1. Field of the Invention
The invention relates to an engine system and a control method for the engine system.
2. Description of Related Art
There is known a turbocharger that utilizes exhaust gas of an internal combustion engine (an engine). A turbine is rotated with the aid of exhaust gas of the engine, and a compressor compresses air and supplies the engine therewith. For example, in Japanese Patent Application Publication No. 2007-16641 (JP-2007-16641 A), there is disclosed an art of supplying a turbine with exhaust gas of a fuel cell as well as exhaust gas of an engine. The electric power generated by the fuel cell is used to charge a battery. In order to restrain the battery from deteriorating, it is preferable to avoid overcharge of the battery. For example, in each of Japanese Patent Application Publication No. 2010-70030 (JP-2010-70030 A) and Japanese Patent Application Publication No. 63-265527 (JP-63-265527 A), there is disclosed an art of controlling the amount of charge of a battery such that the battery can be charged through the use of the electric power regenerated from a motor in braking a vehicle.
In order to enhance transience from a stopped state of the engine to an operating state of the engine, it is preferable that the turbine rotate even during stop of the engine. However, the rotational speed of the turbine may significantly fall during stop of the engine idling (hereinafter referred to as idle-stop). This may cause a deterioration in transience. The invention provides an engine system that can make an improvement in transience.
In a first aspect of the invention, an engine system includes a battery, a fuel cell that charges the battery, a turbocharger that is supplied with exhaust gas discharged from the fuel cell, an internal combustion engine that is supplied with air from the turbocharger, an internal combustion engine control unit that stops the internal combustion engine automatically upon fulfillment of a predetermined stop condition and that starts the internal combustion engine automatically upon fulfillment of a predetermined restoration condition, and a fuel cell control unit configured to stop the fuel cell from charging the battery or limit a charge amount of the battery to a value equal to or smaller than a discharge amount of the battery when the fuel cell is driven during operation of the internal combustion engine and a state of charge of the fuel cell is equal to or larger than a first limit value. In the engine system, the fuel cell control unit being configured not to limit the charge amount when the internal combustion engine control unit stops the internal combustion engine and the fuel cell is driven during stop of the internal combustion engine.
In the aforementioned configuration, the fuel cell control unit may stop the fuel cell from charging the battery or limit the charge amount of the battery to a value equal to or smaller than the discharge amount of the battery when the internal combustion engine control unit stops the internal combustion engine and the state of charge is equal to or larger than a second limit value that is larger than the first limit value. The fuel cell control unit may not limit the charge amount when the internal combustion engine control unit stops the internal combustion engine and the state of charge is smaller than the second limit value.
In the aforementioned configuration, the fuel cell control unit may not limit the charge amount when the state of charge becomes smaller than the first limit value during stop of the internal combustion engine after the internal combustion engine control unit stops the internal combustion engine and the fuel cell stops charging the battery due to the state of charge becoming equal to or larger the second limit value.
In a second aspect of the invention, a control method for an engine system that is equipped with a battery, a fuel cell, a turbocharger, and an internal combustion engine. The control method includes stopping charging the battery or limiting a charge amount of the fuel cell to a value equal to or smaller than a discharge amount of the battery when the fuel cell is driven during operation of the internal combustion engine and a state of charge of the fuel cell is equal to or larger than a first limit value. In the control method, the charge amount is not limited when the internal combustion engine is stopped and the fuel cell is driven during stop of the internal combustion engine.
According to the invention, an engine system that can make an improvement in transience can be provided.
Features, advantages, and technical and industrial significance of an exemplary embodiment of the invention will be described below with reference to the accompanying drawings, in which like numerals denote like elements, and wherein:
The embodiment of the invention will be described using the drawings.
The embodiment of the invention is an example in which the limit value of a state of charge is changed.
As shown in
The battery 12 functions as a power supply for a pump (not shown), valves (not shown), an air-conditioner (not shown), a motor (not shown) and the like. Accordingly, the engine system 100 is not required to be equipped with an alternator. The fuel cell 14 functions as a power supply as is the case with the battery 12, and charges the battery 12. The fuel cell 14 has a structure in which a fuel electrode as an anode, an air electrode as a cathode, and a cell containing an electrolyte are coupled to one another, and generates electric power through an electrochemical reaction of fuel and air. That is, for example, a solid oxide fuel cell (SOFC) can be adopted as the fuel cell 14. The turbocharger 18 is equipped with a turbine 20, and a compressor 22 that is coupled to the turbine 20 by a shaft 24.
Exhaust gas discharged by the engine 16 is supplied to the turbine 20 through an exhaust channel 26. The exhaust channel 26 and an exhaust channel 28 are coupled to each other, and exhaust gas discharged by the fuel cell 14 is supplied to the turbine 20 through the exhaust channels 26 and 28. The turbine 20 rotates through exhaust gas. Exhaust gas is discharged to the outside of the vehicle through an exhaust channel 30. The compressor 22 rotates in synchronization with the turbine 20. The compressor 22 is supplied with air through an intake channel 32. The compressor 22 compresses air and supplies compressed air with the intake channel 34. An intake channel 36 is coupled to the intake channel 34. The air compressed by the compressor 22 is supplied to the engine 16 through the intake channel 34, and is supplied to the fuel cell 14 through the intake channels 34 and 36. As indicated by a broken line, the ECU 10 acquires an operation state of the engine 16 and a state of charge (SOC) of the battery 12, and controls the fuel cell 14. Next, the operation of the engine system 100 will be described referring to an example in which the engine 16 operates, stops in an idle state and starts operating again.
As shown in
As shown in
At the time t2, the engine 16 stops (OFF). The second limit value W2 is adopted as a limit value. At the time t2, the SOC is smaller than the second limit value W2. Thus, the fuel cell 14 turns ON. At a time t3, the SOC becomes equal to the second limit value W2, and hence the fuel cell 14 turns OFF. At this moment, the ECU 10 turns a long-term halt flag ON. The long-term halt flag indicates that the vehicle has been stopped for a long time during parking, halting, traffic congestion or the like. The long-term halt flag will be described later in detail with reference to
At a time t4, the engine 16 starts operating again. This corresponds to, for example, the restart of the engine 16 from idle-stop. In response to the restart of the engine 16, the first limit value W1 is adopted as a limit value. The SOC is larger than the first limit value W1, and hence the fuel cell 14 turns OFF. At a time t5, the SOC becomes smaller than the first limit value W1, and hence the fuel cell 14 turns ON.
An example in which the vehicle is halted longer than in the example of
The operation of the engine system 100 will be described further.
As shown in
If Yes in step S11, the fuel cell control unit 42 determines whether or not the long-term halt flag is ON (step S13, see I in
In step S15, the fuel cell control unit 42 determines whether or not the engine 16 is ON. If Yes in step S15, the fuel cell control unit 42 turns the fuel cell 14 OFF (step S16). This corresponds to the period between the time t1 and the time t2 in
If Yes in step S14, the fuel cell control unit 42 turns the fuel cell 14 OFF (step S17). The fuel cell control unit 42 turns the long-term halt flag ON (step S18). This corresponds to the time t3 in
If the control is resumed after the long-term halt flag turns ON in step S18, the result is Yes in step S13. In this case, the fuel cell control unit 42 determines whether or not the engine 16 is ON (step S19, see II in
If the control is repeated after the long-term halt flag turns OFF in step S20, the result is No in step S13. If No in step S14 and Yes in step S15, the fuel cell control unit 42 turns the fuel cell 14 OFF (step S16). This corresponds to the period between the time t4 and the time t5 in
Exhaust gas is discharged from the engine 16, for example, when the engine 16 is ON. No exhaust gas is discharged from the engine 16, for example, when the engine 16 is OFF. Exhaust gas is discharged from the fuel cell 14, for example, when the fuel cell 14 is ON. No exhaust gas or a slight amount of exhaust gas is discharged from the fuel cell 14, for example, when the fuel cell 14 is OFF. For example, in the case where only the first limit value W1 is used as a limit value, the fuel cell 14 is OFF in the period between the time t2 and the time t4. Since exhaust gas from the fuel cell 14 and the engine 16 is not supplied to the turbine 20 over a long time or the amount of exhaust gas decreases, the rotational speed of the turbine 20 significantly falls. In contrast, according to the embodiment of the invention, between the time t2 and the time t3, as indicated by steps S14 and S15, the fuel cell 14 is ON and the charge amount is not limited even if the SOC is equal to or larger than the first limit value W1 during idle-stop. Thus, even during idle-stop, exhaust gas from the fuel cell 14 is supplied to the turbine 20. Thus, the rotational speed of the turbine 20 is restrained from falling, and therefore, the enhancement of transience is achieved.
In order to maintain the rotational speed of the turbine 20, it is preferable that the period in which the engine 16 and the fuel cell 14 are OFF (the period between the time t3 and the time t4) be short. In other words, it is preferable that a time period Δt between the time t2 and the time t3 be long. Given that the time period Δt represents a general halt time period (an idle-stop time period) in the case where the vehicle waits for a traffic light to change, the time t3 approaches the time t4 or coincides with the time t4. As a result, the rotational speed of the turbine 20 is maintained by exhaust gas from the fuel cell 14, and an improvement in transience is made. Incidentally, the aforementioned general idle-stop time period can be determined by, for example, inspecting in advance a situation where the vehicle is used or the like.
If the difference between the first limit value W1 and the second limit value W2 is small, the SOC swiftly reaches the second limit value W2, and the fuel cell 14 turns OFF. Thus, the time period Δt becomes short, and the time period in which no exhaust gas is supplied or the amount of exhaust gas is reduced becomes long. As a result, a deterioration in transience is caused. In order to make an improvement in transience, it is preferable to adopt the general idle-stop period as the time period Δt as described above, and determine the first limit value W1 on the basis -of the time period Δt. The first limit value W1 is determined according to, for example, a formula shown below.
W1=(W3−W4)×Δt/(C×V)
W3 denotes an amount of electric power generated by the fuel cell 14. The magnitude of W3 is determined such that the fuel cell 14 discharges an amount of exhaust gas that is sufficient to cause rotation of the turbine 20 that is required for the maintenance of transience. W4 denotes an electric power consumed by the auxiliaries. C denotes a rated charge capacity of the battery 12. V denotes an output voltage of the battery 12. By determining the first limit value W1 from the aforementioned formula, the fuel cell 14 remains ON even after the engine 16 turns OFF, and an improvement in transience is made.
If the fuel cell 14 is ON and the SOC is equal to or larger than the first limit value W1 during the period in which the engine 16 is ON as in the period between the time t1 and the time t2 in
If the SOC is smaller than the first limit value W1 during operation of the engine 16 as in the period between 0 and the time t1 in
Although the embodiment of the invention has been described in detail, the invention should not be limited to this specific embodiment thereof, but can be modified or altered in various manners within the scope of the gist of the invention as set forth in the claims.
Number | Date | Country | Kind |
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2012-096015 | Apr 2012 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/IB2013/000508 | 3/15/2013 | WO | 00 |