Method and system for fuel control in a vehicle propulsion system
US-10161348-B1 · Dec 25, 2018 · US
US10508612B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10508612-B2 |
| Application number | US-201815934471-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 23, 2018 |
| Priority date | Mar 23, 2018 |
| Publication date | Dec 17, 2019 |
| Grant date | Dec 17, 2019 |
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Methods and systems are provided for an engine to infer fuel temperature from a measured rate of change in a pressure of a fuel passage between a low pressure fuel pump and a high pressure fuel pump during certain operating conditions, including when the low pressure fuel pump is switched off. The operation of the low pressure fuel pump may be adjusted responsively to a change in the inferred fuel temperature.
Opening claim text (preview).
The invention claimed is: 1. A method for an engine, comprising: adjusting operation of a low-pressure fuel pump based on a fuel temperature indicated from a rate of change in a pressure of a fuel passage between the low-pressure fuel pump and a high-pressure fuel pump during a first condition, including when the low pressure fuel pump is switched off. 2. The method of claim 1 , wherein indicating the fuel temperature from the rate of change in the fuel passage pressure includes inferring the fuel temperature without measuring a fuel system temperature with a temperature sensor. 3. The method of claim 2 , wherein the first condition further includes when the high pressure fuel pump is switched off. 4. The method of claim 3 , wherein the first condition further includes when the engine is operating in a decel-fuel-shut-off (DFSO) mode. 5. The method of claim 2 , wherein the first condition further includes when the high pressure fuel pump is switched on and the fuel passage pressure is between an upper threshold pressure and a lower threshold pressure. 6. The method of claim 5 , further comprising, switching on the low pressure fuel pump to raise the fuel passage pressure to the upper threshold pressure. 7. The method of claim 6 , further comprising, in response to the fuel passage pressure reaching the upper threshold pressure, switching off the low pressure fuel pump and pumping a threshold volume of fuel from the fuel passage with the high pressure fuel pump. 8. The method of claim 6 , further comprising, in response to the fuel passage pressure reaching the upper threshold pressure, switching off the low pressure fuel pump and pumping fuel from the fuel passage with the high pressure fuel pump for a threshold duration. 9. The method of claim 6 , further comprising, in response to the fuel passage pressure reaching the upper threshold pressure, switching off the low pressure fuel pump and pumping fuel from the fuel passage with the high pressure fuel pump until the fuel passage pressure decreases to a lower threshold pressure. 10. An engine system, comprising: a controller with computer readable instructions stored on non-transitory memory that when executed cause the controller to, measure a rate of change in a fuel passage pressure with a pressure sensor during a first condition, including when a low-pressure fuel pump (LPFP) is switched off, infer a fuel temperature from the rate of change in the fuel passage pressure, and adjust operation of the LPFP responsive to a change in the inferred fuel temperature. 11. The engine system of claim 10 , further comprising a temperature sensor, wherein the computer readable instructions causing the controller to infer the fuel temperature include measuring a cylinder head temperature with the temperature sensor. 12. The engine system of claim 10 , further comprising the LPFP, wherein the computer readable instructions causing the controller to adjust operation of the LPFP responsive to a change in the inferred fuel temperature include raising a lower threshold LPFP pressure responsive to a higher inferred fuel temperature and lowering the lower threshold LPFP pressure responsive to a lower inferred fuel temperature. 13. The engine system of claim 12 , wherein the computer readable instructions causing the controller to adjust operation of the LPFP responsive to a change in the inferred fuel temperature include reducing a threshold fuel volume pumped during pulsing of the LPFP above the lower threshold LPFP pressure prior to switching operation of the LPFP from the pulsed mode to the continuous mode. 14. The engine system of claim 13 , further comprising the pressure sensor and a high-pressure fuel pump (HPFP), wherein the pressure sensor is positioned in the fuel passage between the LPFP and the HPFP. 15. The engine system of claim 13 , further comprising the pressure sensor and a high-pressure fuel pump (HPFP), wherein the pressure sensor is positioned in a fuel rail downstream from the HPFP and the inferred fuel temperature corresponds to an inferred fuel rail temperature. 16. A method for an engine, comprising: determining a rate of change of pressure in a fuel passage pressure responsive to a high pressure fuel pump injecting a threshold volume of fuel to the engine while a low pressure fuel pump (LPFP) is off, inferring a fuel temperature from the rate of change in the fuel passage pressure, and adjusting a fuel injection rate to the engine responsive to a change in the inferred fuel temperature. 17. The method of claim 16 , further comprising, determining the rate of change in the fuel passage pressure responsive to trapping fuel in the fuel passage. 18. The method of claim 17 , wherein adjusting the fuel injection rate to the engine responsive to a change in the inferred fuel temperature includes increasing a LPFP pressure in response to a higher inferred fuel temperature, and lowering the LPFP pressure in response to a lower inferred fuel temperature. 19. The method of claim 18 , wherein trapping fuel in the fuel passage includes switching off the LPFP and the HPFP simultaneously. 20. The method of claim 19 , wherein adjusting the fuel injection rate to the engine responsive to a change in the inferred fuel temperature includes increasing power supplied to the low pressure fuel pump responsive to a decrease in the inferred fuel temperature.
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