ship having such a configuration is configured such that the gas supplied from the air injector 131 is supplied to the front of the propeller 4 through the air supply line 130 The valve 30 provided in the air supply line 130 is closed and the engine 20 is closed when the shutdown of the engine or the supply of the fuel gas during the emergency is interrupted, Or discharging the high pressure fuel gas remaining in the fuel gas supply system 10 into the water in front of the propeller 4 of the ship through the first gas discharge line 110 and the second gas discharge line 120, It is possible to minimize the risk of explosion and at the same time to reduce the vibration excitation force of the propeller 4.

In addition, since the existing fuel gas can be easily discharged as a simple structure while using existing equipment as it is, the installation cost can be reduced.

While the present invention has been particularly shown and described with reference to exemplary embodiments thereof, it is clearly understood that the same is by way of illustration and example only and is not to be taken by way of limitation, You will understand. Accordingly, the true scope of the invention should be determined only by the appended claims.

1: Hull 2: Storage tank
10: fuel gas supply system 11: first fuel supply line
12: second fuel supply line 20: engine
21: high pressure gas injection engine 22: low pressure gas injection engine
30: valve 100: gas discharge device
110: first gas discharge line 111: first high-pressure gas discharge line
112: first low-pressure gas discharge line 120: second gas discharge line
121: second high-pressure gas discharge line 122: second low-pressure gas discharge line
130 air supply line 131 air injector

Claims (9)

A gas discharge line including a first gas discharge line connected to the fuel gas supply system which processes and supplies the liquefied fuel stored in the storage tank of the ship in accordance with the requirements of the engine and a second gas discharge line connected to the engine; And
And an air supply line connected to an air injector for supplying gas toward the propeller of the ship,
Wherein the gas discharge line and the air supply line extend toward the propeller,
Wherein the engine includes a high-pressure gas injection engine that operates by receiving a high-pressure fuel gas, and a low-pressure gas injection engine that operates by receiving low-pressure fuel gas,
Wherein the fuel gas supply system includes a first fuel supply line for supplying a high-pressure fuel gas to the high-pressure gas injection engine, and a second fuel supply line for supplying a low-pressure fuel gas to the low-pressure gas injection engine,
The first gas discharge line
A first high-pressure gas discharge line, one end of which is connected to the first fuel supply line, and a first low-pressure gas discharge line, one end of which is connected to the second fuel supply line,
And the other end of the first high-pressure gas discharge line and the other end of the first low-pressure gas discharge line join with the other end of the air supply line and are connected to water in front of the propeller. The method according to claim 1,
Wherein at least one of the fuel gas remaining in the engine, the fuel gas remaining in the fuel gas supply system, and the gas supplied from the air injector is jetted toward the propeller, thereby reducing vibration excitation force generated by the propeller. The method according to claim 1,
Wherein the gas discharge line and the air supply line are connected to each other. delete delete The method according to claim 1,
The second gas discharge line
A second high-pressure gas discharge line, one end of which is connected to the high-pressure gas injection engine, and a second low-pressure gas discharge line, one end of which is connected to the low-pressure gas injection engine,
And the other end of the second high-pressure gas discharge line and the other end of the second low-pressure gas discharge line join with the other end of the air supply line. The method according to claim 1,
Wherein the gas discharge line and the air supply line are each provided with valves for regulating passage or interruption of fuel gas and gas remaining therein. The method according to claim 1,
Wherein the first high-pressure gas discharge line and the first low-pressure gas discharge line are respectively provided with valves for controlling passage or interruption of the remaining fuel gas. The method according to claim 6,
Wherein the second high-pressure gas discharge line and the second low-pressure gas discharge line are respectively provided with valves for regulating passage or blocking of the remaining fuel gas.

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