Method and device for liquefaction of methane
11243026 · 2022-02-08
Assignee
Inventors
Cpc classification
F25J1/0219
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2290/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/004
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/032
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/0275
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/031
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/0254
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2245/90
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2290/62
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/0052
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/01
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C5/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2270/90
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/01
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E50/30
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
F25J1/0022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J1/0212
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/0337
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2230/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2215/60
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F25J1/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C5/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Method of liquefaction of methane and filling a tank (2) with liquefied methane, said method comprising: a step of liquefaction of the methane comprising an operation of cooling the methane to its saturation temperature, a step of filling the tank with the liquefied methane, a step of reinjection of the vaporized methane into the liquefaction system.
Claims
1. A method of liquefaction of methane and filling a transport tank with liquefied methane, comprising: a step of providing gaseous methane to a liquefaction system, a step of cooling the gaseous methane to its saturation temperature in the liquefaction system so as obtain the liquefied methane, a step of filling the transport tank with the liquefied methane, during which, in the transport tank, a fraction of the liquefied methane transitions to a second gaseous methane and the fraction of the liquefied methane that has transitioned to the second gaseous methane in the transport tank is returned to the liquefaction system, wherein: in the step of providing the gaseous methane to the liquefaction system, the gaseous methane arrives in the liquefaction system at a temperature of −100° C., the step of cooling the gaseous methane to its saturation temperature is performed at a pressure of 15 bar, in the filling step of the transport tank, the liquefied methane is introduced into the transport tank at a transport pressure, said transport pressure being less than or of 8 bar, and wherein the step of filling the transport tank with the liquefied methane is done from a buffer tank, and the liquefaction methane is stored in the buffer tank at a pressure of 15 bar and a temperature of −114° C.
2. The method according to claim 1, wherein the step of cooling the gaseous methane to its saturation temperature in the liquefaction system so as obtain the liquefied methane comprises an operation of compression of the gaseous methane.
3. The method according to claim 1, wherein pressure in the transport tank is reduced with the fraction of the liquefied methane that has transitioned to gaseous methane in the transport tank being removed and returned to the liquefaction system.
4. The method according to claim 1, wherein the gaseous methane is compressed at the pressure of 15 bar by a compressor in order to carry out the step of cooling the gaseous methane to its saturation temperature performed at the pressure of 15 bar, and wherein the compressor has a discharge temperature substantially equal to 80° C.
5. The method according to claim 1, wherein the gaseous methane is cooled a first time to a temperature substantially equal to 20° C. in the liquefaction system, then the gaseous methane is cooled a second time to a temperature of −90° C. in the liquefaction system.
6. The method according to claim 5, wherein the gaseous methane is cooled a third time to a temperature of −114° C. in the liquefaction system.
Description
(1) Other objects and advantages of the invention will be seen from the following description of an embodiment, provided with reference to the appended drawings in which:
(2)
(3)
(4)
(5)
(6) Schematically represented in
(7) In one embodiment represented in
(8) The liquefaction system 3 comprises, in the order of passage of the gas (represented in
(9) The filling system 4 takes the liquefied methane from the buffer tank 11 to the transport tank 2.
(10) The filling system 4 comprises a first part 12 and a second part 13 connected to each other by an injection connection 14. The first and second parts 12, 13 respectively comprise a first shutoff valve 15 and a second shutoff valve 16. Said shutoff valves 15, 16 make it possible, when the injection connection 14 is unlocked, to interrupt the flow of methane coming from the buffer tank 11 and from the transport tank 2. The second part 13 further comprises a pressure regulator 17 enabling the pressure of the liquefied methane leaving the buffer tank 11 to be lowered.
(11) The reinjection system 5 connects the buffer tank 11 and the transport tank 2 at the intake of the liquefaction system 3. Thus, the fraction of methane being vaporized in the buffer tank 11 and in the transport tank 2 is recovered and routed to the liquefaction system 3 in order to be processed again. The buffer tank 11 comprises a pressure gauge or pressure sensor (not shown). Said pressure gauge is connected to a computerized unit (not shown). Thus, when the pressure in the buffer tank 11 is too high for one reason or another, the computerized unit controls the relief of the pressure in the buffer tank 11.
(12) The reinjection system 5 connects the buffer tank 11 and the transport tank 2 at the liquefaction system 3. The reinjection system 5 comprises a pressure regulator 18 situated downstream from the buffer tank 11 as well as a reinjection solenoid valve 19, a valve 20 and a pressure gauge 21 (or pressure sensor) situated downstream from the transport tank 2. The reinjection solenoid valve 19 is manipulated by an actuator (not shown), which is also controlled by a computerized unit (not shown). A reinjection connection 22 makes it possible to separate the transport tank 2 from the reinjection system 5. The valves 19, 20 are arranged in such a way as to block any flow of methane out of the transport tank 2 and out of the reinjection system 5 when the reinjection connection 22 is unlocked. The buffer tank 11 is continuously fed by the liquefaction system 3; the pressure there varies, slightly increasing because of the heat gain through the insulation of the buffer tank 11. The pressure regulator 18 enables the pressure in the buffer tank 11 to be regulated. Said regulation is achieved by releasing the fraction of methane that is vaporized due to heat losses in the buffer tank 11, said gaseous methane being returned to the liquefaction system 3.
(13) The liquefaction method will be described in the following, step by step. Said method comprises: a step of liquefaction of the methane with compression thereof and filling of the buffer tank 11, a step of relieving the pressure of the methane leaving the buffer tank 11 to the transport tank 2.
(14) During the liquefaction step, the gaseous methane arrives in the device 1 at a temperature close to −100° C. and enters the first heat exchanger 6 where it is reheated to a temperature of about 20° C. The gaseous methane then enters a compressor 7 in order to be compressed to a pressure of 15 bar. The compressor 7 has a discharge temperature of about 80° C. because it is cooled. The methane leaving the compressor 7 is therefore at a pressure of 15 bar and a temperature of 80° C. The methane is cooled to a temperature of 20° C. in a second heat exchanger 8. The methane then passes again through the first heat exchanger 6 where its temperature is lowered to −90° C. At this stage, the methane is still in a gaseous state. It is liquefied in the liquefaction exchanger 9, where it is cooled to a saturation temperature of close to −114° C., corresponding to the saturation pressure of 15 bar. The liquefied methane is then stored in the buffer tank 11 at a pressure of 15 bar and a temperature of −114° C.
(15) The transport tank 2 is then filled with liquefied methane from the buffer tank 11 at a transport pressure. Typically, the transport pressure is between 1 and 8 bar, while the pressure in the buffer tank 11 is about 15 bar. The liquefied methane is routed from the buffer tank 11 to the transport tank 2 by means of the filling system 4. In the filling system 4, the pressure of the liquefied methane (15 bar) is lowered to the transport pressure (between 1 and 8 bar) by means of the pressure regulator 17. Thus, the transport tank 2 is filled with liquefied methane at the transport pressure.
(16) The saturation pressure and temperature relationship is presented by the pressure—enthalpy diagram illustrated in
(17) It should be noted that the coolant fluids are not identical in each of the heat exchangers. The first heat exchanger 6 is cooled by the flow of gaseous methane entering the device 1. The methane initially being at a temperature near −100° C., this temperature is used to cool the methane coming from the second heat exchanger 8. The second heat exchanger 8 uses water as the coolant fluid. The liquefaction exchanger 9 uses a hydrocarbon mixture as coolant. These fluids are particularly efficient in the cryopreservation industry because of their phase change temperatures.
(18) In the buffer tank 11, a fraction of methane is vaporized continuously because of heat losses. Said gaseous fraction is returned to the liquefaction system 3 by means of the reinjection system 5, thus maintaining a flow of gas in the device 1.
(19) Simultaneously, the transport tank 2 is filled from the buffer tank 11 at the transport pressure of less than 8 bar. As the transport tank is filled, the valve 19 regulates the pressure in the transport tank 2 in order to maintain the desired pressure. This makes it possible not to impede the passage of the methane entering the transport tank 2 while ensuring the safety of the facility. The transport tank 2 and the buffer tank 11 comprise a safety valve 23 that is triggered when the internal pressure of the tanks reaches a predetermined threshold that is deemed critical for the facility. The valves 23 are connected to a gas flare (not shown).
(20) When the transport tank 2 is filled, the injection valves 15, 16 are closed and the valves 19, 20 continue to regulate for a period of time, if necessary, the pressure in the transport tank 2. When said pressure reaches the desired transport pressure (as indicated by the pressure gauge 21), the valves 19, 20 are closed in turn and their connections 14, 22 are unlocked. The transport tank 2 can then be replaced by an empty tank.
(21) The fact that the methane can be liquefied at higher pressures than those of the transport pressure enables substantial energy savings. The saturation temperature of the methane at a pressure of 15 bar is higher than the saturation temperature at a pressure of 4 bar, for example. Thus, to maintain the methane in liquid state, less energy is necessary because the liquefaction temperature is higher. Indeed, it seems that increasing the pressure in the liquefaction system 3 is less energy-intensive than lowering the temperature in said system.
(22) Said finding is validated by a series of calculations that we present below. The thermodynamic data of the methane that are furnished in the calculations are data from the Refprop 9® Software developed and marketed by the National Institute of Standards and Technology (NIST).
(23) During liquefaction, the compression of the gaseous methane and its cooling to a cryopreservation temperature are the most energy-consuming operations.
(24) We are therefore going to compare liquefaction of methane at 15 bar and methane compressed at 4 bar.
(25) The value of 15 bar is not arbitrarily chosen. Said value is the result of calculations made by the applicant. The curves in
(26) In
(27) As can be seen in
(28) Methane compressed at 4 bar is liquefied at a temperature of 131 K. To liquefy the methane, the cooling system uses a cooling fluid at a temperature obviously less than the liquefaction temperature of the methane. Take, for example, a cooling fluid at a temperature of 126 K. We consider the condensation temperature of the system at 20° C. or 293 K, while taking into consideration normal climatic conditions of 15° C. In the calculations that follow, the values are rounded off.
(29) We calculate the coefficient of performance (COP):
(30)
(31) Liquefaction is done ideally with a cooling system having a COP equal to 0.75. By taking a COP of the cooling system of 30% compared to the ideal COP, we calculate a COP of 0.23.
(32) In the device described, the methane initially being at −90° C. or 163 K should go below −142° C. or 131 K. The energy needed is therefore 100 kJ/kg.sub.methane (
(33) The electricity consumption is given by dividing the enthalpy by the COP, i.e.:
(34)
(35) The compression of 1 to 4 bar requires energy of 183 kJ.sub.electricity/kg.sub.methane. Thus, there is a total electricity consumption of 2,694 kJ.sub.electricity/kg.sub.methane.
(36) Let us now take the example of liquefaction at a pressure of 15 bar.
(37) The liquefaction temperature of the methane at 15 bar is −114° C. or 159 K. Under the same climatic conditions as before, the COP is given by the following relationship:
(38)
(39) This gives us an actual COP of 0.33. The cooling from −90° C. or 183 K to −114° C. or 159 K requires energy of 52 kJ/kg.sub.methane. The change-of-state enthalpy equals 378.8 kJ/kg.sub.methane, which makes a total of 430.8 kJ/kg.sub.methane cooling energy needed. The electricity consumption needed is:
(40)
(41) The compression from 1 to 15 bar requires electric energy of 526.5 kJ/kg.sub.methane. Therefore, total energy of 1,822.5 kJ.sub.electricity/kg.sub.methane is needed.
(42) Said liquefaction method therefore enables a savings of electric energy of nearly 48%. At an industrial scale, said method therefore makes it possible to lighten the energy bill considerably, reducing it by nearly half.
(43) Said method can also be applied to gas from natural deposits. In such a case, it is foreseeable to benefit from the pressure of the deposit in order to eliminate the compression step. Liquefaction can therefore be performed at a pressure of 15 bar without first compressing the methane.
(44) Advantageously, the pressure of the methane coming from the buffer tank 11 is relieved as close as possible to the transport tank 2. This arrangement is applicable in a case in which the transport tank 2 is an LNG vessel. Indeed, in port installations, the cryopreservation units are frequently at some distance from the filling terminals of the LNG vessels. Thus, the liquid methane travels sometimes several kilometers in pipelines before being stored in the LNG vessel. Pipelines are generally underwater or underground and are not refrigerated. Consequently, part of the transported methane is vaporized. The idea is therefore to transport the methane at a pressure of about 15 bar and to relieve the pressure just before it enters the LNG vessel. Thus, the temperature difference between the methane and the exterior environment is not as high as if the methane were transported at lower pressures.
(45) However, another solution can be considered. This involves carrying out a pressure-relief stage. Indeed, for various reasons, transporting methane at a pressure of 15 bar may not be possible. Consequently, a first pressure relief can advantageously be effected at the output of the buffer tank 11. The pressure of the methane is then less than 15 bar but higher than the transport pressure. Thus, the methane is transported to the LNG vessel, where the pressure is again relieved before the methane goes on board. This makes it possible to prevent too large a fraction of methane from vaporizing in the pipelines. Overall, the performance is improved since less methane is vaporized and then returned to the cryopreservation unit to be liquefied again. The unit will therefore consume less energy.