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    • 专利摘要:
    Cryogenic heat pump (10) for a liquefied gas treatment device, comprising in closed circuit at least one compressor (12), at least one expander (14), a first cold receiving circuit (16) extending between said at least one compressor and said at least one expander, and a second cold-transmitting circuit (18) extending between said at least one expander and said at least one compressor, said closed circuit having a cryogenic fluid configured to be in a two-phase state in at least a part of this circuit, said second cold-transmitting circuit being configured to have a temperature lower than -40 ° C.
    公开号:FR3066257A1
    申请号:FR1850519
    申请日:2018-01-23
    公开日:2018-11-16
    发明作者:Bernard Aoun
    申请人:Gaztransport et Technigaz SARL；
    IPC主号:
    专利说明:

    Cryogenic heat pump and its use for the treatment of liquefied gas
    TECHNICAL FIELD The invention relates to a heat pump for cryogenic application and its application for the treatment of liquefied gas, for example in a liquefied natural gas transport vessel. It also relates to a device for treating liquefied gas, a ship comprising such a device, as well as methods of treatment. By treatment is meant, for example, the cooling and / or heating of liquefied gas. Furthermore, the liquefied gas may be a liquefied natural gas, mainly comprising methane, or else another liquefied gas such as ethane, propane, butane, LPG, etc.
    STATE OF THE ART
    In order to more easily transport gas, such as natural gas, over long distances, the gas is generally liquefied (to become liquefied natural gas - LNG) by cooling it to cryogenic temperatures, for example -163 ° C at atmospheric pressure. The liquefied gas is then loaded into specialized vessels.
    In a liquefied gas transport ship, for example of the LNG carrier type, machines are provided to supply the energy requirements of the operation of the ship, in particular for the propulsion of the ship and / or the production of electricity for on-board equipment. These machines are generally thermal machines which consume gas which is supplied from the cargo of liquefied gas transported in the tanks of the ship.
    In order to limit the evaporation of the liquefied gas from the tanks, it is known to store it under pressure so as to move over the liquid-vapor equilibrium curve of the liquefied gas considered, thus increasing its vaporization temperature. The liquefied gas can thus be stored at higher temperatures, which has the effect of limiting the evaporation of the gas. Natural evaporation of the gas is however inevitable, this phenomenon being called NBOG which is the acronym of the English Natural Boil-Off Gas (as opposed to the forced evaporation of gas or FBOG, acronym of the English Forced Boil- Off Gas). The gas which evaporates naturally in the tank of a ship is generally used to supply the above-mentioned machines. In the case (first case) where the quantity of naturally evaporated gas is insufficient for the fuel gas demand of the machines, a pump immersed in the tank is actuated to supply more combustible gas after forced evaporation. In the case (second case) where the quantity of evaporated gas is too large compared to the demand of the machines, the excess gas is generally burned in a boiler, which represents a loss of combustible gas.
    In the current technique, the improvements in the tanks are such that the natural evaporation rates (BOR - acronym for the Boil-Off Rate) of the liquefied gases are becoming lower, while the machinery of a ship is becoming more efficient. This has the consequence, in each of the first and second cases mentioned above, that the difference is very large between the quantity of gas naturally produced by evaporation and that required by the installation of a ship.
    Consequently, there is a growing interest in solutions for cooling the liquefied gas contained in a storage tank and for managing the BOG generated in this tank, such as for example reliquefaction or cooling units.
    The present invention provides in particular a solution to this need.
    PRESENTATION OF THE INVENTION The invention relates to a cryogenic heat pump for a liquefied gas treatment device, comprising in closed circuit at least one compressor, at least one pressure reducer, a first cold exchange circuit extending between said at least one compressor and said at least one expansion valve, and a second cold exchange circuit extending between said at least one expansion valve and said at least one compressor, said closed circuit comprising a cryogenic fluid configured to be in a two-phase state in at least part of this circuit, said second circuit being configured to circulate said fluid at a temperature less than or equal to -40 ° C.
    In the present application, the term "cryogenic" means a very low temperature and in particular less than -40 ° C, or even less than -90 ° C, and preferably less than -160 ° C. A fluid or a cryogenic heat pump is thus a fluid or a pump capable of being at or operating at such a low temperature.
    A heat pump is a unit well known per se but not for cryogenic application. A heat pump conventionally comprises in a closed circuit a compressor, an expansion valve, and heat exchange circuits extending between the compressor and the expansion valve. The compressor compresses a refrigerating or cryogenic fluid, which increases its temperature, this heated fluid being able to transmit its heat in one of the aforementioned circuits. At the outlet of this circuit, the fluid is expanded in the expansion valve, which decreases its temperature, this cooled fluid being able to absorb heat in the other of the circuits and then replenishes the compressor. The invention proposes to use this known technology by using a cryogenic fluid and by configuring the various constituent elements of the pump so that one of the circuits, called the first circuit, is a circuit for receiving cold and therefore for warming (the fluid circulating in this circuit having for example a temperature higher than -160 ° C, and for example ranging between -115 ° C and 45 ° C), and the other of the circiits, called second circuit, either a circuit of cold transmission and which can be sought to achieve sub-cooling or even slight heating. The fluid circulating in this second circuit is for example at a temperature between -169 ° C and -161 ° C for the case of a sub-cooling circuit, and at a temperature between -165 ° C and -160 ° C for the case of a low heating product. The fluid thus circulates in this circuit at a temperature less than or equal to -160 ° C. This is in the case where the fluid to be cooled is LNG composed mainly of methane. In the case where the LNG to be cooled consists mainly of ethane, cryogenic fluid would circulate in the second circuit at a temperature less than or equal to -90 ° C. In the case where the LNG to be cooled consists mainly of propane and butane, the cryogenic fluid would thus circulate in the second circuit at a temperature less than or equal to -40 ° C.
    The pump according to the invention may include one or more of the following characteristics, taken in isolation from one another or in combination with each other: - said first circuit is configured to allow the circulation of said fluid from said at least one compressor to to said at least one regulator, - said second circuit is configured to allow the circulation of said fluid from said at least one regulator to audit at least one compressor, - the pump comprises an outlet of said first circuit and the regulator, on the one hand , and the output of said second circuit and the compressor, on the other hand, are connected by third and fourth mutual heat exchange circuits, - said circuits are part of the same heat exchanger, or of two or three exchangers separate heat, - said cryogenic fluid is chosen from N2, CH4 or O2, or a mixture of these gases, - said compressor is able to compress gas intended supplying gas to at least one machine of said vessel, said compressor being further connected by valves to the circuits and to said at least one machine so as to be able to isolate it from the machine, when it is operating for the heat pump, and isolating it from the heat pump, when it is operating for said at least one machine, - said first cold reception circuit is configured to have at its input a temperature less than or equal to -90 ° C, and preferably less than or equal to -160 ° C, and / or at output a temperature greater than or equal to 0 ° C, and preferably greater than or equal to 25 ° C, - said second cold transmission circuit is configured to have at its output a temperature less than or equal to -90 ° C, and preferably less than or equal to -160 ° C.
    The present invention also relates to a device for treating liquefied gas, comprising a pump system intended to be immersed in a tank for storing said liquefied gas, and at least one heat pump as described above, the first cold receiving circuit of which is configured to heat a fifth natural evaporation gas heating circuit intended to be connected to a natural evaporation gas outlet of said tank, and / or a sixth liquefied gas heating circuit connected to said pump system, and the second cold transmission circuit of which is configured to cool or heat a seventh liquefied gas circuit connected to said pump system.
    In the present application, a treatment of liquefied gas is understood to mean, for example, the cooling and / or heating of this liquefied gas. The invention makes it possible to make significant energy savings because the heating of the BOG and the cooling or even also the heating of the LNG are provided by a heat pump which is more efficient than the units known today and used to perform these functions. . The invention can, for example, make it possible not to use seawater to cool the BOG before it is used by machinery of the ship.
    The device according to the invention may include one or more of the following characteristics, taken in isolation from one another or in combination with one another: - an outlet from said seventh circuit is intended to be connected to an inlet for liquefied gas from said tank , and preferably at least one liquefied gas spraying boom in the upper part of the tank and / or at least one means for injecting said liquefied gas at the bottom of this tank, - an outlet from said fifth circuit and / or a output of said sixth circuit are connected to at least one compressor intended to supply gas to at least one machine of a liquefied gas transport ship, such as for example a propulsion engine of said ship, an electric generator, and / or a boiler , - an output of said compressor configured to supply gas to at least one machine, is connected to an eighth heat exchange circuit with said first circuit and / or ledi t fifth circuit and / or said sixth circuit, - an output of said eighth circuit is connected to an input of a ninth heat exchange circuit with said second circuit and / or said seventh circuit, - said at least one compressor is connected by valves respectively at the outlet of the fifth circuit and / or of the sixth circuit, and to said at least one machine, as well as by valves respectively to the first and second circuits, - said circuits are part of the same heat exchanger, or several separate heat exchangers, - the heat pump is configured so that, at the outlet from said expansion valve, the cryogenic fluid has a temperature at least 3 ° C lower than the temperature of the liquefied gas entering said seventh circuit.
    The present invention also relates to a liquefied gas transport vessel, comprising at least one tank for storing this gas and a device as described above.
    The present invention also relates to a method for cooling and / or heating liquefied gas stored in a ship as described above, comprising the steps consisting in: a) taking liquefied gas from the tank and circulating it in said seventh circuit in order to modify its temperature, then b) reinject this liquefied gas into the tank, at the top and / or at the bottom of the tank.
    The method according to the invention can comprise one or more of the following characteristics or steps, taken in isolation from one another or in combination with one another: c) take natural evaporation gas from the tank and circulate it in said fifth circuit in order to increase its temperature, and d) take liquefied gas from the tank and circulate it in said sixth circuit in order to vaporize it and increase its temperature, and / or e) supply said at least one configured compressor for supplying gas to at least one machine of said vessel, with gas leaving said fifth circuit and / or said sixth circuit, and f) optionally taking part of the gas leaving said at least one compressor and circulating this gas in said eighth circuit , or even in said ninth circuit, in order to cool it, and / or g) circulating the gas leaving said eighth circuit in said ninth circuit in order to cool it.
    According to a first mode of operation, steps a), b), c) and d) are carried out simultaneously when said vessel is at a high speed, corresponding for example to a speed greater than a predetermined threshold, liquefied gas being reinjected in tank bottom in step b).
    According to a second operating mode, steps a), b) and c) are carried out simultaneously when said vessel is at cruising speed, corresponding for example to cruising speed, liquefied gas being reinjected at the bottom of the tank at l 'step b).
    According to a third mode of operation, steps a), b) and c) are carried out simultaneously when said vessel is at a low speed, corresponding for example to a speed below a predetermined threshold, liquefied gas being reinjected at the top of the tank in step b).
    According to a fourth operating mode, steps a), b), c), e), f) and g) are carried out simultaneously when said vessel is at low speed, corresponding for example to a speed much lower than a predetermined threshold. , liquefied gas flowing in said seventh circuit for its heating and mixing with gas leaving said ninth circuit, before its reinjection into the tank in step b), preferably at the bottom of the tank.
    According to a fifth mode of operation, steps a), b), c) and e) are carried out simultaneously when said vessel is at a low speed, corresponding for example to a speed much lower than a predetermined threshold, liquefied gas being reinjected in the upper part of the tank in step b).
    The method may further comprise: - a step of using at least one compressor to compress gas for the supply of gas to at least one machine of the ship, and - a step of using the same at minus a compressor to compress cryogenic fluid in the heat pump.
    The present invention also relates to a method of treating gas from a gas storage installation, in particular on board a ship, the method comprising the following steps: - extraction of a portion of a first gas in the liquid state of a tank, - a first sub-cooling of the portion of the first gas in the liquid state, and - storage of the first gas in the liquid state sub-cooled in the lower part of the tank so as to constitute a layer of cold reserve of the first gas in the liquid state at the bottom of the tank.
    The method according to the invention may comprise one or more of the following characteristics or steps, taken in isolation from one another or in combination with one another: - the first gas stored in the cold reserve layer of the tank is used to cooling the first gas in the vapor state located in the upper part of the tank and the first gas in the liquid state, - the first gas stored in the cold reserve layer is sprayed into the tank and in the layer of the first gas in the vapor state, - the first gas stored in the cold reserve layer is extracted from the bottom of the tank and reliquefies the first gas in the vapor state through a heat exchanger, - said lower part s '' extends over approximately less than 30% of the height of the tank measured from its bottom, said bottom being the lowest end of the tank, - the first sub-cooled gas is stored in the cold reserve layer at a temperature between -45 ° and -55 ° C at atmospheric pressure, - the first gas in the liquid state remaining in the tank is at a temperature above -42 ° C, - the first gas is a liquefied natural gas.
    The present invention also relates to a gas treatment system of a gas storage installation, in particular on board a ship, the system comprising: - a tank in which is stored a first gas in the liquid state; a first heat exchanger configured to produce a first sub-cooling of the first gas extracted from the tank by a first pipe, the first pipe opening out at the bottom of the tank so as to store the first sub-cooled gas at the bottom of the tank to form a cold reserve layer of the first gas in the liquid state.
    The system may include one or more of the following characteristics, taken in isolation from one another or in combination with each other: - the tank comprises an outlet connected to a first end of a pipe, the pipe comprising a second end coupled to a spray bar installed in the upper part of the tank, - the system comprises a heater installed on the second pipe in which the second gas heated or vaporized in the first heat exchanger circulates, - the first gas is a liquefied natural gas.
    The characteristics and / or steps of the method and of the system can be combined with those of the other aspects (heat pump, device, etc.) of the invention mentioned in the foregoing. The invention also relates to a ship, in particular for transporting liquefied gas, comprising at least one system of the aforementioned type.
    BRIEF DESCRIPTION OF THE FIGURES The invention will be better understood and other details, characteristics and advantages of the present invention will appear more clearly on reading the description which follows, given by way of nonlimiting example and with reference to the accompanying drawings, in which: - Figures 1 to 20 show several alternative embodiments of the invention, and - Figures 21 and 22 show diagrams of temperature changes as a function of the entropy of a cryogenic fluid flowing in a pump heat according to the invention, as well as the saturation curve of a liquefied natural gas which here is mainly methane, - Figures 23 and 24 show diagrams of temperature evolution as a function of the entropy of a cryogenic fluid circulating in a heat pump according to the invention, as well as the saturation curve of a liquefied natural gas which is here mainly ethane, and - Figures 25 and 26 show diagrams of temperature evolution as a function of the entropy of a cryogenic fluid circulating in a heat pump according to the invention, as well as the saturation curve of a liquefied natural gas which is mainly propane and butane here.
    DETAILED DESCRIPTION The invention uses a cryogenic heat pump, that is to say a unit capable of transferring thermal energy at cryogenic temperatures close to the storage temperature of an LNG.
    The heat pump is in the form of a closed circuit and is designated by the reference 10 in the various drawings. The heat pump 10 comprises four essential elements, namely at least one compressor 12, at least one regulator 14, a first circuit 16 for receiving cold extending between the compressor and the regulator, and a second circuit 18 for transmitting cold extending between the regulator and the compressor.
    A cryogenic fluid, chosen for example from N2, CH4 and O2, or a mixture of these gases, circulates in the heat pump. This fluid is intended to be in the gaseous state or in the two-phase state in the circuit. The fluid circulates for example in the gaseous state in the compressor 12 and in the first circuit 16. It is preferably in the two-phase state at the outlet of the regulator and in the second circuit 18.
    The fluid is intended to be brought to a cryogenic temperature, that is to say up to a very low temperature below -160 ° C in the case where the LNG to be cooled is mainly composed of methane. The examples illustrated by FIGS. 1 to 20 illustrate the invention in the context of an LNG composed mainly of methane but the invention also applies to LNG composed mainly or mainly of ethane, butane and / or propane .
    In order to enhance the performance of the heat pump 10, it can include other heat exchange circuits 20, 22. Thus, the output of the first circuit 16 and the regulator 14 are connected by a third heat exchange circuit 20, and the output of the second circuit 18 and the compressor 12, are connected by a fourth heat exchange circuit 22.
    The two circuits 20, 22 can be part of the same heat exchanger E1 and are configured to exchange calories with each other, the fluid being cooled by circulation in the third circuit, and heated by circulation in the fourth circuit.
    Likewise, as shown in FIG. 8, the first circuit 16 can be integrated into the exchanger comprising the circuits 20, 22. In this case, the circuits 16, 20 can be shared and therefore combined. In the alternative embodiment of FIG. 9, the second circuit 18 is also integrated into the exchanger comprising the circuits 16, 20, 22. In this case, the circuits 16, 20, on the one hand, and the circuits 18, 22, on the other hand, are shared and confused. In yet another variant not shown, the second circuit 18 would be integrated into the exchanger comprising the circuits 20, 22, and the circuit 16 would remain remote and independent.
    Figures 21 to 26 show the advantage of using additional circuits 20, 22 in the heat pump 10.
    In each of these Figures 21 to 26, the curved curve (referenced C1 in Figure 21) is the saturation curve of an LNG, which is mainly methane in Figures 21 and 22, ethane in Figures 23 and 24, and a mixture of propane and butane in FIGS. 25 and 26.
    The curve representing a thermodynamic cycle (referenced C2 or C2 ’in Figures 21 and 22) shows the evolution of the temperature of a cryogenic fluid, such as N2, as a function of the entropy. In FIG. 21, as well as in FIGS. 23 and 25, the heat pump does not have the circuits 20, 22, and in FIG. 22, as well as in FIGS. 24 and 26, the heat pump comprises such circuits 20 , 22. It can be seen that the additional circuits 20 and 22 make it possible to modify the hysteresis curve. At a given entropy, cooling is more effective if the temperature of the cryogenic fluid is significantly lower than the temperature of the LNG to be cooled, for the same entropy on the saturation curve of this LNG. For the various LNG listed above, it can be seen that the circuits 20, 22 allow, for a wide range of entropy values, to guarantee a significant temperature difference between the coldest temperature of the cryogenic fluid, when it leaves regulator, and the temperature of the LNG to cool. This temperature difference is preferably at least 3 ° C. The greater the temperature difference, the more the fluid flow in the heat pump can be minimized. In conclusion, the circuits 20, 22 increase the performance of the heat pump.
    The exchanger (s) used are, for example, of the type with tubes and calenders, with plates, etc.
    The compressor 12 has for example a compression ratio between 10 and 20% and a flow rate between 200 and 2000 m3 / h.
    The regulator 14 has for example an expansion rate between 10 and 20% and a flow rate between 200 and 200 m3 / h. The regulator is for example a Joule-Thomson valve.
    In a particular embodiment of the invention: - the temperature at the outlet of the compressor is between 30 and 60 ° C and is for example of the order of 45 ° C, - the temperature at the outlet of the first circuit 16 is included between -130 ° C and -100 ° C, and is for example of the order of -115 ° C, - the temperature at the outlet of the regulator 14 is between -160 ° C and -200 ° C, and is for example of the order of -170 ° C, and - the temperature at the outlet of the second circuit 18 is between -160 ° C and -200 ° C, and is for example of the order of -170 ° C.
    In the exemplary embodiment of FIG. 1, the heat pump 10 is integrated into a liquefied natural gas (LNG) transport vessel which comprises at least one tank 24 for storing LNG.
    Typically, an LNG tank 24 comprises LNG in the liquid phase and LNG in the gas phase, the latter resulting from the natural evaporation of LNG in the tank. Natural evaporative gas is called BOG or NBOG.
    The tank 24 includes a BOG outlet 26, which is logically located in an upper part of the tank where the BOG naturally accumulates. The tank is also equipped with a pumping system comprising one or more pumps 28, 30 which are immersed in the LNG. The tank 24 of Figure 1 is equipped with a pump 28 and that of Figure 2 is equipped with two pumps 28, 30. The or each pump is connected to a liquefied gas outlet 32, 34 of the tank.
    In the example shown, the output of BOG 26 is connected to a fifth heat exchange circuit 36 with the first circuit 16, and the LNG output 32 is connected to a seventh heat exchange circuit 38 with the second circuit 18.
    In view of the above, depending on the temperature of the fluid in the circuit 18, it is understood that the LNG can be sub-cooled or heated in the circuit 38. For example, in the case where the LNG has at the input of the circuit 38 a temperature between -165 and -161 ° C, it would add a temperature between -170 and -160 ° C at the output. It is further understood that the BOG (which has a temperature between -140 and -120 ° C, and for example of the order of -120 ° C) can be reheated in circuit 36 for example to a temperature comprised between 0 and 45 ° C, and for example of the order of 25 ° C.
    The temperature of the LNG in the tank can vary between a minimum value (-165 ° C) and a maximum value (-161 ° C). The coldest LNG is naturally stored at the bottom of the tank and is represented by layer 40 in tank bottom. The or each pump 28.30 can be located at the bottom of the tank so as to be able to take LNG as cold as possible.
    In the case where cold LNG at -165 ° C for example has been withdrawn, this LNG could circulate in the circuit 38 to cool the fluid in the circuit 18, and therefore be heated by the fluid in the circuit 18. In the case where Less cold LNG would be taken, for example at -161 ° C, this LNG could circulate in circuit 38 to heat the fluid in circuit 18, and therefore be cooled by the fluid in circuit 18.
    In the case shown in FIG. 1, cold LNG is taken from the lower layer 40 and is slightly reheated by circulation in the circuit 38. It emerges for example at a temperature of the order of -160 ° C. and can be reinjected in tank 24.
    The tank thus comprises at least one LNG inlet 42 which is connected to the outlet of the circuit 38 and which is also here connected to a spraying boom 44 located inside the tank, in its upper part, above the maximum level of LNG in the tank. In known manner, LNG is sprayed in the liquid state in the BOG of the tank so as to cool it and to recondense / reliquefy it.
    In the alternative embodiment of Figure 2, identical elements are referenced by the same numbers. This variant differs from the previous variant mainly in that the exit from BOG is not shown. The second pump mentioned in the above is connected to an LNG outlet 34 which is connected to a sixth heat exchange circuit 46 with the first circuit 16.
    The two pumps 28, 30 are preferably located at the bottom of the tank for taking LNG from the layer 40. In this case, the LNG sent to circuit 46 will have a temperature less than or equal to -160 ° C and it will come out heated from this circuit with a temperature between 0 and 45 ° C and for example of the order of 25 ° C.
    The variant of FIG. 3 represents a combination of the variants of FIGS. 1 and 2. There are found the two circuits 36, 46, which exchange heat between them as well as with the first circuit 16. It is thus understood that the BOG and the LNG circulating respectively in circuits 36, 46 will be heated while the fluid circulating in circuit 16 will be cooled.
    Figure 4 shows an LNG recondensation installation in a transport vessel. The BOG leaving the circuit 36 supplies a compressor 48 configured to supply gas to at least one machine of the ship, such as for example a propulsion engine of said ship, an electric generator, and / or a boiler. The compressed gas (BOG) which is not used by the machines can be cooled and liquefied before being reinjected into the tank 24. At least one heat exchanger is used to heat the BOG before supplying the compressor 48 and to cool and re-liquefy the gas leaving the compressor before it is reintroduced into the tank 24. The installation thus comprises an eighth heat exchange circuit 50 with the circuit 36, and a ninth heat exchange circuit 52 with the circuit 38.
    The recondensation system of FIG. 4 comprises a compressor 48. The compressed BOG can be at the input of circuit 50 at a temperature between 20 and 60 ° C, and for example of the order of 45 ° C, and the BOG in input of circuit 52 can be at a temperature between -130 and -90 ° C and for example of the order of -110 ° C. As a result of circuit 52, the BOG, reliquified, can be at a temperature less than or equal to -160 ° C. This liquefied gas can be reinjected at the bottom of the tank 24.
    The variant of FIG. 5 represents the combination of the variant of FIG. 3 with the recondensation installation as shown in FIG. 4.
    In the example shown, three heat exchangers E1, E2, E3 are used but there could be more or less. The E1 exchanger is that of the heat pump. In a second heat exchanger E2, the circuits 36, 46, 50, 16 cooperate so as to heat the BOG before supplying the compressor 48 and to cool the excess BOG (not used by the compressor). In another exchanger E3, the circuits 18, 38 and 52 cooperate so as to cool the BOG obtained above as well as to cool or heat the LNG withdrawn from the tank, as will be seen below.
    The variants of Figures 6 and 7 include a fourth heat exchanger E4. In the case of FIG. 6, the heat exchanger E4 comprises a heat exchange circuit 54 interposed between the LNG outlet 34 and the circuit 46, and another heat exchange circuit 56 interposed between the output of LNG 32 and circuit 38. The LNG outlet 34 can be connected to the inlet of circuit 54 by a pressure reducer. The exchanger E2 comprises circuits 36, 46 and 16, and the exchanger E3 comprises circuits 18 and 38. It is understood that the LNG which circulates in circuit 54 is previously expanded and is therefore colder than the LNG which circulates in the circuit 56. The LNG of circuit 54 will therefore be heated by the exchanger E4 before reaching the exchanger E2, and the LNG of the circuit 56 will therefore be cooled by the exchanger E4 before reaching the exchanger E3.
    The variant of FIG. 7 combines the variants of FIGS. 4 and 6. In this new variant, the exchanger E2 comprises the circuits 36, 46, 50 and 16, and the exchanger E3 comprises the circuits 18, 52 and 38.
    Figures 8 and 9 have been discussed in the foregoing. The exchangers E1 and E2 are combined and form only one in the variant of FIG. 8. In the variant of FIG. 9, the exchangers E1, E2 and E3 form only one.
    The variant embodiments of FIGS. 10 and 11 represent the integration of a heat pump 10 in a ship and the use of this heat pump in relation to machines 58, 60 of the ship such as for example a propulsion engine. , an electric generator, and / or a boiler. The exchanger E2 is of the type shown in FIG. 1. The output of the above-mentioned circuit 36 is here connected to two compressors 48 supplying the machines 58, 60.
    The variants of FIGS. 10 and 11 also show that the outlet of the circuit 38 or the inlet 42 of the tank 24 can be equipped with a three-way valve 62, one passage of which is connected to the outlet of the circuit 38, one passage is connected to the ramp 44 and the other passage is connected to an injection system at the bottom of the tank.
    The variants of FIGS. 12 and 13 are similar to those of FIGS. 10 and 11. The exchanger E2 is here similar to that of FIG. 5 insofar as it comprises the circuit 50 which receives at the inlet gas leaving the compressor (s) 48. The exchanger E3 of FIGS. 12 and 13 is similar to that of FIG. 5 also.
    Figure 14 is similar to Figure 9 and further shows operating temperatures in a particular embodiment of the invention.
    We will now describe five modes of operation of the ship and the associated heat pump.
    The first operating mode is represented in FIGS. 15a and 15b and corresponds to the case where the propulsion speed of the ship is greater than a predetermined threshold value, which is for example 16 knots. In this case, the machines 58, 60 are supplied with BOG which is NBOG or even FBOG and therefore comes from the outlet 26 or the outlets 26, 32 of the tank 24. The cryogenic energy of the heat pump is used here to sub-cool the LNG. This mode optimizes the consumption of the ship for the operation of its machines.
    BOG is naturally produced in the tank 24 and leaves the tank to supply the circuit 36 as well as the compressors 48 and the machines. The tank can be fitted with a pressure sensor to measure the BOG pressure in the tank and thus detect that a predetermined threshold has been exceeded. Generally, the pressure in the tank 24 is between 80 and 150mbarg. During the first operating mode, the pressure in the tank is medium and can be around lOOmbarg.
    If the speed of the ship is very important and the requirements for gaseous LNG are greater than the naturally produced BOG, it is possible to force the generation of BOG and thus form FBOG. LNG is then taken from outlet 36 of the tank and conveyed to circuit 46. In circuits 36, 46, the BOG and LNG are heated by circuit 16 of the heat pump and is found entirely in the gaseous state and at a temperature close to ambient temperature at the inlet of the compressors 48. The compressors increase the gas pressure for the needs of the machines. In parallel, the circuit 18 of the heat pump is used to cool the LNG sampled by the outlet 32 and circulating in the circuit 38, before its reinjection at the bottom of the tank via the valve 62.
    The second operating mode is represented in FIGS. 16a and 16b and corresponds to the case where the propulsion speed of the ship is of the order of the aforementioned threshold value, which is for example 16 knots. The ship's LNG gas requirements are roughly equal to the naturally produced BOG. In this case, the machines are supplied with BOG which is NBOG and therefore comes from outlet 26 of the tank. The cryogenic energy from the heat pump is used here to sub-cool the LNG. During the second operating mode, the pressure in the tank is around 120mbarg.
    The third operating mode is shown in Figures 17a and 17b and corresponds to the case where the ship's propulsion speed is slightly lower than the threshold value, and for example between 14 and 16 knots. In this case, the machines are supplied with BOG which is NBOG alone. The NBOG produced in the tank is sufficient to supply the ship. This NBOG even exceeds the needs of the ship. The generation of NBOG is here limited by spraying LNG into the BOG of the tank, so as to recondense BOG into LNG. During the third operating mode, the pressure in the tank is around 120mbarg.
    For this last part, the circuit 18 of the heat pump is used to cool the LNG sampled by the outlet 32 and circulating in the circuit 38, before its reinjection by the ramp 44 in the tank.
    The fourth operating mode is shown in Figure 18 and corresponds to the case where the ship's propulsion speed is much lower than the threshold value, and for example less than 14 knots. In this case, there is too much NBOG produced relative to the needs of the machines and part of the compressed gas leaving the compressor (s) 48 circulates in the circuit 50 then in the circuit 52 for cooling. The cryogenic energy from the heat pump is used here to sub-cool this gas and recondense it before it is reinjected into the tank. In this case, it is considered that LNG sub-cooled to a temperature of approximately -165 ° C. is stored in layer 40. The pump 28 takes cold LNG from the bottom of the tank, the LNG circulates in circuit 38 and heats up slightly to leave the circuit 38 at a temperature close to or even identical to that of the LNG leaving the circuit 52. The LNG leaving these two outlets are mixed and reinjected by means of the valve 62 at the bottom of the tank. During the fourth operating mode, the pressure in the tank is significant and for example of the order of 140mbarg.
    The fifth mode of operation is shown in Figure 19 and is similar to the previous mode of operation. There is too much NBOG produced in relation to the needs of the machines and part of the compressed gas leaving the compressor (s) 48 is burned in a boiler 64. The generation of NBOG is here limited by spraying LNG into the BOG of the tank , so as to recondense BOG into LNG. The cryogenic energy from the heat pump is used here to sub-cool this gas and recondense it before it is reinjected into the tank. During the fifth operating mode, the pressure in the tank is significant and for example of the order of 140mbarg.
    Finally, FIG. 20 illustrates a last variant embodiment of the invention in which the heat pump 10 uses one or one of the compressors 48 used for supplying the machines 58, 60 of the ship, rather than a dedicated compressor 12. Conversely, it can be considered that the ship's machines are supplied with gas by the compressor of the heat pump. In this case, the input of or one of the compressors 48 is connected on the one hand to the output of the circuit 36 and to the output of the circuit 22, and the output of or one of the compressors 48 is connected on the one hand at the entrance to circuit 16 and to machines 58, 60.
    In practice, there is a redundancy of the compressors 48 supplying the machines for safety reasons. When one of the compressors 48 fails, the other can be used to supply the machines with gas and guarantee the operation and especially the propulsion of the ship. Due to the presence of at least two compressors 48, it is therefore possible, when the first compressor 48 is functional and used to power the machines, to isolate the second compressor 48 and to use it as part of the pump heat 10. Isolation valves 66 are provided upstream and downstream of the second compressor 48, to connect its input and output respectively to the circuit 36 and to the machines 58, 30. Other isolation valves 68 are provided upstream and downstream of the second compressor 48, to connect its input and its output respectively to circuit 22 and to circuit 16.
    It is thus understood that, by default where the first compressor 48 will be functional, the valves 66 will be closed and the valves 68 will be opened so that the second compressor 48 is used in the heat pump. In the event that the first compressor 48 fails, the valves 68 would be closed and the valves 66 would be open. It would then be possible to supply the machines with compressed gas but it would then no longer be possible to use the heat pump 10.
    权利要求:
    Claims (24)
    [1" id="c-fr-0001]
    1. Cryogenic heat pump (10) for a liquefied gas treatment device, comprising in closed circuit at least one compressor (12, 48), at least one pressure reducer (14), a first circuit (16) for receiving cold extending between said at least one compressor and said at least one expansion valve, and a second circuit (18) for transmitting cold extending between said at least one expansion valve and said at least one compressor, said closed circuit comprising a cryogenic fluid configured to be in a two-phase state in at least part of this circuit, said second cold transmission circuit being configured to have an output temperature less than or equal to -40 ° C.
    [2" id="c-fr-0002]
    2. Heat pump (10) according to claim 1, in which the outlet of said first circuit (16) and the pressure reducer (14), on the one hand, and the outlet of said second circuit (18) and the compressor (12) , on the other hand, are connected by third and fourth circuits (20, 22) of mutual heat exchanges.
    [3" id="c-fr-0003]
    3. Heat pump (10) according to claim 1 or 2, wherein said circuits (16, 18, 20, 22) are part of the same heat exchanger, or two or three separate heat exchangers.
    [4" id="c-fr-0004]
    4. Heat pump (10) according to one of the preceding claims, in which said cryogenic fluid is chosen from N2, CH4 or O2, or a mixture of these gases.
    [5" id="c-fr-0005]
    5. Heat pump (10) according to one of the preceding claims, in which said compressor (48) is capable of compressing gas intended to supply gas to at least one machine (58, 60) of said vessel, said compressor being in further connected by valves (66, 68) to the circuits (16, 18) and to said at least one machine so as to be able to isolate it from the machine, when it is operating for the heat pump (10), and to isolating it from the heat pump, when it operates for said at least one machine.
    [6" id="c-fr-0006]
    6. Heat pump (10) according to one of the preceding claims, in which said second cold transmission circuit is configured to have at its output a temperature less than or equal to -90 ° C, and preferably less than or equal to - 160 ° C.
    [7" id="c-fr-0007]
    7. A device for treating liquefied gas, comprising a pump system (28, 30) intended to be immersed in a tank for storing said liquefied gas, and at least one heat pump (10) according to one of the preceding claims, the first cold reception circuit (16) is configured to heat a fifth natural evaporation gas heating circuit (36) intended to be connected to an outlet (26) of natural evaporation gas from said tank, and / or a sixth liquefied gas heating circuit (46) connected to said pump system, and the second cold transmission circuit (18) of which is configured to cool or heat a seventh liquefied gas circuit (38) connected to said pump system (28, 30).
    [8" id="c-fr-0008]
    8. Device according to claim 7, in which an outlet from said seventh circuit (38) is intended to be connected to an inlet (42) for liquefied gas from said tank, and preferably to at least one spraying boom (44). liquefied gas in the upper part of the tank (24) and / or at least one means for injecting said liquefied gas at the bottom of this tank.
    [9" id="c-fr-0009]
    9. Device according to claim 7 or 8, in which an outlet of said fifth circuit (36) and / or an outlet of said sixth circuit (46) are connected to at least one compressor (48) intended to supply gas to at least one machine (58, 60, 64) of a liquefied gas transport ship, such as for example a propulsion engine of said ship, an electric generator, and / or a boiler.
    [10" id="c-fr-0010]
    10. Device according to claim 9, in which an output of said compressor (48) configured to supply gas to at least one machine is connected to an eighth heat exchange circuit (50) with said first circuit (16) and / or said fifth circuit (36) and / or said sixth circuit (46).
    [11" id="c-fr-0011]
    11. Device according to the preceding claim, in which an output of said eighth circuit (50) is connected to an input of a ninth circuit (52) for heat exchange with said second circuit (18) and / or said seventh circuit ( 38).
    [12" id="c-fr-0012]
    12. Device according to one of claims 9 to 11, wherein said at least one compressor (48) is connected by valves (66) respectively to the outlet of the fifth circuit (36) and / or of the sixth circuit (46) , and said at least one machine, as well as by valves (68) respectively to the first and second circuits (16, 18).
    [13" id="c-fr-0013]
    13. Device according to one of claims 7 to 12, wherein said circuits (16, 18, 20, 22, 36, 38, 46, 50, 52) are part of the same heat exchanger, or of several exchangers separate heat.
    [14" id="c-fr-0014]
    14. Device according to one of claims 7 to 13, wherein the heat pump is configured so that, at the outlet of said pressure reducer (14), the cryogenic fluid has a temperature lower by at least 3 ° C at the temperature of the liquefied gas entering said seventh circuit (38).
    [15" id="c-fr-0015]
    15. Liquefied gas transport vessel, comprising at least one tank (24) for storing this gas and a device according to one of claims 7 to 14.
    [16" id="c-fr-0016]
    16. A method of cooling and / or heating liquefied gas stored in a ship according to claim 15, comprising the steps consisting in: a) taking liquefied gas from the tank (24) and circulating it in said seventh circuit (38 ) in order to modify its temperature, then b) reinject this liquefied gas into the tank, at the top and / or at the bottom of the tank.
    [17" id="c-fr-0017]
    17. The method as claimed in claim 16, comprising the steps consisting in: c) taking natural evaporation gas from the tank (24) and circulating it in said fifth circuit (36) in order to increase its temperature, and / or d) taking liquefied gas from the tank and circulating it in said sixth circuit (46) in order to vaporize it and increase its temperature.
    [18" id="c-fr-0018]
    18. Method according to one of claims 17, the device being as defined in claim 9 or 10, comprising the steps consisting in: e) supplying said at least one compressor (48) configured to supply gas to at least one machine (58, 60, 64) of said vessel, with gas leaving said fifth circuit (36) and / or said sixth circuit (46), and f) optionally taking part of the gas leaving said at least one compressor and circulating this gas in said eighth circuit (50), or even in said ninth circuit (52), in order to cool it.
    [19" id="c-fr-0019]
    19. Method according to all of claims 16 and 17, wherein steps a), b), c) and d) are carried out simultaneously when said vessel is at a high speed, corresponding for example to a speed greater than a threshold predetermined, liquefied gas being reinjected at the bottom of the tank in step b).
    [20" id="c-fr-0020]
    20. Method according to all of claims 16 and 17, in which steps a), b) and c) are carried out simultaneously when said vessel is at cruising speed, corresponding for example to a cruising speed, of liquefied gas being reinjected at the bottom of the tank in step b).
    [21" id="c-fr-0021]
    21. Method according to all of claims 16 and 17, in which steps a), b) and c) are carried out simultaneously when said vessel is at a low speed, corresponding for example to a speed below a predetermined threshold, and / or when the pressure in said at least one tank is less than a predetermined threshold, liquefied gas being reinjected in the upper part of the tank in step b).
    [22" id="c-fr-0022]
    22. Method according to all of claims 16 to 18, in which steps a), b), c), e), f) and g) are carried out simultaneously when said vessel is at low speed, corresponding for example to a speed much lower than a predetermined threshold, of the liquefied gas circulating in said seventh circuit with a view to its heating and its mixture with gas leaving said ninth circuit, before its reinjection into the tank in step b), preferably at the bottom tank.
    [23" id="c-fr-0023]
    23. Method according to all of claims 16 to 18, in which steps a), b), c) and e) are carried out simultaneously when said vessel is at a low speed, corresponding for example to a speed much less than a predetermined threshold, liquefied gas being reinjected into the upper part of the tank in step b).
    [24" id="c-fr-0024]
    24. Method according to one of claims 16 to 23, further comprising: - a step of using at least one compressor (48) to compress gas for the supply of gas to at least one machine of the ship, and - a step of using the same at least one compressor to compress cryogenic fluid in the heat pump.
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    同族专利:
    公开号 | 公开日
    KR20200113222A|2020-10-06|
    FR3066257B1|2019-09-13|
    CN111758003A|2020-10-09|
    RU2020125198A3|2022-01-31|
    WO2019145643A1|2019-08-01|
    EP3743652A1|2020-12-02|
    RU2020125198A|2022-01-31|
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    法律状态:
    2018-11-23| PLSC| Publication of the preliminary search report|Effective date: 20181123 |
    2019-01-30| PLFP| Fee payment|Year of fee payment: 2 |
    2020-01-31| PLFP| Fee payment|Year of fee payment: 3 |
    2021-01-27| PLFP| Fee payment|Year of fee payment: 4 |
    2021-11-29| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1850519|2018-01-23|
    FR1850519A|FR3066257B1|2018-01-23|2018-01-23|CRYOGENIC HEAT PUMP AND ITS USE FOR THE TREATMENT OF LIQUEFIED GAS|FR1850519A| FR3066257B1|2018-01-23|2018-01-23|CRYOGENIC HEAT PUMP AND ITS USE FOR THE TREATMENT OF LIQUEFIED GAS|
    FR1851136A| FR3066248B1|2017-05-12|2018-02-09|GAS TREATMENT METHOD AND SYSTEM OF A GAS STORAGE INSTALLATION FOR A GAS TRANSPORT VESSEL|
    JP2020540556A| JP2021512258A|2018-01-23|2019-01-23|Methods and systems for processing gas in gas storage facilities for gas tankers|
    EP19710009.2A| EP3743652A1|2018-01-23|2019-01-23|Cryogenic heat pump and use thereof in the treatment of liquefied gas|
    US17/048,529| US20210164728A1|2018-01-23|2019-01-23|Method and system for processing gas in a gas storage facility for a gas tanker|
    KR1020207023781A| KR20200111208A|2018-01-23|2019-01-23|Methods and systems for gas treatment in gas storage facilities for gas tankers|
    CN201980009856.6A| CN111630313A|2018-01-23|2019-01-23|Method and system for treating gas in a gas storage facility of a gas tanker|
    EP19701513.4A| EP3743651A1|2018-01-23|2019-01-23|Method and system for processing gas in a gas storage facility for a gas tanker|
    RU2020125198A| RU2020125198A3|2018-01-23|2019-01-23|
    PCT/FR2019/050152| WO2019145643A1|2018-01-23|2019-01-23|Cryogenic heat pump and use thereof in the treatment of liquefied gas|
    PCT/EP2019/051590| WO2019145342A1|2018-01-23|2019-01-23|Method and system for processing gas in a gas storage facility for a gas tanker|
    CN201980009682.3A| CN111758003A|2018-01-23|2019-01-23|Cryogenic heat pump and its use in liquefied gas treatment|
    KR1020207023782A| KR20200113222A|2018-01-23|2019-01-23|Use of cryogenic heat pumps and cryogenic heat pumps for liquefied gas treatment|
    RU2020125193A| RU2020125193A3|2018-01-23|2019-01-23|
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