Externally replaceable valve assembly for a turbine engine
An assembly is provided for a turbine engine with an axial centerline. This assembly includes a turbine engine structure and a valve assembly. The turbine engine structure includes an outer duct wall, an inner duct wall, a first flow path and a second flow path. The inner duct wall is radially inward of the outer duct wall. The first flow path is radially inward of the inner duct wall. The second flow path is radially outward of the inner duct wall and is radially inward of the outer duct wall. The valve assembly includes a valve element and a valve actuator. The valve element is configured to regulate flow of fluid between the first flow path and the second flow path. The valve actuator is configured to move the valve element. The valve actuator is positioned entirely radially outward of the outer duct wall.
1. An assembly for a turbine engine with an axial centerline, comprising:
a turbine engine structure including an outer duct wall, an inner duct wall, a first flow path and a second flow path, the inner duct wall radially inward of the outer duct wall, the first flow path radially inward of the inner duct wall, and the second flow path radially outward of the inner duct wall and radially inward of the outer duct wall; and
a valve assembly including a valve element, a valve actuator and a rod, the valve element configured to regulate flow of fluid between the first flow path and the second flow path, the valve actuator configured to move the valve element, the valve actuator positioned entirely radially outward of the outer duct wall, the rod extending within the second flow path and mechanically coupling the valve actuator to the valve element, and the rod connected to the valve element through a pivot joint.
2. The assembly of claim 1 , wherein the valve actuator comprises a piston.
3. The assembly of claim 2 , wherein the valve actuator further comprises a spring element engaging the piston.
4. The assembly of claim 1 , wherein the valve actuator comprises a spring element.
5. The assembly of claim 1 , wherein the valve actuator comprises an electric motor.
6. The assembly of claim 1 , wherein
the valve actuator is configured to translate the valve element between an open position and a closed position;
the first flow path is fluidly coupled with the second flow path through a passage in the inner duct wall; and
the valve element is configured to open the passage when the valve element is in the open position, and the valve element is configured to close the passage when the valve element is in the closed position.
7. The assembly of claim 6 , wherein the valve element is radially outward of the inner duct wall when the valve element is in the open position.
8. The assembly of claim 6 , wherein the valve element is radially inward of the inner duct wall when the valve element is in the open position.
9. The assembly of claim 1 , wherein
the valve element comprises a valve plunger; and
the valve actuator is configured to translate the valve plunger along a longitudinal axis of the valve assembly between an open position and a closed position.
10. The assembly of claim 1 , wherein
the valve assembly further includes a second rod that extends within the second flow path and mechanically couples the rod to the valve element; and
the rod is connected to the second rod through a second pivot joint.
11. The assembly of claim 1 , wherein the pivot joint comprises a ball joint.
12. The assembly of claim 1 , wherein the pivot joint comprises a socket joint.
13. The assembly of claim 1 , wherein the valve assembly is configured for complete removal from the turbine engine structure without access to an interior of the outer duct wall.
14. The assembly of claim 1 , wherein
the valve element is mechanically coupled to the inner duct wall; and
the valve actuator is severable from the valve element and configured for complete removal from the turbine engine structure without access to an interior of the outer duct wall.
15. The assembly of claim 1 , wherein
the turbine engine structure further includes an intermediate structure radially between the inner duct wall and the outer duct wall; and
the second flow path is radially inward of the intermediate structure.
16. The assembly of claim 2 , wherein the rod is fixedly attached to the piston.
17. The assembly of claim 1 , wherein
an inner surface of the inner duct wall at least partially forms the first flow path; and
an outer surface of the inner duct wall at least partially forms the second flow path.
18. An assembly for a turbine engine with an axial centerline, comprising:
a turbine engine structure including an outer duct wall, an inner duct wall, a first flow path and a second flow path, the inner duct wall radially inward of the outer duct wall, the first flow path radially inward of the inner duct wall, and the second flow path radially outward of the inner duct wall and radially inward of the outer duct wall; and
a valve assembly including a valve element, a valve actuator and a rod, the valve element configured to regulate flow of fluid between the first flow path and the second flow path, the valve actuator configured to move the valve element, the valve actuator positioned entirely radially outward of the outer duct wall, the rod extending within the second flow path and mechanically coupling the valve actuator to the valve element, and the rod connected to the valve element through a threaded joint.
19. An assembly for a turbine engine with an axial centerline, comprising:
a turbine engine structure including an outer duct wall, an inner duct wall, a first flow path and a second flow path, the inner duct wall radially inward of the outer duct wall, the first flow path radially inward of the inner duct wall, and the second flow path radially outward of the inner duct wall and radially inward of the outer duct wall; and
a valve assembly including a valve element and a valve actuator, the valve element mechanically coupled to the inner duct wall and configured to regulate flow of fluid between the first flow path and the second flow path, and the valve actuator configured to move the valve element, wherein the valve actuator is severable from the valve element and disposed outside of the turbine engine structure.