Turbomachine blade clearance control system
A turbomachine blade clearance system can include an actuator having an anchor portion for fixation to an interior surface of a turbomachine housing and an actuating portion for actuating movement relative to the anchor portion. A turbomachine blade seal can be operatively connected to the actuating portion of the actuator and configured to move relative to the turbomachine housing to adjust a distance from a turbomachine blade of a turbomachine to maintain a predetermined gap clearance between the blade seal and the blade.
1. A turbomachine blade clearance system, comprising:
an actuator including an anchor portion for fixation to an interior surface of a turbomachine housing and an actuating portion for actuating movement relative to the anchor portion, wherein the actuating portion of the actuator includes bellows having a magneto-rheological fluid disposed therein and the bellows is configured to elongate under influence of a magnetic field to the magneto-rheological fluid; and
a turbomachine blade seal operatively connected to the actuating portion of the actuator and configured to move relative to the turbomachine housing to adjust a distance from a turbomachine blade of a turbomachine to maintain a predetermined gap clearance between the blade seal and the blade.
2. The turbomachine blade clearance system of claim 1 , further comprising a plurality of actuators connected to the turbomachine blade seal.
3. The turbomachine blade clearance system of claim 1 , further comprising a controller configured to control actuation of the actuating portion.
4. The turbomachine blade clearance system of claim 3 , wherein the controller is configured to cause actuation of the actuating portion to move the turbomachine blade seal to a predicted position for a desired blade clearance based on at least one input.
5. The turbomachine blade clearance system of claim 4 , wherein the at least one input is blade rotational speed, temperature, pressure, blade acceleration, or thrust input.
6. The turbomachine blade clearance system of claim 3 , further comprising a sensor configured to sense a blade clearance, the sensor operatively connected to the controller for actuation of the actuating portion to move the turbomachine blade seal to a desired position for a desired blade clearance based on sensed blade clearance.
7. A turbine blade clearance system, comprising:
a plurality of actuators, each including an anchor portion for fixation to an interior surface of a turbomachine housing and an actuating portion for actuating movement relative to the anchor portion, wherein the actuating portion of at least one of the plurality of actuators includes bellows having a magneto-rheological fluid disposed therein and the bellows is configured to elongate under influence of a magnetic field to the magneto-rheological fluid; and
a plurality of turbine blade seals operatively connected to the actuating portions of the actuators and configured to move relative to the turbomachine housing to adjust a distance from a turbine blade seal to a turbine blade of a turbomachine.
8. The turbine blade clearance system of claim 7 , wherein the actuating portion of at least one of the actuators includes a linear mechanical actuator.
9. The turbine blade clearance system of claim 7 , wherein the plurality of actuators are disposed circumferentially around the interior surface of the turbomachine.
10. The turbine blade clearance system of claim 7 , further comprising a controller configured for actuation of the actuating portion of each actuator either independently or together.
11. The turbine blade clearance system of claim 10 , wherein the controller is configured to cause actuation of the actuating portion of each actuator to move the turbine blade seal to a predicted position for a desired blade clearance based on at least one input.
12. The turbine blade clearance system of claim 10 , further comprising a sensor configured to sense a blade clearance, the sensor operatively connected to the controller for actuation of the actuating portion of each actuator to move the turbine blade seal to a desired position for a desired blade clearance based on sensed blade clearance.
13. The turbine blade clearance system of claim 7 , wherein the actuators are radially oriented such that actuation of the actuating portion of each actuator causes radial movement of the turbine blade seal attached thereto.
14. The turbine blade clearance system of claim 7 , wherein the actuators are oriented at an angle oblique to a radial axis with respect to the turbine blade seal such that actuation of the actuating portion of each actuator causes radial and axial movement of the turbine blade seal attached thereto.
15. The turbine blade clearance system of claim 7 , wherein the actuators are axially oriented such that actuation of the actuating portion of each actuator causes axial movement of the turbine blade seal attached thereto.
16. The turbine blade clearance system of claim 7 , wherein the turbine blade seals are disposed in a conical section of a turbomachine such that each blade seal is at an angle to a longitudinal axis of the turbomachine and wherein the actuators are axially arranged such that actuation of the actuating portion of each actuator causes axial movement of the turbine blade seal attached thereto.
17. The turbine blade clearance system of claim 7 , wherein multiple actuators are connected to each turbine blade seal for orientation control.