Gas turbine sequencing method and system

1. A method to develop a software based sequencer for a turbine comprising:

receiving selected options from predefined settings for a general purpose sequencer software module, wherein the general purpose sequencer software module has standardized software for sequencing any one of a plurality of turbines through defined states of operation, the standardized software having software code generic to all implementations of the general purpose sequencer software module, wherein the selected options relate to characteristics of the turbine and to conditions of the turbine which will trigger the sequencer to transition the turbine from one of the defined states to the next defined state;

configuring the general purpose sequencer software module with the selected options; and

storing the configured general purpose sequencer software in a non-transitory memory.

2. The method of claim 1 wherein the sequencer includes a predefined sequence of the states.

3. The method of claim 1 wherein the selected options further comprise settings which will trigger the sequencer to trip the turbine and transition the turbine towards a shut down state.

4. The method of claim 1 wherein the sequencer is a state machine.

5. The method of claim 1 wherein the selected options are received using a graphical user interface on a computer terminal.

6. The method of claim 1 wherein the selected options further comprise conditions of the turbine which are to trigger at least one of the transitions between the states.

7. The method of claim 1 wherein the sequencer is for a gas turbine, and the states include: stopped, start auxiliary systems, crank the gas turbine, start ignition and warm-up, acceleration, no load and full speed operation, operation under load, unload and shutdown and coast down.

8. The method of claim 1 wherein the configured general purpose sequencer software includes the unaltered standardized software.

9. A method to develop a software based sequencer stored in a non-transitory memory of a computer controller of a turbine, the method comprising:

selecting a general purpose sequencer software module having standardized software for sequencing any one of a plurality of turbines through defined states of operation, the standardized software having software code generic to all implementations of the general purpose sequencer software module;

selecting options from predefined settings for the sequencer software module, wherein the selected options relate to characteristics of the turbine and to conditions of the turbine which will trigger the sequencer to transition the turbine from one of the defined states to the next defined state, and

using, by a processor, the general purpose sequencer software stored in a non-transitory memory and configured with the selected options for the settings to transition the turbine between the defined states;

configuring the general purpose sequencer software module for a second turbine;

selecting options for predefined settings of the sequencer software module to define operational events of the second turbine which will trigger the sequencer to transition the second turbine from one of the defined states to the next defined state, wherein the selected options for the settings define conditions indicating that a transition should occur between the states, and

using the general purpose sequencer software configured with the selected settings to cause the second turbine to transition between the defined states.

10. The method of claim 9 wherein the second turbine is a different turbine model than the first turbine.

11. The method of claim 1 further comprising predefining a transition for each trip event as being a transition to a coasting down state.

12. The method of claim 11 where each of the states has a corresponding trip event, except for the coasting down state and the state in the sequence preceding the coasting down state.

13. The method of claim 1 wherein at least one of the states may be disabled by the selected options.

14. The method of claim 1 wherein the selected options include options to configure the sequencer.

15. A sequencer for a turbine comprising:

software module for sequencing any one of a plurality of turbines through defined states of operation that is stored in a non-transitory memory of a computer controller of the turbine; and

settings for the software module that define events which prompt the sequencer to transition the turbine between the states, where the settings are based on selectable options,

wherein the software module is configured to guide the turbine through a defined sequence of states based on the settings,

wherein the software module is standardized to be applicable over a wide variety of turbines, the software module having software code generic to all implementations of the software module.

16. The sequencer as in claim 15 wherein the sequencer is for a gas turbine, and the operating states include: stopped, start auxiliary systems, crank the gas turbine, start ignition and warm-up, acceleration, no load and full speed operation, operation under load, unload and shutdown and coast down.

17. The sequencer as in claim 15 wherein the sequencer is a state machine.

18. The sequencer as in claim 15 wherein the selectable options are selected using a graphical user interface on a computer terminal.

19. The sequencer as in claim 15 wherein the selectable options include conditions of the turbine which are to trigger transitions between the states.

20. The sequencer as in claim 15 wherein the selectable options include conditions of the turbine which are to trigger a trip condition to shut down the turbine.