Systems and method for an engine bypass valve
View Patent ↗Various systems and methods are provided for controlling operation of a turbocharger compressor. In one example, a system includes a turbocharger including a turbine positioned in an exhaust passage and a compressor positioned in an intake passage, an engine bypass passage having an inlet fluidically coupled to an outlet of the compressor and an outlet fluidically coupled to an inlet of the turbine, an engine bypass valve to control flow through the engine bypass passage, and a controller configured to adjust a position of the engine bypass valve to maintain compressor operation within a designated compressor efficiency region.
1. A system, comprising:
a turbocharger including a turbine positioned in an exhaust passage and a compressor positioned in an intake passage;
an engine bypass passage having an inlet fluidically coupled to an outlet of the compressor and an outlet fluidically coupled to an inlet of the turbine;
an engine bypass valve to control flow through the engine bypass passage; and
a controller storing non-transitory instructions in memory executable to adjust a position of the engine bypass valve to maintain compressor operation within a designated compressor efficiency region, the designated compressor efficiency region including a region of a compressor map having a higher compressor efficiency than one or more neighboring regions of the compressor map, the compressor map defined by compressor mass flow and compressor pressure ratio.
2. The system of claim 1 , further comprising:
an engine having a first group of cylinders and a second group of cylinders; and
an exhaust gas recirculation (EGR) system including an EGR passage coupling the first group of cylinders to the intake passage, an EGR metering valve to control flow of exhaust gas through the EGR passage, and an EGR bypass valve to control flow of exhaust gas from the first group of cylinders to the exhaust passage.
3. The system of claim 2 , wherein the instructions are executable to adjust a position of the EGR metering valve based on a target intake oxygen fraction and adjust a position of the EGR bypass valve to maintain a pressure of exhaust gas in the EGR passage above a pressure of intake air downstream of the compressor.
4. The system of claim 2 , wherein the inlet of the turbine is a single inlet configured to receive exhaust gas from the first group of cylinders, exhaust gas from the second group of cylinders, and intake air from the engine bypass passage.
5. The system of claim 2 , wherein the inlet of the turbine is a first inlet, and wherein the turbine includes a second inlet configured to receive exhaust gas from the first group of cylinders and exhaust gas from the second group of cylinders.
6. The system of claim 2 , further comprising a power turbine positioned in the exhaust passage upstream of the turbine.
7. The system of claim 6 , wherein the instructions are executable to adjust operation of the power turbine to maintain a designated expansion ratio across the power turbine, the designated expansion ratio based on a difference between a pressure of exhaust gas in the EGR passage and a pressure of intake air downstream of the compressor.
8. The system of claim 2 , wherein the turbocharger is a first turbocharger including a first turbine and a first compressor, and further comprising a second turbocharger including a second turbine positioned downstream of the first turbine and a second compressor positioned upstream of the first compressor.
9. The system of claim 1 , wherein, to adjust the position of the engine bypass valve to maintain compressor operation within the designated compressor efficiency region, the instructions are executable to open the engine bypass valve responsive to compressor operation within a predefined range of a surge margin of the compressor map, the engine bypass valve opened by an amount that is predicted to move compressor operation to the designated compressor efficiency region.
10. The system of claim 1 , wherein, to adjust the position of the engine bypass valve to maintain compressor operation within the designated compressor efficiency region, the instructions are executable to open the engine bypass valve responsive to one or more of engine speed below a threshold speed or engine load below a threshold load.
11. The system of claim 1 , wherein the instructions are executable to open the engine bypass valve responsive to an intake manifold pressure of an intake manifold coupled to the intake passage exceeding a threshold pressure, and wherein the designated compressor efficiency region is a region of highest compressor efficiency of the compressor map.
12. A method for controlling operation of a turbocharger compressor, comprising:
via a controller,
determining surge conditions during compressor operation;
responsive to compressor operation at a surge margin, opening an engine bypass valve to route intake air from downstream of the turbocharger compressor to upstream of a turbine to prevent a surge event, the engine bypass valve opened by an amount more than needed to prevent the surge event in order to move compressor operation to a region of greater efficiency, the region of greater efficiency including a region of a compressor map having a higher compressor efficiency than one or more neighboring regions of the compressor map, the compressor map defined by compressor mass flow and compressor pressure ratio; and
flowing exhaust gas from a first exhaust manifold of an engine to an intake manifold of the engine based on adjusting an EGR valve.
13. The method of claim 12 , wherein flowing exhaust gas from the first exhaust manifold to the intake manifold comprises flowing a first portion of exhaust gas from the first exhaust manifold to the intake manifold and flowing remaining exhaust gas from the first exhaust manifold to the turbine.
14. The method of claim 13 , further comprising flowing exhaust gas from a second exhaust manifold of the engine to the turbine.
15. The method of claim 14 , further comprising flowing the remaining exhaust gas from the first exhaust manifold, the exhaust gas from the second exhaust manifold, and the intake air routed via the engine bypass valve through a single inlet of the turbine.
16. The method of claim 12 , further comprising opening the engine bypass valve responsive to an intake manifold pressure of the intake manifold exceeding a threshold pressure, and wherein flowing exhaust gas from the first exhaust manifold to the intake manifold includes flowing exhaust gas from the first exhaust manifold to the intake manifold while the engine bypass valve is open and while the intake air from downstream of the compressor is routed to upstream of the turbine.
17. A system, comprising:
an engine having a first group of cylinders and a second group of cylinders, the first group of cylinders coupled to a first exhaust manifold and the second group of cylinders coupled to a second exhaust manifold, both the first group of cylinders and the second group of cylinders coupled to an intake manifold;
an exhaust gas recirculation (EGR) system including an EGR passage coupling the first exhaust manifold to the intake manifold, an EGR metering valve to control flow of exhaust gas through the EGR passage, and an EGR bypass valve to control flow of exhaust gas from the first exhaust manifold to an exhaust passage;
a turbocharger including a turbine positioned in the exhaust passage and a compressor positioned in an intake passage;
an engine bypass passage having an inlet fluidically coupled to an outlet of the compressor and an outlet fluidically coupled to an inlet of the turbine;
an engine bypass valve to control flow through the engine bypass passage; and
a controller storing non-transitory instructions in memory executable to:
responsive to compressor operation at a surge margin, adjust a position of the engine bypass valve to prevent a surge event, the engine bypass valve selectively adjusted by an amount more than needed to prevent the surge event in order to move compressor operation to a region of greater efficiency, the region of greater efficiency including a region of a compressor map having a higher compressor efficiency than one or more neighboring regions of the compressor map, the compressor map defined by compressor mass flow and compressor pressure ratio;
adjust a position of the EGR metering valve based on a target intake oxygen fraction; and
adjust a position of the EGR bypass valve to maintain a pressure of exhaust gas in the EGR passage above a pressure of intake air downstream of the compressor.
18. The system of claim 17 , wherein the instructions are executable to, responsive to adjusting the position of the engine bypass valve, advance fuel injection timing.
19. The system of claim 17 , wherein the instructions are executable to, responsive to adjusting the position of the engine bypass valve, further adjust the position of the EGR metering valve.
20. The system of claim 17 , wherein, to adjust the position of the engine bypass valve to prevent the surge event, the instructions are executable to:
determine a first engine bypass valve position that prevents the surge event, the compressor configured to operate at a first region of efficiency at the first engine bypass valve position;
determine a second engine bypass valve position that moves compressor operation to a second region of efficiency, greater than the first region;
adjust the position of the engine bypass valve to the second engine bypass valve position; and
if boost pressure drops below a threshold pressure, adjust the position of the engine bypass valve to the first engine bypass valve position.