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 an annular substrate extending along an axial direction, the annular substrate including a first surface and a second surface that is radially inward relative to the first surface; an actuator structure coupled to the second surface of the annular substrate; and a smart structure cantilevered from the second surface of the annular substrate, the smart structure including: a support structure, a first region of the support structure coupled to the second surface of the annular substrate, a second region of the support structure coupled to the actuator structure; and a radially inward surface defining a variable surface, the support structure to move the variable surface in a radial direction.
1. A casing for a turbine engine, the casing comprising:
an annular substrate extending along an axial direction, the annular substrate including a first surface, a second surface, and a third surface, the second surface positioned radially inward relative to the first surface and radially outward relative to the third surface to form a trench;
an actuator structure coupled to the third surface of the annular substrate;
a smart structure cantilevered from the third surface of the annular substrate, the smart structure including:
a support structure, a first region of the support structure coupled to the third surface of the annular substrate, a second region of the support structure coupled to the actuator structure; and
a radially inward surface defining a variable surface, the support structure to move the variable surface in a radial direction; and
a filler material positioned within an area of the trench that is not occupied by the smart structure.
2. The casing of claim 1 , wherein the support structure includes a material associated with a first coefficient of thermal expansion and the actuator structure includes a material associated with a second coefficient of thermal expansion, the second coefficient of thermal expansion to be higher than the first coefficient of thermal expansion.
3. The casing of claim 1 , wherein the actuator structure at least one of expands or contracts in response to a change in temperature.
4. The casing of claim 3 , wherein the actuator structure is to expand in the radial direction in response to an increase in temperature to cause the support structure to move the variable surface in a radially inward direction, and wherein the actuator structure is to contract in the radial direction in response to a decrease in temperature to cause the support structure to move the variable surface in a radially outward direction.
5. The casing of claim 3 , further including an external heat supply, the external heat supply to cause the change in the temperature of the actuator structure to cause the actuator structure to expand.
6. The casing of claim 5 , wherein the external heat supply is at least one of (a) an induction coil or (b) an inflow of a liquid, the liquid having a temperature that is higher than a temperature of the actuator structure.
7. The casing of claim 1 , further including a proximity sensor to detect a tip clearance between the variable surface and a tip of a rotor blade that is radially inward from the variable surface.
8. The casing of claim 1 , wherein the support structure is axially constrained.
9. The casing of claim 1 , wherein the support structure is circumferentially constrained.
10. The casing of claim 1 , wherein the variable surface includes an abradable material coupled thereto.
11. The casing of claim 1 , wherein the variable surface includes an abradable material coupled thereto, the abradable material including a first rabbet at a circumferential end of the abradable material that opposes a second rabbet of an adjacent abradable material of an adjacent variable surface.
12. A casing for a turbine engine, the casing comprising:
substrate means to circumferentially surround a component of the turbine engine, the substrate means having an inner surface and an outer surface, the substrate means extending along an axial direction, the substrate means including a recessed surface positioned radially inward relative to the outer surface and radially outward relative to the inner surface to form a trench, the trench including a filler material;
actuation means coupled to the recessed surface of the substrate means, the actuation means including movement means, the movement means to move the actuation means in response to a change in temperature of the movement means;
support means cantilevered from the recessed surface of the substrate means, the support means operatively coupled to the actuation means, the filler material positioned in an area of the trench not occupied by the actuation means and the support means; and
variable surface means, the support means to move the variable surface means in a radial direction.
13. The casing of claim 12 , wherein the casing surrounds a rotor blade of the turbine engine, and the movement means include a smart material having a positive coefficient of thermal expansion (CTE) that is higher than a CTE of each of (a) a first material corresponding to the support means and (b) a second material corresponding to the rotor blade.
14. The casing of claim 13 , wherein the movement means is to expand in the radial direction in response to an increase in temperature to cause the support means to move the variable surface means in a radially inward direction, and wherein the movement means is to contract in the radial direction in response to a decrease in temperature to cause the support means to move the variable surface means in a radially outward direction.
15. The casing of claim 12 , further including external heat means, the external heat means to cause the change in the temperature of the movement means to cause the movement means to expand.
16. The casing of claim 15 , wherein the external heat means include an inflow of a liquid, the liquid having a temperature that is higher than a temperature of the movement means.
17. The casing of claim 16 , wherein the liquid includes at least one of lube, oil, or bleed air.
18. The casing of claim 12 , further including tip clearance detection means to detect a tip clearance between the variable surface means and a tip of a rotor blade that is radially inward from the variable surface means.
19. A turbine engine comprising:
a rotor blade extending from a rotor end radially outward to a rotor blade tip;
a substrate surrounding the rotor blade, the substrate having a first surface and a second surface that is radially inward relative to the first surface, the substrate including a trench defined by a recess extending radially outward from the second surface of the substrate to a trench ceiling;
a variable flowpath component positioned at least partially within the trench, the variable flowpath component including:
an actuator structure coupled to the trench ceiling; and
a support structure having a material associated with a relatively low coefficient of thermal expansion (CTE), the support structure including (a) a first portion cantilevered from the trench ceiling (b) a second portion operatively coupled to the actuator structure, and (c) a third portion defining a variable surface; and
a trench filler positioned in an area of the trench that is not occupied by the variable flowpath component.
20. The turbine engine of claim 19 , further including:
a sensor to identify tip clearance, wherein the sensor is communicatively coupled to a controller;
a heat source communicatively coupled to the controller;
wherein the controller is to cause the heat source to increase a temperature of the actuator structure in response to the sensor detecting the tip clearance that is beyond a threshold value; and
wherein, in response to the increase in the temperature of the actuator structure, the actuator structure is to radially expand to move the support structure in a radially inward direction to cause the variable surface to move in the radially inward direction to reduce a clearance between the variable surface and the rotor blade tip.