초록 ▼

A gas turbine (12) capable of combusting a low quality gaseous fuel having a ratio of flammability limits less than 2, or a heat value below 100 BTU/SCF. A high quality fuel is burned simultaneously with the low quality fuel to eliminate instability in the combustion flame. A sensor (46) is used to

A gas turbine (12) capable of combusting a low quality gaseous fuel having a ratio of flammability limits less than 2, or a heat value below 100 BTU/SCF. A high quality fuel is burned simultaneously with the low quality fuel to eliminate instability in the combustion flame. A sensor (46) is used to monitor at least one parameter of the flame indicative of instability. A controller (50) having the sensor signal (48) as input is programmed to control the relative flow rates of the low quality and high quality fuels. When instability is detected, the flow rate of high quality fuel is automatically increased in relation to the flow rate of low quality fuel to restore stability.

대표청구항 ▼

1. A method of combusting fuel comprising: providing a supply of a first fuel exhibiting a first quality parameter; providing a supply of a second fuel exhibiting a second quality parameter; combusting simultaneously in a combustor a flow of the first fuel and a flow of the second fuel; monito

1. A method of combusting fuel comprising: providing a supply of a first fuel exhibiting a first quality parameter; providing a supply of a second fuel exhibiting a second quality parameter; combusting simultaneously in a combustor a flow of the first fuel and a flow of the second fuel; monitoring at least one parameter Indicative of a level of stability of combustion in the combustor during the step of combusting; and controlling relative flow rates of the first fuel and the second fuel in response to the at least one parameter. 2. The method of claim 1, wherein the step of monitoring at least one parameter further comprises monitoring electromagnetic radiation in the combustor. 3. The method of claim 1, wherein the step of monitoring at least one parameter further comprises monitoring pressure in the combustor. 4. The method of claim 1, wherein the step of monitoring at least one parameter further comprises monitoring ionization potential in the combustor. 5. The method of claim 1, wherein the first fuel exhibits a higher heat value than the second fuel, and further comprising increasing the relative flow rate of the first fuel compared to that of the second fuel when the step of monitoring the at least one parameter Indicates that combustion in the combustor is unstable. 6. The method of claim 1, wherein the first fuel exhibits a higher ratio of flammability limits than the second fuel, and further comprising increasing the relative flow rate of the first fuel compared to that of the second fuel when the step of monitoring the at least one parameter indicates that combustion in the combustor is unstable. 7. The method of claim 1, wherein the first fuel is a high quality fuel and the second fuel is a low quality fuel, and further comprising: initiating combustion in the combustor with only the first fuel; after stable combustion is established with only the first fuel, initiating the flow of the second fuel; decreasing the flow of the first fuel relative to the flaw of the second fuel to a point whereat the at least one parameter indicates instability; and increasing the flow of the first fuel relative to the flow of the second fuel to eliminate the instability. 8. The method of claim 7, wherein the flow of the first fuel relative to the flow of the second fuel is increased by a predetermined amount above the point whereat the at least one parameter indicates instability. 9. A method of combusting fuel, the method comprising: simultaneously combusting a low quality fuel and a high quality fuel in a combustor; monitoring a parameter responsive to combustion instability conditions in the combustor; and controlling the relative amounts of low quality fuel and high quality fuel being combusted in the combustor in response to the parameter. 10. The method of claim 9, further comprising: monitoring pressure in the combustor to detect combustion instability; and increasing the flow rate of the high quality fuel in relation to the flow rate of the low quality fuel in response to detecting combustion instability. 11. The method of claim 9, further comprising: reducing the amount of the high quality fuel in relation to the amount of the low quality fuel until the parameter indicates combustion instability in the combustor; and increasing the amount of the high quality fuel in relation to the amount of the low quality fuel to eliminate the combustion instability.