Clearance control for a turbine
A system for operating a turbine includes a rotating component and a non-rotating component separated from the rotating component by a clearance. A first actuator is connected to the non-rotating component, and the first actuator comprises a shape-memory alloy. A method for operating a turbine includes sensing a parameter reflective of a clearance between a non-rotating component and a rotating component and generating a parameter signal reflective of the clearance. The method further includes generating a control signal to at least one actuator based on the parameter signal and moving at least a portion of the non-rotating component relative to the rotating component to change the clearance.
1. A turbine, comprising:
an outer shroud segment fixed to a casing, the outer shroud segment having a forward end, an aft end, an outer portion fixed to the outer casing and an inner portion;
an inner shroud segment disposed proximate to the inner portion, the inner shroud segment having a first end, a second end and an inner surface, the first end pivotally connected to the outer shroud proximate to the forward end;
a rotatable blade having a tip portion, the tip portion radially separated from the inner surface to form a clearance therebetween; and
an actuator extending radially inwardly from the outer shroud segment and in contact with the inner shroud segment at one end of the actuator proximate to the second end of the inner shroud segment,
2. The turbine as in claim 1 , wherein the actuator actuates radially inwardly to reposition the second end of the inner shroud to adjust the clearance between the tip portion and the inner surface.
3. The turbine as in claim 1 , wherein the actuator actuates in an entirely linear motion.
4. The turbine as in claim 1 , wherein the actuator comprises a shape-memory alloy.
5. The turbine as in claim 4 , wherein the shape-memory alloy comprises approximately 15-35% by weight platinum.
6. The turbine as in claim 1 , wherein the first end of the inner shroud is pivotally connected to the outer shroud segment via a hinge.
7. The turbine as in claim 1 , further comprising bristle strands extending inwardly from the inner surface of the inner shroud segment towards the tip portion of the rotatable blade.
8. The turbine as in claim 7 , wherein the bristle strands comprise shape-memory alloy.
9. The turbine as in claim 1 , further comprising a sensor that provides a parameter signal reflective of at least one of a maximum or a minimum clearance between the inner surface of the inner shroud segment and the tip portion of the rotatable blade.
10. The turbine as in claim 9 , further comprising a controller connected to the sensor, wherein the controller receives the parameter signal from the sensor and generates a control signal to the actuator based on the parameter signal.