Gas turbine engine dump valve

• US 4,016,716 A
• Filed: 04/20/1970
• Issued: 04/12/1977
• Est. Priority Date: 04/20/1970
• Status: Expired due to Term

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Americas Company (Caterpillar Incorporated)
• Inventors: Evans, Duane E., Tyler, David A., Tabor, Thomas M.
• Primary Examiner(s): Gordon, Clarence R.
• Application Number:
  US05/030,081
• Time in Patent Office: 2,549 Days
• Field of Search: 60/39.28, 60/39.09, 137/107, 137/117
• US Class Current: 60/39.091
• 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: F02G 3/00 Combustion-product positive-displacement engine plants
• CPC Class Codes: F05D 2260/602 Drainage
• CPC Class Codes: Y10T 137/2557 Waste responsive to flow stoppage

Abstract

A valve actuated in response to a drop in fuel pressure across a fuel supply valve that will drain the fuel from a fuel line but not leak when exposed to high fuel pressures during normal operation. The dump valve is particularly applicable to the draining of fuel from a gas turbine engine fuel nozzle line after shutoff of the engine fuel supply valve.

Claims

1. A fuel system for a gas turbine engine comprising a fuel supply, fuel metering means, pump means connecting said supply to said metering means, a fuel supply valve including an inlet port and an outlet port, said valve operable to selectively open or close communication between said inlet and outlet ports, a nozzle for introducing fuel to a combustion chamber, a fuel line connecting said metering means to said inlet port, a second fuel line connecting said outlet port to said nozzle, and a dump valve, said dump valve comprising a body having drain, inlet, and pilot ports and a valve seat circumscribing an opening communicating said inlet and drain ports of said dump valve, a spool slidably mounted in said body and having a valve tip engagable with said seat, means spring loading said spool to normally resiliently engage said tip with said seat, means communicating said inlet and pilot ports of said dump valve with said first and second opposed faces of said spool to expose same to pressures at said inlet and pilot ports of said dump valve, said first face being disposed such that force due to pressure acting thereon is directed to aid the force of the spring loading means, said second face being disposed such that force due to pressure acting thereon is directed to oppose the force of said spring loading means, and means connecting said pilot and inlet ports of said dump valve to said inlet and outlet ports of said supply valve.

2. A fuel supply system according to claim 1, further defined by said seat being a recess and said tip being bevelled to mate with the seat recess.

3. A fuel supply system according to claim 1, further defined by said body having a bore extending therethrough, said bore stepped intermediate its length whereby one end portion is of enlarged diameter and the other end portion is of reduced diameter, said seat disposed in the reduced portion of said bore, means defining said drain port in the outer end of said reduced portion of said bore, said inlet port of said dump valve communicating with said reduced portion of said bore at a point adjacent said seat on the opposite side thereof from said drain port, said spool having an enlarged central portion sealingly slidably engagable with the wall of said enlarged portion of said bore, the opposite faces of said central portion of said spool being said first and second opposed faces of said spool, said central portion of said spool dividing said enlarged portion of said bore into first and second chambers respectively communicating with said first and second spool faces, said central portion of said spool inwardly stepped at said first face to define a stem projecting coaxially of said first chamber, said central portion inwardly stepped at said second face to define a reduced portion projecting coaxially of said second chamber and through said reduced portion of said bore in sealing sliding engagement with the wall thereof, the end of said reduced portion of said stem defining said valve tip, said spring loading means being a spring disposed coaxially about said stem and acting between a head wall at the outer end of said enlarged portion of said bore and said first face, said dump valve pilot port communicating with said second chamber, and said body having a passage communicating said dump valve inlet port and said first chamber.

4. A fuel supply system according to claim 3, further defined by said passage having an orifice adjacent its point of communication with said first chamber.

5. A fuel supply system according to claim 3, further defined by said seat being a recess and said tip being bevelled to mate with said seat recess.

6. A fuel supply system according to claim 5, further defined by said passage having an orifice adjacent its point of communication with said first chamber.

7. A fuel supply system according to claim 1, further defined by said supply valve having a second outlet port, said supply valve being operable to individually selectively communicate said first and second outlet ports thereof with said inlet port thereof, and a line including a restrictor connecting said second outlet port of said supply valve to the inlet side of said pump means.

8. A fuel supply system according to claim 7, further defined by said seat being a recess and said tip being bevelled to mate with said seat recess.

9. A fuel supply system according to claim 3, further defined by said supply valve having a second outlet port, said supply valve being operable to individually selectively communicate said first and second outlet ports thereof with said inlet port thereof, and a line including a restrictor connecting said second outlet port of said supply valve to the inlet side of said pump means.

10. A fuel supply system according to claim 9, further defined by said passage having an orifice adjacent its point of communication with said first chamber.

11. A fuel supply system according to claim 9, further defined by said seat being a recess and said tip being bevelled to mate with said seat recess.