Dual fuel common rail transient pressure control and engine using same

Patent metadata

Field	Value
Publication number	US-9518518-B2
Application number	US-201313866303-A
Country	US
Kind code	B2
Filing date	Apr 19, 2013
Priority date	Apr 19, 2013
Publication date	Dec 13, 2016
Grant date	Dec 13, 2016

Abstract

A compression ignition engine is fueled from common rail fuel injectors that predominately inject natural gas fuel that is compression ignited with a small pilot injection of liquid diesel fuel. Before and after a rapid load loss transient, the liquid and gaseous rail pressures are controlled toward respective pressures based upon engine speed and load. During the transient, the liquid rail pressure is controlled relative to the gas rail pressure in order to maintain the liquid rail pressure greater than the gas pressure during the transient to avoid migration gaseous fuel into the liquid fuel side of the system.

First claim

What is claimed is:

1. A method of operating an engine comprising the steps of:
injecting gaseous fuel and liquid fuel directly into an engine cylinder from a gaseous nozzle outlet set and a liquid nozzle outlet set, respectively, of a fuel injector;
compression igniting the injected liquid fuel to ignite the gaseous fuel;
inhibiting migration of gaseous fuel into liquid fuel within the fuel injector by maintaining a liquid rail pressure greater than a gas rail pressure;
the inhibiting step includes executing a first rail pressure control algorithm before and after a transient, and executing a second rail pressure control algorithm during the transient;
initiating the transient by changing from a high fuel demand state of a first speed and load to a low fuel demand state of a second speed and load.

2. The method of claim 1 wherein execution of the first rail pressure control algorithm includes:
controlling a liquid rail pressure toward a first predetermined target pressure based upon the first engine speed and load, and controlling a gaseous rail pressure toward a first gas pressure that is lower than the first predetermined pressure prior to the transient; and
controlling the liquid rail pressure toward a second predetermined target pressure based upon the second engine speed and load, and controlling the gaseous rail pressure toward a second gas pressure that is lower than the second predetermined pressure after the transient; and
execution of the second rail pressure control algorithm includes:
controlling the liquid rail pressure toward a transient target pressure that equals the gas rail pressure plus a bias pressure, and controlling the gaseous rail pressure toward the second gas pressure during the transient.

3. The method of claim 1 includes a step of closing a shut off valve fluidly positioned between a gaseous fuel rail and a gaseous fuel supply system during the transient.

4. The method of claim 1 including a step of injecting gaseous fuel and liquid fuel into less than all of a plurality of engine cylinders in at least one engine cycle during the transient.

5. The method of claim 1 wherein each liquid injection event during the transient corresponds to a predetermined minimum injection quantity; and
allocating a remainder of an engine fuel demand to injection of gaseous fuel during the transient.

6. The method of claim 1 including a step of avoiding venting gaseous fuel from a gaseous fuel rail to atmosphere during the transient.

7. The method of claim 6 wherein execution of the first rail pressure control algorithm includes:
controlling a liquid rail pressure toward a first predetermined target pressure based upon the first engine speed and load, and controlling gaseous rail pressure toward a first gas pressure that is lower than the first predetermined pressure prior to the transient; and
controlling the liquid rail pressure toward a second predetermined target pressure based upon the second engine speed and load, and controlling gaseous rail pressure toward a second gas pressure that is lower than the second predetermined pressure after the transient; and
execution of the second rail pressure control algorithm includes:
controlling the liquid rail pressure toward a transient target pressure that equals the gas rail pressure plus a bias pressure, and controlling the gaseous rail pressure toward the second gas pressure during the transient.

8. The method of claim 7 includes a step of closing a shut off valve fluidly positioned between a gaseous fuel rail and a gaseous fuel supply system during the transient.

9. The method of claim 7 including a step of injecting gaseous fuel and liquid fuel into less than all of a plurality of engine cylinders in at least one engine cycle during the transient.

10. The method of claim 7 wherein each liquid injection event during the transient corresponds to a predetermined minimum injection quantity; and
allocating a remainder of an engine fuel demand to injection of gaseous fuel during the transient.

11. An engine that comprising:
an engine housing that defines a plurality of cylinders within which a plurality of respective pistons reciprocate to define a compression ratio greater the 14:1;
a gaseous fuel common rail and a liquid fuel common rail fluidly connected to each of a plurality of fuel injectors that each include a gaseous nozzle outlet set and a liquid nozzle outlet set positioned for direct injection into one of the cylinders;
means, including electronic controller configured to execute a first rail pressure control algorithm to maintain a liquid rail pressure greater than a gas rail pressure before and after a transient, and execute a second rail pressure control algorithm to maintain the liquid rail pressure greater than the gas rail pressure during the transient, for inhibiting migration of gaseous fuel into liquid fuel within the fuel injector;
wherein the transient includes changing from a high fuel demand state of a first speed and load to a low fuel demand state of a second speed and load.

12. The engine of claim 11 wherein the first rail pressure control algorithm is configured to control the liquid rail pressure toward a first predetermined target pressure based upon the first engine speed and load, and control the gaseous rail pressure toward a first gas pressure that is lower than the first predetermined target pressure prior to the transient; and
configured to control the liquid rail pressure toward a second predetermined target pressure based upon the second engine speed and load, and control the gaseous rail pressure toward a second gas pressure that is lower than the second predetermined pressure after the transient; and
the second rail pressure control algorithm is configured to control the liquid rail pressure toward a transient target pressure that equals the gas rail pressure plus a bias pressure, and control the gaseous rail pressure toward the second gas pressure during the transient.

13. The engine of claim 11 includes a shut off valve fluidly positioned between a gaseous fuel rail and a gaseous fuel supply system.

14. The engine of claim 13 wherein the second pressure control algorithm is configured to close the shut off valve during the transient.

15. The engine of claim 11 wherein the second pressure control algorithm is configured to inject gaseous fuel and liquid fuel into less than all of a plurality of engine cylinders in at least one engine cycle during the transient.

16. The engine of claim 11 wherein the second pressure control algorithm is configured to avoid venting gas from a gaseous fuel rail to atmosphere during the transient.

17. The engine of claim 16 wherein the first rail pressure control algorithm is configured to control a liquid rail pressure toward a first predetermined target pressure based upon the first engine speed and load, and control a gaseous rail pressure toward a first gas pressure that is lower than the first predetermined pressure prior to the transient; and
configured to control the liquid rail pressure toward a second predetermined target pressure based upon the second engine speed and load, and control the gaseous rail pressure toward a second gas pressure that is lower than the second predetermined pressure after the transient; and
the second rail pressure control algorithm is configured to control the liquid rail pressure toward a transient target pressure that equals the gas rail pressure plus a bias pressure, and control the gaseous rail pressure toward the second gas pressure during the transient.

Assignees

• Caterpillar Inc
• Caterpillar Inc

Inventors

• Coldren Dana R
• Grant Steven Thomas
• Lombardi Frank
• Puckett Daniel R

Classifications

• F02D2200/0602

  Fuel pressure · CPC title

• F02D41/0025 Primary

  Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures · CPC title

• F02D2041/3881

  with multiple common rails, e.g. one rail per cylinder bank, or a high pressure rail and a low pressure rail · CPC title

• F02D19/061

  by controlling fuel injectors · CPC title

• F02D41/3836

  Controlling the fuel pressure · CPC title