초록 ▼

A method for operating a turbocharged engine is disclosed. In one example, during a first condition an engine operation is adjusted in response to a turbocharger expansion ratio exceeding a first limit and during a second condition an engine operation is adjusted in response to the turbocharger expa

A method for operating a turbocharged engine is disclosed. In one example, during a first condition an engine operation is adjusted in response to a turbocharger expansion ratio exceeding a first limit and during a second condition an engine operation is adjusted in response to the turbocharger expansion ratio exceeding a second limit that differs from the first limit. Degradation of the engine may be reduced under some engine operating conditions by adjusting engine operation in response to the turbocharger expansion ratio.

대표청구항 ▼

1. An engine operating method, comprising: direct injecting fuel to an engine with a turbocharger;during a first condition, adjusting engine operation in response to a turbine expansion ratio exceeding a first turbine expansion ratio limit of the turbocharger; andduring a second condition, adjusting

1. An engine operating method, comprising: direct injecting fuel to an engine with a turbocharger;during a first condition, adjusting engine operation in response to a turbine expansion ratio exceeding a first turbine expansion ratio limit of the turbocharger; andduring a second condition, adjusting engine operation in response to a turbine expansion ratio exceeding a second turbine expansion ratio limit of the turbocharger that differs from the first turbine expansion ratio limit. 2. The engine operating method of claim 1, further comprising delaying a particulate filter regeneration at a higher altitude until the engine is at a lower altitude. 3. The engine operating method of claim 1, wherein different turbine expansion ratio limits are selected for different exhaust gas flow rates. 4. The engine operating method of claim 1, further comprising limiting or modifying regeneration of a particulate filter in response to a turbine expansion ratio exceeding one of the turbine expansion ratio limits. 5. The engine operating method of claim 1, where the first turbine expansion ratio limit and the second turbine expansion ratio limit vary in response to an exhaust gas flow rate. 6. The engine operating method of claim 1, where the second turbine expansion ratio limit is less than the first turbine expansion ratio limit for a given exhaust gas flow rate. 7. The engine operating method of claim 1, where the adjusting operation of the engine includes reducing an available amount of engine torque to limit the turbine expansion ratio. 8. The engine operating method of claim 1, where the adjusting operation of the engine includes adjusting an actuator to limit the turbine expansion ratio. 9. The engine operating method of claim 1, where the adjusting operation of the engine includes setting a desired boost level to an actual boost level, and maintaining the desired boost level at the actual boost level until the turbine expansion ratio is reduced below a limit. 10. The engine operating method of claim 1, where the first condition is a steady state condition and the second condition is a transient condition, and wherein the turbocharger includes a turbine coupled to a compressor via a shaft. 11. The engine operating method of claim 10, where the engine operates in the transient condition when a rate of change of engine speed and a fuel amount is greater than a threshold level. 12. An engine operating method, comprising: operating an engine with a turbocharger and a direct fuel injector;during a steady state condition, adjusting operation of the engine in response to a turbine expansion ratio exceeding a first turbine expansion ratio limit of the turbocharger;during a transient condition, adjusting operation of the engine in response to a turbine expansion ratio exceeding a second turbine expansion ratio limit of the turbocharger that is less than the first turbine expansion ratio limit for a given exhaust gas flow rate; anddelaying a particulate filter regeneration based on altitude. 13. The engine operating method of claim 12, wherein the first turbine expansion ratio limit and the second turbine expansion ratio limit vary in response to an exhaust gas flow rate, and where the adjusting operation of the engine includes reducing an available amount of engine torque to limit the turbine expansion ratio. 14. The engine operating method of claim 12, where the adjusting operation of the engine includes adjusting an actuator to limit the turbine expansion ratio. 15. The engine operating method of claim 12, where the adjusting operation of the engine includes setting a desired boost level to an actual boost level, and maintaining the desired boost level at the actual boost level until the turbine expansion ratio is reduced below a limit. 16. The engine operating method of claim 12, where the adjusting operation of the engine includes reducing an available amount of torque output of the engine in response to the turbine expansion ratio exceeding the turbine expansion ratio limit. 17. An engine system, comprising: an engine having a turbocharger;a direct fuel injector coupled to a cylinder of the engine; anda controller, the controller including instructions for, during a steady state mode, adjusting operation of the engine in response to a turbine expansion ratio of the turbocharger exceeding a first turbine expansion ratio limit, and during a transient mode, adjusting operation of the engine in response to a turbine expansion ratio of the turbocharger exceeding a second turbine expansion ratio limit that is less than the first turbine expansion ratio limit for a given exhaust gas flow rate. 18. The engine system of claim 17, where the controller includes further instructions for limiting an amount of fuel injected in response to the turbine expansion ratio exceeding the turbine expansion ratio limit. 19. The engine system of claim 17, wherein the first turbine expansion ratio limit and the second turbine expansion ratio limit vary in response to an exhaust gas flow rate, and where the adjusting operation of the engine includes setting a desired boost level to an actual boost level, and maintaining the desired boost level at the actual boost level until the turbine expansion ratio is reduced below a limit. 20. The engine system of claim 19, where the turbocharger is a variable geometry turbocharger, and where the boost level is adjusted by adjusting a vane position of the variable geometry turbocharger.