Internal combustion engine control device and method
US-2015219024-A1 · Aug 6, 2015 · US
US10006384B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10006384-B2 |
| Application number | US-201514693253-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 22, 2015 |
| Priority date | Apr 24, 2014 |
| Publication date | Jun 26, 2018 |
| Grant date | Jun 26, 2018 |
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A time point t 0 represents a time point when a turbocharged engine is brought into a decelerating state, and an opening degree of a throttle valve is decreased. A time point t 1 represents a time point when an opening command to an ABV is issued. When the ABV has an abnormality, and when a WGV is stuck open, a turbocharging pressure before the time point t 0 shows a tendency to fall below a target turbocharging pressure, and a turbocharging pressure after the time point t 1 reduces slowly to approach a predetermined pressure. When the WGV is stuck closed, a turbocharging pressure before the time point t 0 shows a tendency to exceed the target turbocharging pressure, and the turbocharging pressure after the time point t 1 reduces with vigor to approach the predetermined pressure.
Opening claim text (preview).
The invention claimed is: 1. A control device for an internal combustion engine including a first cylinder group to which a first intake manifold and a first exhaust manifold are connected; a second cylinder group to which a second intake manifold and a second exhaust manifold are connected; a first upstream intake passage and a second upstream intake passage that are connected to the first intake manifold and the second intake manifold via a common downstream intake passage; a first air bypass valve provided in a passage bypassing a first compressor mounted to the first upstream intake passage; a second air bypass valve provided in a passage bypassing a second compressor mounted to the second upstream intake passage; a first wastegate valve provided in a passage bypassing a first turbine that is mounted to the first exhaust manifold and that is connected to the first compressor; and a second wastegate valve provided in a passage bypassing a second turbine that is mounted to the second exhaust manifold and that is connected to the second compressor, the control device comprising: a throttle valve that is provided in the downstream intake passage; a pressure sensor that measures a turbocharging pressure upstream of the throttle valve in the downstream intake passage; feedback control means configured to correct opening degrees of the first wastegate valve and the second wastegate valve so that the measured turbocharging approaches a target turbocharging pressure; first rate of reduction calculating means configured to issue an opening command to the first air bypass valve at a time of deceleration of the internal combustion engine when an absolute value of a feedback correction amount by the feedback control means exceeds a predetermined value, and to calculate a first rate of reduction of the measured turbocharging pressure; second rate of reduction calculating means configured to issue an opening command to the second air bypass valve at the time of deceleration of the internal combustion engine when the absolute value exceeds the predetermined value again after calculation of the first rate of reduction of the measured turbocharging pressure, and to calculate a second rate of reduction of the measured turbocharging pressure; and abnormality determining means configured to determine to which one of the first air bypass valve, the second air bypass valve, the first wastegate valve, and the second wastegate valve, an abnormality occurs, based on the feedback correction amount, the first rate of reduction of the measured turbocharging pressure, and the second rate of reduction of the measured turbocharging pressure. 2. The control device according to claim 1 , wherein the abnormality determining means compares the first rate of reduction of the measured turbocharging pressure with the second rate of reduction of the measured turbocharging pressure when the feedback correction amount has a positive value, determines that the abnormality occurs to the first wastegate valve when the first rate of reduction of the measured turbocharging pressure is lower than the second rate of reduction of the measured turbocharging pressure, and determines that the abnormality occurs to the second wastegate valve when the second rate of reduction of the measured turbocharging pressure is lower than the first rate of reduction of the measured turbocharging pressure. 3. The control device according to claim 1 , wherein the abnormality determining means compares the first rate of reduction of the measured turbocharging pressure with the second rate of reduction of the measured turbocharging pressure when the feedback correction amount has a negative value, determines that the abnormality occurs to the first wastegate valve when the first rate of reduction of the measured turbocharging pressure is higher than the second rate of reduction of the measured turbocharging pressure, and determines that the abnormality occurs to the second wastegate valve when the second rate of reduction of the measured turbocharging pressure is higher than the first rate of reduction of the measured turbocharging pressure. 4. The control device according to claim 2 , wherein the abnormality determining means compares the first rate of reduction of the measured turbocharging pressure and the second rate of reduction of the measured turbocharging pressure with a predetermined rate of reduction of the measured turbocharging pressure before comparing the first rate of reduction of the measured turbocharging pressure with the second rate of reduction of the measured turbocharging pressure, determines that the abnormality occurs to the first air bypass valve when the first rate of reduction of the measured turbocharging pressure is lower than the predetermined rate of reduction of the measured turbocharging pressure, and determines that the abnormality occurs to the second air bypass valve when the second rate of reduction of the measured turbocharging pressure is lower than the predetermined rate of reduction of the measured turbocharging pressure. 5. The control device according to claim 3 , wherein the abnormality determining means compares the first rate of reduction of the measured turbocharging pressure and the second rate of reduction of the measured turbocharging pressure with a predetermined rate of reduction of the measured turbocharging pressure before comparing the first rate of reduction of the measured turbocharging pressure with the second rate of reduction of the measured turbocharging pressure, determines that the abnormality occurs to the first air bypass valve when the first rate of reduction of the measured turbocharging pressure is lower than the predetermined rate of reduction of the measured turbocharging pressure, and determines that the abnormality occurs to the second air bypass valve when the second rate of reduction of the measured turbocharging pressure is lower than the predetermined rate of reduction of the measured turbocharging pressure. 6. The control device according to claim 2 , further comprising countermeasure control means configured to perform countermeasure control when the abnormality of the first wastegate valve or the second wastegate valve is determined. 7. The control device according to claim 3 , further comprising countermeasure control means configured to perform countermeasure control when the abnormality of the first wastegate valve or the second wastegate valve is determined. 8. An internal combustion engine comprising: a first cylinder group to which a first intake manifold and a first exhaust manifold are connected; a second cylinder group to which a second intake manifold and a second exhaust manifold are connected; a first upstream intake passage and a second upstream intake passage that are connected to the first intake manifold and the second intake manifold via a common downstream intake passage; a first compressor mounted to the first upstream intake passage; a second compressor mounted to the second upstream intake passage; a first turbine mounted to the first exhaust manifold and connected to the first compressor; a second turbine mounted to the second exhaust manifold and connected to the second compressor; a first air bypass valve provided in a first passage bypassing the first compressor; a second air bypass valve provided in a second passage bypassing the second compressor; a first wastegate valve provided in a third passage bypassing the first turbine; a second wastegate valve provided in a fourth passage bypassing the second turbine; a throttle valve that is provided in the downstream intake passage; a pressure sensor that measures a turbocharging pressure upstream of the throttle valve in the downstream intake passage; and a controller pr
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