Model-based rotor speed keep out zone control
A system includes a gas turbine engine and a controller operable to determine a closing threshold with respect to an upper limit and an opening threshold with respect to a lower limit of a movement range of an effector of the gas turbine engine based on an on-board model, where the upper limit and the lower limit are defined for a target parameter of the gas turbine engine. The controller determines a projected state of the target parameter absent a correction command to the effector, applies a closing correction to the effector based on determining that the projected state of the target parameter would result in being above the closing threshold, and applies an opening correction to the effector based on determining that the projected state of the target parameter would result in being below the opening threshold.
1. A system comprising:
a gas turbine engine comprising at least one compressor section and at least one turbine section operably coupled to a shaft of a spool; and
a controller operable to:
determine a closing threshold with respect to an upper limit and an opening threshold with respect to a lower limit of a movement range of an effector of the gas turbine engine based on an on-board model, wherein the upper limit and the lower limit are defined for a target parameter of the gas turbine engine; and
apply a correction to the effector based on a projected state of the target parameter of the gas turbine engine with respect to the closing threshold and the opening threshold.
2. The system of claim 1 , wherein the closing threshold and the opening threshold define a switch hysteresis band, and the upper limit and the lower limit define a keep out zone width with respect to the target parameter of the gas turbine engine.
3. The system of claim 1 , wherein the spool is a high speed spool, and the gas turbine engine further comprises a low speed spool, wherein the low speed spool comprises a low pressure compressor section and a low pressure turbine section.
4. The system of claim 3 , wherein the target parameter is a speed of the high speed spool, and the effector is a high pressure compressor stator vane actuator.
5. The system of claim 4 , wherein the controller is further configured to:
select between a closing correction and an opening correction based on comparing the projected state of the target parameter with the closing threshold and the opening threshold to determine the correction command; and
add the correction command to a high pressure compressor stator vane schedule to control a position of a plurality of high pressure compressor stator vanes using the high pressure compressor stator vane actuator.
6. The system of claim 5 , wherein the correction command is rate limited, and the closing correction and the opening correction are range limited.
7. The system of claim 1 , wherein the controller is further configured to:
determine an adder authority as an adder value to define the upper limit and the lower limit based on at least one speed and at least one vane angle of the gas turbine engine; and
split the adder value between an opening direction and a closing direction of the effector.
8. The system of claim 7 , wherein the closing threshold and the opening threshold are determined with respect to the adder value, a change rate of the at least one speed, and a change rate of the at least one vane angle.
9. The system of claim 8 , wherein the projected state of the target parameter is determined based on a value of the at least one speed, the adder value, the change rate of the at least one speed, and the change rate of the at least one vane angle.
10. The system of claim 1 , wherein the controller is further configured to:
apply a closing proportional-integral control to the target parameter with respect to the upper limit to determine a closing correction; and
apply an opening proportional-integral control to the target parameter with respect to the lower limit to determine an opening correction.
11. A method for control in a gas turbine engine, the method comprising:
determining a closing threshold with respect to an upper limit and an opening threshold with respect to a lower limit of a movement range of an effector of the gas turbine engine based on an on-board model, wherein the upper limit and the lower limit are defined for a target parameter of the gas turbine engine; and
applying a correction to the effector as a correction command based on a projected state of the target parameter of the gas turbine engine with respect to the closing threshold and the opening threshold.
12. The method of claim 11 , wherein the closing threshold and the opening threshold define a switch hysteresis band, and the upper limit and the lower limit define a keep out zone width with respect to the target parameter of the gas turbine engine.
13. The method of claim 11 , wherein the gas turbine engine comprises a high speed spool and a low speed spool, the high speed spool comprising at least one compressor section and at least one turbine section operably coupled to a shaft, and the low speed spool comprising a low pressure compressor section and a low pressure turbine section.
14. The method of claim 13 , wherein the target parameter is a speed of the high speed spool, and the effector is a high pressure compressor stator vane actuator.
15. The method of claim 14 , further comprising:
selecting between a closing correction and an opening correction based on comparing the projected state of the target parameter with the closing threshold and the opening threshold to determine the correction command; and
adding the correction command to a high pressure compressor stator vane schedule to control a position of a plurality of high pressure compressor stator vanes using the high pressure compressor stator vane actuator, wherein the correction command is rate limited, and the closing correction and the opening correction are range limited.
16. The method of claim 11 , further comprising:
determining an adder authority as an adder value to define the upper limit and the lower limit based on at least one speed and at least one vane angle of the gas turbine engine; and
splitting the adder value between an opening direction and a closing direction of the effector.
17. The method of claim 16 , wherein the closing threshold and the opening threshold are determined with respect to the adder value, a change rate of the at least one speed, and a change rate of the at least one vane angle, and wherein the projected state of the target parameter is determined based on a value of the at least one speed, the adder value, the change rate of the at least one speed, and the change rate of the at least one vane angle.
18. The method of claim 11 , further comprising:
applying a closing proportional-integral control to the target parameter with respect to the upper limit to determine a closing correction; and
applying an opening proportional-integral control to the target parameter with respect to the lower limit to determine an opening correction.
19. A system for keep out zone control comprising:
a gas turbine engine; and
a means for:
determining a closing threshold with respect to an upper limit and an opening threshold with respect to a lower limit of a movement range of an effector of the gas turbine engine, wherein the upper limit and the lower limit define a keep out zone of the gas turbine engine; and
applying a correction to the effector based on a projected state of the gas turbine engine with respect to the closing threshold and the opening threshold.
20. The system of claim 19 , wherein the closing threshold and the opening threshold define a switch hysteresis band, and the upper limit and the lower limit define a keep out zone width with respect to a target parameter of the gas turbine engine.