Gas turbine power augmentation by the addition of nitrogen and moisture to the fuel gas

• US 6,343,462 B1
• Filed: 11/13/1998
• Issued: 02/05/2002
• Est. Priority Date: 11/13/1998
• Status: Expired due to Fees

• Current Assignee: Praxair Technology Incorporated (Linde Plc)
• Original Assignee: Praxair Technology Incorporated (Linde Plc)
• Inventors: Drnevich, Raymond Francis, Ahmed, M. Mushtaq
• Primary Examiner(s): Kim, Ted
• Application Number:
  US09/191,945
• Time in Patent Office: 1,180 Days
• Field of Search: 60/390.5, 60/395.3, 60/395.4, 60/395.5, 607/36
• US Class Current: 60/775
• CPC Class Codes: F01K 21/047 having at least one combustion gas turbine
• CPC Class Codes: F02C 3/305 Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids F01K21/04 takes precedence

Abstract

A method and apparatus for increasing power output and efficiency of gas turbines. Power output is enhanced and NOx emissions are lowered while heat rate penalties are minimized by adding nitrogen or a mixture of nitrogen and water vapor to the gas turbine in conjunction with the use of low pressure steam.

Claims

1. An apparatus for the addition of nitrogen and moisture derived from low pressure steam to the fuel gas utilized to drive a gas turbine comprising:

(a) a saturator tower adapted for the contacting of nitrogen gas with a hot water stream to form a mixture of water vapor and nitrogen gas;

(b) conduit means for passing the mixture of water vapor and nitrogen gas to a heat exchanger unit where low pressure steam is used to produce a superheated mixture of water vapor and nitrogen gas;

(c) conduit means for passing the superheated mixture to a chamber for mixing with feed gas to form a fuel gas mixture;

(d) conduit means for passing the fuel gas mixture of fuel gas, nitrogen and water vapor mixture to a heat exchanger where low pressure steam is used to produce a superheated fuel gas mixture;

(e) conduit means for passing the superheated fuel gas mixture to a gas turbine combustor.

2. The apparatus of claim 1 with:

(a) pressure reduction means for water leaving the saturator to facilitate heating of the water by direct contact with low pressure steam, or condensate, or two phase steam-condensate mixture;

(b) repressurization means to return the hot water to the saturator; and

,

(c) indirect heating means to heat the water from the saturator for recycle to the saturator.

3. An apparatus for the addition of nitrogen and moisture to fuel gas utilized to drive a gas turbine, the gas turbine having a minimum fuel delivery pressure, comprising:

(a) a feed line for feeding a high calorific fuel gas and nitrogen gas;

(b) a saturator tower connected to the feed line, the saturator tower being adapted for the contacting of both the nitrogen gas and the high calorific fuel gas with a hot water stream to form a fuel mixture of water vapor, nitrogen gas, and fuel gas;

(c) a conduit for passing the fuel mixture to a heat exchanger unit where low pressure steam produces a superheated fuel mixture, the low pressure steam having a pressure less than the minimum fuel delivery pressure of the gas turbine;

(d) a conduit for mixing the low pressure steam from the heat exchanger unit with the hot stream of water for heating the hot stream of water for use in the saturator; and

(e) a conduit for passing the superheated fuel mixture to a gas turbine combustor.

4. A process for increasing the power output of a gas turbine system having an air compressor for producing compressed air and an air compressor discharge for discharging air into a combustor for heating said compressed air and producing hot gases, which are exhausted through a combustor exhaust into an expander responsive to said hot gases for driving said air compressor and a load, the gas turbine having a minimum fuel delivery pressure, comprising the steps of:

a) contacting nitrogen gas with a hot water stream in a saturator tower to form a mixture of water vapor and nitrogen gas;

b) passing the mixture of water vapor and nitrogen gas to a heat exchanger unit where low pressure steam produces a superheated mixture of water vapor and nitrogen gas, the low pressure steam having a pressure less than the minimum fuel delivery pressure of the gas turbine;

c) mixing low pressure steam from the heat exchanger unit with the hot water stream to heat the hot water stream for use in step a);

d) passing fuel gas to the combustor; and

e) passing the mixture of water vapor and nitrogen gas to at least one of the air compressor discharge, combustor and combustor exhaust.

5. The method of claim 4 wherein the passing introduces the mixture of water vapor and nitrogen gas to the air compressor discharge of the gas turbine.

6. The method of claim 4 wherein the passing introduces the mixture of water vapor and nitrogen gas to the combustor of the gas turbine.

7. The method of claim 4 wherein the passing introduces the mixture of water vapor and nitrogen gas to the combustor exhaust of the gas turbine.

8. A process for adding nitrogen and moisture to fuel gas utilized to drive a gas turbine, the gas turbine having a minimum fuel delivery pressure, comprising the steps of:

a) contacting a mixture of high calorific fuel gas and nitrogen gas with a hot water stream in a saturator tower to form a fuel mixture of water vapor, nitrogen gas and fuel gas;

b) passing the fuel mixture of water vapor, nitrogen gas and fuel gas to a heat exchanger unit where low pressure steam produces a superheated fuel mixture of water vapor, nitrogen gas and fuel gas, the low pressure steam having a pressure less than the minimum fuel delivery pressure of the gas turbine;

c) mixing low pressure steam from the heat exchanger unit with the hot water stream to heat the hot water stream for use in step b);

d) passing the fuel mixture of water vapor, nitrogen gas and fuel gas to the combustor.

9. An apparatus for increasing the power output of a gas turbine system having an air compressor for producing compressed air and an air compressor discharge for discharging air into a combustor for heating said compressed air and producing hot gases, which are exhausted through a combustor exhaust into an expander responsive to said hot gases for driving said air compressor and a load, the gas turbine having a minimum fuel delivery pressure, comprising:

(a) a feed line for feeding a nitrogen gas;

(b) a saturator tower connected to the feed line, the saturator tower being adapted for the contacting of the nitrogen gas with a hot water stream to form a mixture of water vapor and nitrogen gas;

(c) a conduit for passing the mixture of water vapor and nitrogen gas to a heat exchanger unit where low pressure steam produces a superheated mixture of water vapor and nitrogen gas, the low pressure steam having a pressure less than the minimum fuel delivery pressure of the gas turbine;

(d) a conduit for mixing the low pressure steam from the heat exchanger unit with the hot stream of water for heating the hot stream of water for use in the saturator; and

(e) a conduit for passing the superheated mixture of water vapor and nitrogen gas to at least one of the air compressor discharge, combustor and combustor exhaust.

10. The apparatus of claim 9 wherein the conduit of item (e) passes the mixture of water vapor and nitrogen gas to the air compressor discharge of the gas turbine.

11. The apparatus of claim 9 wherein the conduit of item (e) passes the mixture of water vapor and nitrogen gas to the combustor of the gas turbine.

12. The apparatus of claim 9 wherein the conduit of item (e) passes the mixture of water vapor and nitrogen gas to the combustor exhaust of the gas turbine.