초록

An embodiment of the present invention takes the form of a system that uses exhaust from the combustion turbine engine to heat the fuel gas consumed by a combustion turbine engine. The benefits of the present invention include reducing the need to use a parasitic load to heat the fuel gas.

대표청구항 ▼

1. A system comprising: a combustion turbine engine that operatively discharges an exhaust stream;a stack fluidly connected to a downstream section of the combustion turbine engine; wherein the stack comprises: an opening through which some of the exhaust stream discharges into atmosphere;a stack pe

1. A system comprising: a combustion turbine engine that operatively discharges an exhaust stream;a stack fluidly connected to a downstream section of the combustion turbine engine; wherein the stack comprises: an opening through which some of the exhaust stream discharges into atmosphere;a stack penetration integrated with the stack, wherein the stack penetration directs an exhaust stream portion away from the opening;a stack return integrated with the stack, wherein the stack returns the exhaust stream portion to the stack;a heat exchanger fluidly connected downstream of the stack penetration, wherein the heat exchanger comprises an exhaust inlet port that receives the exhaust stream portion originating at the stack penetration, and an exhaust outlet port that discharges the exhaust stream portion to the stack;an exhaust flow circuit fluidly connected between the stack and the heat exchanger; wherein the exhaust flow circuit comprises: an exhaust supply path comprising: a first end integrated with a discharge of the stack penetration; a bypass valve located downstream of the first end, and a second end connected to the exhaust inlet port of the heat exchanger;an exhaust return path comprising: a first end connected to the stack return, and a second end connected to the exhaust outlet port of the heat exchanger;a fuel gas flow circuit fluidly connected to the heat exchanger; the fuel gas flow circuit comprising: a fuel supply path comprising: a supply end integrated with a fuel gas supply system; and a discharge end connected to a fuel inlet port of the heat exchanger; anda fuel return path comprising: a first end connected to a fuel outlet port of the heat exchanger; and a second end connected to a fuel system; andwherein the heat exchanger operatively transfers heat from the exhaust stream portion, flowing through the exhaust flow circuit; to fuel gas, flowing through the fuel gas flow circuit. 2. The system of claim 1, wherein the exhaust return path comprises an isolation valve located between the first end and the second end. 3. The system of claim 2 further comprising an exhaust bypass circuit that fluidly connects the exhaust supply path and the exhaust return path. 4. The system of claim 3 further comprising an exhaust bypass valve. 5. The system of claim 1, wherein the exhaust return path comprises a device that moves the exhaust stream portion from the exhaust outlet port to the stack return. 6. The system of claim 1 further comprising a cooling circuit connected between the stack penetration and the bypass valve of the exhaust supply path; wherein the cooling circuit comprise a fluid circulation device, which operatively supplies a cooling fluid to the exhaust supply path. 7. The system of claim 1 further comprising at least one temperature measuring device that measures a temperature of fluid within the exhaust supply path. 8. The system of claim 1 further comprising: at least one temperature measuring device that measures a temperature of fluid within the exhaust return path. 9. The system of claim 1 further comprising: at least one temperature control valve fluidly located within the fuel supply path. 10. The system of claim 1 further comprising a fuel bypass circuit that fluidly connects the fuel supply path and the fuel discharge path. 11. The system of claim 6 further comprising at least one temperature control valve fluidly located within the exhaust supply path. 12. The system of claim 1 further comprising at least one temperature measuring device that measures a temperature of fuel within the fuel discharge path. 13. The system of claim 1 further comprising an alternate stack fluidly integrated with the exhaust return path. 14. The system of claim 13, wherein the alternate stack discharges the exhaust stream portion received from the exhaust return path. 15. A system comprising: a gas turbine comprising: an inlet section, a compressor section, a combustion section, and an exhaust section that operatively discharges an exhaust stream;a stack fluidly connected to a downstream section of the exhaust section;wherein the stack comprises: an opening through which some of the exhaust stream discharges into atmosphere;a stack penetration integrated with the stack, wherein the stack penetration directs an exhaust stream portion away from the opening;a stack return integrated with the stack, wherein the stack return directs the exhaust stream portion to the stack;a fuel gas heater fluidly connected downstream of the stack penetration, wherein the fuel gas heater comprises an exhaust inlet port that receives the exhaust stream portion originating at the stack penetration, and an exhaust outlet port that discharges the exhaust stream portion to the stack;an exhaust flow circuit fluidly connected between the stack and the fuel gas heater; wherein the exhaust flow circuit comprises: an exhaust supply path comprising: a first end integrated with a discharge of the stack penetration; a bypass valve located downstream of the upstream end, and a second end connected to the exhaust inlet port of the fuel gas heater;an exhaust return path comprising: a first end connected to the stack return, a second end connected to the exhaust outlet port of the fuel gas heater, and a blower that drives the exhaust stream portion from the exhaust outlet port to the stack return;a fuel gas flow circuit fluidly connected to the fuel gas heater; the fuel gas flow circuit comprising: a fuel supply path comprising: a supply end integrated with a fuel gas supply system; and a discharge end connected to a fuel inlet port of the fuel gas heater; anda fuel discharge path comprising: a first end connected to a fuel outlet port of the fuel gas heater; and a second end connected to a fuel system; andwherein the fuel gas heater operatively heats the fuel gas from a first temperature to a second temperature. 16. The system of claim 15 further comprising a cooling circuit connected between the stack penetration and the stop valve of the exhaust supply path; wherein the cooling circuit comprise an air circulating device that operatively supplies a cooling fluid to the exhaust supply path. 17. The system of claim 15 further comprising a fuel bypass circuit comprising a fuel bypass circuit valve; wherein the fuel bypass circuit connects the fuel supply path and the fuel discharge path.