Patent Application
20240175546
This application claims priority to Japanese Patent Application No. 2022-187644 filed on Nov. 24, 2022, which is incorporated herein by reference in its entirety including the specification, claims, drawings, and abstract.
The present specification discloses a liquid hydrogen system for storing hydrogen in a liquid state, converting the hydrogen into a gaseous state, and supplying the hydrogen in the gaseous state to a hydrogen engine.
Conventionally, liquid hydrogen systems in which hydrogen to be supplied to a hydrogen engine is stored in a liquid state have been known. For example, Patent Document 1 discloses a system in which liquid hydrogen stored in a hydrogen tank is extracted by a pump and evaporated to obtain a hydrogen gas which is supplied to a hydrogen engine. When hydrogen is stored in the liquid state as described above, a storage quantity of hydrogen can be increased as compared to a case where hydrogen is stored in the gaseous state.
In liquid hydrogen systems, when a quantity of hydrogen consumed by the hydrogen engine increases abruptly, a huge quantity of liquid hydrogen is extracted, as a matter of course, from the hydrogen tank in a short time. Extraction of the huge quantity of liquid hydrogen might cause an excessive decrease in the internal pressure of the hydrogen tank. When the internal pressure of the hydrogen tank is excessively decreased, the pump might fail to discharge the liquid hydrogen.
Conventional techniques, such as a technique of Patent Document 1, have not considered such a decrease in the internal pressure resulting from extraction of liquid hydrogen. As a result, in the conventional techniques there may be cases where hydrogen cannot be supplied to the hydrogen engine appropriately.
Under the circumstances, the present specification discloses a liquid hydrogen system capable of appropriately supplying hydrogen to a hydrogen engine.
A liquid hydrogen system disclosed herein includes a hydrogen tank mounted on a vehicle and configured to store liquid hydrogen, a supply circuit configured to supply a hydrogen engine with a hydrogen gas which is converted from the liquid hydrogen extracted from the hydrogen tank, and a return circuit branched from the supply circuit and connected to the hydrogen tank, the return circuit being configured to return the hydrogen gas into the hydrogen tank in such a manner that an internal pressure of the hydrogen tank matches or exceeds a predetermined reference pressure.
When the return circuit for returning the hydrogen gas is arranged, an excessive decrease in the internal pressure of the hydrogen tank can be prevented. In this way, failure of the pump to discharge liquid hydrogen can be prevented. As a result, hydrogen can be appropriately supplied to the hydrogen engine.
In an aspect of this disclosure, the liquid hydrogen system may further include a controller and a pressure sensor configured to detect the internal pressure of the hydrogen tank as a tank internal pressure. In the liquid hydrogen system, the return circuit may include a return gate valve which is electrically openable and closeable, and the controller may be configured to open the return gate value when the tank internal pressure becomes lower than the reference pressure.
With the above-described configuration, it can be ensured that the internal pressure of the hydrogen tank is maintained at or above the reference pressure.
In another aspect of the disclosure, the return circuit may further include a return pressure reducing value which is disposed on a hydrogen tank side of the return gate valve and is configured to output the hydrogen gas after reducing a pressure thereof.
The above-described configuration can prevent an excessive rise in the internal pressure of the hydrogen tank.
In a further aspect of the disclosure, the supply circuit may include a chamber which is fluid connected to the supply circuit upstream from a branch point of the return circuit, and the chamber is configured to temporarily store the hydrogen gas.
With the configuration described above, a small amount of excess or deficiency of hydrogen gas can be compensated for by the hydrogen gas stored in the chamber. As a result, pressure variations of the hydrogen gas can be suppressed, and a response delay in control of hydrogen supply can be accommodated by the chamber. Further, with the above-described configuration, because a return flow quantity of the hydrogen gas can be ignored without causing any problem in calculation of a supply quantity of hydrogen, control of the hydrogen supply can be simplified.
In another aspect of the disclosure, a booster pump configured to pressurize the liquid hydrogen and discharge the pressurized liquid hydrogen may be installed for extracting the liquid hydrogen from the hydrogen tank.
When the booster pump is used, a pressure resistance required of the hydrogen pump can be decreased to a lower level. It should be noted that the use of the booster pump may increase a possibility that the pump becomes unable to discharge the liquid hydrogen as the tank internal pressure is decreased. However, in the liquid hydrogen system disclosed herein, even when the booster pump is used, occurrence of such a situation where the pump fails to discharge the liquid hydrogen can be prevented.
The liquid hydrogen system disclosed herein can appropriately supply hydrogen to the hydrogen engine.
Embodiments of the present disclosure will be described based on the following figures, wherein:
Hereinafter, a configuration of a liquid hydrogen system 10 will be described with reference to the drawings.
The liquid hydrogen system 10 includes a hydrogen tank 12 in which liquid hydrogen is stored. The liquid hydrogen tank 12 stores the liquid hydrogen in a thermally insulated manner. For the liquid hydrogen tank 12, a double structure vessel may be used, for example. In this case, the hydrogen tank 12 has an inner tank 14, an outer tank 16 which encloses the inner tank 14, and a vacuum heat insulating layer formed between the inner tank 14 and the outer tank 16.
The hydrogen tank 12 is formed in a spherical or barrel shape in order to maintain exertion of a uniform pressure on an interior wall of the hydrogen tank 12. In addition, the bottom of the hydrogen tank 12 has a collector portion 18 which is depressed from the other portion of the bottom around the collector portion 18. A hydrogen pump 26, which will be described below, is placed in the collector portion 18. In this way, even when a quantity of liquid hydrogen remaining in the hydrogen tank 12 becomes small, the hydrogen pump 26 can be submerged in the liquid hydrogen, which allows the liquid hydrogen to be discharged almost completely.
The liquid hydrogen is maintained at low temperature within the hydrogen tank 12. Further, in the hydrogen tank 12, the pressure of the liquid hydrogen is substantially equal to an atmospheric pressure or slightly higher than the atmospheric pressure, and is 1 Mpa or less, for example. Here, the inner tank 14 is thermally insulated by a vacuum. However, because heat input cannot be prevented completely, the liquid hydrogen stored in the inner tank 14 is naturally evaporated over time. A hydrogen gas (i.e., boil off gas) generated by such natural evaporation of the liquid hydrogen is retained in an upper region within the hydrogen tank 12.
The liquid hydrogen is filled from an external unit through a filling circuit 19 into the hydrogen tank 12. The filling circuit 19 includes a filling channel 20 for delivering the liquid hydrogen, and a release channel 22 for directing the hydrogen gas to the outside. Both the filling channel 20 and the release channel 22 extend from a connector 24 to the inside of the hydrogen tank 12. The filling circuit 19 is configured to be connected via the connector 24 to a filling hose (not illustrated in
The hydrogen tank 12 is equipped with the hydrogen pump 26 for discharging the stored liquid hydrogen toward the hydrogen engine 100. In this example, the hydrogen pump 26 is a booster pump which discharges liquid hydrogen while increasing a pressure of the liquid hydrogen. The hydrogen pump 26 may be, for example, a piston pump in which a plunger is reciprocated within a cylinder placed in a liquid, to suck and discharge the liquid. In this case, both a suction port and a discharge port of the cylinder are equipped with a check valve. The hydrogen pump 26 is driven by a pump motor 28. When the hydrogen pump 26 having such a pressure increasing function is installed, a level of the pressure resistance required of the hydrogen tank 12 can be lowered.
Specifically, the hydrogen engine 100 in this example is of the direct injection type and is configured to inject the hydrogen gas directly into the engine cylinder as described above. It is necessary that a directly injected hydrogen gas have a pressure (for example, from 5 Mpa to a few tens of Mpa) that is drastically higher than the atmospheric pressure. To acquire such a high-pressure hydrogen gas, the liquid hydrogen must have a sufficiently high pressure before it is evaporated; i.e., when it is in a liquid state. To achieve this, it may be considered to store liquid hydrogen having a high pressure (such as, a few tens of Mpa, for example) within the hydrogen tank 12. This case, however, requires that the pressure resistance of the hydrogen tank 12 be enhanced, which will increase both cost for the hydrogen tank 12 and the weight thereof.
On the other hand, in this example, the pressure of the liquid hydrogen within the hydrogen tank 12 is maintained substantially equal to or slightly higher than the atmospheric pressure, and in an operation to evaporate the liquid hydrogen, only a required quantity of the liquid hydrogen is discharged after the liquid hydrogen is sufficiently pressurized by the hydrogen pump 26. In this way, a hydrogen gas having a sufficiently high pressure can be acquired while avoiding the necessity for enhancing the pressure resistance of the hydrogen tank 12. Further, when a required level of the pressure resistance of the hydrogen tank 12 is lowered, the costs for manufacturing the hydrogen tank 12 can be decreased, and the weight of the hydrogen tank 12 can be accordingly decreased. Moreover, when the required level of the pressure resistance is lowered, it becomes possible to form the hydrogen tank 12 in a shape other than the spherical shape or the barrel shape, leading to a high degree of flexibility in design of the shape of the hydrogen tank 12.
The liquid hydrogen discharged from the hydrogen pump 26 is directed through a supply circuit 30 to the hydrogen engine 100. The supply circuit 30 includes a liquid flow channel 32, a gas flow channel 33, an evaporator 34, a pressure chamber 40, and a supply pressure reducing valve 50. The liquid flow channel 32 is a flow channel designed to direct the liquid hydrogen discharged from the hydrogen pump 26 to the evaporator 34. The evaporator 34 is a heat exchanger configured to exchange heat between the liquid hydrogen and a refrigerant, to thereby convert the liquid hydrogen into a hydrogen gas. The hydrogen gas generated in the evaporator 34 is output to the gas flow channel 33.
A refrigerant flow channel 36 is arranged within the evaporator 34. The refrigerant flow channel 36 is designed to circulate the refrigerant between the evaporator 34 and a heat source 110. The refrigerant is not limited to any specific material, and may be, for example, a gas, such as helium, or a liquid, such as water. Also, no particular limitation is imposed on the heat source 110. Therefore, the heat source 110 may be, for example, the hydrogen engine 110 or a heater which generates heat by electric power. The refrigerant heated by the heat source 110 heats the liquid hydrogen in the evaporator 34. As a result, the liquid hydrogen is evaporated, and the hydrogen gas is generated accordingly. Hydrogen is significantly increased in its volume through evaporation. Here, the refrigerant is pressurized and delivered by a refrigerant pump 38.
The gas flow channel 33 is a flow path designed to direct the hydrogen gas from the evaporator 34 into an injector 52. The gas flow channel 33 is connected via an inflow channel 42 and an outflow channel 44 to the pressure chamber 40. The pressure chamber 40 is a container in which the hydrogen gas is temporarily stored. The pressure chamber 40 is configured to have a hydrogen gas capacity sufficient for covering a response delay in control of hydrogen gas supply. For example, the pressure chamber 40 has a capacity equivalent to several seconds' to 60 seconds' worth of hydrogen consumed at the maximum flow rate by the hydrogen engine 100. When the thus-configured pressure chamber 40 is installed, occurrence of a shortage of hydrogen gas can be prevented even when a quantity of hydrogen consumed by the hydrogen engine 100 is abruptly changed.
The inflow channel 42 is equipped with a check valve 46 to check the flow of the hydrogen gas from the pressure chamber 40 toward the gas flow channel 33. The outflow channel 44 is equipped with a chamber gate valve 48. The chamber gate valve 48 is basically opened while the hydrogen engine 100 is being driven. The inflow channel 42 is located upstream of the outflow channel 44. For this reason, when the pressure in the gas flow channel 33 is higher than the internal pressure of the pressure chamber 40, the check valve 46 is opened to thereby allow the hydrogen gas to flow into the pressure chamber 40. On the other hand, when the internal pressure of the pressure chamber 40 is higher than the pressure in the gas flow channel 33, the hydrogen gas stored in the pressure chamber 40 is supplied through the outflow channel 44 into the gas flow channel 33. As a result, the pressure of the hydrogen gas supplied to the supply pressure reducing valve 50 becomes substantially equal to the internal pressure of the pressure chamber 40.
A pressure sensor 41 detects the internal pressure of the pressure chamber 40. Hereinafter, a value detected by the pressure sensor 41 is referred to as a “hydrogen gas pressure Pgh”. As will be described in detail below, a controller 80 is configured to control a rotation speed of the pump motor 28 in such a manner that the hydrogen gas pressure Pgh matches a predetermined target hydrogen gas pressure Pgh*.
The supply pressure reducing valve 50 is arranged downstream of the outflow channel 44. The supply pressure reducing valve 50 reduces the pressure of the hydrogen gas to a pressure suitable for the hydrogen engine 100. The pressure reduced hydrogen gas is supplied through the injector 52 to the hydrogen engine 100. A flow quantity of the hydrogen gas supplied to the hydrogen engine 100 is detected by a flowmeter 54. Hereinafter, the flow quantity of the hydrogen gas detected by the flowmeter 54 is referred to as a “hydrogen gas flow quantity Qgh”.
A return circuit 60 is branched from the supply circuit 30 and configured to return the hydrogen gas to the hydrogen tank 12. The return circuit 60 includes a return flow channel 62, a return gate valve 64, a return pressure reducing valve 66, and a check valve 68. The return flow channel 62 is branched from the gas flow channel 33 at a location downstream of the outflow channel 44 and upstream of the supply pressure reducing valve 50. The return flow channel 62 branched from the gas flow channel 33 extends to the hydrogen tank 12 so as to communicate with the inside of the hydrogen tank 12.
The return gate valve 64 is a valve for opening and closing the return flow channel 62, and is controlled to be opened and closed by the controller 80. When the return gate valve 64 is opened, a part of the hydrogen gas flowing through the supply circuit 30 is caused to flow back to the hydrogen tank 12. The return pressure reducing valve 66 is arranged on a downstream side of the return gate valve 64, the downstream side being located farther away from a branching point. The return pressure reducing valve 66 reduces the pressure of the hydrogen gas to a level at which the hydrogen gas can be returned to the hydrogen tank 12 without causing any problems. The check valve 68 is arranged downstream of the return pressure reducing valve 66. The check valve 68 allows only a flow of the hydrogen gas flowing from the return pressure reducing valve 66 toward the hydrogen tank 12 and checks a backflow of the hydrogen gas. The reason for arranging the return circuit 60 will be further described below.
The hydrogen tank 12 is further connected to a boil off channel 72. The boil off channel 72 is configured to be opened when the internal pressure of the hydrogen tank 12 exceeds a predetermined safety value Psf. Once the boil off channel 72 is opened, a part of the hydrogen gas accumulated in the hydrogen tank 12 is released through the boil off channel 72 to the outside. This can prevent an excessive increase in the internal pressure of the hydrogen tank 12. That is, as described above, the inner tank 14 is thermally insulated by a vacuum, although entry of heat into the inner tank 14 is not completely prevented. This causes a part of the stored liquid hydrogen to be naturally evaporated, and a hydrogen gas (so called boil off gas) is accordingly generated. Leaving the thus-generated hydrogen gas as it is will excessively increase the internal pressure of the hydrogen tank 12. To avoid this, the boil off channel 72 is opened to release a part of the hydrogen gas from the hydrogen tank 12 when the internal pressure of the hydrogen tank 12 exceeds the predetermined safety value Pfs.
It should be noted that
The internal pressure and temperature of the hydrogen tank 12 are detected by a pressure sensor 78 and a temperature sensor 76, respectively. Hereinafter, an internal pressure of the hydrogen tank 12 detected by the pressure sensor is referred to as a “tank internal pressure Pt”.
The controller 80 controls operation of the liquid hydrogen system 10. The controller 80 is physically implemented by a computer incorporating a processor 82 and a memory 84. The “computer” includes a microcontroller in which a computer system is incorporated into a single integrated circuit. However, the controller 80 is not limited to such a single computer, and may be composed of two or more computers which are physically separated from each other. The controller 80 controls, based on values detected by various sensors, actuation of a plurality of valves and pumps installed in the liquid hydrogen system 10.
Specifically, the controller 80 controls a supply flow quantity of a hydrogen gas supplied to the hydrogen engine 100 in response to a request from an engine controller (not illustrated). The supply flow quantity of the hydrogen gas is proportional to a discharge flow quantity Qlh of liquid hydrogen, and the discharge flow quantity Qlh is proportional to a rotation speed Nm of the pump motor 28. Then, the controller 80 performs feedback control of the rotation speed of the pump motor 28 using, as a feedback value, the hydrogen gas flow quantity Qgh detected by the flowmeter 54. Meanwhile, in addition to the flow quantity of the hydrogen gas, a pressure of the hydrogen gas must be maintained at a suitable value, in order to appropriately drive the hydrogen engine 100. To achieve this, the controller 80 feeds back the hydrogen gas pressure Pgh detected by the pressor sensor 41, to control the rotation speed Nm of the pump motor 28.
As shown in
Further, a pressure deviation is calculated by subtracting the hydrogen gas pressure Pgh detected by the pressure sensor 41 from a target hydrogen gas pressure Pgh*. The pressure controller 88 receives, as an input, the pressure deviation and outputs a second command value C2. Here, the target hydrogen gas pressure Pgh* is a value determined based on characteristics of the hydrogen engine 100 and is basically a fixed invariable value. The controller 80 determines a sum of the first command value C1 and the second command value C2 as a motor rotation speed command Nm*, and controls operation of the pump motor 28 based on the motor rotation speed command Nm*.
As is evident from the above explanation, the controller 80 operates the pump motor 28 to discharge liquid hydrogen from the hydrogen tank 12 in response to the request from the hydrogen engine 100. When a quantity of hydrogen consumed by the hydrogen engine 100 is increased, the discharge flow quantity Qlh of liquid hydrogen is accordingly increased, which may, in some cases, cause a decrease of the internal pressure of the hydrogen tank 12.
Specifically, a small quantity of the boil off gas (i.e., hydrogen gas) is always generated within the hydrogen tank 12. Once the discharge flow quantity Qlh of the liquid hydrogen becomes greater than a generation quantity of the boil off gas (hereinafter, referred to as a “boil off quantity Qbf”), a tank internal pressure Pt is gradually decreased.
When the tank internal pressure Pt is excessively decreased, the hydrogen pump 26 is unable to properly discharge liquid hydrogen. In particular, in a case where the hydrogen pump 26 is the booster pump which pressurizes liquid hydrogen, it is necessary that the pressure of liquid hydrogen be increased to a high discharge pressure in order to discharge the liquid hydrogen. However, when the tank internal pressure Pt is decreased and thus the pressure of liquid hydrogen is dropped, the liquid hydrogen cannot be pressurized to the high discharge pressure, resulting in a failure in proper discharging of the liquid hydrogen. To avoid the failure, the tank internal pressure Pt is maintained at or above a predetermined reference pressure; in this example, by releasing the return circuit 60 as appropriate to return a part of the hydrogen gas flowing through the supply circuit 30 back into the hydrogen tank 12.
More specifically, in this example, when the tank internal pressure Pt detected by the pressure sensor 78 becomes lower than a predetermined reference pressure Pst, the return gate valve 64 is opened to direct the hydrogen gas to the hydrogen tank 12. It should be noted that the hydrogen gas flowing through the return gate valve 64 has a pressure higher than the internal pressure of the hydrogen tank 12. For this reason, the return pressure reducing valve 66 is disposed downstream of the return gate valve 64 in this example to decrease the pressure of the hydrogen gas to a pressure suitable for flowing into the hydrogen tank 12. For example, the return pressure reducing valve 66 decreases the pressure of the hydrogen gas to a pressure higher than the reference pressure Pst and lower than the safety value Psf. In this way, the hydrogen gas flowing through the supply circuit 30 is partially returned to the hydrogen tank 12, which can prevent an excessive decrease of the internal pressure of the hydrogen tank 12, and can, in turn, allow the hydrogen pump 26 to continue appropriate discharge of the liquid hydrogen.
It should be noted that, of course, the reference pressure Pst is sufficiently lower than the safety value Psf which causes the boil off channel 72 to be opened. Further, the reference pressure Pst may not necessarily be set to a single value, and may be set using a certain extent of a hysteresis band.
In an example shown in
After the return gate valve 64 is opened, the controller 80 monitors whether the tank internal pressure Pt crosses a point of the upper reference pressure Pst_up in the process of an increase of the tank internal pressure Pt (step S14). When the tank internal pressure Pt does not exceed the upper reference pressure Pst_up (No is determined in step S14), the controller 80 maintains the return gate valve 64 in its opened state. Since the return gate valve 64 is opened, the hydrogen gas is directed to flow into the hydrogen tank 12, which gradually increases the tank internal pressure Pt. Then, when the tank internal pressure Pt exceeds the upper reference pressure Pst_up (Yes is determined in step S14), the controller 80 closes the return gate valve 64 (step S16). Following this, the controller 80 returns to step S10 and repeats similar processing in the above-described steps.
It should be noted that the above-described control operation is presented as an example. The control operation to open and close the return channel 62 may be changed as appropriate so long as the tank internal pressure Pt can be maintained at or above the reference pressure Pst. For example, in the above explanation, the return gate valve 64 is controlled to be opened and closed based on a feedback value of the tank internal pressure Pt detected by the pressure sensor 78. However, the return gate valve 64 may be controlled to be opened and closed based on a parameter other than the tank internal pressure Pt. For example, the return gate valve 64 may be controlled to be opened and closed based on the discharge flow quantity Qlh of liquid hydrogen.
Next, the controller 80 subtracts the boil off quantity Qbf from the discharge flow quantity Qlh to calculate a hydrogen increase or decrease quantity ΔQ (step S22). For the boil off quantity Qbf, a predetermined fixed value may be used, or a variable value varying depending on the temperature detected by the temperature sensor 76 may be used.
Then, the controller 80 inputs the hydrogen increase or decrease quantity ΔQ and a value of zero into a MAX function to calculate a hydrogen decrease Qd=MAX (ΔQ, 0) (step S24). It should be noted that the MAX function is a function designed to output a maximum value among a plurality of variables having been input. In step S24, when the hydrogen increase or decrease quantity ΔQ is greater than zero, the MAX function returns Qd=ΔQ, and when the hydrogen increase or decrease quantity ΔQ is smaller than or equal to zero, the MAX function returns Qd=0. When the hydrogen decrease Qd is greater than 0, the tank internal pressure Pt is gradually decreased so long as no operation is performed. Therefore, the controller 80 opens the return gate valve 64 for a time period of (Qd×Kt) seconds (step S26) where the coefficient Kt is a predetermined fixed value. Then, after the expiration of the time period of (Qd×Kt) seconds, the controller 80 closes the return gate valve 64, and returns to step S20. Here, in a case of Qd=0, the return gate valve 64 is continuously closed, of course, and the hydrogen gas is not returned.
When the time period during which the return gate valve 64 is opened is changed based on the discharge flow quantity Qlh as described above, the hydrogen gas can be returned to the hydrogen tank 12 before the tank internal pressure Pt is decreased, which can ensure that suitable operation of the hydrogen pump 26 can be maintained.
In another embodiment, the return flow channel 62 may be configured in such a manner that the return flow channel 62 will open and close depending on a release pressure of the check valve 68. For example, as illustrated in
Here, a pressure on a primary side of the check valve 68 is substantially equal to the hydrogen gas pressure Pgh detected by the pressure sensor 41. In addition, the controller 80 performs the feedback control so as to match the hydrogen gas pressure Pgh with the target hydrogen gas pressure Pgh*. For this reason, the pressure on the primary side of the check valve 68 becomes substantially equal to the target hydrogen gas pressure Pgh*. When the internal pressure of the hydrogen tank 12 is decreased to be lower than the reference pressure Pst, the release pressure Pvo or a pressure higher than the release pressure Pvo is exerted on the check valve 68, to thereby open the check valve 68. This causes the hydrogen gas to flow back to the hydrogen tank 12, which increases the tank internal pressure Pt. When a pressure difference between the primary side and the secondary side of the check valve 68 becomes smaller than the release pressure Pvo after the tank internal pressure Pt is increased, the check valve 68 is automatically closed, which stops the flow of the hydrogen gas returning to the hydrogen tank 12. In this way, the return flow channel 62 can be automatically opened and closed by the check valve 68 depending on the circumstances, which can, in turn, simplify the control operation of the controller 80.
In a case where the hydrogen gas is partially returned to the hydrogen tank 12, an additional quantity of hydrogen gas is needed correspondingly. For example, in a case where a return quantity Qr of hydrogen gas is returned to the hydrogen tank 12, the liquid hydrogen system needs, as a whole, hydrogen gas in a quantity equal to the sum of the return quantity Qr and the target hydrogen gas flow quantity Qgh* supplied to the hydrogen engine 100. Therefore, in the example illustrated in
Here, the return quantity Qr is significantly smaller than the flow quantity Qgh of the hydrogen gas to be supplied to the hydrogen engine 100. Further, in this example, the pressure chamber 40 is installed at some intermediate point in the supply circuit 30 to temporarily store the hydrogen gas. A certain extent of excess or deficiency of the hydrogen gas can be accommodated by the hydrogen gas temporarily stored in the pressure chamber 40. Therefore, in this example in which the pressure chamber 40 is installed, the return quantity Qr is ignored in the calculation of the motor rotation speed command Nm*. In this example, because the pressure chamber 40 is installed, a shortage of the hydrogen gas can be prevented even though the return quantity Qr is ignored. Further, when the return quantity Qr is ignored in the calculation of the motor rotation speed command Nm*, the amount of computation for the control operation can be reduced.
However, of course, the return quantity Qr may be incorporated in the control of the motor rotation speed. Specifically, the parameter Qgh* shown in
In another embodiment, the tank internal pressure Pt may be fed back, as shown in
When the return quantity Qr of the hydrogen gas is added to the target flow quantity, or the tank internal pressure Pt is fed back as described above, a more suitable quantity of liquid hydrogen can be discharged, which can ensure that variations in pressure of the hydrogen gas can be suppressed in the gas flow channel 33.
The above-described configurations are presented by way of illustration. The configurations may be changed other than a feature that the liquid hydrogen system 10 includes the return circuit 60 through which a part of the hydrogen gas flowing through the supply circuit 30 is returned to the hydrogen tank 12. For example, although in
| Number | Date | Country | Kind |
|---|---|---|---|
| 2022-187644 | Nov 2022 | JP | national |
