System and method for starting a gas turbine engine with inoperable exhaust gas turbine temperature sensor
First Claim
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1. A gas turbine engine system, comprising:
- a gas turbine engine adapted to receive fuel and air and configured to (i) controllably combust a mixture of the fuel and the air and (ii) discharge at least a portion of the combusted fuel air mixture as exhaust gas;
an exhaust gas temperature (EGT) sensor configured to sense exhaust gas temperature and supply an EGT sensor signal representative thereof; and
a controller configured to implement a plurality of speed-referenced acceleration rate schedules, the controller coupled to receive the EGT sensor signal and operable to;
(i) determine whether the EGT sensor signal is available or unavailable,(ii) command a nominal acceleration rate of the gas turbine engine during a start-up operation of the gas turbine engine if the EGT sensor signal is available, and(iii) command an off-nominal acceleration rate of the gas turbine engine during a start-up operation of the gas turbine engine if the EGT sensor signal is unavailable, wherein the off-nominal acceleration rate is lower than the nominal acceleration rate,wherein the acceleration rate that the controller commands is supplied from one of the speed-referenced acceleration rate schedules.
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Abstract
A system and method are provided for controlling the start-up of a gas turbine engine having an exhaust gas temperature (EGT) sensor. A determination is made as to whether the EGT sensor is available or unavailable. The gas turbine engine is commanded to accelerate at a nominal acceleration rate during the start-up operation if the EGT sensor is available, and to accelerate at an off-nominal acceleration rate during the start-up operation if the EGT sensor is unavailable. The off-nominal acceleration rate is lower than the nominal acceleration rate.
32 Citations
15 Claims
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1. A gas turbine engine system, comprising:
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a gas turbine engine adapted to receive fuel and air and configured to (i) controllably combust a mixture of the fuel and the air and (ii) discharge at least a portion of the combusted fuel air mixture as exhaust gas; an exhaust gas temperature (EGT) sensor configured to sense exhaust gas temperature and supply an EGT sensor signal representative thereof; and a controller configured to implement a plurality of speed-referenced acceleration rate schedules, the controller coupled to receive the EGT sensor signal and operable to; (i) determine whether the EGT sensor signal is available or unavailable, (ii) command a nominal acceleration rate of the gas turbine engine during a start-up operation of the gas turbine engine if the EGT sensor signal is available, and (iii) command an off-nominal acceleration rate of the gas turbine engine during a start-up operation of the gas turbine engine if the EGT sensor signal is unavailable, wherein the off-nominal acceleration rate is lower than the nominal acceleration rate, wherein the acceleration rate that the controller commands is supplied from one of the speed-referenced acceleration rate schedules. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. An engine controller for a gas turbine engine having an exhaust gas temperature (EGT) sensor, the engine controller comprising:
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light-off logic operable to selectively supply an enable signal; and acceleration command logic coupled to receive the enable signal from the light-off logic and adapted to receive an EGT loss signal whenever a sensor signal from the EGT sensor is unavailable, the acceleration command logic operable, upon receipt of the enable signal, to supply acceleration rate commands, wherein; the acceleration rate commands are nominal acceleration rate commands if the EGT loss signal is not received, the acceleration rate commands are off-nominal acceleration rate commands if the EGT loss signal is received, for equivalent conditions, the off-nominal acceleration rate commands are lower than the nominal acceleration rate commands, the acceleration command logic includes a plurality of speed-referenced acceleration rate schedules, and the acceleration rate commands are supplied from one of the speed-referenced acceleration rate schedules. - View Dependent Claims (9, 10, 11, 12, 13)
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14. A method of controlling a gas turbine engine during a start-up operation, for a gas turbine engine having an exhaust gas temperature (EGT) sensor, the method comprising the steps of:
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determining whether the EGT sensor is available or unavailable; commanding the gas turbine engine to accelerate at a nominal acceleration rate during the start-up operation, if the EGT sensor is available, and commanding the gas turbine engine to accelerate at an off-nominal acceleration rate during the start-up operation if the EGT sensor is unavailable, wherein the off-nominal acceleration rate is lower than the nominal acceleration rate; wherein the acceleration rate that is commanded is supplied from one of a plurality of speed-referenced acceleration rate schedules. - View Dependent Claims (15)
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Specification