System for staged chilling of inlet air for gas turbines

US 6,769,258 B2
Filed: 07/26/2002
Issued: 08/03/2004
Est. Priority Date: 08/06/1999
Status: Expired due to Term

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1. A method of chilling inlet air for a gas turbine power plant, compromise:

(a) passing inlet air through an air chiller that includes an opening for receiving the inlet air and that is operable connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;

(b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;

(c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;

(d) reducing the flow rate of the liquid water passing through the water chillers;

(e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the flow rate; and

(f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air.

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Abstract

A method for cooling inlet air to a gas turbine is provided. For example, a method is described including passing inlet air through a cooling coil that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant. The gas turbine power plant may include at least one gas turbine, and at least one gas turbine inlet which receives the inlet air. The method may further include passing circulating water through a water chiller at a first flow rate to reduce the temperature of the circulating water, the water chiller including a conduit through which the circulating water is capable of passing and passing the circulating water having the first flow rate through the cooling coil in an amount sufficient to lower the temperature of the inlet air. Additionally, the method may include reducing the flow rate of the circulating water passing through the water chiller, passing the circulating water through a water chiller at a second flow rate to reduce the temperature of the circulating water, the second flow rate being lower than the first flow rate, and passing the circulating water having the second flow rate through the cooling coil in an amount sufficient to lower the temperature of the inlet air.

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27 Claims

1. A method of chilling inlet air for a gas turbine power plant, compromise:
- (a) passing inlet air through an air chiller that includes an opening for receiving the inlet air and that is operable connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reducing the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air.
- View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17)
- - 2. The method of claim 1, additionally comprising passing the liquid water through a pump prior to passing the liquid water through the sequentially positioned water chillers.
  - 3. The method of claim 1, additionally comprising determining a preselected leaving air temperature, passing the liquid water through a pump, reducing the liquid water flowrate, and decreasing the temperature of the liquid water in an amount sufficient to maintain a preselected leaving air temperature.
  - 4. The method of claim 1, additionally comprising passing the liquid water through two or more pumps and reducing the flow rate of the liquid water by shutting off at least one of the two or more pumps.
  - 5. The method of claim 1, additionally comprising passing the liquid water through two or more pumps mounted in parallel with one another and reducing the flow rate of the liquid water by shutting off at least one of the two or more pumps during partial load conditions and restarting the pump during full load conditions.
  - 6. The method of claim 1, additionally comprising passing the liquid water through at least one pump that includes a motor with a variable frequency drive and reducing the flow rate of the liquid water by lowering the speed (RPM) of the pump via the variable frequency drive.
  - 7. The method of claim 1, in which the gas turbine inlet air temperature leaving the cooling coil is about 40°
    - F. to about 60°
      
      F.
  - 8. The method of claim 1, in which the chilled water temperature entering the air chiller is about 34°
    - F. to about 45°
      
      F.
  - 9. The method of claim 1, in which the air chiller includes a multipass cooling coil.
  - 10. The method of claim 1, in which the air chiller includes a four pass cooling coil.
  - 11. The method of claim 1, in which the air chiller includes a six pass cooling coil.
  - 12. The method of claim 1, in which each of the water chillers include an evaporator.
  - 13. The method of claim 1, additionally compromising providing a thermal water storage tank which is operably connected to at least one of the water chillers.
  - 14. The method of claim 1, additionally compromising providing a thermal water storage tank which is operably connected to the water chillers and, during a charge cycle, removing a first portion of liquid water from the thermal water storage tank, passing the removing first portion of water through the water chillers to lower the temperature of the remove first portion of liquid water and to provide a chilled removed first portion of water, and then introducing the chilled removed first portion of water into the thermal water storage tank, wherein the chilled removed first portion of water is introduced to the tank in an amount sufficient to lower the average temperature of the liquid water in the thermal water storage tank.
  - 15. The method of claim 1, additionally comprising providing a thermal water storage tank which is operably connected to the water chillers and, during a discharge cycle, chilling the inlet air by removing a second portion of liquid water from the thermal water storage tank and then passing the second portion of liquid water to the air chiller to make heat transfer contact between the second portion of the liquid water and the inlet air, such that the temperature of the inlet air is lowered.
  - 16. The method of claim 1, further comprising providing multiple gas turbines, each gas turbine having a different preselected inlet air temperature for the turbine controlling inlet air temperature of the multiple gas turbines by throttling the flow of liquid water to the air chiller of the gas turbine having the lowest turbine inlet air temperature.
  - 17. The method of claim 1, further comprising controlling the inlet air temperature of multiple gas by throttling the flow of circulating water to the air chiller of the gas turbine which has the lowest turbine inlet air temperature and resetting the supply circulating water setpoint higher once the last gas turbine circulating water is throttled to maintain the desired turbine inlet air temperature until at least one of the gas turbines meets the desired inlet air temperature without throttling more than about 25% of fully open.

18. A method of chilling inlet air for a gas turbine power plant, comprising:
- (a) passing inlet air through an air chiller coil that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reducing the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperture of the liquid water, the second flow rate being lower than the first flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air, (g) wherein the method additionally comprises adding an additive to the liquid water in an amount sufficient to depress the freezing point of the liquid water.
- View Dependent Claims (19, 20)
- - 19. The method of claim 18, wherein the additive includes sodium nitrate.
  - 20. The method of claim 18, wherein the additive includes potassium formate.

21. A method of chilling inlet air for a gas turbine power plant, comprising:
- (a) passing inlet air through an air chiller coil that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reduced the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the first flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air, (g) wherein the method additionally comprises adding salt additive to the liquid water in an amount sufficient to depress the freezing point of the liquid water.

22. A method of chilling inlet for a gas turbine power plant, comprising:
- (a) passing inlet air through an air chiller that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reducing the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the first flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air, (g) wherein the method additionally comprises determining a set point that depends on or reflects a temperature difference or enthalpy difference, and reducing the flow rate of the liquid water passing through the water chillers when the condition is met.

23. A method of chilling inlet air for a gas turbine power plant, comprising:
- (a) passing inlet air through an air chiller that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reducing the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the first flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air, (g) wherein the method additionally comprises determining a leaving chilled water temperature set point and increasing the setpoint at reduced off-design ambient temperatures to maintain the desire air temperature off the coil until the temperature difference between the circulating water entering the cooling coil and the circulating water leaving the cooling reaches a minimum set point and reducing the flow rate of the circulating water passing through the water chiller and reducing the leaving chilled water temperature setpoint to maintain the desired air temperature off the coil.

24. A method of chilling inlet air for a gas turbine power plant, comprising:
- (a) passing inlet air through an air chiller that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reducing the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the first flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air, (g) wherein the method additionally comprises providing a first temperature sensor to contact the inlet air entering the air chiller and a second temperature sensor to contact the inlet air leaving the air chiller.

25. A method of chilling inlet air for a gas turbine power plant, comprising:
- (a) passing inlet air through an air chiller that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reducing the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the first flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air, (g) wherein the method additionally comprises providing a temperature sensor contacting the inlet air leaving the air chiller and lowering the temperature of the liquid water responsive to an increase in the inlet air temperature.

26. A method of chilling inlet air for a gas turbine power plant, comprising:
- (a) passing inlet air through an air chiller that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reducing the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the first flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air, (g) wherein the method additionally comprises providing a wet bulb temperature sensor to monitor the air wet bulb temperature of inlet air entering the air chiller.

27. A method of chilling inlet air for a gas turbine power plant, comprising:
- (a) passing inlet air through an air chiller that includes an opening for receiving the inlet air and that is operably connected to a gas turbine power plant that includes at least one gas turbine, and at least one gas turbine inlet which receives the inlet air;
  
  (b) passing liquid water through two or more sequentially positioned water chillers at a first flow rate to reduce the temperature of the liquid water, each water chiller including a conduit through which the liquid water is capable of passing;
  
  (c) passing the liquid water having the first flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air;
  
  (d) reducing the flow rate of the liquid water passing through the water chillers;
  
  (e) passing the liquid water through the water chillers at a second flow rate to reduce the temperature of the liquid water, the second flow rate being lower than the first flow rate; and
  
  (f) passing the liquid water having the second flow rate through the air chiller in an amount sufficient to lower the temperature of the inlet air, (g) wherein the method additionally comprises providing a temperature sensor to contact the inlet air leaving the air chiller and to monitor an inlet air temperature and providing a control system to lower the circulating water flowrate in response to a decrease in the temperature difference between the liquid water entering the air chiller and the liquid water leaving the air chiller.

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Litigation Data

Current Assignee
TAS Energy Incorporated
Original Assignee
Tom L. Pierson
Inventors
Pierson, Tom L.
Primary Examiner(s)
Yu, Justine R.
Assistant Examiner(s)
Rodriguez, William H.

Application Number

US10/206,856
Publication Number

US 20040011046A1
Time in Patent Office

739 Days
Field of Search

607/72, 607/28, 621/75
US Class Current

60/772
CPC Class Codes

F01K 23/10   with exhaust fluid of one c...

F02C 7/143   before or between the compr...

F24F 3/06   characterised by the arrang...

F24F 5/0017   using cold storage bodies, ...

F25B 2339/047   Water-cooled condensers

F25B 2400/06   Several compression cycles ...

F25B 27/02   using waste heat, e.g. from...

Y02A 30/274   using waste energy, e.g. fr...

Y02E 20/16   Combined cycle power plant ...

Y02E 60/14   Thermal energy storage

System for staged chilling of inlet air for gas turbines

First Claim

7 Assignments

Litigations

1 Petition

Accused Products

Abstract

70 Citations

27 Claims

Specification

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System for staged chilling of inlet air for gas turbines

First Claim

7 Assignments

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Litigations

1 Petition

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Accused Products

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Abstract

70 Citations

27 Claims

Specification

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Solutions

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