Pressurized damping fluid injection for damping turbine blade vibration
A blade vibration damping system impacts a pressurized damping fluid on a surface of at least one of a plurality of blades of a turbine in opposition to a vibratory movement thereof to cause damping of vibration of the blade(s) during operation of the turbine. The system includes a fluid injection nozzle in a stationary component adjacent the plurality of blades. A valve selectively admits the pressurized damping fluid to the fluid injection nozzle from a source of pressurized damping fluid, and a control system controls the valve to operate the fluid injection nozzle in response to an operational parameter exceeding a threshold during operation of the turbine. A related turbine casing and method are also provided.
1. A casing for a turbine, comprising:
a stationary component defining at least a portion of a working fluid path for directing a working fluid across a blade stage including a plurality of blades operatively coupled to a rotor; and
a fluid injection nozzle in the stationary component configured to impact a pressurized damping fluid on a surface of at least one of the plurality of blades of the blade stage in opposition to a vibratory movement thereof to cause damping of vibration of the at least one of the plurality of blades during operation of the turbine.
2. The casing of claim 1 , further comprising:
a valve for selectively admitting the pressurized damping fluid to the fluid injection nozzle from a source of pressurized damping fluid; and
a control system for controlling the valve,
wherein the control system opens the valve to operate the fluid injection nozzle in response to an operational parameter of the turbine.
3. The casing of claim 2 , wherein the pressurized damping fluid is injected in a substantially constant flow, changing a flow field about the blade stage.
4. The casing of claim 2 , wherein the pressurized damping fluid is injected in a pulsed flow counteracting a phase of the vibratory movement of the at least one of the plurality of blades of the blade stage.
5. The casing of claim 2 , wherein the fluid injection nozzle includes a plurality of fluid injection nozzles circumferentially spaced in the stationary component, each fluid injection nozzle including a respective valve for selectively admitting the pressurized damping fluid to the fluid injection nozzle from the source of pressurized damping fluid under control of the control system, and further comprising:
a sensor system operatively associated with the plurality of blades for determining an amplitude and a phase of vibration of the at least one of the plurality of blades, and
wherein the control system opens at least one valve to operate at least one respective fluid injection nozzle in response to at least one of the amplitude and the phase of vibration of the at least one of the plurality of blades exceeding a threshold during operation of the turbine.
6. The casing of claim 1 , wherein the stationary component includes a tip shroud extending circumferentially about the plurality of blades.
7. The casing of claim 1 , wherein the stationary component includes a part of a nozzle section extending circumferentially about the plurality of blades.
8. The casing of claim 1 , wherein the fluid injection nozzle is aimed at the surface of an outer tip of the at least one of the plurality of blades.
9. The casing of claim 1 , wherein the pressurized damping fluid includes at least one of pressurized air, water, steam, or a combination thereof.
10. The casing of claim 1 , wherein the rotor includes a plurality of blade stages, and wherein the at least one of the plurality of blades is part of a last stage of the plurality of blade stages.
11. The casing of claim 1 , wherein the surface of the at least one of the plurality of blades is an airfoil of the at least one of the plurality of blades, and the fluid injection nozzle is positioned to inject the pressurized damping fluid in a direction perpendicular to the surface.
12. The casing of claim 1 , wherein the fluid injection nozzle includes a nozzle insert in an opening in the stationary component.
13. The casing of claim 1 , wherein the fluid injection nozzle is integrally formed in the stationary component.
14. A blade vibration damping system for a turbine, the system comprising:
a fluid injection nozzle in a stationary component adjacent a plurality of blades in the turbine, the fluid injection nozzle configured to impact a pressurized damping fluid on a surface of at least one of the plurality of blades in opposition to a vibratory movement thereof to cause damping of vibration of the at least one of the plurality of blades during operation of the turbine;
a valve for selectively admitting the pressurized damping fluid to the fluid injection nozzle from a source of pressurized damping fluid; and
a control system for controlling the valve to operate the fluid injection nozzle in response to an operational parameter exceeding a threshold during operation of the turbine.
15. The system of claim 14 , wherein the pressurized damping fluid is injected in a substantially constant flow.
16. The system of claim 14 , wherein the fluid injection nozzle includes a plurality of fluid injection nozzles circumferentially spaced in the stationary component, each fluid injection nozzle including a respective valve for selectively admitting the pressurized damping fluid to the fluid injection nozzle from the source of pressurized damping fluid under control of the control system,
wherein the control system opens at least one valve to operate at least one respective fluid injection nozzle in response to an amplitude of vibration of the at least one of the plurality of blades exceeding the threshold during operation of the turbine.
17. The system of claim 14 , wherein the fluid injection nozzle is aimed at the surface of an outer tip of the at least one of the plurality of blades.
18. The system of claim 14 , further comprising a sensor system operatively associated with a plurality of blades in the turbine, the sensor system configured to determine an amplitude and a phase of vibration of the at least one of the plurality of blades, and
wherein the operational parameter includes at least one of the amplitude of vibration and the phase of vibration of the at least one of the plurality of blades exceeding a threshold during operation of the turbine.
19. A method, comprising:
operating a turbine by transmitting a working fluid through a working fluid path defined between a stationary component of a casing and a rotor and across a plurality of blades operatively coupled to the rotor; and
damping vibration of at least one of the plurality of blades during the operating of the turbine by impacting a pressurized damping fluid on a surface of the at least one of the plurality of blades in opposition to a vibratory movement thereof.
20. The method of claim 19 , wherein the damping includes, during the operating the turbine, selectively operating a valve configured to selectively admit the pressurized damping fluid from a source of pressurized damping fluid to a fluid injection nozzle configured to impact the pressurized damping fluid on the surface of the at least one of the plurality of blades.