Method and apparatus for combined cycle power plant operation

• US 7,107,774 B2
• Filed: 06/17/2004
• Issued: 09/19/2006
• Est. Priority Date: 08/12/2003
• Status: Expired due to Fees

• Current Assignee: Washington Group International Incorporated (Aecom Incorporated)
• Original Assignee: Washington Group International Incorporated (Aecom Incorporated)
• Inventors: Radovich, Michael J.
• Primary Examiner(s): KIM, TAE JUN
• Application Number:
  US10/870,006
• Publication Number:
  US 20050034445A1
• Time in Patent Office: 824 Days
• Field of Search: 60/391.82, 60/395, 607/87, 60/392.1, 607/78, 122/7.R, 122/7.B
• US Class Current: 60/778
• CPC Class Codes: F01K 13/02 Controlling, e.g. stopping or starting
• CPC Class Codes: F01K 23/10 with exhaust fluid of one cycle heating the fluid in another cycle F01K17/025 takes precedence
• CPC Class Codes: F05B 2220/704 the other apparatus being a gas turbine
• CPC Class Codes: F05B 2260/85 Starting
• CPC Class Codes: Y02E 20/16 Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Abstract

Methods and apparatus are disclosed for starting up a combined cycle plant using a startup duct to connect an auxiliary engine to the inlet of a plurality of HRSGs or other heat recovery systems. Each HRSG is fed by a combustion turbine. Dampers are supplied to isolate each HRSG from the startup duct and its CTG. The auxiliary engine is also ported to a stack allowing simple cycle operation. Dampers are also supplied to isolate the auxiliary engine from the startup duct and from its stack. During startups, the large CTGs will be isolated and the auxiliary engine will be connected to the HRSGs and started, allowing the HRSG to pressurize. As each HRSG pressurizes, it is isolated from the startup duct and connected to its respective CTG. The CTG is then started and loaded. The auxiliary engine is turned off and isolated when the last HRSG pressurizes.

Claims

1. In a combined cycle power plant apparatus adapted for starting up or changing the load of the plant, said apparatus comprising in combination a plurality of combustion turbines, each having at least a turbine exhaust, and systems for recovering heat, each such system having an inlet coupled to an exhaust from a combustion turbine, the improvements comprising:

(a) an assembly for isolating said combustion turbines from said systems for recovering heat;

(b) an auxiliary engine or other hot gas generator;

(c) an auxiliary engine stack conveying exhaust from said auxiliary engine or other hot gas generator to the atmosphere;

(d) an assembly for isolating said auxiliary engine or other hot gas generator from said auxiliary engine stack;

(e) at least a startup duct system coupling exhaust from said auxiliary engine or other hot gas generator to inlets of each of said systems for recovering heat;

(f) a first damper assembly for periodically isolating said startup duct system from each of said systems for recovering heat; and

,

(g) a second damper assembly for periodically isolating said startup duct system from said auxiliary engine or other hot gas generator.

2. In a combined cycle power plant apparatus adapted for starting up or changing the load of the plant, said apparatus comprising a plurality of combustion turbines, each having at least a turbine exhaust, and systems for recovering heat, each such system having an inlet coupled to an exhaust from a combustion turbine, the improvements comprising:

(a) an assembly for isolating said combustion turbines from said systems for recovering heat;

(b) at least a startup duct system connecting the inlets of all of said systems for recovering heat; and

,

(c) a first damper assembly for periodically isolating said startup duct system from each of said systems for recovering heat.

3. A method of operating a combined cycle power plant for start up, said plant comprising in combination two or more combustion turbines, each having at least a turbine exhaust, said turbines being associated with one or more systems for recovering heat, each such system having an inlet coupled to a turbine exhaust;

at least an auxiliary engine or other hot gas generator and an associated auxiliary engine stack, and at least a startup duct system coupling exhaust from said auxiliary engine or other hot gas generator to inlets of each of said systems for recovering heat, said method comprising the sequential steps of;

(a) isolating said combustion turbines from said systems for recovering heat;

(b) isolating said auxiliary engine from said auxiliary engine stack;

(c) connecting said auxiliary engine to said startup duct system;

(d) connecting the startup duct system to each system for recovering heat;

(e) starting and loading said auxiliary engine;

(f) heating said systems for recovering heat with exhaust from said auxiliary engine by passing exhaust from the auxiliary engine through said startup duct system;

(g) connecting said systems for recovering heat to their respective associated combustion turbines when a predetermined pressure or temperature or demand for electrical power is reached;

(h) starting and loading one or more of said two or more combustion turbines

(i) turning off said auxiliary engine or other hot gas generator;

(j) starting and loading any unstarted combustion turbines; and

,

(k) isolating said systems for recovering heat from said startup duct system.

5. A method of operating a combined cycle plant following start up according to either of claims 3 or 4 for subsequently quickly cooling down the systems for recovering heat, said method comprising the additional steps of:

(a) turning off all combustion turbines and isolating them;

(b) connecting the inlets of all systems for recovering heat to the startup duct system;

(c) connecting the auxiliary engine or other hot gas generator to the startup duct system;

(d) starting the auxiliary engine or other hot gas generator and operating it to produce low temperature exhaust; and

,

(e) operating the auxiliary engine or other hot gas generator until the cool exhaust has cooled the systems for recovering heat.

6. A method of operating a combined cycle plant following start up according to either of claims 3 or 4 for subsequently maintaining the plant in hot standby, said method comprising the additional steps of:

(a) turning off a plurality of combustion turbines while keeping at least one operating;

(b) isolating the turned off combustion turbines;

(c) connecting all systems for recovering heat to the startup duct system; and

,

(d) maintaining a predetermined temperature in those systems for recovering heat which are connected to the turned-off combustion turbines with exhaust from the operating turbines by passing the exhaust through the startup duct system.

7. A method of operating a combined cycle plant following start up according to either of claims 3 or 4 for subsequently maintaining the plant in hot standby, said method comprising the additional steps of:

(a) turning off at least some of the combustion turbines;

(b) isolating the turned off combustion turbines;

(c) connecting all systems for recovering heat to the startup duct system;

(d) connecting the auxiliary engine or other hot gas generator to the startup duct system;

(e) starting and loading the auxiliary engine or other hot gas generator; and

,

(f) maintaining a predetermined temperature in those systems for recovering heat which are connected to the turned-off combustion turbines with exhaust from the auxiliary engine or other hot gas generator by passing the exhaust through the startup duct system.

8. A method according to claim 7 wherein the auxiliary engine or other hot gas generator is connected to the startup duct system and started before turning off the combustion turbines.

4. A method of operating a combined cycle power plant for start up, said plant comprising in combination two or more combustion turbines, each having at least a turbine exhaust, said turbines being associated with one or more systems for recovering heat, each such system having an inlet coupled to a turbine exhaust;

at least an auxiliary engine or other hot gas generator and an associated auxiliary engine stack, and at least a startup duct system coupling exhaust from said auxiliary engine or other hot gas generator to inlets of each of said systems for recovering heat, said method comprising the sequential steps of;

(a) isolating all combustion turbines from said systems for recovering heat except for a lead combustion turbine;

(b) connecting the inlets of all systems for recovering heat to said startup duct system;

(c) starting and loading the lead combustion turbine;

(d) heating said systems for recovering heat with exhaust from the lead combustion turbine by passing exhaust from said lead combustion turbine through the startup duct system or directly to the systems for recovering heat;

(e) connecting remaining combustion turbines to said associated systems for recovering heat when a predetermined pressure or temperature or electrical demand is reached, except for that system for recovering heat which is directly connected to the lead combustion turbine;

(f) starting and loading remaining combustion turbines; and

,

(g) isolating the inlets of all systems for recovering heat from said startup duct system.

9. A combined cycle power plant assembly comprising in combination:

(a) at least a combustion turbine unit comprising a turbine unit exhaust;

(b) a heat recovery system connected to a combustion turbine unit, said heat recovery system comprising a heat recovery system inlet fluidically coupled to the turbine unit exhaust;

(c) a hot gas source unit capable of generating not more than a limited amount of heat in the form of hot gas exhaust, which limited amount of heat is substantially less than the amount of heat in the form of hot gas produced under normal operating conditions by the combustion turbine unit, said hot gas source unit comprising a hot gas exhaust outlet fluidically coupled both to a heat recovery system inlet and to a vent;

(d) a duct system comprising duct portions connecting the hot gas exhaust outlet to a heat recovery system inlet and directly to a vent without passing through a heat recovery system, and also duct portions connecting each turbine unit exhaust to a heat recovery system inlet; and

,

(e) a fluid flow control system associated with said duct system comprising separate fluid flow control devices in each of the following duct portions of said duct system;

(i) in each first duct portion connecting the hot gas exhaust outlet to a heat recovery system inlet;

(ii) in a second duct portion directly connecting the hot gas exhaust outlet to a vent without passing through a heat recovery system; and

(iii) in each third duct portion connecting a turbine unit exhaust to a heat recovery system inlet.

10. A combined cycle power plant assembly according to claim 9 wherein said hot gas source unit is selected from the group consisting of small gas turbines, small diesel generators, and small burner units.

11. A combined cycle power plant assembly according to claim 9 wherein said hot gas source unit is sized to produce not more than a limited amount of heat primarily in the form of hot gas exhaust that is about 1% to about 15% of the heat produced under normal operating conditions by the combustion turbine unit.

12. A combined cycle power plant assembly according to claim 9 wherein said hot gas source unit is sized to produce not more than a limited amount of heat primarily in the form of hot gas exhaust that is less than about 10% of the heat produced under normal operating conditions by the combustion turbine unit.

13. A combined cycle power plant assembly according to claim 9 wherein said fluid flow control devices are damper elements.

14. A combined cycle power plant assembly according to claim 9 wherein said fluid flow control devices are selected from the group consisting of guillotine, spectacle, louver, sickle, butterfly or flap-type dampers.

15. A combined cycle power plant assembly according to claim 9 wherein said heat recovery system comprises in combination a diffuser, a superheater, an evaporator, a carbon monoxide catalyst, a selective reduction catalyst, an economizer, a feedwater pump, a preheater, and a vent stack.

16. A combined cycle power plant assembly according to claim 9 wherein said heat recovery system comprises a carbon monoxide catalyst, a selective reduction catalyst, or both.

17. A combined cycle power plant assembly according to any of claims 9–

16 wherein at least two combustion turbine units, each comprising a turbine unit exhaust, are connected respectively to at least two associated heat recovery systems, each comprising a heat recovery system inlet fluidically coupled to at least two of the combustion turbine unit exhausts.

18. A combined cycle power plant assembly according to claim 17 wherein said duct system further comprises duet portions connecting the hot gas exhaust outlet to each of the heat recovery system inlets.

19. A combined cycle power plant assembly according to claim 18 wherein said fluid flow control system comprises a separate fluid flow control device in each of the duct portions of said duct system connecting the hot gas exhaust outlet to each of the heat recovery system inlets and also in each of the duct portions connecting a turbine unit exhaust to an associated heat recovery system inlet.

20. A combined cycle power plant assembly according to any of claims 9–

16 wherein at least three combustion turbine units, each comprising a turbine unit exhaust, are connected respectively to at least two associated heat recovery systems, each comprising a heat recovery system inlet fluidically coupled to at least two of the combustion turbine unit exhausts.

21. A combined cycle power plant assembly according to any of claims 9–

16 further comprising an automated control system for controlling the fluid flow control system responsive to signals from position switches associated with the fluid flow control devices.

22. A combined cycle power plant assembly according to claim 9 further wherein each of said fluid flow control devices comprises a duct portion flap-type damper which, when at least partly open, permits fluid flow in either direction through said flap-type damper or, alternatively, when closed substantially prevents fluid flow in either direction through the flap-type damper.

23. A combined cycle power plant assembly according to claim 9 wherein each first duct portion connecting the hot gas exhaust outlet to a heat recovery system inlet comprises at least two separate fluid flow control devices along a flow path between the hot gas exhaust outlet and a heat recovery system inlet.

24. A combined cycle power plant assembly according to claim 9 comprising at least two combustion turbine units, each comprising a turbine unit exhaust fluidically coupled to a heat recovery system inlet of an associated heat recovery system, further wherein the hot gas exhaust outlet of said hot gas source unit is fluidically coupled to each of the heat recovery system inlets by respective first duct portions containing fluid flow control devices.

25. A combined cycle power plant assembly according to claim 24 wherein each first duct portion connecting the hot gas exhaust outlet to a heat recovery system inlet comprises at least two separate fluid flow control devices along a flow path between the hot gas exhaust outlet and a heat recovery system inlet.

26. A combined cycle power plant assembly according to claim 9 wherein said assembly is an open combined cycle power plant assembly wherein substantially none of the exhaust from a heat recovery system is returned to a combustion turbine unit.

27. A method of operating a combined cycle power plant for start up, said plant comprising in combination a combustion turbine having a turbine exhaust, said turbine being associated with a system for recovering heat, such system having an inlet coupled to said turbine exhaust;

at least an auxiliary engine or other hot gas generator connected directly to an associated auxiliary engine stack without passing through said system for recovering heat, and at least a startup duct system coupling exhaust from said auxiliary engine or other hot gas generator to said inlet of said system for recovering heat, said method comprising the sequential steps of;

(a) isolating said combustion turbine from said system for recovering heat and isolating said auxiliary engine from said auxiliary engine stack;

(b) connecting said auxiliary engine to said startup duct system and connecting the startup duct system to the system for recovering heat;

(c) starting and loading said auxiliary engine;

(d) heating said system for recovering heat with exhaust from said auxiliary engine by

passing exhaust from the auxiliary engine through said startup duct system;

(e) connecting said system for recovering heat to the associated combustion turbine

when a predetermined pressure or temperature or demand for electricity is reached;

(f) starting and loading the combustion turbine;

(g) turning off said auxiliary engine or other hot gas generator; and

,

(h) isolating said system for recovering heat from said startup duct system.

28. A method of operating a combined cycle plant following start up according to claim 27 for subsequently quickly cooling down the system for recovering heat, said method comprising the additional steps of:

(a) turning off the combustion turbine and isolating it;

(b) connecting the inlet of the system for recovering heat to the startup duct system;

(c) connecting the auxiliary engine or other hot gas generator to the startup duct system;

(d) starting the auxiliary engine or other hot gas generator and operating it to produce low temperature exhaust; and

,

(e) operating the auxiliary engine or other hot gas generator until the cool exhaust has cooled the system for recovering heat.