Supercharged combined cycle system with air flow bypass to HRSG and fan
A supercharging system includes a fan providing an air flow, and a prime mover that drives the fan. A duct directs a first portion of the air flow to a gas turbine system, a main bypass subsystem diverts a second portion of the air flow to a heat recovery steam generator; and a drive bypass subsystem that diverts a third portion of the air flow to the prime mover. The prime mover may be one of an aeroderivative gas turbine, a gas turbine, a reciprocating engine, a steam turbine and an induction motor and a variable frequency drive.
1. A combined cycle system, comprising:
a gas turbine subsystem having a compressor and an output side that provides an exhaust;
an exhaust duct coupled to the gas turbine subsystem;
a heat recovery steam generation subsystem coupled to the exhaust duct;
a fan that produces an air flow;
a prime mover that drives the fan, the prime mover having a drive exhaust;
a ducting assembly coupled to the fan that conveys at least a portion of the air flow to the compressor;
a main bypass coupled to the fan and the exhaust duct to selectively convey at least a portion of the air flow to an exhaust duct; and
a drive bypass coupled to the fan and the prime mover to selectively convey at least a portion of the air flow to the prime mover, wherein the prime mover provides a drive exhaust conduit and further comprising drive ducting assembly that conveys a portion of the drive exhaust to the exhaust duct, the heat recovery steam generation subsystem, and the fan.
2. The combined cycle system of claim 1 , wherein the prime mover comprises an aeroderivative gas turbine.
3. The combined cycle system of claim 1 , wherein the prime mover comprises a gas turbine.
4. The combined cycle system of claim 1 , wherein the prime mover comprises a reciprocating engine.
5. The combined cycle system of claim 1 , wherein the prime mover comprises a steam turbine.
6. The combined cycle system of claim 1 , wherein the prime mover comprises an induction motor.
7. A supercharging system for a combined cycle system,
the combined cycle system comprising:
a gas turbine subsystem having a compressor and an output side that provides an exhaust;
an exhaust duct coupled to the gas turbine subsystem;
a heat recovery steam generation subsystem coupled to the exhaust duct;
wherein the supercharging system comprises;
a fan providing an air flow;
a prime mover coupled to the fan, the prime mover having a drive exhaust;
a duct that directs a first portion of the air flow to the gas turbine system;
a main bypass subsystem that diverts a second portion of the air flow to the heat recovery steam generator; and
a drive bypass subsystem that diverts a third portion of the air flow to the prime mover, wherein the prime mover provides a drive exhaust conduit and further comprising drive ducting assembly that conveys a portion of the drive exhaust to the exhaust duct, the heat recovery steam generation subsystem, and the fan.
8. The supercharging system of claim 7 , wherein the prime mover comprises an aeroderivative gas turbine.
9. The supercharging system of claim 7 , wherein the prime mover comprises a gas turbine.
10. The supercharging system of claim 7 , wherein the prime mover comprises a reciprocating engine.
11. The supercharging system of claim 7 , wherein the prime mover comprises a steam turbine.
12. The supercharging system of claim 7 , wherein the prime mover comprises an induction motor.
13. A method of operating a combined cycle system, comprising:
determining a first operating state;
determining a desired operating state;
determining a first mass flow quantity of air to be provided to a gas turbine compressor to achieve the desired operating state;
determining a second mass flow quantity of air to be provided to a heat recovery steam generator to achieve the desired operating state;
determining a third mass flow quantity of air to be provided to a prime mover to achieve the desired operating state;
driving a fan with a prime mover to provide an air flow;
dividing the air flow from the prime mover into a first mass flow portion associated with the first mass flow quantity of air, a second mass flow portion associated with the second mass flow quantity of air, and a third mass flow portion associated with the third mass flow quantity of air;
conveying the first mass flow portion into a compressor;
conveying the second mass flow quantity of air to the heat recovery steam generator;
conveying the third mass flow quantity of air to the prime mover; and
conveying exhaust developed by the prime mover to an exhaust duct coupled to the gas turbine, the heat recovery steam generator, and the fan.
14. The method of claim 13 , wherein driving a fan with a prime mover comprises driving the fan with an aeroderivative gas turbine.
15. The method of claim 13 , wherein driving a fan with a prime mover comprises driving a fan with a gas turbine.
16. The method of claim 13 , wherein the wherein driving a fan with a prime mover comprises driving a fan with a reciprocating engine.
17. The method of claim 13 , wherein driving a fan with a prime mover comprises driving a fan with a steam turbine.
18. The method of claim 13 , wherein driving a fan with a prime mover comprises driving a fan with an induction motor.
19. The method of claim 13 , wherein the selectively conveying the third mass flow quantity of air comprises conveying the third mass flow quantity of air through a drive bypass to the prime mover.