Variable flowpath casings for blade tip clearance control
Disclosed herein are example variable flowpath casings for blade tip clearance control. An example casing for a turbine engine includes a first annular substrate extending along an axial direction; a second annular substrate positioned radially inward relative to the first annular substrate, the second annular substrate movably coupled to the first annular substrate; and an actuator coupled to the second annular substrate such that a force applied by the actuator moves the second annular substrate relative to the first annular substrate to adjust a tip clearance.
1 . A casing for a turbine engine, the casing comprising:
a first annular substrate extending along an axial direction;
a second annular substrate extending along the axial direction positioned inward relative to the first annular substrate and movable relative to the first annular substrate, wherein the second annular substrate includes an abradable layer; and
an actuator coupled to the abradable layer such that a force applied by the actuator causes the abradable layer to move relative to the axial direction to adjust tip clearance between a rotor blade tip and the abradable layer.
2 . The casing of claim 1 , wherein the abradable layer includes at least one of rubber, nickel-aluminum, or rub strips with supporting lips.
3 . The casing of claim 1 , wherein the abradable layer is connected to the actuator via a hinge rod with a slider joint.
4 . The casing of claim 1 , wherein the actuator applies a first force to cause the abradable layer to move from a first position to a second position in the axial direction.
5 . The casing of claim 4 , wherein the actuator applies a second force to cause the abradable layer to move from the second position to a third position in a radial direction.
6 . The casing of claim 1 , wherein the force applied by the actuator causes the abradable layer to move from a first position to a second position in an axial-radial direction.
7 . The casing of claim 1 , wherein movement of the abradable layer causes movement of the second annular substrate, wherein the movement of the second annular substrate causes a change in a spacing between the first annular substrate and the second annular substrate.
8 . An apparatus to control tip clearance of a turbine engine, comprising:
interface circuitry;
machine-readable instructions; and
one or more processors to execute the machine-readable instructions to:
monitor tip clearance between a rotor blade tip and an abradable layer of a first substrate, wherein the first substrate extends along an axial direction, is positioned inward relative to a second substrate, and is movable relative to the second substrate; and
in response to a determination that the tip clearance is below a threshold value, apply a force via an actuator coupled to the abradable layer to cause the abradable layer of the first substrate to move relative to the axial direction, wherein the determination that the tip clearance is below the threshold value is based on the monitoring of the tip clearance.
9 . The apparatus of claim 8 , wherein the abradable layer includes at least one of rubber, nickel-aluminum, or rub strips with supporting lips.
10 . The apparatus of claim 8 , wherein the abradable layer is connected to the actuator via a hinge rod with a slider joint.
11 . The apparatus of claim 8 , wherein the machine-readable instructions are to cause the one or more processors to apply a first force to cause the abradable layer to move from a first position to a second position in the axial direction.
12 . The apparatus of claim 11 , wherein the machine-readable instructions are to cause the one or more processors to apply a second force to cause the abradable layer to move from the second position to a third position in a radial direction.
13 . The apparatus of claim 8 , wherein the machine-readable instructions are to cause the one or more processors to cause the abradable layer to move from a first position to a second position in an axial-radial direction based on the applied force, wherein the applied force is a tangential force.
14 . The apparatus of claim 8 , wherein movement of the abradable layer causes movement of the second substrate, wherein the movement of the second substrate causes a change in a spacing between the first substrate and the second substrate.
15 . A casing for a turbine engine, the casing comprising:
a first substrate means, the first substrate means extending along an axial direction;
a second substrate means, the second substrate means extending along the axial direction positioned inward relative to the first substrate means and movable relative to the first substrate means, wherein the second substrate means includes an abradable layer; and
a means for actuating, the means for actuating coupled to the abradable layer such that a force applied by the means for actuating causes the abradable layer to move relative to the axial direction to adjust tip clearance between a rotor blade tip and the abradable layer.
16 . The casing of claim 15 , wherein the abradable layer includes at least one of rubber, nickel-aluminum, or rub strips with supporting lips.
17 . The casing of claim 15 , wherein the abradable layer is connected to the means for actuating via a hinge rod with a slider joint.
18 . The casing of claim 15 , wherein the means for actuating applies a first force to cause the abradable layer to move from a first position to a second position in the axial direction.
19 . The casing of claim 18 , wherein the means for actuating applies a second force to cause the abradable layer to move from the second position to a third position in a radial direction.
20 . The casing of claim 15 , wherein the force applied by the means for actuating causes the abradable layer to move from a first position to a second position in an axial-radial direction.