Title of Invention

"GAS SUPPLY ARRANGEMENT OF A MARINE VESSEL AND METHOD OF PROVIDING GAS IN A MARINE VESSEL"

Abstract Gas supply arrangement ( 1 ) of a marine vessel (6) being adapted to carry liquefied gas in its gas tank (4) having an ullage space section (4,1 ) and a liquid phase section (4.2), which arrangement provides the gas for demands of the vessel the arrangement comprising; a gas supply line (2) provided for delivering the gas formed in the gas tank to a consumption device (5); a piping (.3,1) extending front the liquid phase section (4.2) to the ullage space section (4.1) of the gas tank (4) being provided with at least a pump (3,1). for introducing gas into the ullage space section. The piping is provided with a deal transfer unit (3,6) for effecting on the temperature of the introduced gas. Invention relates also to method of providing gas in a marine vessel (6) with liquefied gas tank.
Full Text GAS SUPPLY ARRANGEMENT OF A MARINE VESSEL AND METHOD OF PROVIDING GAS IN A MARINE VESSEL
Invention relates to a gas supply arrangement of a marine vessel according to preamble of claim 1 and to method of providing gas in a gas supply arrangement of a marine vessel according to the preamble of claim 5.
The usage of gas as energy source in marine vessels is advantageous due to its efficient burning and low emissions. Usually gas is stored in liquefied form because less space is required for the storage that way.
The propulsion system of LNG (Liquified Natural Gas) tankers is usually powered by making use of the cargo. Storing of the gas in the tanker is arranged by Using heat insulated cargo tanks into which an ullage space section and a liquid phase section are formed. The pressure in the cargo tanks is approximately at atmospheric pressure level and the temperature of the liquefied gas is about minus 163 °C. Although the insulation of the cargo tank is extremely good, gradually increasing of the LNG temperature causes formation of so called natural boil-off gas. The boil-off gas must be removed in order to avoid extensive increasing of pressure in the cargo tanks, that is because the cargo tanks are very sensitive to pressure changes. The boil-off gas may be utilised in tanker's consumption devices like propulsion system. However, the amount of natural boil-off gas is not sufficient for providing all propulsion energy required in all circumstances and therefore the vessel must be provided with additional means for acquiring extra gas, so called forced boil-off gas.
For example in a patent publication FR 2722760 there is shown an arrangement in which liquid gas is supplied to a forced boiling vaporiser in which the liquid gas vaporises into gas form, which in turn may be combined with the natural boil-off gas stream.

EP 1348620 A1 shows a gas supply apparatus in which the natural boil-off gas is led to a compressor, which increase the pressure of the gas prior to feeding it to consumption via a feed line. Additionally, the apparatus also includes a forced boiling vaporiser in which the liquid gas previously pumped to the higher pressure is vaporised. In this arrangement the forced boiling gas portion is combined to the natural boil-off gas after the pressure of the natural boil-off gas has been increased. It is, however, somewhat complicated system requiring two parallel gas feed systems from the cargo tank to gas main supply line. That kind of an arrangement requires also somewhat complicated control system.
An objective of the invention is to provide a gas supply arrangement for a marine vessel, which solves the above mentioned and other problems of the prior art. It is also an objective of the invention to provide a straightforward and reliable arrangement and method for a marine vessel with liquefied gas tank, which provides even pressure at the supply line and reliable gas supply for consumption devices of the vessel.
Objectives of the invention are met substantially as is disclosed in claims 1 and 5, and in more detailed manner in other claims. In the following the invention will be described with a reference mainly to one gas tank. However, it is clear that a marine vessel may be provided with several gas tanks each having an individual gas supply arrangement or several gas tanks may be connected parallel having a shared gas supply arrangement.
Gas supply arrangement of a marine vessel being adapted to carry liquefied gas in its gas tank having an ullage space section and a liquid phase section. According to the invention arrangement provides gas for demands of the vessel, the arrangement comprising a gas supply line provided for delivering the gas formed in the gas tank to a consumption device. The basic idea of the invention is to control-lably evaporate gas in the gas tank itself by providing advantageous circumstances

for phase transition phenomenon particularly in the ullage space section and/or above the surface of the liquid phase section.
According to a preferred embodiment the arrangement is provided with a piping extending from the liquid phase section to the ullage space section of the gas tank being provided with at least a pump, for introducing gas into the ullage space section. The piping is provided with a heat transfer unit for effecting on the temperature of the introduced gas. This way the arrangement is capable of producing controllable amount of gaseous gas for the demands of the vessel. The arrangement is advantageously provided with a first sensor, which is adapted for measuring the pressure in the ullage space section of the gas tank. The piping is provided with a control valve for controlling the flow of the gas in the piping and the first sensor is arranged in control communication with the control valve. This way the flow rate of the gas through the piping is controlled based on the measured pressure in the ullage space section of the gas tank.
The heat transfer unit comprises a heat exchanger. The heat exchanger is arranged in the piping so that the gas may flow through it. The piping is provided also with a bypass conduit passing by the heat exchanger and with a three-way valve for controlling the gas flow between the heat exchanger and the bypass conduit. The arrangement is advantageously provided with a second sensor, which is adapted for measuring the temperature in the ullage space section of the gas tank. The second sensor is arranged in control communication with the three-way valve, which thus divides the flow of gas between the heat exchanger and the bypass conduit based on the temperature prevailing the ullage space section.
According to the invention, in the method of providing gas a marine vessel with liquefied gas tank having an ullage space section and liquid phase section, and a gas consumption device, gas is evaporated in the gas tank and led to the consumption device via a gas supply line. Simultaneously the pressure in the gas tank is substantially continuously measured by a first sensor. The evaporation rate of the gas in the gas tank is controlled by controllably spraying liquefied gas into the ullage

space section and the flow rate of sprayed liquefied gas is controlled based on the pressure measurement of the first sensor. This way circumstances for phase transition phenomenon in the ullage space section and/or above the surface of the liquid phase section is provided, and the phase transition controlled based on the pressure measurement of the first sensor.
The temperature of the sprayed gas is controlled based on temperature value measured by a second sensor provided in connection with the gas tank ullage space section.
The invention has several advantages. First of all, the number of required components is minimised, which leads to easy and space-saving installation. The pressure and gaseous gas production con-^l is also very accurate due to the novel way of controlling the pressure. With the invention it is also possible to provide more suitable gas for gas engine operation by minimising the evaporation of the heavy hydrocarbons from the liquefied gas.
In the following the invention will be described with the reference to the accompanying schematic drawing, in which figure 1 shows an exemplary embodiment of the gas supply arrangement according to the invention.
Figure 1 depicts schematically cross section of a marine vessel 6, like LNG tanker. The vessel 6 is adapted to carry liquefied gas in its gas tanks 4. Normally there are several tanks in an LNG tanker, but in the figure only one gas tank 4 is shown for clarity reasons. The gas tank 4 is filled so that there is always an ullage space section 4.1 filled with gas in gaseous form and a liquid phase section 4.2 filled with liquefied gas. During the storing of the liquefied gas the gas is evaporating changing its phase and transferring to the ullage space 4.1 section. The evaporated gas may be utilised in a consumption device 5 of the vessel 6. The consumption device 5 may be e.g. a gas engine providing propulsion power for the vessel. In the figure 1 there is only one consumption device 5 is shown but it is clear that there may be several devices.

The vessel 6 is provided with a gas supply arrangement 1, which comprises a gas supply line 2 being provided with a compressor unit 2.1. The gas supply line 2 extends from an ullage space section 4.1 of the gas tank 4 to a consumption device 5. Other gas tanks (not shown) are also connected to inlet side of the compressor unit 2.1 correspondingly. The gas supply line 2 is arranged for delivering the evaporated boil-off gas from the gas tank 4 to the consumption device 5 of the vessel 6. The gas tank 4 is maintained slightly over-pressurised. The gas supply line 2 is provided with the compressor unit 2.1 for maintaining the pressure in the gas tank 4 at desired level and for raising the pressure of the boil-off gas to an adequate level for usage in the consumption device 5. The lower limit is typically ruled by requirements of the gas engines of the vessel being as the consumption device 5. Desired pressure level in the gas tank 4 is maintained by the compressor unit 2.1 The compressor unit 2,1 is preferably controlled by making use of a first pressure measurement device 10 provided in the gas supply line 2 after the compressor and a second pressure measurement device 10' provided in the gas supply line 2 before the compressor. The compressor unit may be provided with inlet vane control, which allows certain variation in the capacity. In case the pressure in the gas main supply line (measured by the device 10) is decreasing and simultaneously the pressure in the gas tank is too low, an alternate way of producing greater amount of gas must be provided. This will be described in the following.
The gas tank 4 is provided with arrangement 3 for producing gaseous gas from the liquefied gas in the gas tank 4. The arrangement shown in the figure comprises a piping 3.1, which extends from the liquid phase section 4.2 to the ullage space section 4.1 of the gas tank 4. Even not shown it is conceivable to arrange the piping extending between two separate gas tanks. The piping comprises a pump 3.2, positioned preferably at the liquid phase section of the gas tank 4. The other end of the piping 3.1 is provided with a nozzle unit 3.4, which is arranged to open into the ullage space section 4.1 of the gas tank 4. The piping is also provided with a control valve 3.5 for controlling the flow rate in the piping 3.1. In practise the piping

comprise any suitable ducting, like tube system or channels integral to other devices in the arrangement.
Additionally there is a heat transfer unit 3.6 provided in the piping 3.1 by means of which it is possible to control the temperature of the sprayed liquefied gas. The heat transfer unit is provided with a heat exchanger 3.7 arranged in the piping after the control valve 3.5 in the gas flow direction, through which gas may flow and heat up. The heat exchanger 3.7 is connected to a heat transfer circuit 3.8 in which e.g. water-glycol mixture is arranged to flow for heating the gas. The heat transfer circuit 3.8 may also be connected to a second heat exchanger 2.3 for controlling the temperature of the gas in the gas supply line 2 and a third heat exchanger 5.1 recovering heat from the consumption device 5. This way excess heat in the consumption device 5 may be utilised effectively. As shown schematically by the dotted lines the heat transfer circuit may include also other parts and elements.
The piping 3.1 is additionally provided with a bypass conduit 3.10 through which water-glycol mixture may pass by the heat exchanger 3.7. The bypass flow is controlled by a three-way valve 3.9, which is positioned in the piping after the heat exchanger 3.7 in the gas flow direction. The tree-way valve combines the flow routes through the heat exchanger 3.7 and through the bypass conduit 3.10. This coupling provides a gas temperature control function for the gas sprayed through the nozzle unit 3.4.
In connection with the gas tank there are at least two sensors provided, which have been provided to be used for operating of the gas supply arrangement 1. A first sensor 3.3 is provided for measuring the pressure in the ullage space section 4.1 of the gas tank 4 and a second sensor 3.11 is provided for measuring the temperature in the ullage space section 4.1 of the gas tank 4.
The basic idea of the invention is to controllably evaporate gas in the gas tank 4 by providing advantageous circumstances for phase transition phenomenon particularly in the ullage space section and/or above the surface of the liquid phase sec-

tion. This is advantageously accomplished as explained in the following. Liquefied gas is introduced from the liquid phase section to the ullage space section without substantially increasing the temperature of the liquefied gas in liquid phase section of the tank. The temperature in the ullage space section 4.1 is higher than the temperature of the liquefied gas and in the present invention this fact is controllably utilised in connection with controlling the evaporation of the gas.
When the amount of natural boil-off gas is not enough to feed the consumption device 5 additional boil-off gas is needed. According to the invention, greater amount of gas than produced by natural evaporation may be accomplished by controllably spraying liquefied gas in to the ullage space section 4.1. An actuator of the valve 3.5 is controlled making use of the pressure value obtained from the first sensor 3.3. In case the consumption of the gas increases through the gas supply line 2 the pressure in the ullage space section will decrease, which will be registered by a control system (not shown) based on the measurement of the first sensor 3.3. Subsequently the control system will drive the valve 3.5 to open more, which causes the flow rate of sprayed gas to increase. Naturally the pump 3.2 is in operation also. The flow pattern of the sprayed gas is such that the droplets are very small or possibly even mist. Since the temperature in the ullage space section is higher than the liquefied gas, a part of the sprayed gas will evaporate, and thus compensate the consumption of the gas, and also the pressure drop in the ullage space section. Thus advantageous circumstances for phase transition phenomenon in the ullage space section and/or above the surface of the liquid phase section are provided. This way the pressure level in the ullage space section 4.1 is maintained at desired level and also additional gas is produced from the liquefied gas according to the invention.
The evaporation of the gas consumes energy and the temperature in the ullage space section tends to decrease accordingly while gas is evaporated. The temperature in the ullage space section 4.1 is registered by a control system (not shown) based on the measurement of the second sensor 3.11. Now the control system will drive the three-way valve 3.9 to pass more gas through the heat ex-
changer 3.7 and warm up the sprayed gas. This result in less heat consumption in the evaporation of the gas. According to the invention the temperature of the sprayed gas is maintained approximately at minus 130°C. Maintaining the gas approximately at this temperature assists the fractionation of gas in a manner that, for the most part, only nitrogen and methane will be evaporated. The heavier hydrocarbons contained by the liquefied gas will remain in liquid phase and return to the liquid phase section 4.1 of the gas tank 4.
For ballast conditions there may be a connection between at least two tanks (no shown) in order to transfer liquefied gas from one tank to other. It is also possible to leave the tank properly filled for ballast voyage.
For situations when there will be a low load on the consumption device 5, a thermal oxidiser 11 is installed. The intention is to burn all surplus boil-off gas in the thermal oxidiser when the boil-off gas production from the gas tank is higher than the consumption. Control dependencies in the figure 1 is shown informally by dotted lines for clarity reasons. However, it is clear that the control system may be realised by various manners, using centralised or distributed control arrangements.
The invention is not limited to the embodiment shown but several modifications of the invention are conceivable within the scope of the appending claims





CLAIMS
1. Gas supply arrangement (1) of a marine vessel (6) being adapted to carry lique
fied gas in its gas tank (4) having an ullage space section (4.1) and a liquid phase
section (4.2), which arrangement provides the gas for demands of the vessel, the
arrangement comprising:
- a gas supply line (2) provided for delivering the gas formed in the gas tank to a
consumption device (5),
- a piping (3.1) extending from the liquid phase section (4.2) to the ullage space
section (4.1) of the gas tank (4) being provided with at least a pump (3.1), for in-
troducing gas into the ullage space section, characterised in that the piping is pro-
vided with a heat transfer unit (3.6) for effecting on the temperature of the intro-
duced gas.

2. Gas supply arrangement (1) of a marine vessel (6) according to claim 1, char-
acterised in that the arrangement is provided with a first sensor (3.3) adapted for
measuring the pressure in the ullage space section (4.1) of the gas tank (4), and
that the piping is provided with a control valve (3.5), and that the first sensor (3.3)
is arranged in control communication with the control valve (3.5).
3. Gas supply arrangement (1) of a marine vessel (6) according to claim 1, char
acterised in that the heat transfer unit (3.6) comprises a heat exchanger (3.7) ar
ranged in the piping, and that the piping is provided with a bypass conduit (3.10)
passing by the heat exchanger (3.7) and with a three-way valve (3.9) for control the
gas flow between the heat exchanger and the bypass conduit (3.10).
4. Gas supply arrangement (1) of a marine vessel (6) according to claim 3, char
acterised in that the arrangement is provided with a second sensor (3.11) adapted
for measuring the temperature in the ullage space section (4.1) of the gas tank (4),
and that the second sensor (3.11) is arranged in control communication with the
three-way valve (3.5).
5. Method of providing gas in a marine vessel (6) with liquefied gas tank (4) hav
ing an ullage space section (4.1) and liquid phase section (4.2), and a gas con
sumption device (5), in which arrangement gas is evaporated in the gas tank (4)
and led to the consumption device (5) via a gas supply line (2) while the pressure
in the gas tank (4) is substantially continuously measured by a first sensor 1,2,3),
characterised in that the evaporation rate of the gas in the gas tank (4'1 is con
trolled, by controllably spraying liquefied gas into the ullage space section and that
the flow rate of sprayed liquefied gas is controlled based on the pressure meas
urement of the first sensor (3.3).
6. Method of providing gas in a marine vessel (6) according to claim 5, character
ised in that the evaporation rate of the gas is controlled by controlling the tempera
ture of the sprayed gas.
7. Method of providing gas in a marine vessel (6) according to claim 6, character
ised in that the temperature of the sprayed gas (3.4) is controlled based on tem
perature value measured by a second sensor (3.11) provided in connection with
the gas tank (4) ullage space section (4.1).



Documents:

4008-delnp-2006-Abstract-(23-07-2013).pdf

4008-delnp-2006-abstract.pdf

4008-delnp-2006-Claims-(23-07-2013).pdf

4008-delnp-2006-claims.pdf

4008-DELNP-2006-Correspondence Others-(03-11-2011).pdf

4008-delnp-2006-Correspondence Others-(05-02-2014).pdf

4008-delnp-2006-Correspondence Others-(23-07-2013).pdf

4008-delnp-2006-Correspondence Others-(24-01-2014).pdf

4008-delnp-2006-Correspondence Others-(24-05-2013).pdf

4008-delnp-2006-correspondence-others-1.pdf

4008-delnp-2006-correspondence-others.pdf

4008-delnp-2006-description (complete).pdf

4008-delnp-2006-Drawings-(23-07-2013).pdf

4008-delnp-2006-drawings.pdf

4008-delnp-2006-form-1.pdf

4008-delnp-2006-form-18.pdf

4008-delnp-2006-Form-2-(23-07-2013).pdf

4008-delnp-2006-form-2.pdf

4008-delnp-2006-Form-3-(23-07-2013).pdf

4008-delnp-2006-form-3.pdf

4008-delnp-2006-form-5.pdf

4008-delnp-2006-GPA-(23-07-2013).pdf

4008-delnp-2006-gpa.pdf

4008-delnp-2006-pct-210.pdf

4008-delnp-2006-pct-220.pdf

4008-delnp-2006-pct-237.pdf

4008-delnp-2006-pct-304.pdf

4008-delnp-2006-pct-311.pdf

4008-delnp-2006-Petition-137-(05-02-2014).pdf

4008-delnp-2006-Petition-137-(23-07-2013).pdf

abstract.jpg


Patent Number 259304
Indian Patent Application Number 4008/DELNP/2006
PG Journal Number 11/2014
Publication Date 14-Mar-2014
Grant Date 07-Mar-2014
Date of Filing 12-Jul-2006
Name of Patentee WÄRTSILÄ FINLAND OY
Applicant Address Tarhaajantie 2, 65380 VAASA (FI).
Inventors:
# Inventor's Name Inventor's Address
1 JOHNNY KACKUR Airikintie 1 F 28, FI-20100 TURKU (FI).
PCT International Classification Number B63J 5/00
PCT International Application Number PCT/FI2005/050072
PCT International Filing date 2005-03-10
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 20045081 2004-03-17 Finland