Liquid fuel reverse purge

• US 6,536,217 B2
• Filed: 12/20/2000
• Issued: 03/25/2003
• Est. Priority Date: 12/20/2000
• Status: Expired due to Fees

• Current Assignee: Honeywell Space Systems Incorporated
• Original Assignee: Honeywell Space Systems Incorporated
• Inventors: Lipinski, John, Rodriguez, Fredd, Fukumoto, Paul, Schott, David K.
• Primary Examiner(s): KIM, TAE JUN
• Application Number:
  US09/742,207
• Publication Number:
  US 20020073687A1
• Time in Patent Office: 825 Days
• Field of Search: 60/390.94, 607/72, 417/291, 417/326
• US Class Current: 60/772
• CPC Class Codes: F02C 7/232 Fuel valves control of fuel supply by means of fuel metering valves F02C9/263; Draining valves or systems valves in general F16K
• CPC Class Codes: F05D 2260/602 Drainage

Abstract

Devices and methods for liquid fuel reverse purge on shutdown of turbines are provided. The device and method may utilize a liquid fuel reverse purge control system that includes an induction motor associated with a pump, together with fuel system solenoid valves, an electronic control unit and associated software logic. The device and method may alternative utilize a liquid fuel valve manifold including an assembly for mechanical reverse purging of liquid fuel from the atomizer fuel manifold and supply lines thereto, optionally together with an assembly for controlling the flow of the reverse-purged fuel through a re-circulation circuit used to preheat fuel prior to system start-up under cold conditions.

Claims

1. A liquid fuel reverse purge control system for purging a turbine fuel manifold on shutdown of a turbine, the system comprising:

a reversible fuel pump for pressurizing fuel from a fuel supply;

a fuel manifold in fluidic connection with the reversible fuel pump;

at least one solenoid-controlled shutoff valve located in fluidic connection between the reversible fuel pump and the fuel manifold; and

an electronic control unit and associated software logic, which electronic control unit is in electronic contact with the reversible fuel pump and the at least one solenoid-controlled shutoff valve, so that on system shutdown the electronic control unit and associated software logic commands the reversible fuel pump to reverse the direction of pumping for a set period of time to purge residual fuel from the fuel manifold, and after such set period of time commands the at least one solenoid-controlled shutoff valve to close.

2. The system of claim 1 wherein the electronic control unit and associated software logic commands the reversible fuel pump to reverse the direction of pumping within approximately ten seconds of system shutdown.

3. The system of claim 2 wherein the electronic control unit and associated software logic commands the reversible fuel pump to reverse the direction of pumping within approximately one second of system shutdown.

4. The system of claim 1 wherein the electronic control unit and associated software logic commands the reversible fuel pump to reverse the direction of pumping for a set period of time sufficient to reverse purge all fuel downstream from the reversible fuel pump.

5. The system of claim 1 wherein the electronic control unit and associated software logic commands the reversible fuel pump to reverse the direction of pumping for a set period of time sufficient to reverse purge a volume of fuel equal to at least about 0.8 cubic inches.

6. The system of claim 1, wherein after the at least one solenoid-controlled shutoff valve is commanded to close all fuel has been purged between the at least one solenoid-controlled shutoff valve and the fuel manifold.

7. The system of claim 1, wherein the fuel manifold further comprises an atomizer.

8. A method for purging a turbine fuel manifold on shutdown of a turbine, the system comprising a reversible fuel pump for pressurizing fuel from a fuel supply, a fuel manifold in fluidic connection with the reversible fuel pump, at least one solenoid-controlled shutoff valve located in fluidic connection between the reversible fuel pump and the fuel manifold, and an electronic control unit and associated software logic, which electronic control unit is in electronic contact with the reversible fuel pump and the at least one solenoid-controlled shutoff valve, comprising:

commanding the reversible fuel pump to reverse the direction of pumping for a set period of time to purge residual fuel from the fuel manifold; and

after the set period of time, commanding the at least one solenoid-controlled shutoff valve to close.

9. The method according to claim 8, wherein said set period of time is sufficient to reverse purge all fuel downstream from the reversible fuel pump.

10. The method according to claim 8, wherein said reverse pumping occurs within about 10 seconds of system shutdown.

11. The method according to claim 10, wherein said reverse pumping occurs within about 1 second of system shutdown.

12. A liquid fuel reverse purge control system for purging a turbine fuel manifold on shutdown of a turbine, the system comprising:

a reversible fuel pump for pressurizing fuel from a fuel supply;

an atomizer fuel manifold in fluidic connection with the reversible fuel pump, said atomizer fuel manifold delivering fuel to said turbine during normal operation;

at least one solenoid-controlled shutoff valve located in fluidic connection between the reversible fuel pump and the fuel manifold; and

an electronic control unit and associated software logic, which electronic control unit is in electronic contact with the reversible fuel pump and the at least one solenoid-controlled shutoff valve, so that within ten seconds of system shutdown the electronic control unit and associated software logic commands the reversible fuel pump to reverse the direction of pumping for a set period of time to purge residual fuel from the fuel manifold, and after such set period of time commands the at least one solenoid-controlled shutoff valve to close.