Fuel system having multiple combustion modes

Patent metadata

Field	Value
Publication number	US-9695758-B2
Application number	US-201414511918-A
Country	US
Kind code	B2
Filing date	Oct 10, 2014
Priority date	Oct 10, 2014
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

A fuel system is disclosed that is capable of operating in multiple combustion modes. A method is also disclosed of operating a dual fuel engine in conjunction with the fuel system. The method may include detecting a performance parameter of gaseous fuel in the fuel system. The method may also include selecting a combustion mode from a plurality of combustion modes based on the performance parameter. The method may further include injecting gaseous fuel and liquid fuel into at least one cylinder of the engine according to an injection timing corresponding to the selected combustion mode.

First claim

What is claimed is:

1. A method of operating a dual fuel engine, comprising:
detecting a performance parameter of gaseous fuel in a fuel system;
selecting a combustion mode from a plurality of combustion modes based on the performance parameter,
wherein the plurality of combustion modes include a first mode in which the gaseous fuel is injected after the liquid fuel during a combustion cycle and at least one second mode in which the gaseous fuel is injected before the liquid fuel during a combustion cycle, and
wherein the first mode includes injecting the gaseous fuel at a time during the combustion cycle when a piston is between 15° before top dead center and 40° after top dead center; and

injecting gaseous fuel and liquid fuel into at least one cylinder of the engine according to an injection timing corresponding to the selected combustion mode.

2. The method of claim 1 , wherein a pressure of the gaseous fuel injected into the at least one cylinder in the first mode is greater than a pressure of the gaseous fuel injected into the at least one cylinder in the second mode.

3. The method of claim 1 , wherein the at least one second mode includes injecting the gaseous fuel at a time during the combustion cycle when the piston is between 180° before top dead center and 30° before top dead center.

4. The method of claim 1 , wherein the at least one second mode includes at least two modes including a first gas blending mode and a second gas blending mode.

5. The method of claim 4 , wherein:
the first gas blending mode includes injecting the gaseous fuel at a time during the combustion cycle when a piston is between 180° before top dead center and 100° before top dead center, and
the second gas blending mode includes injecting the gaseous fuel at a time during the combustion cycle when the piston is between 100° before top dead center and 30° before top dead center.

6. The method of claim 1 , wherein detecting the performance parameter includes measuring a pressure of the gaseous fuel.

7. The method of claim 6 , further including implementing the at least one second mode based on the pressure of the gaseous fuel being below a first threshold.

8. The method of claim 7 , wherein the at least one second mode includes a first blending mode and a second blending mode, and further including implementing the first blending mode if the pressure is below a second threshold and implementing the second blending mode if the pressure is above the second threshold.

9. The method of claim 7 , further including:
detecting a second performance parameter;
pressurizing the gaseous fuel based on the second performance parameter; and
implementing the first mode to inject the pressurized gaseous fuel.

10. The method of claim 9 , wherein detecting the second performance parameter includes detecting a temperature of the gaseous fuel.

11. A fuel system for a dual fuel engine, comprising:
at least one pump for receiving gaseous fuel from a tank;
a liquid fuel reservoir;
at least one fuel injector fluidly connected to the at least one pump and the liquid fuel reservoir and configured to inject the gaseous fuel and the liquid fuel into at least one cylinder of the engine;
a sensor configured to generate a signal indicative of a performance parameter of the gaseous fuel; and
a controller configured to:
select a combustion mode from a plurality of combustion modes based on the signal, and
control the at least one fuel injector to implement the selected combustion mode.

12. The fuel system of claim 11 , wherein the at least one fuel injector is a dual fuel injector with a first nozzle for injecting the gaseous fuel and a second nozzle for injecting the liquid fuel.

13. The fuel system of claim 12 , wherein the at least one fuel injector is configured to use a pressure of the liquid fuel to open and close a valve that delivers the gaseous fuel to the first nozzle.

14. The fuel system of claim 11 , wherein the plurality of combustion modes include a first mode in which the gaseous fuel is injected after the liquid fuel during a combustion cycle and at least one second mode in which the gaseous fuel is injected before the liquid fuel during a combustion cycle.

15. The fuel system of claim 14 , wherein the sensor is a pressure sensor and the performance parameter is a pressure of the gaseous fuel.

16. The fuel system of claim 15 , further including a gaseous fuel rail connected between the at least one pump and the at least one fuel injector, and the performance parameter is a pressure of gaseous fuel in the gaseous fuel rail.

17. The fuel system of claim 15 , further including a temperature sensor configured to generate a signal indicative of a temperature of the gaseous fuel, and wherein the controller is configured to:
implement the at least one second mode based on the pressure of the gaseous fuel being below a first threshold;
pressurize the gaseous fuel when the temperature decreases below a second threshold; and
implement the first mode when the pressure increases above the first threshold.

18. A train consist, comprising:
a tender car including a tank configured to store liquefied gaseous fuel;
a locomotive including a dual fuel engine having a plurality of cylinders; and
a fuel system, the fuel system comprising:
the tank;
a low pressure pump fluidly connected to the tank;
a high pressure pump fluidly connected to the low pressure pump and configured to pressurize the liquefied gaseous fuel;
a vaporizer fluidly connected to the high pressure pump and configured to convert the liquefied gaseous fuel to a supercritical gas;
a liquid fuel reservoir;
an injection system configured to inject the gaseous fuel and the liquid fuel into the plurality of cylinders; and
a control system configured to:
detect a pressure of the gaseous fuel;
compare the pressure of the gaseous fuel to a threshold;
implement a first mode in which the gaseous fuel is injected after the liquid fuel during a combustion cycle when the pressure of the gaseous fuel is less than the first threshold, and
implement a second mode in which the gaseous fuel is injected before the liquid fuel during a combustion cycle when the pressure of the gaseous fuel is greater than the first threshold.

Assignees

• Caterpillar Inc
• Caterpillar Inc

Inventors

• Coldren Dana Ray
• Steffen Joshua Wayne
• Campion Robert Michael

Classifications

• F02D41/3017

  characterised by the mode(s) being used · CPC title

• F02M43/00

  Fuel-injection apparatus operating simultaneously on two or more fuels, or on a liquid fuel and another liquid, e.g. the other liquid being an anti-knock additive · CPC title

• F02D19/061

  by controlling fuel injectors · CPC title

• B61C17/02

  Bunkers; Tanks; Tenders (coachwork B61D); Water or fuel pick-up or scoop apparatus; Water or fuel supply fittings (trackside installations, e.g. bunkers, tanks, for filling locomotives with sand or water B61K11/00) · CPC title

• Y02T10/36

  Cross-Sectional Technologies · mapped topic