WO2018008997A1

WO2018008997A1 - System using cold energy

Info

Publication number: WO2018008997A1
Application number: PCT/KR2017/007226
Authority: WO
Inventors: 명섭 리마이클
Original assignee: 주식회사 싸이트로닉
Priority date: 2016-07-06
Filing date: 2017-07-06
Publication date: 2018-01-11

Abstract

According to embodiments of the present invention, a system using cold energy comprises: a fuel storage tank for storing a liquefied fuel; a reformer for extracting a reformed gas from boiled-off gas (BOG) naturally generated from the liquefied fuel stored in the fuel storage tank; a hydrogen liquefaction device for generating liquefied hydrogen by liquefying the hydrogen gas transferred from the reformer; a heat exchanger for transferring, to a refrigerant, cold energy contained in the liquefied fuel transferred from the fuel storage tank and the liquefied hydrogen transferred from the hydrogen liquefaction device; one or more superconducting devices; and a refrigerant line for supplying the refrigerant from the heat exchanger to the hydrogen liquefaction device or to the one or more superconducting devices, wherein the hydrogen liquefaction device or the one or more superconducting devices maintain the superconductive state by means of the cold energy contained in the refrigerant and are operated in the superconductive state.

Description

Cold heat system

Embodiments according to the concept of the present invention relates to a system using cold heat, and more particularly to a cold heat utilization system that efficiently utilizes the cold heat contained in the cryogenic liquefied fuel.

Superconductivity is a phenomenon in which a material has an electrical resistance of zero and pushes back an internal magnetic field. Superconductor is a material that exhibits this superconductivity.

In general, in the case of a superconducting system using a superconducting device including a superconductor, separate cooling facilities are required to cool the temperature of the superconductor below a critical temperature. However, these separate cooling facilities occupy a lot of space, there is a problem that the operation, maintenance, management of the cooling system is difficult.

There is a technology to replace the cooling facilities by supplying LNG from the LNG storage tank to the refrigerant of the refrigerant circulating in the superconducting device, but since the LNG is used only as the refrigerant of the refrigerant, its utilization is low in a system using various energy sources. However, there is a problem of low energy efficiency.

An object of the present invention is to provide a cold heat utilization system that efficiently utilizes cold heat contained in liquefied fuel.

The system for using cold heat according to embodiments of the present invention includes a fuel storage tank for storing liquefied fuel, a reformer for extracting reformed gas from BOG generated from liquefied fuel stored in the fuel storage tank, and the reformed gas delivered from the reformer. A reformed gas liquefaction apparatus for producing liquefied reformed gas by liquefaction, a heat exchanger for transferring cool heat contained in the liquefied fuel delivered from the fuel storage tank and the liquefied reformed gas delivered from the reformed gas liquefaction apparatus to a refrigerant, or one Two or more superconducting devices and a refrigerant line for supplying the refrigerant from the heat exchanger to the reforming gas liquefaction device or the one or more superconducting devices, wherein the reforming gas liquefaction device or the one or more superconducting devices comprises The refrigerant delivered from the heat exchanger To, and operates in a superconducting state.

The system for using cold heat according to embodiments of the present invention includes a fuel storage tank for storing liquefied fuel, a reformer for extracting reformed gas from BOG generated from liquefied fuel stored in the fuel storage tank, and the reformed gas delivered from the reformer. A reformed gas liquefaction apparatus for producing liquefied reformed gas by liquefaction, a heat exchanger for transferring cold heat contained in the liquefied fuel delivered from the fuel storage tank and the liquefied reformed gas delivered from the reformed gas liquefaction apparatus to a refrigerant, the heat exchanger An engine that generates mechanical energy using gaseous fuel delivered from a gas, a superconducting generator that maintains a superconducting state by using cooling heat included in the refrigerant, and a superconducting generator that converts mechanical energy delivered from the engine into electrical energy and the refrigerant Maintain superconductivity by using cold heat contained in And, a superconducting power apparatus comprising a reformed gas liquefaction apparatus, and the consumption of the electric energy to maintain a superconducting state by using the cold heat contained in the refrigerant, operate in the superconducting state.

The cold heat utilization system according to the embodiments of the present invention includes a fuel storage tank for storing liquefied fuel, a BOG storage tank for storing BOG generated from liquefied fuel stored in the fuel storage tank, and the BOG transferred from the BOG storage tank. A liquefaction apparatus for liquefying and delivering a liquefied BOG to the fuel storage tank, a reformer for extracting reformed gas from the BOG delivered from the BOG storage tank, and a liquefied reformed gas by liquefying the reformed gas delivered from the reformer. A reforming gas liquefaction apparatus to be produced, a heat exchanger for transferring cold heat contained in the liquefied fuel delivered from the fuel storage tank and the liquefied reformed gas delivered from the reformed gas liquefaction apparatus to a refrigerant, one or more superconducting devices, and The fuel liquefaction device, the reformed gas liquefaction device from the heat exchanger Or a coolant line for supplying the coolant to the one or more superconducting devices, wherein the fuel liquefaction device, the reforming gas liquefaction device or the one or more superconducting devices utilize superconductivity using cold heat contained in the coolant. Maintain state and operate in the superconducting state.

The cold heat utilization system according to the embodiments of the present invention has the effect of utilizing the cold heat contained in the liquefied fuel in various ways.

The cold heat utilization system according to the embodiments of the present invention can build the cryogenic environment of devices that require cryogenic environment, such as a liquefied device or a superconducting device, to cool the heat contained in the liquefied fuel (or liquefied reformed gas), thereby efficiently saving energy. Can be used.

The system for using a cold heat according to embodiments of the present invention maintains the superconducting state of a superconducting generator using the cold heat contained in the liquefied fuel stored in a fuel storage tank and simultaneously converts the mechanical energy generated from the engine using the liquefied fuel into the superconducting generator. It can be converted into electrical energy by using, it is possible to use energy efficiently.

1 conceptually illustrates an energy conversion system according to embodiments of the present invention.

2 is a diagram illustrating an example in which a portion of a fuel delivery line surrounds an energy conversion device in a coil form according to embodiments of the present disclosure.

3 conceptually illustrates an energy conversion system according to embodiments of the present invention.

4 is a flowchart illustrating a numerical analysis for the diagnosis / control function of the energy conversion system and the monitoring / measuring method according to the embodiments of the present invention.

FIG. 5 is a flowchart illustrating a method for synchronizing transmission time of a signal related to measurement of an energy conversion system according to embodiments of the present disclosure.

6 conceptually illustrates a hybrid system including an energy conversion system according to embodiments of the present invention and utilizing cold heat of a liquefied fuel.

7 conceptually illustrates a cold heat utilization system according to embodiments of the present invention.

Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings.

1 conceptually illustrates an energy conversion system according to embodiments of the present invention. Referring to FIG. 1, an energy conversion system 100 according to embodiments of the present invention may include a fuel storage tank (or a fuel storage device 110), an energy conversion device 120, a fuel delivery line 130, and a condition control device. 140 may be included.

The fuel storage tank 110 stores liquefied fuel. Liquefied fuel stored in the fuel storage tank 110 may be supplied to a driving device or a fuel cell. The driving device may be an engine or an internal combustion engine, but is not limited thereto. Although one fuel storage tank 110 is shown in FIG. 1, the fuel storage tank 110 may be one or more.

Liquefied fuel stored in fuel storage tank 110 may be in a low temperature (eg, below zero) or high pressure state. For example, the liquefied fuel may include at least one of liquefied petroleum gas (LPG), liquefied natural gas (LNG), and liquefied hydrogen (liquefied hydrogen). The LPG, the LNG, and the liquefied hydrogen are gas phases at 25 ° C. and 1 atmosphere (eg, standard state), so that the LPG, the LNG, and the liquefied hydrogen are brought into the liquid phase. In order to maintain, the fuel storage tank 110 should be in a low temperature or high pressure state.

Liquefied fuel stored in the fuel storage tank 110 may be replaced by electrical energy (or electric power) or mechanical energy (or power) before being transferred from the fuel storage tank 110 to the energy conversion device 120. The fuel storage tank 110 may transfer the converted electrical energy or mechanical energy to the energy conversion device 120.

The energy conversion device 120 may convert the electrical energy transferred from the fuel storage tank 110 into mechanical energy (for example, by using a motor) or convert the transmitted mechanical energy into electrical energy ( For example, using a generator).

The energy conversion device 120 may exhibit an optimal conversion efficiency in a specific low temperature section. According to embodiments, the energy conversion device 120 may provide an optimal energy conversion efficiency in the cryogenic section. For example, the energy conversion device 120 may be implemented as a superconductor motor or a superconducting generator having an optimal conversion efficiency in the specific cryogenic section.

In the present specification, the ultra low temperature means a temperature at which superconductivity can be exhibited (or observed). For example, the ultra low temperature may mean a temperature of 40 degrees or less of the absolute temperature, but is not limited thereto.

The fuel delivery line 130 may be a passage or a device for delivering liquefied fuel stored in the fuel storage tank 110 to a driving device or a fuel cell.

According to embodiments, the fuel delivery line 130, using the heat generated in the energy conversion device 120, vaporizes the liquefied fuel supplied from the fuel storage tank 110, the vaporized fuel is the drive unit or the fuel Can be delivered to the battery.

According to embodiments, some of the fuel delivery line 130 may surround the exterior of the energy conversion device 120. For example, as shown in FIG. 2, some of the fuel delivery lines 130 may have a pipe structure surrounding the energy conversion device 120 in the form of a coil. In this case, the fuel delivery line 130 may also wrap the power line, thereby minimizing power loss while using the heat exchanger.

According to embodiments, at least some of the fuel delivery line 130 may be implemented to surround all external volumes of the energy conversion device 120.

When the temperature of the energy conversion device 120 is lowered as a part of the energy conversion device 120 and the fuel delivery line 130 exchanges heat, the condition control device 140 has a temperature of ( The fuel delivery line 130 may be controlled to be set to a reference temperature section.

According to embodiments, the condition control device 140 may include a temperature sensor that can measure the temperature of the energy conversion device 120. The condition controller 140 may monitor the temperature of the energy conversion device 120 using a temperature sensor, and detect whether the temperature of the energy conversion device 120 is out of the reference temperature range according to the result of the monitoring. have.

The energy conversion system 100 illustrated in FIG. 1 may be included in a vessel, a vehicle, a rocket, or a generator, but is not limited thereto.

The energy conversion system 100 may operate to prevent accidents related to liquefied fuel stored in the fuel storage tank 110.

The energy conversion system 100 may provide cool heat energy (or cold heat) related to liquefied fuel stored in the fuel storage tank 110 to a superconducting motor, generator, power cable, secondary cell, or fuel cell through a refrigerant. Can be. For example, the refrigerant may be inert gases. Thus, the superconducting motor, the generator, the power cable, the secondary cell, or the fuel cell can operate under optimal conditions (eg, conditions that can lead to superconducting conditions) and thus can provide optimum efficiency. .

The energy conversion system 100 may further include a gas analyzer capable of monitoring inert gas or air. According to embodiments, the gas analyzer may have an input terminal (between the fuel storage tank 110 and the energy conversion device 120) or an output terminal (between the fuel delivery line 130 and the drive unit, or the fuel delivery line) of inert gas or air. 130) and the fuel cell).

For example, the gas analyzer may be an analyzer using absorption spectrometry, combustion analysis, chemical analysis, and / or instrumental analysis. For example, the gas analyzer may be a spectrometer or a gas absorption technique based analyzer.

Thus, the energy conversion system 100 can monitor inert gas or air and use the monitor results to prevent possible explosions.

The energy conversion system 100 may measure the structure including the energy conversion system 100 or the energy conversion system 100 using an electrical measuring technique or an optical measuring technique. For example, the energy conversion system 100 may be included in a ship, a car, a rocket, or a generator that generates power in response to external force (eg, a wind generator, a tidal current generator, a hydroelectric generator, or an ocean current generator). It may mean a ship, the vehicle, the rocket, or the generator.

According to embodiments, the energy conversion system 100 may measure the external force acting on the structure or the response of the structure to the external force by using an electrical measurement technology or an optical measurement (or light measurement) technology. have. For example, the external force may be wind load, wave load, or current load, and the response of the structure to the external force may be displacement, deformation, or movement. motion or vortex.

According to embodiments, the energy conversion system 100 may measure the internal force acting on the structure or the response of the structure to the internal force by using an electrical measurement technique or an optical measurement technique. For example, the load capacity may be included in the energy conversion system 100 (eg, fuel storage tank 110 or 320, energy conversion device 120 or 330,

fuel delivery line

130 or 140, or condition control device 140). Or 350) a sloshing load, a flow load, a pressure load, or a thermal load, wherein the response of the structure to the load is dependent on displacement, It may be deformation, movement, walking, buckling or vortex.

For example, the energy conversion system 100 may include a rider, particle tracking velocimetry, particle image velocimetry, strain sensor, accelerometer, ammeter, acoustic Acoustic emission tester, seismometer, current meter, thermal sensor or optical time domain reflectometer (OTDR), distinctive temperature sensor (DTS), BOTRA It can be measured using a brillouin optical time domain reflectometry analyzer (BOTDR), a brillouin optical time domain reflectometry (BOTDR), a distributed acoustic sensor (DAS), or a distributed vibration sensor (DVS).

The energy conversion system 100 may perform a diagnostic function or a prognostic function through a result of measurement or condition based maintenance.

According to embodiments, the energy conversion system 100 may have a control function including predictive control (temperature and gas or fluid dynamics and pressure, instrumentation, diagnostics and control) or self control, or EC (emergency control) or ESD (emergency) safety features including shut down).

According to embodiments, the energy conversion system 100 may monitor the condition or position of the operator of the offshore structure through a heart beat or behavior sensor or a position sensor, depending on the results of the monitor An alarm or alarm can be generated when the worker is in a dangerous state.

According to embodiments, the energy conversion system 100 may provide a maintenance function through state-based maintenance.

When the structure to be measured is a conductor or when the energy conversion system 100 performs measurement in an electromagnetic field, the energy conversion system 100 performs experiments (or observations) using optical measurement (for example, optical wired measurement or optical wireless measurement). Error range of the measurement result or the empirical data can be minimized. According to embodiments, the energy conversion system 100 may process (or process) the measurement result or the proof data by using context awareness technology to minimize an error range of the measurement result or the proof data. have.

Therefore, the energy conversion system 100 can eliminate the uncertainty of the measurement and can improve the accuracy or repeatability of the measurement.

According to embodiments, an error range of the measurement result or the empirical data may be minimized by using artificial intelligence or machine learning. Thus, the energy conversion system 100 can be (semi) automated.

According to embodiments, the energy conversion system 100 may perform an optical wired measurement function using an optical fiber sensor. According to embodiments, the optical fiber sensor may measure the temperature or tension of the structure to be measured.

The optical fiber sensor may include an optical signal transmission fiber. The optical fiber sensor may include an optical signal transmission fiber including silica, quartz, or polymer, and the optical signal transmission fiber is functional for temperature insulation function or tension reinforcement function. The composite can be a coated or packaged fiber.

3 conceptually illustrates an energy conversion system according to embodiments of the present invention. Referring to FIG. 3, the energy conversion system 300 includes a fuel generating device 310, a fuel storage tank 320, an energy conversion device 330, a fuel delivery line 340, and a condition control device 350. can do. According to embodiments, the energy conversion system 300 of FIG. 3 may be included in a generator that can use water. For example, energy conversion system 300 may be included in a water wind generator, a tidal current generator, an ocean current generator, or a hydroelectric generator.

The energy conversion system 300 of FIG. 3 further includes a fuel generating device 310 for generating hydrogen fuel, which differs from the energy conversion system 100 of FIG. 1 in that hydrogen fuel is used among liquefied fuels. . Each of the energy conversion device 330, the fuel delivery line 340, and the condition control device 350 of FIG. 3 is the energy conversion device 120, the fuel delivery line 130, and the condition control device 140 of FIG. 1. It may be understood that among the respective functions, the functions related to the hydrogen fuel may be performed, and thus, detailed descriptions of these 320, 330, 340, and 350 are omitted.

The fuel generating device 310 generates hydrogen fuel using water available to the energy conversion system 300 (eg, water adjacent to the energy conversion system 300), and generates the generated hydrogen fuel in the fuel storage tank 320. Can be supplied as The fuel storage tank 320 may store the hydrogen fuel delivered from the fuel generating device 310.

4 is a flowchart illustrating a numerical analysis or a monitoring (or measuring) method for a diagnostic function (or control function) of an energy conversion system according to embodiments of the present invention.

1 through 4, an energy conversion system 100 or 300 (hereinafter referred to as 100) may be a gas, using numerical analysis (or numerical modeling) based on multiphysics or similar techniques. The result of dynamic simulation of fluid or thermal dynamics may be set as a boundary condition (S410). For example, the condition may be a condition related to external force or internal force.

The energy conversion system 100 uses a fluid structure interaction (FSI) technique or the like for the above conditions to perform numerical (or numerical) modeling for the diagnostic (or control) function in the experiment (or observation). Optimization (or validation) according to the measurement result or the empirical data by the method, and extracts the optimal (or simple) method (or equation) according to the result of the optimization (S420). For example, the energy conversion system 100 may optimize the numerical analysis method for the diagnostic function (or control function) in a method suitable for the measurement result.

The energy conversion system 100 monitors, measures, or analyzes at least one of gas, fluid, or thermodynamics, position, and shape based on the optimal method extracted in step S420 to control (eg, feed forward or It can be predicted (S430).

Accordingly, the energy conversion system 100 may reduce fuel consumption of the energy conversion system 100 (or a structure including the energy conversion system 100), perform a safe operation, or extend a safe operation time.

According to embodiments, the energy conversion system 100 may perform steps S410 to S430 of FIG. 4 using artificial intelligence or machine learning techniques. The energy conversion system 100 can thus be (semi) automated.

The energy conversion system 100 performs measurement on the structure, and according to the measurement result, the appearance of the structure may be processed by using a pulsed laser (ie, laser scanning) and processed into a 3D image for display. Can be.

FIG. 5 is a flowchart illustrating a method for synchronizing transmission time of a signal related to measurement of an energy conversion system according to embodiments of the present disclosure. 1 to 5, the energy conversion system 100 measures a first time required for the first signal generated by the measuring instrument to be transferred from the measuring instrument to the sensor mounted on the structure (S510). The first signal may be a signal that enables or activates the sensor. For example, the first signal may be a turn-on signal or an operating voltage. The energy conversion system 100 measures a second time required for the second signal generated by the sensor to be transferred from the sensor to the measuring instrument in response to the first signal (S520). The second signal may be a detection signal generated by the sensor. For example, the second signal may include measurement information.

The energy conversion system 100 measures the third time required to quantify the measurement information included in the second signal, and extract the measurement value corresponding to the measurement information according to the result of the quantification. (S530).

The energy conversion system 100 synchronizes the measured first time, the measured second time, or the measured third time with the standard time used in the energy conversion system 100 (S540).

Referring to FIG. 6, renewable power 601 and boiler turbine power 602, such as wind, tidal, wave, geothermal, or solar energy, are transmitted to a turbine (or steam turbine) 603. Turbine 603 may be a generator capable of generating electrical energy. According to embodiments, the turbine 603 may produce electrical energy using the transmitted

powers

601 and 602.

The turbine 603 may receive the cold heat energy of the liquefied fuel through the heat exchange 604 to produce electric energy (or electricity). The produced electrical energy is stored via battery charge 613. In some embodiments, the heat exchanger 604 of FIG. 6 may be the energy conversion device 120 of FIG. 1.

According to embodiments, the turbine 603 may be included in a hybrid vehicle, a ship, a rocket, or the like.

An on-vehicle generator included in a hybrid vehicle is described by way of example. The vehicle generator is connected to the engine of the vehicle through a belt. In this case, the belt is connected to a rotating body (eg, a rotor) of the vehicle generator, and when the engine is driven, the rotating body of the vehicle generator rotates, and thus the vehicle generator produces electric energy. That is, the vehicle generator converts the mechanical energy generated by the engine into electrical energy.

The vehicle generator induces a predetermined AC voltage according to the rotation of the rotating body, rectifies the AC voltage to generate a DC component voltage, and is connected between the output terminal of the generator and the ground and the electrical energy supplied from the generator. A storage battery for accumulating the battery, a warning light having one end connected to an output terminal of the generator, a warning light driving transistor connected between the other end of the warning light and ground, and terminals configured as inputs, and the terminals being short-circuited. In this case, it may include a detection device for controlling to turn on the warning light by turning on the warning light driving transistor. A protection diode may be connected between the terminals, and a load may be connected to an output terminal of the generator.

The vehicle generator has a warning light when one of the terminals is short-circuited, the other terminal that is not short-circuited to continue to generate electricity is supplied to the storage battery or load without interruption.

The heat exchanger 604 heat-exchanges the liquefied fuel stored in the fuel container 605 through the BOG 607 made through the BOG (boiled off gas) Liquification 606 to generate cold heat energy. According to embodiments, the fuel container 605 may be the fuel storage tank 110 of FIG. 1.

The cold heat energy may be delivered to the gas supply system 608. According to embodiments, the gas air raid system 608 may be a fueled gas supply system.

The gas supply system 608 may be the condition control device 104 of FIG. 1.

According to embodiments, the gas supply system 608 may include at least one of a motor for compressor, a pump, and a valve.

The gas supply system 608 may transfer the received cold heat energy to the first engine 609 and the second engine 610.

The first engine 609 may be driven through the cold heat energy, and operate the turbine 603 to produce electricity. In addition, the first engine 609 may store the CO 2 liquefied gas in the CO 2 reservoir 612 according to the CO 2 liquefaction or hydrate process 611. For example, the first engine 609 may be a low pressure engine.

The second engine 610 may be driven according to the received cold heat energy, and may drive a propellant 615 in cooperation with a motor 614 driven by receiving electrical energy from the turbine 603. The propellant 615 may be a propeller or a wheel, but is not limited thereto.

For example, the second engine 610 may be a high pressure engine and may operate in the range of 2 to 3000 RPM.

BOG 607 may be passed to reformer 616. The reformer 616 may extract hydrogen from the BOG 607 and store the extracted hydrogen in a hydrogen reservoir 617. According to embodiments, the hydrogen liquefied fuel generated by the liquefaction process 620 may be stored in the hydrogen reservoir 617. For example, the liquefaction process 620 may use the cold heat energy generated through the heat exchange 604.

The hydrogen liquefied fuel may be supplied to the fuel cell 619.

The hydrogen or oxygen reformer 618 may use the energy (eg, electrical energy) delivered to the motor 614 to extract oxygen or hydrogen and deliver the extracted oxygen or hydrogen to the fuel cell 619.

The hydrogen or oxygen reformer 618 may process the extracted hydrogen in the liquefaction process 620 and store the liquefied hydrogen in the hydrogen reservoir 617.

The hydrogen or oxygen reformer 618 may process the extracted oxygen in a liquefaction process 620 and store the liquefied oxygen in an oxygen storage container.

Although the hybrid system of FIG. 6 is illustrated as including one hydrogen reservoir 617, the hybrid system may include a separate oxygen reservoir in addition to the hydrogen reservoir 617.

7 conceptually illustrates a cold heat utilization system according to embodiments of the present invention. Referring to FIG. 7, a cold heat utilization system 700 includes a fuel storage tank 710, a heat exchanger 720, a reformer 730, a reforming gas liquefaction device 740, a fuel cell 750, and a superconducting device. 760 may include. According to embodiments, the cold heat utilization system 700 may further include a boil off gas (BOG) storage tank 712, a fuel liquefaction apparatus 714, and / or a reformed gas storage tank 732.

The cold heat utilization system 700 of FIG. 7 may correspond to the hybrid system shown in FIG. 6.

The fuel storage tank 710 may correspond to the fuel container 605 of FIG. 6, the heat exchanger 720 may correspond to the heat exchange 604 of FIG. 6, and the reformer 730 may be the reformer 616 of FIG. 6. ), The reformed gas liquefaction apparatus 740 may correspond to the liquefaction process 620 of FIG. 6, the fuel cell 750 may correspond to the fuel cell 619 of FIG. 6, and superconductivity. The apparatus 760 may correspond to the turbine 603, the first engine 609, the second engine 610, or the motor 614 of FIG. 6, but is not limited thereto.

The fuel storage tank 710 may store the liquefied fuel LF. Liquefied fuel LF has a state of very low temperature, and thus has a cold heat energy. The cold heat energy refers to ultra low temperature heat energy contained in a low temperature object.

According to embodiments, the liquefied fuel LF may be any one of LPG, LNG, and liquefied hydrogen, but is not limited thereto. The liquefied fuel LF may include all materials including hydrogen and capable of storing cold heat. . For example, the liquefied fuel (LF) may be a natural chemical or a synthetic chemical including at least one of hydrogen, carbon, and oxygen.

As described above, ultra low temperature means the temperature at which superconductivity can be exhibited (or observed). For example, the ultra low temperature may mean a temperature of 40 degrees or less of the absolute temperature, but is not limited thereto.

The fuel storage tank 710 may further include a control device for maintaining the interior of the fuel storage tank 710 at a low temperature or a high pressure state. For example, fuel storage tank 710 may comprise a temperature sensor or a pressure sensor.

The fuel storage tank 710 may deliver the liquefied fuel LF to the heat exchanger 720. Liquefied fuel LF may be delivered through a fuel line connected between fuel storage tank 710 and heat exchanger 720.

BOG (BG) generated from fuel storage tank 710 may be delivered to reformer 730. BOG BG refers to a gas generated as the liquefied fuel LF stored in the fuel storage tank 710 naturally evaporates. According to embodiments, the BOG (BG) may be a gas generated from the liquefied fuel LF at a standard state (eg, 25 ° C or 1 atmosphere).

According to embodiments, the fuel storage tank 710 may include a relief valve 711. The relief valve 711 automatically opens when the pressure in the fuel storage tank 710 exceeds the reference pressure as the BOG (BG) is generated in the fuel storage tank 710. And to the BOG storage tank 712.

The BOG storage device 712 may store the BOG (BG) delivered from the fuel storage tank 710. BOG storage 712 may deliver BOG (BG) to fuel liquefaction device 714 and / or reformer 730.

The fuel liquefaction apparatus 714 may liquefy the delivered BOG (BG) and deliver the liquefied BOG to the fuel storage tank 710. The liquefied BOG may be the same material as the liquefied fuel LF.

According to embodiments, the fuel liquefaction apparatus 714 liquefies the BOG (BG) and cools the liquefied BOG to the fuel storage tank 710 by using the cold heat included in the cryogenic refrigerant REF delivered from the heat exchanger 720. ) Can be delivered.

The BOG (BG) generated from the fuel storage tank 710 may be stored in the BOG storage device 712.

The heat exchanger 720 may transfer the cool heat included in the liquefied fuel LF delivered from the fuel storage tank 710 and the liquefied reformed gas LRG delivered from the reformed gas liquefaction apparatus 740 to the refrigerant REF. .

The refrigerant REF may be a material capable of transferring thermal energy (eg, cold heat energy). In some embodiments, the refrigerant REF may be a liquefied fuel LF or any one of an inert gas, ammonia, nitrogen, and an antifreeze, but is not limited thereto. Means a material that can maintain.

According to embodiments, the heat exchanger 720 passes the liquefied fuel line (or the liquefied hydrogen line through which the liquefied reforming gas LRG is delivered) to the refrigerant REF, thereby passing the liquefied fuel LF. (Or liquefied reforming gas (LRG)) may be transferred to the coolant (REF).

According to embodiments, the heat exchanger 720 may vaporize the liquefied fuel LF to generate the vaporized fuel GF, and may transmit the cold heat of the liquefied fuel LF to the refrigerant REF by using the generated vaporized heat. have.

The heat exchanger 720 may deliver the refrigerant REF to the devices included in the cold heat utilization system 700. According to embodiments, the heat exchanger 720 may deliver the refrigerant REF to the fuel liquefaction apparatus 714, the reformed gas liquefaction apparatus 740, or the superconductor 760.

According to embodiments, the cold heat utilization system 700 may further include a refrigerant line 722 for delivering the refrigerant REF to each device.

The heat exchanger 720 may deliver the vaporized fuel GF to the engine 770. According to embodiments, a heat exchanger 720 is a vaporizer for heating the liquefied fuel to produce a vaporized fuel, a compressor for compressing the vaporized fuel delivered from the vaporizer to a high pressure or an injector for delivering the compressed vaporized fuel to the engine. It may include.

The reformer 730 may reform the BOG (BG) delivered from the fuel storage tank 710 (or BOG storage tank 712) and extract the reformed gas RG from the BOG (BG) as a result of the reforming. have. According to embodiments, the reformer 730 may extract hydrogen, oxygen, or carbon from BOG (BG).

According to embodiments, the reforming gas RG may include hydrogen, oxygen, carbon, or a combination thereof. For example, the reforming gas RG may be hydrogen gas, oxygen gas, carbon gas, hydrocarbon or hydrocarbon oxide, but is not limited thereto.

The extracted reformed gas RG may be stored in the reformed gas storage tank 732. Although the cold heat utilization system 700 is shown in FIG. 7 as including one reformed gas storage tank 732, in some embodiments, the cold heat utilization system 700 may include a plurality of reformed gas storage tanks. The reformed gas RG may be stored separately according to its properties.

According to embodiments, the reformer 730 may extract the reformed gas (RG) from the BOG (BG) by using the heat energy generated by the operation of the engine 770.

The reformer 730 may deliver the extracted reformed gas RG to the reformed gas liquefaction apparatus 740 and / or the fuel cell 750. According to embodiments, the reformer 730 may deliver the extracted reformed gas RG to the reformed gas storage tank 732.

The reformed gas storage tank 732 may deliver the stored reformed gas RG to the reformed gas liquefaction apparatus 740 and / or the fuel cell 750.

The reformed gas liquefaction apparatus 740 may liquefy the delivered reformed gas (RG), generate liquefied reformed gas (LRG), and deliver the resulting liquefied reformed gas (LRG) to the heat exchanger 720. According to embodiments, the reformed gas liquefaction apparatus 740 may liquefy the reformed gas RG by using the cold heat included in the cryogenic refrigerant REF transferred from the heat exchanger 720.

The fuel cell 750 may generate electrical energy (or electric power PW) using the reformed gas RG delivered from the reformer 730. According to embodiments, the fuel cell 750 may generate electrical energy PW using hydrogen gas or oxygen gas delivered from the reformer 730.

The fuel cell 750 may transfer the generated electrical energy PW to the superconducting device 760.

The superconducting device 760 may be a device including a superconductor. The superconducting device 760 may be a device that operates using a superconducting phenomenon in an ultra low temperature state. According to embodiments, the superconducting device 760 may maintain the superconducting state by using the cold heat included in the refrigerant REF transferred from the heat exchanger 720, and operate in the superconducting state.

The cold heat utilization system 700 may include one superconducting device 760 or two or more superconducting devices 760.

According to embodiments, when including two or more superconducting devices 760, the superconducting devices 760 may include a superconducting generator 761, a superconducting power device 763, and / or a superconducting power storage device 765. Can be.

The superconducting generator 761 may maintain the superconducting state by using the cold heat stored in the refrigerant REF, and generate electric energy (or electric power PW) in the superconducting state. According to embodiments, the superconducting generator 761 may convert the mechanical energy ME transmitted from the engine 770 into the electrical energy PW in the superconducting state.

According to embodiments, the superconducting generator 761 may include a superconducting electromagnet and a superconducting rotor (eg, a coil). The superconducting electromagnet may surround the superconducting coil and generate an electromagnetic field. When the engine 770 rotates, the superconducting coil may rotate in an electromagnetic field generated by the superconducting electromagnet to convert mechanical energy ME into electrical energy PW.

The superconducting power device 763 may maintain the superconducting state by using the cold heat stored in the refrigerant REF, and consume electric energy PW in the superconducting state. According to embodiments, the superconducting power device 763 may consume electrical energy PW delivered from the fuel cell 750.

The superconducting power storage device 765 maintains the superconducting state by using the cold heat stored in the refrigerant REF, and stores the electrical energy PW produced from the superconducting generator 761 in the superconducting state. The superconducting power storage device 765 may deliver the stored electrical energy PW to a device (eg, superconducting power device 763) included in the cold heat utilization system 700.

According to embodiments, the superconducting power storage device 765 converts and stores the electrical energy PW produced from the superconducting generator 761 into magnetic energy, and converts the stored magnetic energy into electrical energy PW to store the superconducting power device. (763).

According to embodiments, the superconducting power storage device 765 may be a flywheel for converting and storing electrical energy PW generated from the superconducting generator 761 into mechanical energy.

According to embodiments, the superconducting devices 760 may further include a superconducting cable 767 for transferring electrical energy (PW) between the

devices

750, 761, 763 or 765. According to embodiments, the superconducting cable 767 may deliver electrical energy PW generated in the superconducting generator 761 or the fuel cell 750 to respective devices of the cold heat utilization system 700.

According to embodiments, the superconducting cable 761 may be surrounded by the refrigerant line 721. For example, superconducting cable 761 may be comprised of a composite cable that transfers electrical energy PW and refrigerant REF between

devices

750, 761, 763 or 765.

Engine 770 may be an internal combustion engine that produces mechanical energy using gaseous fuel GF delivered from heat exchanger 720. According to embodiments, thermal energy generated by the engine 770 may be used by the reformer 730. For example, engine 770 may be a rocket engine or a jet engine.

According to the cold heat utilization system 700, since the cold heat contained in the liquefied fuel LF (or liquefied reforming gas LRG) can be constructed in the cryogenic environment of devices that require an ultra low temperature environment such as a liquefied device or a superconducting device, Energy can be used efficiently.

For example, according to the cold heat utilization system 700, the superconducting devices 760 are maintained in the superconducting state by using the cold heat included in the liquefied fuel LF, and the gaseous hydrogen GH extracted from the liquefied fuel LF is stored. The generated power energy may be supplied to the superconducting devices 760.

Although the present invention has been described with reference to the embodiments illustrated in the drawings, this is merely exemplary, and it will be understood by those skilled in the art that various modifications and equivalent other embodiments are possible. Therefore, the true technical protection scope of the present invention will be defined by the technical spirit of the appended claims.

An embodiment according to the concept of the present invention relates to a cold heat utilization system using cold heat.

Claims

A fuel storage tank for storing liquefied fuel;

A reformer for extracting reformed gas from a boiled off gas (BOG) generated from liquefied fuel stored in the fuel storage tank;

A reforming gas liquefaction apparatus for producing a liquefied reforming gas by liquefying the reformed gas delivered from the reformer;

A heat exchanger for transferring cold heat contained in the liquefied fuel delivered from the fuel storage tank and the liquefied reformed gas delivered from the reformed gas liquefaction apparatus as a refrigerant;

One or more superconducting devices; And

A refrigerant line for supplying said refrigerant from said heat exchanger to said reforming gas liquefaction device or said one or more superconducting devices,

The reformed gas liquefaction apparatus, or the one or more superconducting apparatuses, operates in a superconducting state using the cold heat contained in the refrigerant.
The method of claim 1,

The cold heat utilization system further comprises an engine,

The heat exchanger generates vaporized fuel by vaporizing the liquefied fuel delivered from the fuel storage tank, delivers the vaporized fuel to the engine,

And the engine uses the vaporized fuel to produce mechanical energy.
The method of claim 1,

The cold heat utilization system,

An engine generating mechanical energy; And

Further comprising the two or more superconducting devices,

The two or more superconducting devices include a superconducting generator, a superconducting cable, and a superconducting power device,

The superconducting generator, in the superconducting state, converts the mechanical energy delivered from the engine into electrical energy,

The superconducting cable, in the superconducting state, supplies the electrical energy generated by the superconducting generator to the superconducting power device,

And the superconducting power device consumes the electrical energy in the superconducting state.
The method of claim 1,

The cold heat utilization system,

A drive engine for generating mechanical energy; And

Further comprising the two or more superconducting devices,

The two or more superconducting devices include a superconducting generator, a superconducting storage device, a superconducting cable, and a superconducting power device,

The superconducting generator, in the superconducting state, converts the mechanical energy delivered from the engine into electrical energy,

The superconducting cable, in the superconducting state, supplies the electrical energy generated by the superconducting generator to the superconducting storage device,

The superconducting storage device converts and stores electrical energy produced from the superconducting generator into magnetic energy, converts stored magnetic energy into the electrical energy, and supplies the superconducting power device to the superconducting power device through the superconducting cable.

And the superconducting power device consumes the electrical energy supplied from the superconducting storage device via the superconducting cable.
The method of claim 1,

The cold heat utilization system further includes a drive engine for generating mechanical energy,

And the reformer extracts the reformed gas from the BOG using heat energy generated according to the operation of the engine.
The method of claim 1,

And a fuel cell that generates electrical energy using the reformed gas delivered from the reformer.
The method of claim 1,

And the reforming gas comprises at least one of hydrogen, oxygen, and carbon.
The method of claim 1,

And the coolant is one of the liquefied fuel or an inert gas, ammonia, and nitrogen.
The method of claim 1,

And the refrigerant line has a pipe structure surrounding at least a portion of the heat exchanger, the reforming gas liquefaction device, or the one or more superconducting devices.
The method of claim 1,

The cold heat utilization system is included in a ship, a car, a rocket, or a generator.
A fuel storage tank for storing liquefied fuel;

A reformer for extracting reformed gas from a boiled off gas (BOG) generated from liquefied fuel stored in the fuel storage tank;

A reforming gas liquefaction apparatus for producing a liquefied reforming gas by liquefying the reformed gas delivered from the reformer;

A heat exchanger which transfers the cold heat contained in the liquefied fuel delivered from the fuel storage tank and the liquefied reformed gas delivered from the reformed gas liquefaction apparatus as a refrigerant, and generates a gaseous fuel by vaporizing the liquefied fuel;

An engine that generates mechanical energy using gaseous fuel delivered from the heat exchanger;

A superconducting generator that maintains a superconducting state by using cold heat included in the refrigerant and converts mechanical energy transferred from the engine into electrical energy; And

A superconducting power device that maintains a superconducting state by using cold heat contained in the refrigerant and consumes the electrical energy;

The reformed gas liquefaction apparatus maintains a superconducting state by using cold heat contained in the refrigerant, and operates in the superconducting state.
The method of claim 11,

And a refrigerant line for supplying said refrigerant from said heat exchanger to said reforming gas liquefaction device or said one or more superconducting devices.
The method of claim 11,

And a superconducting cable for maintaining a superconducting state by using the cold heat contained in the refrigerant, and supplying the electric energy generated by the superconducting generator to the superconducting power device.
The method of claim 13,

The superconducting cable is a cold heat utilization system for transferring the refrigerant delivered from the heat exchanger to a superconducting generator and a superconducting power device.
The method of claim 11,

And a superconducting power storage device for storing the electrical energy produced from the superconducting generator and supplying the stored electrical energy to the superconducting power device.
A fuel storage tank for storing liquefied fuel;

A BOG storage tank storing BOG (boiled off gas) generated from liquefied fuel stored in the fuel storage tank;

A fuel liquefaction apparatus for liquefying the BOG delivered from the BOG storage tank and delivering the liquefied BOG to the fuel storage tank;

A reformer for extracting reformed gas from the BOG delivered from the BOG storage tank;

A reforming gas liquefaction apparatus for producing a liquefied reforming gas by liquefying the reformed gas delivered from the reformer;

A heat exchanger for transferring cold heat contained in the liquefied fuel delivered from the fuel storage tank and the liquefied reformed gas delivered from the reformed gas liquefaction apparatus as a refrigerant;

One or more superconducting devices; And

A refrigerant line for supplying said refrigerant from said heat exchanger to said fuel liquefaction device, said reforming gas liquefaction device or said one or more superconducting devices,

And the fuel liquefaction apparatus, the reforming gas liquefaction apparatus, or the one or more superconducting devices maintain a superconducting state using cold heat contained in the refrigerant, and operate in the superconducting state.
The method of claim 16, wherein the cold heat utilization system,

Optical measurement function, diagnostic function through condition-based maintenance, control function including predictive control or self control, safety function including emergency control (EC) or emergency shut down (ESD), monitoring function of worker status, location of the worker A cold heat utilization system that provides a monitoring function of, or maintenance by the condition-based maintenance.
The method of claim 17,

The cold heat utilization system,

A cold heat utilization system that performs a temperature measurement or a tension measurement function using an optical fiber sensor.
The method of claim 18,

The optical fiber sensor is a cold heat utilization system comprising a fiber for optical signal transmission coated or packaged with a functional composite for thermal insulation or tension reinforcement.
The method of claim 17, wherein the cold heat utilization system,

Using numerical modeling based on multiphysics techniques to condition dynamic simulations of gas, fluid, or thermal dynamics,

Extracts an optimal simple equation for the diagnostic function or the control function using the FSI technique for the condition,

Monitor at least one of the gas, the fluid or the thermodynamics based on the extracted simple equation,

And a cold heat utilization system that performs the control function according to the monitoring result.
21. The cold heat utilization system of claim 20, wherein the cold heat utilization system performs the control function using a machine learning technique.
The method of claim 17, wherein the cold heat utilization system,

An optical heat utilization system that measures a structure including the cold heat utilization system using optical measurement technology, processes the measurement result according to the measurement by using situation recognition technology, and minimizes an error range of the measurement result according to the processing result. .
23. The cold heat utilization system of claim 22, wherein the cold heat utilization system minimizes an error range of the measurement result by using a machine learning technique.
The method of claim 16, wherein the cold heat utilization system,

The first time required for the first signal generated by the meter to be transmitted from the meter to the sensor mounted on the structure, and the second signal generated by the sensor in response to the first signal is transmitted from the sensor to the meter. And a second time required for the second time, or a third time required for the second signal to arrive at the measuring device and to be quantified and extracted with the standard time.