Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is apparent that the described embodiments are some embodiments of the present invention, but not all embodiments of the present invention. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
Unless otherwise defined herein, technical or scientific terms used herein should be given the ordinary meaning as understood by one of ordinary skill in the art to which this invention belongs. Unless explicitly described as such, the words "first," "second," and similar words used herein do not denote any order, quantity, or importance, but rather are used to distinguish one element from another. The word "comprising" or "comprises", and the like, means that elements or items preceding the word are meant to encompass the elements or items listed thereafter and equivalents thereof without excluding other elements or items. The terms "connected" or "connected," and the like, are not limited to physical or mechanical connections, but may include electrical connections, whether direct or indirect. In order to keep the following description of the embodiments of the present invention clear and concise, well-known functions, known components, or detailed descriptions that are common general knowledge are omitted. Under the condition of no conflict, all the technical features in the embodiments of the present invention can be combined with each other, and the combined embodiments still belong to the protection scope of the present invention.
The embodiment of the invention discloses a coupling system for liquid air energy storage and liquefied natural gas regasification, which specifically comprises an LAES subsystem, an LNG-RG subsystem and a coupled cooling subsystem as shown in figures 1-8;
The LAES subsystem is used for converting the ambient air into liquid air for storage under a charging working condition and converting the liquid air into regasified air for expansion working under a discharging working condition, and concretely comprises a heat storage tank HD, a normal temperature compressor C1, a multi-stage low temperature compressor unit consisting of at least 2 low temperature compressors, a low temperature expander CE, a liquid-air separator LAS, a liquid air storage tank LAD, a discharging low temperature pump DCP and an expander E, wherein the normal temperature compressor C1 is sequentially connected in series. The device comprises a normal temperature compressor C1, a multi-stage low temperature compressor unit formed by at least 2 low temperature compressors which are sequentially connected in series, a low temperature expander CE, a liquid-air separator LAS and a liquid air storage tank LAD, wherein the normal temperature compressor C1, the multi-stage low temperature compressor unit formed by at least 2 low temperature compressors which are sequentially connected in series, the low temperature expander CE, the liquid air separator LAS and the liquid air storage tank LAD form an ambient air liquefaction path under a charging working condition of the low temperature compressor unit, the ambient air is converted into liquid air for storage, and the liquid air storage tank LAD, a discharge low temperature pump DCP and an expander E form a liquid air regasification path under a discharging working condition of the liquid air storage tank LAD, the discharge low temperature pump DCP and the expander E are sequentially connected in series, so that the liquid air is converted into regasified air for expansion work. The heat storage tank HD recovers compression heat energy from ambient air discharged from the normal temperature compressor C1 under a charging condition, and supplies the compression heat energy to regasified air under a discharging condition to heat and expand the regasified air.
The LNG-RG subsystem is used to convert Liquefied Natural Gas (LNG) to Natural Gas (NG), and specifically includes an LNG cryogenic pump (not shown) and an LNG regasification line (LNG to NG path in the illustration).
The coupled cooling exchanging subsystem comprises a cold accumulating device and a cooling exchanging device, wherein the cooling exchanging device is used for constructing a cooling exchanging system between the LAES subsystem and the LNG-RG subsystem, at least supporting the LNG-RG subsystem to output cold energy to the LAES subsystem, and storing and releasing the cold energy of the LNG-RG subsystem and the LAES subsystem, for example supporting the LNG-RG subsystem to output cold energy to the LAES subsystem, the LNG-RG subsystem to output cold energy to the cold accumulating device and the cold accumulating device to output cold energy to the LAES subsystem, and the cold accumulating device is used for storing and releasing the cold energy of the two subsystems. Wherein, in some embodiments, the cold storage device can have the functions of cold storage and cold exchange at the same time, and further can replace at least part of the cold exchange device.
Under the charging working condition of the LAES subsystem, the ambient air is compressed by the normal temperature compressor in sequence and outputs the compression heat energy to the heat storage tank, the coupled cooling exchanging subsystem utilizes the cryogenic energy generated by the LNG-RG subsystem and the cold energy stored under the discharging working condition of the LAES subsystem to cool to cryogenic temperature, the coupled cooling exchanging subsystem is compressed to cryogenic temperature to enter the next-stage low-temperature compressor for compression, the ambient air with target pressure is obtained after the ambient air is compressed by the last-stage low-temperature compressor, the coupled cooling exchanging subsystem is cooled to cryogenic temperature, and the converted liquid air is stored in the liquid-air separator to the liquid air storage tank after the cryogenic energy is expanded by the low-temperature expander.
The cryogenic temperature is the pressurized outlet temperature in the regasification process of the liquefied natural gas, and the cryogenic temperature is the ambient air outlet temperature after the ambient air is compressed at a low temperature.
Specifically, the pressurized outlet temperature during the regasification of lng refers to the temperature at the outlet location of the lng cryogenic pump during the regasification of lng, and the ambient air outlet temperature after the ambient air is cryogenically compressed refers to the temperature at the outlet location of each cryogenic compressor during the liquefaction of ambient air.
Further, the cold storage device comprises a cryogenic tank DCD in a cold exchange system of the access coupling cold exchange subsystem, and the cryogenic tank DCD is at least used for storing and releasing cryogenic energy generated by the LNG-RG subsystem. In some embodiments, the cryogenic tank may be further configured to store and release cryogenic energy generated during a discharging condition of the LAES subsystem, and further the coupled cooling exchange subsystem may utilize the cryogenic energy of the LNG-RG subsystem and the cryogenic energy stored during the discharging condition of the LAES subsystem to cool ambient air to a cryogenic temperature, where, when the cryogenic tank is involved in a cooling condition of the LAES subsystem or when the LNG-RG subsystem outputs the cryogenic energy to the cryogenic tank, the cold end temperature is the cryogenic temperature, that is, the temperature of the liquefied natural gas after being pressurized by the liquefied natural gas discharging cryopump before being heated by any heat source, is the lowest temperature of the cold energy outputted by the LNG-RG, and the hot end temperature is the shallow cooling temperature, that is, the ambient air outlet temperature after the ambient air is compressed at a low temperature.
In general, the temperature of the pressurized outlet in the process of regasification of the LNG will only exist on the LNG-RG subsystem side, after being subjected to cold exchange, the temperature of the LNG reaches the side of the coupled cold exchange subsystem (for example, cold storage equipment such as a cryogenic tank) and the temperature of the LNG at the side of the liquid air energy storage system will be affected by factors such as heat exchange efficiency and heat exchanger pinch point, and the pressurized outlet temperature in the process of regasification of the LNG cannot be kept continuously, which is common knowledge in the art, and for easy understanding, the cryogenic temperature of the LNG at the side of the coupled cold exchange subsystem (for example, cold storage equipment such as a cryogenic tank) and the LNG at the side of the liquid air energy storage system is set as the pressurized outlet temperature in the process of regasification of the LNG; it should be noted, however, that in practical applications, the cryogenic temperature is slightly different from the pressurized outlet temperature during LNG regasification, and that the difference between the actual cryogenic temperature and the pressurized outlet temperature during LNG regasification depends on the specific implementation parameters, but such differences do not affect the coverage and protection of the present invention.
According to the invention, the coupling cooling exchange subsystem is established between the LAES subsystem and the LNG-RG subsystem, and the high-grade cold energy of the LNG-RG subsystem is utilized to directly reduce the temperature of the ambient air before entering the low-temperature compressor to the cryogenic temperature through the double-temperature compression mode of normal-temperature compression and multi-stage low-temperature compression, so that the power consumption of the air compression process of the LAES subsystem can be reduced, and the charge and discharge efficiency of the whole LAES subsystem can be further improved.
The multi-stage low-temperature compressor unit in the embodiment of the invention is composed of at least 2 low-temperature compressors which are sequentially connected in series, such as a two-stage low-temperature compressor unit, a three-stage low-temperature compressor unit, a four-stage low-temperature compressor unit and the like. The multistage low-temperature compressor unit is mainly used for gradually compressing the ambient air to the target pressure so as to collect the ambient air with the target volume, and therefore, the stage number of the multistage low-temperature compressor unit can be set according to the design requirement of the system.
It should be noted that as the ambient air is compressed to gradually increase its pressure, the present invention cools the ambient air to a cryogenic temperature, at which time the dew point of the ambient air may be already higher than the cryogenic temperature, thereby causing a potential risk of equipment loss for the cryogenic compressors of the next stage, so that the temperature of the ambient air before entering each stage of the cryogenic compressors needs to be controlled to be lower than the dew point temperature of the ambient air.
For a typical system design, the ambient air dew point may be higher than the cryogenic temperature, which occurs after the penultimate low temperature compression or during the final low temperature compression, and therefore the ambient air temperature prior to entering the final low temperature compressor must be controlled to be not lower than the ambient air dew point temperature. Preferably, the ambient air entering the final stage cryocompressor is at least 5 degrees above the dew point temperature.
On the other hand, in the multi-stage low-temperature compression process, the high-pressure ambient air cooled to the cryogenic temperature is possibly completely liquefied, and the low-temperature compressor cannot continue to be suitable for subsequent compression at the moment, so that the low-temperature pump can continue to complete subsequent compression, and the high-pressure liquid air with the target volume is collected.
Further, the LAES subsystem may further include a charge cryopump for further compressing air to a higher pressure in a liquid or supercritical state at cryogenic temperatures;
The normal temperature compressor, the multi-stage low temperature compressor unit, the charging low temperature pump, the low temperature expander, the liquid-air separator and the liquid air storage tank are connected in sequence to form the ambient air liquefaction path;
and in the charging working condition of the LAES subsystem, the ambient air is compressed by the multi-stage low-temperature compressor, cooled to the cryogenic temperature by the coupling cooling subsystem, enters a complete liquefaction or supercritical state, is compressed to the higher pressure required by design by the charging low-temperature pump, is cooled to the cryogenic temperature by the coupling cooling subsystem, and enters the low-temperature expander.
In some embodiments, the cold storage device of the coupled cold exchange subsystem of the present invention may further comprise a shallow cold tank SCD for storing and releasing at least the shallow cold energy generated by the LNG-RG subsystem. The cold end temperature of the shallow cooling tank is the hot end temperature of the deep cooling tank, and the hot end temperature of the shallow cooling tank is the ambient temperature.
In some embodiments, the temperatures of the hot end and the cold end of the cryogenic tank and the shallow cold tank are defined in the invention, and certain differences exist according to the practical working conditions and the practical design parameter selection. For example, the shallow cooling temperature defined by the invention is the temperature of the ambient air discharged by the low-temperature compressor, and the temperature of the ambient air discharged by the low-temperature compressors of different stages can slightly differ, depending on the actual working condition and the setting of the compression ratio of the low-temperature compressor. The invention sets the temperature of the hot end of the cryogenic tank, and is used for matching the temperature of the ambient air before and after the low-temperature compressor to the greatest extent, so that the heat exchange efficiency is improved. The existence of such differences, which are well known in the art, does not affect the scope or content of the present invention.
At this time, the cryogenic tank DCD and the shallow tank SCD in the coupled refrigeration subsystem may be used to sequentially and stepwise recover and release the cryogenic energy and the shallow cold energy generated by the LNG-RG subsystem (and/or the LAES subsystem).
In some embodiments, the shallow cooling tank SCD in the embodiments of the present invention may be also matched with the cryogenic tank DCD to recover the shallow cooling energy generated by regasifying the liquid air under the discharging condition of the LAES subsystem, and the cryogenic energy and the shallow cooling energy generated by regasifying the liquid air are released through the recovery of the cryogenic tank DCD and the shallow cooling tank SCD in sequential steps.
Furthermore, the coupling cooling exchange subsystem in the embodiment of the invention can pre-cool the ambient air which completes the compression heat recovery under the charging working condition of the LAES subsystem by utilizing the shallow cold energy generated by the LNG-RG subsystem and/or the shallow cold energy in the shallow cold tank, and cool the ambient air at the stage to the shallow cold temperature, and then cool the ambient air to the deep cold temperature, so that the consumption of the deep cold energy can be reduced, thereby reasonably utilizing the cold energy resource and reducing the consumption of the high-quality cold energy.
Further, the recovery of the shallow cold energy generated by the regasification of the liquid air from the discharge condition of the LAES subsystem is sufficient to pre-cool the ambient air to a shallow cold temperature under the charge condition of the LAES subsystem, so that the process does not consume the shallow cold energy from the LNG-RG subsystem basically, and the shallow cold energy in the shallow cold tank can be applied to the outside of the coupling system through the coupling and cooling subsystem under any condition of the LAES subsystem, thereby generating economic benefits. In addition, the shallow cooling energy of the two subsystems is recovered through the shallow cooling tank, so that the equipment cost is reduced.
In some embodiments, the LAES subsystem of the present invention may further include an ultra-cold tank UCD for storing and releasing the ultra-cold energy generated during the discharging operation of the LAES subsystem, wherein the ultra-cold tank UCD recovers the ultra-cold energy from the regasification of the liquid air during the discharging operation, and provides the ultra-cold energy for the ambient air after completing the multi-stage low-temperature compression and cooling to the cryogenic temperature during the charging operation, so that the temperature of the ambient air at the stage is cooled to the ultra-cold temperature, the ultra-cold temperature is the outlet temperature of the pressurizing pressure during the regasification of the liquid air, and the ultra-cold temperature is lower than the cryogenic temperature, so that the ambient air reaching the ultra-cold temperature is subjected to low-temperature expansion, and the liquefaction efficiency of the ambient air is improved.
The pressurized outlet temperature in the process of regasifying the liquid air refers to the outlet temperature of a low-temperature pump at a discharge point in the process of regasifying the liquid air.
Because the super cooling temperature of super cooling energy is lower than the pressurized outlet temperature in the regasification process of liquefied natural gas, the pressurized outlet temperature is more, and the pressurized outlet temperature cannot be provided by the LNG-RG subsystem, the cooling value is highest in the coupling system, and the liquefied efficiency of the ambient air can be effectively improved through the recovery and release of the super cooling tank UCD.
Specifically, under the charging condition of the LAES subsystem, after the ambient air is cooled to a cryogenic temperature through the low-temperature compression and coupling cooling subsystem of the last-stage low-temperature compressor, the ambient air enters the hot end of the super-cooling tank UCD, flows out of the cold end of the super-cooling tank UCD, sequentially enters the low-temperature expander CE and the liquid-air separator LAS, and the converted liquid air is stored in the liquid air storage tank LAD through the liquid-air separator LAS. The super-cold reflux air output by the liquid-air separator LAS firstly enters the cold end of the super-cold tank UCD and flows out from the hot end of the super-cold tank UCD, so that the recovery of super-cold energy in the super-cold reflux air is completed.
In some embodiments, the LAES subsystem of the present invention may further comprise a return air compressor C-UCA and a return air expander E-UCA, wherein at least a portion of the return air flowing from the hot end of the super-cooled tank UCD is compressed and warmed by the return air compressor C-UCA, cooled to cryogenic temperature by the coupled cooling subsystem, expanded and cooled by the return air expander E-UCA, and then is introduced into the super-cooled return air outputted from the liquid-air separator LAS and entering the cold end of the super-cooled tank UCD under the charging condition of the LAES subsystem, thereby supplementing super-cooled energy.
In some embodiments, the LAES subsystem according to the embodiments of the present invention may further comprise an air purifier APU disposed between the normal temperature compressor C1 and the multi-stage low temperature compressor unit for removing carbon dioxide and water from the ambient air entering the LAES subsystem, so that the ambient air without carbon dioxide and water is subjected to subsequent low temperature compression. Specifically, under the charging condition of the LAES subsystem, ambient air is compressed by the normal temperature compressor C1 and compressed heat energy is output to the heat storage tank HD, and then enters the air purifier APU, and after being purified, the ambient air is cooled to a cryogenic temperature by the coupled cooling subsystem and then enters the low temperature compressor unit.
The principle of the air purifier for removing carbon dioxide and water in the ambient air is that carbon dioxide and water in the ambient air are adsorbed by the molecular sieve, so that at least part of the regasified air output by the expander can be discharged to the environment after flowing through the air purifier under the discharge working condition of the LAES subsystem, and the desorption of the carbon dioxide and water in the air purifier is completed by utilizing the part of the ambient air, thereby achieving the circulating operation of the air purifier in the charge and discharge process.
In some embodiments, the coupling system of the embodiments of the present invention may further comprise an external heat source for providing external heat energy, wherein the external heat source is not limited to ambient air, seawater, or other ambient heat sources, solar energy, or industrial waste heat.
Under the discharging working condition of the liquid air subsystem, the heat storage tank HD and the external heat source can jointly provide compression heat energy and external heat energy for the regasified air to heat and expand.
Optionally, the expander E in the embodiment of the present invention may be a multi-stage expansion unit formed by a plurality of sequentially connected expanders, and the temperature of the regasified air entering each expander may be raised and expanded by using the compression heat energy and the external heat energy. Including but not limited to, the regasified air absorbing external heat energy provided by an external heat source prior to entering the preceding expander and absorbing compression heat energy provided by a thermal storage tank prior to entering the second expander, or the regasified air absorbing compression heat energy provided by a thermal storage tank prior to entering the first expander and absorbing external heat energy provided by an external heat source prior to entering the following expander
In some embodiments, the cold storage medium of the cold storage device of the coupled cold exchange subsystem in the embodiment of the invention can be a solid medium or a liquid medium, the cold exchange device can be a heat exchanger, and the heat exchanger is matched with the cold storage device to construct a cold exchange system of the coupled cold exchange subsystem, so that cold energy exchange among the cold storage device, the LAES subsystem and the LNG-RG subsystem is realized. The number and implementation positions of the heat exchangers can be determined by the design requirements of the system, and the selected heat exchange medium can be selected according to different temperature requirements, so that the invention is not limited to the above.
In one embodiment, the cold storage device of the coupled cooling exchange subsystem is a solid packed bed, the heat exchange device is a heat exchanger, and the heat exchanger constructs a cooling exchange system of the LAES subsystem, the LNG-RG subsystem and the solid packed bed, and the cooling exchange is realized through a heat exchange medium.
In another embodiment, the cold storage device of the coupled cooling exchange subsystem in the embodiment of the invention is a solid packed bed, and integrates a part of heat exchange device functions, and is connected to an ambient air liquefying path under a charging working condition and an ambient air regasification path under a discharging working condition of the LAES subsystem at the same time, at this time, cold storage medium in the solid packed bed can exchange cold energy with ambient air under the charging and discharging working conditions of the LAES subsystem through pipe walls directly. And the other part of heat exchange equipment is a heat exchanger, and the heat exchanger can realize cold energy exchange between the LNG-RG subsystem and the solid packed bed, so that cold energy exchange among the LNG-RG subsystem and the solid packed bed is realized.
In another embodiment, the cold storage device (such as a cryogenic tank) of the coupled cold exchange subsystem in the embodiment of the invention comprises 2 independent heat insulation containers which are respectively used as a hot end and a cold end of the cold storage device, wherein the heat exchange device is a heat exchanger, the hot end of the heat exchanger is connected with the hot end of the cold storage device, and the cold end of the heat exchanger is connected with the cold end of the cold storage device to form the cold exchange system. The heat-insulating container is filled with a liquid heat exchange medium (such as liquid propane) to store and exchange cold energy, and the heat exchanger adopts the same liquid heat exchange medium. When the cold storage device stores cold energy, the heat exchange medium flows into the cold end (the second heat insulation container) of the cold storage device from the hot end (the first heat insulation container) of the cold storage device through the heat exchanger and absorbs cold energy from the heat exchanger in the transferring process, and when the cold storage device releases cold energy, the heat exchange medium flows into the hot end (the first heat insulation container) of the cold storage device from the cold end (the second heat insulation container) of the cold storage device through the heat exchanger and outputs cold energy through the heat exchanger in the transferring process.
In order to facilitate those skilled in the art to quickly understand the different collocation structures of the coupling and cooling subsystem, the present invention discloses a preferred embodiment of 2 coupling systems with different structures for different structures of the coupling and cooling subsystem, where it should be understood that the specific coupling system disclosed in the embodiment of the present invention is only used to quickly understand the different construction structures, and should not limit the practical protection scope of the present invention.
As shown in fig. 1, the embodiment of the invention discloses a coupling system for liquid air energy storage and liquefied natural gas regasification, which comprises an LAES subsystem, an LNG-RG subsystem and a coupling refrigeration subsystem;
the LAES subsystem comprises a heat storage tank HD, an ultra-cold tank UCD, a normal temperature compressor C1, a heat storage charging heat exchanger HXC-H, an air purifier APU, a secondary low temperature compressor unit consisting of 2 low temperature compressors (C2 and C3) which are sequentially connected in series, a charging low temperature pump CCP, an ultra-cold charging heat exchanger HXC-UC, a low temperature expander CE, a liquid-air separator LAS, a liquid air storage tank LAD, a discharging low temperature pump DCP, an ultra-cold discharging heat exchanger HXD-UC, a heat storage discharging heat exchanger HXD-H and an expansion unit (a first expansion machine E1, a second expansion machine E2, a third expansion machine E3 and a fourth expansion machine E4), a return air compressor C-UCA and a return air expansion machine E-UCA. The heat storage tank HD, the heat storage charging heat exchanger HXC-H and the heat storage discharging heat exchanger HXD-H are respectively connected at the hot ends through a first valve V1, the cold ends are respectively connected through a second valve V2, a specific heat exchange loop can be controlled by the first valve V1 and the second valve V2, the super-cooling tank UCD, the super-cooling charging heat exchanger HXC-UC and the super-cooling discharging heat exchanger HXD-UC are respectively connected at the hot ends through a third valve V3, the cold ends are respectively connected through a fourth valve V4, and the specific heat exchange loop can be controlled by the third valve V3 and the fourth valve V4. Wherein, liquid air storage tank LAD is connected through tenth valve V10 between liquid air separator LAS and the discharge cryopump DCP. The heat exchanger HXD2 is arranged between the first expander E1 and the second expander E2, the heat exchanger HXD3 is arranged between the second expander E2 and the third expander E3, the heat exchanger HXD4 is arranged between the third expander E3 and the fourth expander E4, and the heat exchanger HXD2, the heat exchanger HXD2 and the heat exchanger HXD2 acquire environmental heat from environmental heat sources.
An LNG-RG subsystem includes a liquefied natural gas cryopump and a liquefied natural gas regasification line.
The coupled cooling subsystem comprises a shallow cooling tank SCD, a cryogenic tank DCD, a shallow cooling charging heat exchanger HXC-SC, a shallow Leng Fangdian heat exchanger HXD-SC, a first cryogenic charging heat exchanger HXC-DC1, a second cryogenic charging heat exchanger HXC-DC2, a third cryogenic charging heat exchanger HXC-DC3, a fourth cryogenic charging heat exchanger HXC-DC4, a cryogenic discharging heat exchanger HXD-DC, a natural gas cryogenic heat exchanger HXNG-DC and a natural gas shallow Leng Huanre device HXNG-SC.
The shallow-cold charge heat exchanger HXC-SC, the shallow Leng Fangdian heat exchanger HXD-SC, the first cryogenic charge heat exchanger HXC-DC1, the second cryogenic charge heat exchanger HXC-DC2, the third cryogenic charge heat exchanger HXC-DC3, the fourth cryogenic charge heat exchanger HXC-DC4 and the cryogenic discharge heat exchanger in the LAES subsystem are coupled, so that the charging path of the LAES subsystem sequentially comprises a normal temperature compressor C1, a heat accumulating charge heat exchanger HXC-H, an air purifier APU, the shallow-cold charge heat exchanger HXC-SC, the first cryogenic charge heat exchanger HXC-DC1, a first-stage low temperature compressor HXC 2, the second cryogenic charge heat exchanger HXC-DC2, the second-stage low temperature compressor C3, the third cryogenic charge heat exchanger HXC-DC3, a charge low temperature pump CCP, the fourth cryogenic charge heat exchanger HXC-DC4, an ultra-cold charge heat exchanger HXC-UC, a liquid air separator LAS and a liquid air separator LAD; the discharging path of the LAES subsystem sequentially comprises a liquid air storage tank LAD, a discharging cryogenic pump DCP, an ultra-cold discharging heat exchanger HXD-UC, a deep-cold discharging heat exchanger HXD-DC, a shallow Leng Fangdian heat exchanger HXD-SC, a heat accumulating discharging heat exchanger HXD-H, a first expander E1, a second environmental heat exchanger HXD2, a second expander E2, a third environmental heat exchanger HXD3, a third expander E3, a fourth environmental heat exchanger HXD4 and a fourth expander E4.
The natural gas cryogenic heat exchanger HXNG-DC and the natural gas shallow Leng Huanre device HXNG-SC in the coupled cold exchange subsystem are coupled in the LNG-RG subsystem, so that the natural gas cryogenic heat exchanger HXNG-DC and the natural gas shallow Leng Huanre device HXNG-SC are sequentially arranged on the liquefied natural gas regasification pipeline along the liquefied natural gas regasification direction.
The hot ends of the shallow cooling tank SCD, the shallow cooling charging heat exchanger HXC-SC, the shallow Leng Fangdian heat exchanger HXD-SC and the natural gas shallow Leng Huanre device HXNG-SC are respectively connected through a fifth valve V5, the cold ends are respectively connected through a sixth valve V6, and a specific cooling circuit can be controlled by the fifth valve V5 and the sixth valve V6. The hot ends of the cryogenic tank DCD, the first cryogenic charging heat exchanger HXC-DC1, the second cryogenic charging heat exchanger HXC-DC2, the third cryogenic charging heat exchanger HXC-DC3, the fourth cryogenic charging heat exchanger HXC-DC4, the cryogenic discharging heat exchanger HXD-DC and the natural gas cryogenic heat exchanger HXNG-DC are respectively connected through a seventh valve V7, the cold ends are respectively connected through an eighth valve V8, and a specific cold exchange loop can be controlled by the seventh valve V7 and the eighth valve V8.
The super-cold reflux air led out from a gas phase outlet of a liquid-air separator LAS in the LAES subsystem sequentially enters an super-cold charging heat exchanger HXC-UC, a first cryogenic charging heat exchanger HXC-DC1 and a shallow cooling charging heat exchanger HXC-SC, and then returns to an inlet of a normal-temperature compressor C1. A ninth valve V9 is arranged on an ultra-cold reflux air pipeline between the liquid-air separator LAS and the ultra-cold charging heat exchanger HXC-UC, and a path of reflux air led out by the ninth valve V9 sequentially enters the reflux air compressor C-UCA, the first cryogenic charging heat exchanger HXC-DC1 and the reflux air expander E-UCA and returns to an inlet of the ultra-cold reflux air of the ultra-cold charging heat exchanger HXC-UC.
As shown in fig. 2, under the charging condition of the LAES subsystem, the LNG-RG subsystem is operated, a heat exchange loop is formed between the heat storage tank HD and the heat storage charging heat exchanger HXC-H, a cooling loop is formed between the shallow cooling tank SCD, the natural gas shallow Leng Huanre unit HXNG-SC, and the shallow cooling charging heat exchanger HXC-SC, and a cooling loop is formed between the cryogenic tank DCD, the natural gas cryogenic heat exchanger HXNG-DC, the first cryogenic charging heat exchanger HXC-DC1, the second cryogenic charging heat exchanger HXC-DC2, the third cryogenic charging heat exchanger HXC-DC3, and the fourth cryogenic charging heat exchanger HXC-DC 4.
At this time, the ambient AIR AIR sequentially enters a normal temperature compressor C1, a heat storage charging heat exchanger HXC-H, an AIR purifier APU, a shallow cold charging heat exchanger HXC-SC, a first cryogenic charging heat exchanger HXC-DC1, a first stage low temperature compressor C2, a second cryogenic charging heat exchanger HXC-DC2, a second stage low temperature compressor C3, a third cryogenic charging heat exchanger HXC-DC3, a charging low temperature pump CCP, a fourth cryogenic charging heat exchanger HXC-DC4, an ultra-cold charging heat exchanger HXC-UC, a low temperature expander CE, a liquid AIR separator LAS and a liquid AIR storage tank LAD, and the ultra-cold return AIR discharged from the liquid AIR separator LAS sequentially enters the ultra-cold charging heat exchanger HXC-UC, the first cryogenic charging heat exchanger HXC-DC1, the shallow cold charging heat exchanger HXC-SC and the return AIR returned to the inlet of the compressor C1, wherein part of the return AIR discharged from the ultra-cold charging heat exchanger HXC-UC sequentially enters the return AIR compressor C-UCC, the first cryogenic charging heat exchanger HXC-UC, and the ultra-cold return AIR from the ultra-cold charging heat exchanger UCC-UCC.
As shown in fig. 3, under the standing condition of the LAES subsystem, the LNG-RG subsystem operates, a cooling circuit is formed between the shallow cooling tank SCD and the natural gas shallow Leng Huanre device HXNG-SC, and a cooling circuit is formed between the cryogenic tank DCD and the natural gas cryogenic heat exchanger HXNG-DC.
At this time, the cryogenic energy and the shallow cooling energy of the LNG-RG subsystem are respectively output to the cryogenic tank DCD and the shallow cooling tank SCD.
As shown in fig. 4, under the discharging working condition of the LAES subsystem, the LNG-RG subsystem is operated, a heat exchange loop is formed between the heat storage tank HD and the heat storage discharging heat exchanger HXD-H, a cooling loop is formed between the shallow cooling tank SCD, the natural gas shallow Leng Huanre device HXNG-SC and the shallow Leng Fangdian heat exchanger HXD-SC, a cooling loop is formed between the cryogenic tank DCD, the natural gas cryogenic heat exchanger HXNG-DC and the cryogenic discharging heat exchanger HXD-DC, and a cooling loop is formed between the super cooling tank UCD and the super cooling discharging heat exchanger HXD-UC.
At this time, the liquid air in the liquid air storage tank LAD is pressurized by a discharge cryopump DCP, and then sequentially enters an ultra-cold discharge heat exchanger HXD-UC, a deep-cold discharge heat exchanger HXD-DC, a shallow Leng Fangdian heat exchanger HXD-SC, a heat storage discharge heat exchanger HXD-H, a first expander E1, a second environmental heat energy heat exchanger HXD2, a second expander E2, a third environmental heat energy heat exchanger HXD3, a third expander E3, a fourth environmental heat energy heat exchanger HXD4 and a fourth expander E4.
As shown in fig. 5, the embodiment of the invention discloses a coupling system for liquid air energy storage and liquefied natural gas regasification, which comprises an LAES subsystem, an LNG-RG subsystem and a coupling cooling subsystem, wherein the heat exchange equipment of the LAES subsystem has heat storage and heat exchange functions at the same time, and the cold storage equipment in the LAES subsystem and the coupling cooling subsystem has cold storage and cooling functions at the same time, in particular:
the LAES subsystem comprises a normal temperature compressor C1, a heat storage tank HD, an air purifier APU, a first-stage low-temperature compressor C2, a second-stage low-temperature compressor C3, an ultra-cold tank UCD, a low-temperature expander CE, a liquid-air separator LAS, a liquid air storage tank LAD, a discharge low-temperature pump DCP and an expander E.
An LNG-RG subsystem includes a liquefied natural gas regasification line.
The coupled cooling subsystem comprises a shallow cooling tank SCD, a first cryogenic tank DCD1, a second cryogenic tank DCD2, a third cryogenic tank DCD3, a natural gas cryogenic heat exchanger HXNG-DC and a natural gas shallow Leng Huanre device HXNG-SC.
The shallow cooling tank SCD, the first cryogenic tank DCD1, the second cryogenic tank DCD2 and the third cryogenic tank DCD3 in the coupled refrigeration subsystem are coupled in the LAES subsystem, so that a charging path of the LAES subsystem sequentially comprises a normal temperature compressor C1, an eleventh valve V11, a heat storage tank HD, a twelfth valve V12, an air purifier APU, a thirteenth valve V13, a shallow cooling tank SCD, a first cryogenic tank DCD1, a fourteenth valve V14, a first stage low temperature compressor C2, a fifteenth valve V15, a second cryogenic tank DCD2, a sixteenth valve V16, a second stage low temperature compressor C3, a seventeenth valve V17, a third cryogenic tank DCD3, an ultra-cold tank UCD, an eighteenth valve V18, a low temperature expander CE, a liquid air separator LAS 11, a nineteenth valve V19 and a liquid air storage tank LAD, and a discharging path of the LAES subsystem sequentially comprises a liquid air storage tank LAD, a nineteenth valve V19, an ultra-cold tank DCP V18, a seventeenth valve V12, a seventeenth valve V14, a seventeenth valve V3, a third cryogenic tank DCD, a seventeenth valve V12 and a seventeenth valve D. Wherein, the charge path and partial path of the discharge path of the LAES subsystem are multiplexed, but the air flows in opposite directions.
The natural gas cryogenic heat exchanger HXNG-DC and the natural gas shallow Leng Huanre device HXNG-SC in the coupled cold exchange subsystem are coupled in the LNG-RG subsystem, so that the natural gas cryogenic heat exchanger HXNG-DC and the natural gas shallow Leng Huanre device HXNG-SC are sequentially arranged on the liquefied natural gas regasification pipeline along the liquefied natural gas regasification direction.
The hot ends of the shallow cooling tank SCD and the natural gas shallow Leng Huanre device HXNG-SC are respectively connected, the cold ends are respectively connected, the hot ends of the first cryogenic tank DCD1, the second cryogenic tank DCD2, the third cryogenic tank DCD3 and the natural gas cryogenic heat exchanger HXNG-DC are respectively connected through a twenty-second valve V22 and a twenty-third valve V23, the cold ends are respectively connected through a twenty-fourth valve V24 and a twenty-fifth valve V25, and a specific cold exchange loop can be controlled through the twenty-second valve V22, the twenty-third valve V23, the twenty-fourth valve V24 and the twenty-fifth valve V25.
The super-cold reflux air led out from the gas phase outlet of the liquid-air separator in the LAES subsystem sequentially enters a twentieth valve V20, a super-cold tank UCD, a twenty-first valve V21, a natural gas cryogenic heat exchanger HXNG-DC and a natural gas shallow Leng Huanre device HXNG-SC, and then returns to the inlet of the normal-temperature compressor C1. One path of return air is led out from the pipeline of the super-cold return air flowing out of the super-cold tank LAD through a twenty-first valve V21, sequentially enters a return air compressor C-UCA, a natural gas cryogenic heat exchanger HXNG-DC and a return air expander E-UCA, and then returns to the inlet of the super-cold return air of the super-cold tank UCD from a twentieth valve V20.
As shown in fig. 6, during the charging operation of the LAES subsystem, the LNG-RG subsystem is operated, and a cooling loop is formed between the shallow cooling tank SCD and the natural gas shallow Leng Huanre unit HXNG-SC, and a cooling loop is formed between the first cryogenic tank DCD1, the second cryogenic tank DCD2, the third cryogenic tank DCD3, and the natural gas cryogenic heat exchanger HXNG-DC.
At this time, the ambient AIR sequentially enters the normal temperature compressor C1, the heat accumulator HD, the AIR purifier APU, the shallow cooling tank SCD, the first cryogenic tank DCD1, the first stage low temperature compressor C2, the second cryogenic tank DCD2, the second stage low temperature compressor C3, the third cryogenic tank DCD3, the super cooling tank UCD, the low temperature expander CE, the liquid-AIR separator LAS and the liquid AIR storage tank LAD, and the super cooling reflux AIR discharged from the liquid-AIR separator LAS sequentially enters the super cooling tank UCD, the natural gas cryogenic heat exchanger HXNG-DC, the natural gas shallow Leng Huanre device HXNG-SC and the return normal temperature compressor C1 inlet, wherein part of reflux AIR discharged from the super cooling tank UCD sequentially enters the reflux AIR compressor C-UCA, the natural gas cryogenic heat exchanger HXNG-DC, the reflux AIR expander E-UCA and the super cooling reflux AIR inlet returned to the super cooling tank UCD.
As shown in fig. 7, under the standing condition of the LAES subsystem, the LNG-RG subsystem is operated, a cooling circuit is formed between the shallow cooling tank SCD and the natural gas shallow Leng Huanre device HXNG-SC, and a cooling circuit is formed between the first cryogenic tank DCD1, the second cryogenic tank DCD2, the third cryogenic tank DCD3 and the natural gas cryogenic heat exchanger HXNG-DC.
At this time, the cryogenic energy and the shallow cooling energy of the LNG-RG subsystem are respectively output to the first cryogenic tank DCD1, the second cryogenic tank DCD2, the third cryogenic tank DCD3 and the shallow cooling tank SCD.
As shown in fig. 8, during the discharging operation of the LAES subsystem, the LNG-RG subsystem is operated, a cooling circuit is formed between the shallow cooling tank SCD and the natural gas shallow Leng Huanre device HXNG-SC, and a cooling circuit is formed between the first cryogenic tank DCD1, the second cryogenic tank DCD2, the third cryogenic tank DCD3 and the natural gas cryogenic heat exchanger HXNG-DC.
At this time, the liquid air in the liquid air storage tank is pressurized by the discharge cryopump DCP and then sequentially enters the super-cooling tank, the third cryogenic tank DCD3, the second cryogenic tank DCD2, the first cryogenic tank DCD1, the shallow cooling tank SCD, the heat storage tank HD and the expander E.
The LAES subsystem in the coupling system can be matched with the coupling cooling exchanging subsystem to independently operate, the LNG-RG subsystem can also independently operate, and the LAES subsystem can be coupled with the LNG-RG subsystem to operate through the coupling cooling exchanging subsystem under the charging working condition, the standing working condition and the discharging working condition. The cooling system comprises an LNG-RG subsystem, a LAES subsystem, a coupling cooling exchange subsystem and a cooling exchange subsystem, wherein the LNG-RG subsystem is used for storing cold energy generated by the LNG-RG subsystem, and the coupling cooling exchange subsystem is used for directly storing the cold energy generated by the LNG-RG subsystem. And when the LNG-RG subsystem is out of operation, the LAES subsystem can be matched with the coupled cooling exchanging subsystem to independently operate, and when the LAES subsystem is out of operation, the LNG-RG subsystem can be matched with the coupled cooling exchanging subsystem to independently operate.
To more clearly illustrate the method of implementation and implementation advantages of the present invention, a thermodynamic model of an embodiment was simulated using ASPEN HYSYS software for the embodiment described in fig. 1 of the present disclosure. The simulation results are shown in table 1 below:
TABLE 1 LAES subsystem Key modeling assumptions and simulation results
From the simulation results, the power consumed by the cryogenic compression process is much smaller than that of normal temperature compression, and the power consumed by the cryogenic pump to further compress the ambient air (134.1K, 4.34 MPa) which has entered the supercritical state is much smaller than that of low temperature compression. The LAES subsystem charge and discharge efficiency in Table 1 is achieved with the assistance of ambient heat sources and without accounting for the possible power generated by the LNG-RG subsystem, and the isentropic efficiency of the key equipment is 85% for the compressor, 90% for the expander and 75% for the cryopump, which are all assumed parameters commonly used in the art.
Further, the embodiment of the invention also discloses a coupling method of liquid air energy storage and liquefied natural gas regasification, which can be applied to the coupling system of any one of the above, and specifically comprises the following steps:
The cryogenic energy generated by the LNG-RG subsystem is output to the coupled cold exchange subsystem under any working condition of the LAES subsystem, and is stored in a cryogenic tank to realize the regasification of liquefied natural gas;
in the charging working condition of the LAES subsystem, the ambient air is output to a heat storage tank for storage through compression heat energy generated by normal-temperature compression, and then the ambient air entering and exiting each low-temperature compressor is cooled to a cryogenic temperature through a coupling cooling subsystem, so that the liquefaction of the ambient air is realized;
and under the discharge working condition of the LAES subsystem, the cryogenic energy generated by the LAES subsystem is output and coupled with the cold exchange subsystem, and is stored in a cryogenic tank to realize the regasification of liquid air.
In some embodiments, the coupling method may further comprise:
outputting shallow cold energy generated by the LNG-RG subsystem to a shallow cold tank of the coupled cold exchange subsystem for storage under any working condition of the LAES subsystem;
in the discharging working condition of the LAES subsystem, the shallow cold energy output generated by the LAES subsystem is coupled with the cold exchange subsystem and is stored in a shallow cold tank;
In the charging working condition of the LAES subsystem, firstly, the shallow cold energy in the shallow cold tank is utilized to cool the ambient air to the shallow cold temperature, and then the deep cold energy in the deep cold tank is utilized to cool the ambient air entering and exiting each low-temperature compressor to the deep cold temperature;
And under any working condition of the coupling system, outputting the superfluous shallow cooling energy in the shallow cooling tank to the external application of the coupling system.
In some embodiments, the coupling method may further comprise:
Outputting the super-cooling energy generated by the LAES subsystem to a super-cooling tank for storage under the discharge working condition of the LAES subsystem;
And under the charging working condition of the LAES subsystem, the super-cold energy in the super-cold tank is utilized to cool the ambient air which is discharged from the multi-stage low-temperature compressor and is cooled to the cryogenic temperature by the coupled cooling-exchanging subsystem to the super-cold temperature, wherein the super-cold temperature is the pressurized outlet temperature in the regasification process of the liquid air.
In some embodiments, the coupling method may further comprise:
When the LAES subsystem is in a charging working condition, the ambient air with the temperature reaching the super-cooling temperature sequentially enters a low-temperature expander and a liquid-air separator to generate liquid air and super-cooling reflux air;
wherein, the super-cold return air is recycled by the super-cold tank to be converted into the return air with the cryogenic temperature;
the reflux air with partial cryogenic temperature sequentially enters a reflux air compressor to be compressed and heated, the cryogenic energy in a cryogenic tank of the coupled cooling-exchanging subsystem is cooled to cryogenic temperature, and the reflux air enters a reflux air expander to be expanded and cooled and then is converged into the super-cooled reflux air output by the liquid-air separation tank.
In some embodiments, the coupling method may further comprise:
In the charging working condition of the LAES subsystem, after the compression heat energy is output to the heat storage tank, the ambient air is led into the air purifier to carry out adsorption treatment of carbon dioxide and water, and then the ambient air entering and exiting each low-temperature compressor is cooled to a cryogenic temperature by utilizing the coupling cooling subsystem;
At least part of regasified air discharged through the expander is led into an air purifier for desorption treatment of carbon dioxide and water under the discharge working condition of the LAES subsystem.
It will be appreciated by those skilled in the art that embodiments of the coupling method of embodiments of the present invention may be combined with each other.
In some embodiments, the invention also discloses a coupling method of LAES and LNG-RG, so as to solve the technical problems in the prior art.
In some illustrative embodiments, the coupling method of LAES and LNG-RG comprises the steps of converting ambient air into liquid air for storage under a charging condition, wherein the process comprises the steps of compressing the ambient air at normal temperature, recovering compression heat energy generated by compression, reducing the temperature of the ambient air after normal-temperature compression to the ambient temperature, and carrying out multi-stage low-temperature compression to obtain the ambient air with target pressure, wherein the ambient air before and after each stage of low-temperature compression is cooled to a cryogenic temperature by using cryogenic energy in a cryogenic tank, wherein the cryogenic energy in the cryogenic tank is from a liquefied natural gas regasification process and a liquid air regasification process, the cold end temperature of the cryogenic tank is the cryogenic temperature, the cryogenic temperature is the pressurized outlet temperature in the liquefied natural gas regasification process, the hot end temperature of the cryogenic tank is the shallow cooling temperature, and the shallow cooling temperature is the ambient air outlet temperature after the ambient air is subjected to low-temperature compression.
In some alternative embodiments, the liquefaction phase transition temperature of the ambient air under the target pressure is higher than the cryogenic temperature, the process of cooling the ambient air before and after each stage of low-temperature compression to the cryogenic temperature by utilizing the cryogenic energy in the cryogenic tank comprises the steps of cooling the ambient air after the last stage of low-temperature compression to the cryogenic temperature to obtain the liquid air under the target pressure, converting the ambient air into the liquid air for storage under the charging condition, and further comprises the steps of compressing the liquid air under the target pressure to a higher pressure and then performing low-temperature expansion.
In some alternative embodiments, the process of converting ambient air to liquid air for storage during charging conditions further comprises cooling the ambient air to a shallow cooling temperature using shallow cooling energy in the shallow cooling tank prior to cooling the ambient air to the cryogenic temperature using cryogenic energy in the cryogenic tank, wherein the shallow cooling energy in the shallow cooling tank is from a liquefied natural gas regasification process and a liquid air regasification process.
In some alternative embodiments, the coupling method further comprises the step of converting the liquid air into the regasified air for heating expansion under the discharging condition, wherein the step of recovering the super-cold energy in the regasified air in the regasification process of the liquid air by using the super-cold tank, the step of converting the ambient air into the liquid air for storage under the charging condition, and the step of cooling the ambient air with the target pressure from the cryogenic temperature to the super-cold temperature, wherein the cold end temperature of the super-cold tank is the super-cold temperature, the hot end temperature of the super-cold tank is the super-cold temperature, and the super-cold temperature is the pressurized outlet temperature in the regasification process of the liquid air.
In some alternative embodiments, the process of converting the ambient air into liquid air for storage under the charging working condition further comprises the steps of carrying out low-temperature expansion on the ambient air with super-cooling temperature to generate liquid air and super-cooling reflux air, separating and discharging the super-cooling reflux air, recovering super-cooling energy in the super-cooling reflux air through a super-cooling tank to convert the super-cooling energy into reflux air with cryogenic temperature, compressing at least part of the reflux air with cryogenic temperature, cooling part of the reflux air after compression and heating to cryogenic temperature by utilizing the cryogenic energy in the super-cooling tank, then carrying out low-temperature expansion on the reflux air, and then collecting the part of the reflux air after expansion and cooling into the separated and discharged super-cooling reflux air again.
In some alternative embodiments, the process of converting the ambient air into liquid air for storage under the charging working condition further comprises the steps of adsorbing carbon dioxide and water in the ambient air which is compressed at normal temperature and recovered by heat energy through an air purifier before the multi-stage low-temperature treatment, and the process of converting the ambient air into liquid air for storage under the charging working condition further comprises the step of introducing at least part of the re-gasified air after expansion work into the air purifier for desorption treatment of the carbon dioxide and the water.
As shown in fig. 9, fig. 9 shows steps of a flow of a charging condition and a discharging condition of a LAES subsystem of a coupling system in an embodiment of the present invention, including:
s1, compressing ambient Air at normal temperature to obtain first ambient Air1;
Step S2, after the compression heat energy in the first ambient Air1 is output to the heat storage tank HD, the temperature of the first ambient Air1 is reduced, and a second ambient Air2 is obtained;
s3, outputting shallow cooling energy in the shallow cooling tank SCD to the second ambient Air2, and reducing the temperature of the second ambient Air2 to the shallow cooling temperature to obtain third ambient Air3;
Wherein, the shallow cold energy in the shallow cold tank SCD can come from the regasified natural gas of the LNG-RG subsystem and the regasified air of the LAES subsystem under the discharging working condition;
S4, performing multistage low-temperature compression on the third ambient Air3 to gradually compress the third ambient Air3 to a target pressure to obtain fourth ambient Air4;
Before each stage of low-temperature compression, outputting the cryogenic energy in the cryogenic tank DCD to the third ambient Air3, reducing the temperature of the third ambient Air3 to the cryogenic temperature, and then implementing the low-temperature compression of each stage of the third ambient Air3 with the cryogenic temperature until the multistage low-temperature compression is completed, and cooling the third ambient Air3 to the cryogenic temperature through the cryogenic energy in the cryogenic tank DCD, thereby obtaining fourth ambient Air4 with the cryogenic temperature;
wherein, the cryogenic energy in the cryogenic tank DCD can be from the regasified natural gas of the LNG-RG subsystem and the regasified air of the LAES subsystem under the discharging condition;
Besides the cryogenic energy of the cryogenic tank DCD, the cryogenic energy generated in real time by the LNG-RG subsystem can be directly utilized.
S5, outputting the super-cooling energy in the UCD to the fourth ambient Air4, and reducing the temperature of the fourth ambient Air4 to the super-cooling temperature to obtain the fifth ambient Air5 with the super-cooling temperature, wherein the super-cooling temperature is the pressure outlet temperature in the regasification process of the liquid Air;
Step S6, carrying out adiabatic expansion on the fifth ambient Air5, obtaining a sixth ambient Air6 mixed with gas and liquid in a liquid-Air separator LAS, and storing liquid Air in the sixth ambient Air6 into a liquid Air storage tank LAD;
The super-cold return air obtained in the liquid-air separator LAS can be used for completing super-cold energy, deep cold energy and shallow cold energy recovery of the super-cold return air and super-cold energy regeneration by referring to the embodiment.
Optionally, between steps S2 and S3, the purification treatment of carbon dioxide and water in the second ambient Air2 may be further completed by the Air purifier APU, so as to obtain the second ambient Air2 without carbon dioxide and water.
The liquefaction and storage of the ambient air under the charging condition of the LAES subsystem are completed.
Step S7, releasing liquid Air from a liquid Air storage tank LAD, and pressurizing by a discharge cryopump DCP to obtain seventh ambient Air7 with mixed gas and liquid;
S8, recycling super-cooling energy in the regasified Air in the gas-liquid mixed Air6 through a super-cooling tank UCD, and raising the temperature of the regasified Air to the cryogenic temperature to obtain eighth ambient Air8;
s9, recycling the cryogenic energy in the seventh ambient Air7 through a cryogenic tank DCD, and raising the temperature of the seventh ambient Air7 to the shallow cooling temperature to obtain ninth ambient Air9;
S10, recovering shallow cold energy in ninth ambient Air9 through a shallow cold tank SCD, and raising the temperature of the ninth ambient Air9 to the ambient temperature to obtain tenth ambient Air10;
Step S11, outputting compression heat energy in the heat storage tank HD to the decade-environment Air10 to obtain eleventh environment Air11 with temperature rising expansion, and performing expansion work by using the eleventh environment Air 11;
the compressed heat energy and the environmental heat energy can be output to the tenth environmental Air10 together for further heating expansion.
The regasification and expansion work of the liquid air under the discharging working condition of the LAES subsystem is completed.
And the LNG-RG subsystem can output cold energy to the shallow cooling tank and the deep cooling tank under the charging working condition, the discharging working condition and the standing working condition of the LAES subsystem, and the working condition state of the LAES subsystem is not required to be considered, so that the coupling adaptability of the LNG-RG subsystem and the LAES subsystem can be improved.
The super-cooling temperature, the cryogenic temperature, the shallow cooling temperature and the environmental temperature in the embodiment of the invention are mainly used for distinguishing temperature changes in different areas and different states, and basically, the super-cooling temperature is lower than the cryogenic temperature, the cryogenic temperature is lower than the shallow cooling temperature and the shallow cooling temperature is lower than the environmental temperature.
Illustratively, the super-cooling temperature in the embodiments of the present invention may be in a temperature range between-192 ℃ and-162 ℃, the sub-cooling temperature may be in a temperature range between-162 ℃ and-100 ℃, the sub-cooling temperature may be in a temperature range between-100 ℃ and-30 ℃, and the ambient temperature may be in a temperature range between-30 ℃ and 40 ℃. In some embodiments of the present invention, the temperature of the ambient air flowing out of the compressor may be higher than-30 ℃ by increasing the compression ratio of the compressor during the LAES subsystem charging condition, and in some embodiments of the present invention, the temperature of the ambient air flowing out of the different compressors may be slightly different, which are all embodiments that would be available to one of ordinary skill in the art without inventive effort and are within the scope of the present invention.
In summary, the advantages of the coupling system and the coupling method in the embodiment of the invention include:
1. And a coupling cooling exchange subsystem is established between the LAES subsystem and the LNG-RG subsystem to uniformly manage deep cooling energy and shallow cooling energy, so that the following combined functions are realized:
1.1, inputting deep cooling energy and shallow cooling energy generated under various working conditions in an LNG-RG subsystem and an LAES subsystem into a cold accumulation tank of a coupled cold exchange subsystem, solving the intermittent problem of the cooling energy output of the LNG-RG, and ensuring the centralized storage of the deep cooling energy and the shallow cooling energy;
1.2, realizing centralized output of cryogenic energy, and using LNG-RG cryogenic energy to the greatest extent to manufacture liquid air;
1.3, realizing the centralized output of the shallow cold energy, and externally applying the superfluous shallow cold energy of the output subsystem;
1.4, through the redundant cold energy reserve (for example, after the LAES subsystem discharges) and the heat energy reserve (for example, after the LAES subsystem charges) in the coupled cooling subsystem, the coupled operation of the LNG-RG subsystem and the LAES subsystem under different working conditions can be met in the redundant capacity range, and the independent operation of the LNG-RG subsystem and the LAES subsystem is also supported, so that the coupled adaptability between the LNG-RG subsystem and the LAES subsystem is improved;
And 1.5, the ambient air is compressed by the cryogenic energy which is stored in the coupling cooling subsystem and is mainly provided at the lowest temperature by the cold energy output by the LNG-RG subsystem, the cryogenic energy of the liquefied natural gas regasification of the LNG-RG is fully utilized, the power consumption of a compressor is reduced, and the charge and discharge efficiency of the coupling system is improved.
2. Through the dual-temperature compression mode of normal-temperature compression and multi-stage low-temperature compression, the ambient air is compressed to a certain pressure before the multi-stage low-temperature compression, and then the ambient air cooled to the cryogenic temperature enters the low-temperature compressor, and the advantages of the dual-temperature compression mode include:
2.1, primary normal temperature, namely, firstly compressing at normal temperature to generate compression heat and provide the compression heat for a discharge working condition, wherein the ambient air with a certain compressed ambient temperature is convenient for air purification, dehydration and decarbonization, and the air purification treatment is carried out on the ambient air after the compression heat energy is recovered, so that the carbon dioxide and water in the ambient air are prevented from liquefying or icing in the subsequent process, and partial equipment and pipelines are prevented from being damaged;
2.2, multistage deep cooling, namely after primary compression, the main compression process is completed through multistage low-temperature compression at the deep cooling temperature which is the lowest temperature which can be output by LNG-RG, so that the overall compression power consumption is reduced conveniently.
3. The low-temperature energy storage device can utilize low-cost and even free environmental heat energy to the greatest extent under the discharge working condition of the LAES subsystem, improves the charge and discharge efficiency of the coupling system, and reduces the system cost, wherein the shallow cold energy stored by the coupling cold exchange subsystem can be completely output to external applications, and the normal operation of the coupling system is not affected.
It should be noted that the above embodiments are merely for illustrating the technical solution of the present invention and not for limiting the same, and although the present invention has been described in detail with reference to the above embodiments, it should be understood by those skilled in the art that the technical solution described in the above embodiments may be modified or some or all of the technical features may be equivalently replaced, and these modifications or substitutions do not make the essence of the corresponding technical solution deviate from the scope of the technical solution of the embodiments of the present invention.