초록 ▼

Systems and methods of determining a flame state within a combustor of a turbine engine make use of characteristics of an output pressure of a compressor of the turbine engine and a temperature of exhaust gases of the turbine engine to make a determination. If the first and/or second derivatives of

Systems and methods of determining a flame state within a combustor of a turbine engine make use of characteristics of an output pressure of a compressor of the turbine engine and a temperature of exhaust gases of the turbine engine to make a determination. If the first and/or second derivatives of the output pressure of the compressor and the first and/or second derivatives of the exhaust gas temperature of the turbine engine are all positive during at least portions of a predetermined period of time, one can determine that a flame has ignited in the combustor. If those values are negative during at least portions of a predetermined period of time, one can determine that a flame has been extinguished in the combustor.

대표청구항 ▼

1. A method of determining a flame state of a combustor of a turbine engine, comprising: determining at least one of a first derivative and a second derivative of an output pressure of the compressor of the turbine engine;determining at least one of a first derivative and a second derivative of a te

1. A method of determining a flame state of a combustor of a turbine engine, comprising: determining at least one of a first derivative and a second derivative of an output pressure of the compressor of the turbine engine;determining at least one of a first derivative and a second derivative of a temperature of the exhaust gases output by the turbine engine; anddetermining a flame state of a combustor of the turbine engine based on the determined derivatives of the output pressure of the compressor and the temperature of the exhaust gases. 2. The method of claim 1, wherein the step of determining a flame state of the combustor comprises determining that a flame has ignited in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both positive during a predetermined period of time, and at least one of the first derivative of the output pressure of the compressor and the first derivative of the exhaust gas temperature is greater than a threshold value. 3. The method of claim 1, wherein the step of determining a flame state of the combustor comprises determining that a flame has ignited in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both positive during at least portions of a predetermined period of time, the first derivative of the output pressure of the compressor is greater than a first threshold value and the first derivative of the exhaust gas temperature is greater than a second threshold value during the predetermined period of time. 4. The method of claim 1, wherein the step of determining a flame state of the combustor comprises determining that a flame has ignited in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both positive during at least a portion of the same predetermined period of time. 5. The method of claim 1, wherein the step of determining a flame state of the combustor comprises determining that a flame has ignited in the combustor if the first derivative of the output pressure of the compressor is positive during a first portion of a predetermined period of time and the first derivative of the temperature of the exhaust gases is positive during a second portion of the predetermined period of time, the second portion being subsequent to the first portion. 6. The method of claim 1, wherein the first determining step comprises determining the first and second derivatives of the output pressure of the compressor, wherein the second determining step comprises determining the first and second derivatives of the temperature of the exhaust gases output by the turbine engine, and wherein the step of determining a flame state of a combustor of the turbine engine is based on the determined first and second derivatives of the output pressure of the compressor and the temperature of the exhaust gases. 7. The method of claim 6, wherein the step of determining a flame state of the combustor comprises determining that a flame has ignited in the combustor if the first and second derivatives of the output pressure of the compressor and the first and second derivatives of the temperature of the exhaust gases are both positive over portions of a predetermined period of time. 8. The method of claim 6, wherein the step of determining a flame state of the combustor comprises determining that a flame has ignited in the combustor if the first and second derivatives of the output pressure of the compressor are both positive and above threshold values during a first portion of a predetermined period of time, and if the first and second derivatives of the temperature of the exhaust gases are both positive and above threshold values during a second portion of the predetermined period of time. 9. The method of claim 6, wherein the step of determining a flame state of the combustor comprises determining that a flame has been extinguished in the combustor if the first and second derivatives of the output pressure of the compressor and the first and second derivatives of the temperature of the exhaust gases are all negative over at least portions of a predetermined period of time. 10. The method of claim 1, wherein the step of determining a flame state of the combustor comprises determining that a flame has been extinguished in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both negative during portions of a predetermined period of time, and at least one of the first derivative of the output pressure of the compressor and the first derivative of the exhaust gas temperature is below a threshold value. 11. The method of claim 1, wherein the step of determining a flame state of the combustor comprises determining that a flame has been extinguished in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both negative during portions of a predetermined period of time, the first derivative of the output pressure of the compressor is smaller than a first threshold value during a portion of the predetermined period of time, and the first derivative of the exhaust gas temperature is smaller than a second threshold value during a portion of the predetermined period of time. 12. A system for determining a flame state of a combustor of a turbine engine, comprising: means for determining at least one of a first derivative and a second derivative of an output pressure of the compressor of the turbine engine;means for determining at least one of a first derivative and a second derivative of a temperature of the exhaust gases output by the turbine engine; andmeans for determining a flame state of a combustor of the turbine engine based on the determined derivatives of the output pressure of the compressor and the temperature of the exhaust gases. 13. A system for determining a flame state of a combustor of a turbine engine, comprising: a pressure change determining unit that determines at least one of a first derivative and a second derivative of the output pressure of the compressor of the turbine engine;a temperature change determining unit that determines at least one of a first derivative and a second derivative of the temperature of the exhaust gases output by the turbine engine; anda flame state determining unit that determines a flame state of a combustor of the turbine engine based on outputs of the pressure change determining unit, and the temperature change determining unit. 14. The system of claim 13, wherein the flame state determining unit determines that a flame has ignited in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both positive during at least portions of a predetermined period of time, and at least one of the first derivative of the output pressure of the compressor and the first derivative of the exhaust gas temperature is greater than a threshold value. 15. The system of claim 13, wherein the flame state determining unit determines that a flame has ignited in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both positive during at least portions of a predetermined period of time, the first derivative of the output pressure of the compressor is greater than a first threshold value, and the first derivative of the exhaust gas temperature is greater than a second threshold value. 16. The system of claim 13, wherein the flame state determining unit determines that a flame has been extinguished in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both negative during at least portions of a predetermined period of time, and at least one of the first derivative of the output pressure of the compressor and the first derivative of the exhaust gas temperature is lower than a threshold value. 17. The system of claim 13, wherein the flame state determining unit determines that a flame has been extinguished in the combustor if the first derivative of the output pressure of the compressor and the first derivative of the temperature of the exhaust gases are both negative during at least portions of a predetermined period of time, the first derivative of the output pressure of the compressor is lower than a first threshold value during a portion of the predetermined period of time, and the first derivative of the exhaust gas temperature is lower than a second threshold value during a portion of the predetermined period of time. 18. The system of claim 13, wherein the pressure change determining unit also determines both the first and second derivatives of the output pressure of the compressor of the turbine engine, wherein the temperature change determining unit determines both the first and second derivatives of the temperature of the exhaust gases output by the turbine engine, and wherein the flame state determining unit determines a flame state of a combustor of the turbine engine based on the determined first and second derivatives of the output pressure of the compressor and the temperature of the exhaust gases output by the turbine engine. 19. The system of claim 18, wherein the flame state determining unit determines that a flame has ignited in the combustor if the first and second derivatives of the output pressure of the compressor and the first and second derivatives of the temperature of the exhaust gases are all positive during at least portions of a predetermined period of time. 20. The system of claim 18, wherein the flame state determining unit determines that a flame has been extinguished in the combustor if the first and second derivatives of the output pressure of the compressor and the first and second derivatives of the temperature of the exhaust gases are all negative during at least portions of a predetermined period of time.