Exhaust system for an engine
US-12162562-B2 · Dec 10, 2024 · US
US9989002B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9989002-B2 |
| Application number | US-201414485533-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 12, 2014 |
| Priority date | Dec 3, 2013 |
| Publication date | Jun 5, 2018 |
| Grant date | Jun 5, 2018 |
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Disclosed are a turbocharger for a combustion engine and a method of operating a turbocharger. The turbocharger may include a variably positionable flow restrictor for restricting flow in a turbocharger inlet of the turbocharger by an amount dependent on a flow restrictor position. The method may include determining an operating point variable of the combustion engine, controlling a first actuator to exert on the flow restrictor a first actuating force for varying the flow restrictor position depending on the operating point variable, determining a crank angle variable of the combustion engine, and controlling a second actuator to exert on the flow restrictor a second actuating force for varying the flow restrictor position depending on the crank angle variable.
Opening claim text (preview).
What is claimed is: 1. A method of operating a turbocharger for a combustion engine, the turbocharger including a variably positionable flow restrictor for restricting flow in a turbocharger inlet of the turbocharger by an amount dependent on a flow restrictor position, the method comprising the steps of: determining an operating point variable including both of an engine speed and an engine load of the combustion engine by an operating point variable sensor; controlling by a first controller, a first actuator to exert, on the flow restrictor, a first actuating force for varying the flow restrictor position depending on the operating point variable; determining by a crank angle variable sensor, a crank angle variable including a crank angular position of the combustion engine, wherein the crank angular position is determined independent from the engine speed; and controlling by a second controller, a second actuator to exert, on the flow restrictor, a second actuating force for further varying the flow restrictor position depending on the crank angle variable, after the first actuator is controlled based on the operating point variable of the engine speed and the engine load, wherein the first and second actuators are engaged to each other and the second actuator is relatively movable with respect to the first actuator according to operation of the first actuator. 2. The method according to claim 1 , further comprising a step of providing a modulation function, which defines a desired modulation of the flow restrictor position, wherein the controlling of the second actuator by the second controller is performed based on the modulation function. 3. The method according to claim 2 , wherein the modulation function comprises at least one adjustable parameter for adjusting the modulation function, and the step of providing the modulation function comprises determining the at least one adjustable parameter based on the operating point variable. 4. The method according to claim 3 , wherein the at least one adjustable parameter comprises at least one of an offset having a crank angle spaced from an angler of a top dead center of the combustion engine, a modulation base level defined on the flow restrictor position, a modulation amplitude of the module function, a positive modulation amplitude ramp time during which the modulation function rises, a negative modulation amplitude ramp time during which the modulation function falls, and a modulation period of the modulation function. 5. The method according to claim 2 , wherein the modulation function is sinusoidal. 6. The method according to claim 1 , wherein the controlling of the second actuator by the second controller is performed selectively depending on the operating point variable. 7. A computer program product comprising computer non-transitory executable instructions, which when executed by a computer or a control device cause the computer or the control device to perform the method according to claim 1 . 8. A turbocharger for a combustion engine, comprising: a variably positionable flow restrictor configured for restricting flow in a turbocharger inlet of the turbocharger by an amount dependent on a flow restrictor position; an operating point variable sensor configured for determining an operating point variable including both of an engine speed and an engine load of the combustion engine; a first actuator configured for exerting, on the flow restrictor, a first actuating force for varying the flow restrictor position depending on the operating point variable; a crank angle variable sensor configured for determining a crank angle variable including a crank angular position of the combustion engine, wherein the crank angular position is determined independent from the engine speed; and a second actuator configured for exerting, on the flow restrictor, a second actuating force for further varying the flow restrictor position depending on the crank angle variable after the first actuator is controlled based on the operating point variable of the engine speed and the engine load, wherein the first and second actuators are engaged to each other and the second actuator is relatively movable with respect to the first actuator according to operation of the first actuator. 9. The turbocharger according to claim 8 , wherein at least one of the first and/or second actuators comprises a fluidic actuator. 10. The turbocharger according to claim 9 , wherein the first actuator comprises a first fluid valve and the second actuator comprises a second fluid valve, the first and second fluid valves being connected to a same fluidic cylinder for actuating the flow restrictor. 11. The turbocharger according to claim 8 , wherein the second actuator comprises an excenter. 12. A combustion engine equipped with the turbocharger according to claim 8 .
the characteristics being related to the exhaust flow · CPC title
the characteristics being an exhaust gas pressure · CPC title
Arrangements of actuators or linkage for bypass valves · CPC title
Cross-Sectional Technologies · mapped topic
by varying cross-section of exhaust passages or air passages {, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits} (F02B37/24 takes precedence) · CPC title
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