Method for operating a supercharged internal combustion engine and device for providing combustion air for a supercharged internal combustion engine
US-2024344477-A1 · Oct 17, 2024 · US
US10100753B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10100753-B2 |
| Application number | US-201615047012-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 18, 2016 |
| Priority date | Feb 20, 2015 |
| Publication date | Oct 16, 2018 |
| Grant date | Oct 16, 2018 |
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In a multiple cylinder supercharged engine, when reduced cylinder operation is executed, a throttle, which is located downstream of a compressor driven by a turbine provided in an exhaust passage, through which exhaust gas of a cylinder group flows, is operated to a fully closed state, wherein the reduced cylinder operation is applied to the cylinder group. A fuel injection amount of at least one cylinder included in the cylinder group is made smaller than a fuel injection amount of a cylinder included in another cylinder group, and this at least one cylinder is operated, in order to increase rotational speed of the compressor, so that a value of pressure of an upstream side of the throttle is controlled to a value, which is equal to or larger than a value of pressure of a downstream side of the throttle.
Opening claim text (preview).
What is claimed is: 1. A supercharged engine comprising: a plurality of cylinders that are grouped into a plurality of cylinder groups, each of the plurality of cylinders having an intake valve and an exhaust value, a plurality of intake passages provided independently from one another, a number of the intake passages being equal to a number of the cylinder groups, a plurality of exhaust passages having a one to one relationship with the cylinder groups, a plurality of compressors, each of the compressors being provided in each of the intake passages, a plurality of turbines having a one to one relationship with the compressors and connected to the compressors, each of the turbines being provided in each of the exhaust passages, a plurality of throttles located downstream of the compressors, each of the throttles being provided in each of the intake passages, a common intake passage formed by gathering the intake passages on a downstream side of the throttles, and commonly shared among the cylinder groups, a first pressure sensor configured to measure pressure upstream of the plurality of throttles and a second pressure sensor configured to measure pressure downstream of the plurality of throttles, and a control device, wherein the control device is configured to execute reduced cylinder operation, and while the reduced cylinder operation is executed, fuel injection with respect to at least one of the cylinder groups is stopped, and at least one of the intake valves and the exhaust valves of said at least one of the cylinder groups are stopped in a closed state, wherein the control device is configured to operate one of the plurality of throttles to a fully closed state while the reduced cylinder operation is executed, wherein the one of the plurality of throttles is located downstream of one of the plurality of compressors, the one of the plurality of compressors is driven by one of the plurality of turbines, the one of the plurality of turbines is provided in one of the plurality of exhaust passages, exhaust gas of one of the plurality of cylinder groups flows through the one of the plurality of exhaust passages; and wherein the control device is configured, while the reduced cylinder operation is executed, and in response to the pressure of an upstream side of the one of the plurality of throttles being smaller than the pressure of a downstream side of the one of the plurality of throttles, to operate at least one cylinder, which is included in the one of the plurality of cylinder groups, and control an amount of fuel injection with respect to the at least one cylinder to be less than an amount of fuel injection with respect to a second cylinder which has not been stopped, to increase exhaust gas energy which is supplied to the one of the plurality of turbines to increase rotational speed of the one of the plurality of compressors, so that the pressure of the upstream side of the one of the plurality of throttles is controlled to be equal to or greater than the pressure of the downstream side of the one of the plurality of throttles. 2. The supercharged engine according to claim 1 , wherein the control device controls the pressure of the upstream side of the one of the plurality of throttles to be equal to the pressure of the downstream side of the one of the plurality of throttles. 3. The supercharged engine according to claim 1 , wherein the supercharged engine further comprises an actuator that is provided in the one of the plurality of exhaust passages, the actuator being configured to regulate the exhaust gas energy supplied to the one of the plurality of turbines, and wherein the control device is configured to operate the actuator so that the exhaust gas energy supplied to the one of the plurality of turbines becomes a maximum while the pressure control portion operates said at least one cylinder included in the one of the plurality of cylinder groups. 4. The supercharged engine according to claim 1 , wherein the control device is configured to regulate the amount of the fuel injection with respect to said at least one cylinder included in the one of the plurality of cylinder groups in accordance with a difference between a measured value of the pressure of the upstream side of the one of the plurality of throttles and a target value, wherein the target value is set to be equal to or greater than a value of the pressure of the downstream side of the one of the plurality of throttles. 5. The supercharged engine according to claim 1 , wherein the control device is configured to operate said at least one cylinder included in the one of the plurality of cylinder groups, while the pressure of the downstream side of the one of the plurality of throttles is equal to or greater than ambient pressure, and wherein the control device is configured to continue preventing operation of all cylinders included in the one of the plurality of cylinder groups, while the pressure of the downstream side of the one of the plurality of throttles is less than the ambient pressure.
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