Purge system for a dual-fuel engine

Patent metadata

Field	Value
Publication number	US-9732713-B2
Application number	US-201514684327-A
Country	US
Kind code	B2
Filing date	Apr 10, 2015
Priority date	Apr 10, 2015
Publication date	Aug 15, 2017
Grant date	Aug 15, 2017

Abstract

A fuel system for an engine has a cylinder with an inlet air port, an air box surrounding the inlet air port, and a gaseous fuel injector positioned in the air box and having a nozzle located at the inlet air port. The fuel system also has a gaseous fuel control valve, a fuel supply line fluidly extending from the gaseous fuel control valve to the gaseous fuel injector, a purge valve, and a purge fluid supply line fluidly extending from the purge valve to at least one of the fuel supply line and the gaseous fuel injector. The fuel system also has a return valve and a return line fluidly extending from at least one of the fuel supply line and the gaseous fuel injector.

First claim

What is claimed is:

1. A fuel system for an engine having a cylinder with an inlet air port, the fuel system comprising:
an air box surrounding the inlet air port;
a gaseous fuel injector positioned in the air box and having a nozzle located at the inlet air port;
a gaseous fuel control valve;
a fuel supply line fluidly extending from the gaseous fuel control valve to the gaseous fuel injector;
a purge valve fluidly coupled to a purge fluid supply;
a purge fluid supply line fluidly extending from the purge valve to at least one of the fuel supply line and the gaseous fuel injector;
a return valve fluidly coupled to an accumulator; and
a return line fluidly extending from at least one of the fuel supply line and the gaseous fuel injector to the return valve.

2. The fuel system of claim 1 , wherein the purge valve is an admittance valve enabling the purge fluid to flow from the supply of purge fluid into the at least one of the fuel supply line and the gaseous fuel injector.

3. The fuel system of claim 1 , further including a regulator coupled to the return valve.

4. The fuel system of claim 1 , further including a controller that opens the purge valve at about 1-5° of crank angle rotation before closing the gaseous fuel control valve.

5. The fuel system of claim 1 , further including a controller that keeps the return valve open throughout an engine cycle.

6. The fuel system of claim 1 , further including a controller that closes the purge valve at about 1-3° of crank angle rotation after the inlet air port closes.

7. The fuel system of claim 1 , further including a controller that closes the purge valve at about 1-3° of crank angle rotation after opening the return valve.

8. The fuel system of claim 1 , further including a controller that causes the return valve to remain at least partially open throughout an engine cycle.

9. The fuel system of claim 1 , further including a controller that opens the purge valve at about 231° of crank angle rotation after top dead center.

10. A method of directing gaseous fuel into an engine having a cylinder with an inlet air port, the method comprising:
supplying gaseous fuel from a gaseous fuel storage tank through a gaseous fuel control valve to a fuel supply line;
controlling a gaseous fuel injector to inject the gaseous fuel from the fuel supply line through the inlet air port into the cylinder;
supplying a purge fluid from a purge fluid supply through a purge valve and a purge fluid supply line to displace residual gaseous fuel in at least one of the supply line and the gaseous fuel injector at a conclusion of an injection event; and
maintaining a negative pressure differential between at least one of the fuel supply line and the gaseous fuel injector and a return line to draw the residual gaseous fuel through the return line and a return valve to an accumulator.

11. The method of claim 10 , wherein supplying the purge fluid includes supplying the purge fluid at about 1-5° of crank angle rotation before controlling the gaseous fluid injector to stop injecting the gaseous fuel.

12. The method of claim 10 , further including controlling the purge valve to close about 1-3° of crank angle rotation after the inlet air port closes.

13. The method of claim 12 , further including controlling the return valve to open at about the same time that the inlet air port closes.

14. The method of claim 10 , further including accumulating residual gaseous fuel vacuumed through the return valve.

15. The method of claim 14 , further including supplying the accumulated residual gaseous fuel from an accumulator to the fuel supply line.

16. The method of claim 10 , wherein supplying the purge fluid includes supplying a volume of the purge fluid approximately equal to a volume of the supply line.

17. The method of claim 10 , wherein supplying the purge fluid includes supplying a volume of the purge fluid approximately equal to a volume of the gaseous fuel injector.

18. The method of claim 10 , further including controlling the purge valve to close at about the same time that the inlet air port closes.

19. The method of claim 9 , further including controlling the purge valve to close at about 1-3° of crank angle rotation after causing the return valve to open.

20. A fuel system, comprising:
an engine block defining a plurality of cylinders;
an air box connected to a side of the engine block;
a cylinder liner disposed in each of the plurality of cylinders and having a plurality of radially located air intake ports;
a gaseous fuel injector positioned in the air box and having a nozzle located at a first air intake port of the plurality of air intake ports and configured to inject gaseous fuel radially through the first air intake port;
a gaseous fluid control valve fluidly coupled to the gaseous fuel injector;
a supply line fluidly extending from the gaseous fluid control valve to the gaseous fluid injector;
a purge valve fluidly coupled to a purge fluid supply;
a purge fluid supply line fluidly extending from the purge valve to the supply line, the gaseous fluid injector, or both;
a return valve fluidly coupled to an accumulator; and
a return line fluidly extending from the supply line, the gaseous fluid injector, or both to the return valve.

Assignees

• Electro Motive Diesel Inc

Inventors

• Bandyopadhyay Deep
• Devani Farhan F
• Timmons John P
• Montgomery David T
• Foege Aaron G

Classifications

• F02D41/3047

  said means being a secondary injection of fuel · CPC title

• F02D2400/04

  Two-stroke combustion engines with electronic control · CPC title

• F02D19/0621

  Purging of the fuel system · CPC title

• F02M37/0052 Primary

  Details on the fuel return circuit; Arrangement of pressure regulators · CPC title

• F02M25/0854

  Details of the absorption canister · CPC title