SYSTEM FOR CONTROLLING AN AIR HANDLING SYSTEM INCLUDING A DUAL-STAGE VARIABLE GEOMETRY TURBOCHARGER

• US 20130074492A1
• Filed: 09/25/2011
• Published: 03/28/2013
• Est. Priority Date: 09/25/2011
• Status: Active Grant

• Current Assignee: Cummins Incorporated
• Original Assignee: Cummins Incorporated
• Inventors: Mulloy, John M., Popuri, Sriram S., Frazier, Timothy R., Books, Martin T., Brahma, Indranil, Wei, Xi, Rajamohan, Divakar, Chi, John N.
• Granted Patent: US 8,567,192 B2
• Time in Patent Office: Days
• US Class Current: 60/602
• CPC Class Codes: F02B 37/004 with exhaust drives arranged in series
• CPC Class Codes: F02B 37/013 with exhaust-driven pumps arranged in series
• CPC Class Codes: F02B 37/12 Control of the pumps
• CPC Class Codes: F02B 37/18 by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
• CPC Class Codes: F02D 2041/0017 by simultaneous control of throttle and exhaust gas recirculation
• CPC Class Codes: F02D 2041/141 using a feed-forward control element
• CPC Class Codes: F02D 2041/1433 using a model or simulation of the system
• CPC Class Codes: F02D 2200/0402 the parameter being determined by using a model of the engine intake or its components
• CPC Class Codes: F02D 2200/0406 Intake manifold pressure
• CPC Class Codes: F02D 2200/0414 Air temperature
• CPC Class Codes: F02D 2200/703 Atmospheric pressure
• CPC Class Codes: F02D 23/02 the engines being of fuel-injection type
• CPC Class Codes: F02D 41/0007 for control of turbo-charged or super-charged engines control of the pumps per se F02B37/12
• CPC Class Codes: F02D 41/0052 Feedback control of engine parameters, e.g. for control of air/fuel ratio or intake air amount
• CPC Class Codes: F02D 41/0072 Estimating, calculating or determining the EGR rate, amount or flow sensors in EGR systems F02M26/45
• CPC Class Codes: F02D 41/1401 characterised by the control or regulation method F02D41/1473, F02D41/1477 take precedence
• CPC Class Codes: F02D 41/1447 with determination means using an estimation
• CPC Class Codes: F02D 41/145 with determination means using an estimation
• CPC Class Codes: F02D 41/18 by measuring intake air flow
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies
• CPC Class Codes: Y02T 10/40 : Engine management systems

Abstract

A system is provided for controlling an air handling system for an internal combustion engine. A dual-stage turbocharger includes a high-pressure compressor and variable geometry turbine combination fluidly coupled to a low-pressure compressor and variable geometry turbine combination. A control circuit includes a memory having instructions stored therein that are executable by the control circuit to determine a target low-pressure compressor ratio, a target high-pressure compressor ratio, a target high-pressure compressor inlet temperature and a target high-pressure compressor inlet pressure as a function of a target outlet pressure of the high-pressure compressor and a temperature, a pressure and a target flow rate of air entering the air inlet of the low-pressure compressor, and to control the geometries of the low-pressure and high-pressure turbines as a function of the target low-pressure compressor ratio the target high-pressure compressor ratio respectively.

Claims

1. An air handling system for an internal combustion engine, comprising:

a dual stage turbocharger including a high-pressure turbine having an exhaust gas inlet fluidly coupled to an exhaust manifold of the engine and an exhaust gas outlet, and a low-pressure turbine having an exhaust gas inlet fluidly coupled to the exhaust gas outlet of the high-pressure turbine and an exhaust gas outlet fluidly coupled to ambient,

a turbine bypass passageway having one end fluidly coupled to the exhaust gas inlet of the high-pressure turbine and an opposite end fluidly coupled to the exhaust gas outlet of the high-pressure turbine,

a turbine bypass throttle disposed in-line with the turbine bypass passageway, the turbine bypass throttle controllable between fully closed and fully open positions to control a flow of exhaust gas through the turbine bypass passageway, and

a control circuit including a memory having instructions stored therein that are executable by the control circuit to determine a turbine bypass control signal as a function of a target flow rate of exhaust gas through the turbine bypass throttle, a target temperature of the exhaust manifold and a target outlet temperature of the high pressure turbine, and to control a position of the turbine bypass throttle between the fully closed and fully open positions using the turbine bypass control signal to selectively divert exhaust gas flow from the exhaust manifold away from the exhaust gas inlet of the high-pressure turbine.

2. The air handling system of claim 1 wherein the instructions stored in the memory further include instructions executable by the control circuit to determine the target flow rate of exhaust gas through the turbine bypass throttle as a function of a speed error corresponding to a difference between a target and an actual or estimated rotational speed of the high pressure turbine, a target flow rate of fresh air flow into the turbocharger and a target fuel rate of the engine.

3. The air handling system of claim 2 wherein the instructions stored in the memory further include instructions executable by the control circuit to determine the turbine bypass control signal further as a function of a target pressure within the exhaust manifold and a target outlet pressure of the high pressure turbine.

4. The air handling system of claim 3 wherein the instructions stored in the memory further include instructions executable by the control circuit to determine the turbine bypass control signal by computing a target flow orifice size of the turbine bypass throttle as a function of the target flow rate of exhaust gas through the turbine bypass throttle, the target temperature of the exhaust manifold, the target outlet temperature of the high pressure turbine, the target pressure within the exhaust manifold and the target outlet pressure of the high pressure turbine, and to TBVFR, (EMT +HPTOTT)/2, MIN(1, HPTOPT/EMP) and MAX(1, EMP), and then converting the target flow orifice size of the turbine bypass throttle to the turbine bypass control signal.

5. The air handling system of claim 1 wherein the instructions stored in the memory further include instructions executable by the control circuit to determine the turbine bypass control signal further as a function of a target pressure within the exhaust manifold and a target outlet pressure of the high pressure turbine.

6. An air handling system for an internal combustion engine, comprising:

a dual stage turbocharger including a low-pressure compressor rotatably coupled to a low-pressure variable geometry turbine, the low-pressure compressor having an air inlet fluidly coupled to ambient and an air outlet, and a high-pressure compressor rotatably coupled to a high-pressure variable geometry turbine, the high-pressure compressor having an air inlet fluidly coupled to the air outlet of the low-pressure compressor and an air outlet fluidly coupled to an intake manifold of the engine,

a low-pressure turbine actuator responsive to a low-pressure variable geometry turbine control signal to control a geometry of the low-pressure variable geometry turbine,

a high-pressure turbine actuator responsive to a high-pressure variable geometry turbine control signal to control a geometry of the high-pressure variable geometry turbine, and

a control circuit including a memory having instructions stored therein that are executable by the control circuit to determine a target low-pressure compressor ratio, a target high-pressure compressor ratio, a target high-pressure compressor inlet temperature and a target high-pressure compressor inlet pressure as a function of a target outlet pressure of the high-pressure compressor and a temperature, a pressure and a target flow rate of air entering the air inlet of the low-pressure compressor, to produce the low-pressure variable geometry turbine control signal as a function of the target low-pressure compressor ratio and to produce the high-pressure variable geometry control signal as a function of the target high-pressure compressor ratio, the target high-pressure compressor inlet temperature and a target high-pressure compressor inlet pressure.

7. The air handling system of claim 6 wherein the instructidns stored in the memory further include instructions executable by the control circuit to determine an initial target low-pressure compressor ratio and a target low-pressure compressor outlet temperature as a function of the target flow rate, temperature and pressure of air entering the air inlet of the low-pressure compressor, to compute an unadjusted high-pressure compressor ratio target as a function of the target outlet pressure of the high-pressure compressor, the initial target low-pressure compressor ratio and the pressure of air entering the air inlet of the low-pressure compressor, to compute a temperature-based high-pressure compressor ratio target as a function of the target low-pressure compressor outlet temperature, and to determine the target low-pressure compressor ratio to be the initial target low-pressure compressor ratio if the temperature-based high-pressure compressor ratio target is equal to the unadjusted high-pressure compressor ratio target.

8. The air handling system of claim 7 wherein the instructions stored in the memory further include instructions executable by the control circuit to correct the target low-pressure compressor ratio for altitude as a function of ambient pressure to which the engine is exposed.

9. The air handling system of claim 7 wherein the instructions stored in the memory further includes instructions executable by the control circuit to determine the target high-pressure compressor ratio to be the temperature-based high-pressure compressor ratio target.

10. The air handling system of claim 7 wherein the instructions stored in the memory further include instructions executable by the control circuit to compute a modified target low-pressure compressor ratio target as a function of the temperature-based high-pressure compressor ratio target, the target high-pressure compressor outlet pressure and the pressure of air entering the air inlet of the low-pressure compressor, and to determine the target low-pressure compressor ratio to be the modified target low-pressure compressor ratio if the temperature-based high-pressure compressor ratio target is not equal to the unadjusted high-pressure compressor ratio target.

11. The air handling system of claim 10 wherein the instructions stored in the memory further include instructions executable by the control circuit to correct the target low-pressure compressor ratio for altitude as a function of ambient pressure to which the engine is exposed.

12. The air handling system of claim 10 wherein the instructions stored in the memory further includes instructions executable by the control circuit to determine the target high-pressure compressor ratio to be the temperature-based high-pressure compressor ratio target.

13. The air handling system of claim 6 further comprising an inter-stage cooler interposed between and fluidly coupled to the air outlet of the low-pressure compressor and the air inlet of the high-pressure compressor.

14. The air handling system of claim 13 wherein the instructions stored in the memory further include instructions executable by the control circuit to determine an initial target low-pressure compressor ratio and a target low-pressure compressor outlet temperature as a function of the target flow rate, temperature and pressure of air entering the air inlet of the low-pressure compressor, to determine a target pressure ratio and a target outlet temperature of the inter-stage cooler as a function of the initial target low-pressure compressor ratio, the target low-pressure compressor outlet temperature, the target flow rate and pressure of air entering the inlet of the low-pressure compressor, to compute an unadjusted high-pressure compressor ratio target as a function of the target outlet pressure of the high-pressure compressor, the initial target low-pressure compressor ratio, the target pressure ratio of the inter-stage cooler and the pressure of air entering the air inlet of the low-pressure compressor, to compute a temperature-based high-pressure compressor ratio target as a function of the target outlet temperature of the inter-stage cooler, and to determine the target low-pressure compressor ratio to be the initial target low-pressure compressor ratio if the temperature-based high-pressure compressor ratio target is equal to the unadjusted high-pressure compressor ratio target.

15. The air handling system of claim 14 wherein the instructions stored in the memory further include instructions executable by the control circuit to correct the target low-pressure compressor ratio for altitude as a function of ambient pressure to which the engine is exposed.

16. The air handling system of claim 14 wherein the instructions stored in the memory further includes instructions executable by the control circuit to determine the target high-pressure compressor ratio to be the temperature-based high-pressure compressor ratio target.

17. The air handling system of claim 14 wherein the instructions stored in the memory further include instructions executable by the control circuit to compute a modified target low-pressure compressor ratio target as a function of the temperature-based high-pressure compressor ratio target, the target high-pressure compressor outlet pressure, the pressure of air entering the air inlet of the low-pressure compressor and the target pressure ratio of the inter-stage cooler, and to determine the target low-pressure compressor ratio to be the modified target low-pressure compressor ratio if the temperature-based high-pressure compressor ratio target is not equal to the unadjusted high-pressure compressor ratio target.

18. The air handling system of claim 17 wherein the instructions stored in the memory further include instructions executable by the control circuit to correct the target low-pressure compressor ratio for altitude as a function of ambient pressure to which the engine is exposed.

19. The air handling system of claim 17 wherein the instructions stored in the memory further includes instructions executable by the control circuit to determine the target high-pressure compressor ratio to be the temperature-based high-pressure compressor ratio target.

20. The air handling system of claim 14 wherein the instructions stored in the memory further include instructions executable by the control circuit to determine the target outlet temperature of the inter-stage cooler as a function of the target low-pressure compressor outlet temperature, the target flow rate of air entering the inlet of the low-pressure compressor and ambient temperature to which the engine is exposed.