A rotating element for a rotating machine, in particular for a turbine machine, is provided with a vibration damper for vibrations of the rotating element during operation of the machine. The vibration damper includes a closed cavity in the body of the rotating element. In the closed cavity there is
A rotating element for a rotating machine, in particular for a turbine machine, is provided with a vibration damper for vibrations of the rotating element during operation of the machine. The vibration damper includes a closed cavity in the body of the rotating element. In the closed cavity there is located a movable solid damping body as well as a damping medium. The damping medium is based on a metal which is in liquid state at the operation temperature where damping is desired. It furthermore relates to turbo machines equipped with such rotating elements as well as to uses of liquid metal for such vibration dampers.
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1. A rotating element for a turbine machine comprising an airfoil having a tip shroud, the rotating element comprising: a vibration damper for damping vibrations of the element during operation of the machine, wherein the vibration damper comprises a closed cavity in a body of the element, wherein i
1. A rotating element for a turbine machine comprising an airfoil having a tip shroud, the rotating element comprising: a vibration damper for damping vibrations of the element during operation of the machine, wherein the vibration damper comprises a closed cavity in a body of the element, wherein in said closed cavity a movable solid damping body as well as a damping medium are located, wherein the closed cavity, the movable solid damping body, and the damping medium are arranged in a lengthwise center of the airfoil, and wherein said damping medium comprises a metal which at rest is in a cool state being a solid, and during start-up, the metal liquefies and is in a liquid state at an operation temperature where damping is desired, andthe damping medium is a dispersion of solid particles in the metal which is in the liquid state at the operation temperature where damping is desired, wherein the solid particles have a melting point above 800° C. 2. The rotating element according to claim 1, wherein the metal of the damping medium has a melting point in the range of 150-800° C. 3. The rotating element according to claim 1, wherein the metal of the damping medium has a melting point in the range of 200-500° C. 4. The rotating element according to claim 1, wherein the metal of the damping medium has a boiling point above 800° C. 5. The rotating element according to claim 1, wherein the metal of the damping medium has a boiling point above 1000° C. 6. The rotating element according to claim 1, wherein the metal of the damping medium has a boiling point above 2000° C. 7. The rotating element according to claim 1, wherein the metal of the damping medium is based on at least one metal selected from the group of: aluminum, magnesium, zinc, tin, lead, copper, silver, manganese or alloys thereof or alloys of one or several members of this group as principal constituents in an amount of more than 50 weight percent with another metal. 8. The rotating element according to claim 1, wherein the damping medium is a dispersion of solid particles in a metal which is in liquid at the operation temperature where damping is desired, wherein the solid particles have a melting point above 1000° C. 9. The rotating element according to claim 1, wherein the damping medium is a dispersion of solid particles in a metal which is in liquid at the operation temperature where damping is desired, wherein the solid particles have a melting point above 2000° C. 10. The rotating element according to claim 1, wherein the solid particles are inorganic particles, based on elementary metal or metal alloy or based on metal oxides. 11. The rotating element according to claim 8, wherein the solid particles are inorganic particles, based on elementary metal or metal alloy or based on metal oxides. 12. The rotating element according to claim 9, wherein the solid particles are inorganic particles, based on elementary metal or metal alloy or based on metal oxides. 13. The rotating element according to claim 1, wherein the particles have an average size of less than 1 mm. 14. The rotating element according to claim 1, wherein the particles have an average size of less than 500 μm. 15. The rotating element according to claim 1, wherein the particles have an average size of less than 200 μm. 16. The rotating element according to claim 1, wherein the particles have an average size of less than 100 μm. 17. The rotating element according to claim 1, wherein adjustment of the viscosity of the damping medium by adjustment of the concentration and/or the particle size of the particles is used for adjusting the damping characteristics of the vibration damper. 18. The rotating element according to claim 1, wherein the movable solid damping body is a ball, and wherein the shape of the cavity is chosen such that damping takes place at least partly by impact damping on the walls of the cavity. 19. The rotating element according to claim 1, wherein the rotating element is a rotating blade of compressor or a turbine. 20. A turbo machine comprising: at least one rotating element according to claim 1, wherein the rotating element is a rotating blade of a compressor and/or a turbine thereof and wherein all rotating blades of a row of blades are equipped with the vibration damper. 21. A method for damping vibrations of a rotating element of a rotating machine during operation of the machine, wherein the rotating element comprises an airfoil having a tip shroud, the method comprising: locating in a closed cavity in the body of the rotating element, wherein in said closed cavity a movable solid damping body and a liquid metal as a damping medium, wherein said liquid metal at rest is in a cool state being a solid, and liquefying said metal during start-up, wherein said metal is in a liquid state at an operation temperature where damping is desired; andarranging the closed cavity, the movable solid damping body, and the damping medium in a lengthwise center of the airfoil, andthe damping medium is a dispersion of solid particles in the liquid metal which is in the liquid state at the operation temperature where damping is desired, wherein the solid particles have a melting point above 800° C. 22. The method according to claim 21, wherein the liquid metal is a dispersion of solid particles in a metal which is in liquid state at the operation temperature where damping is desired, wherein the solid particles have a melting point above 1000° C. 23. The method according to claim 21, wherein the liquid metal is a dispersion of solid particles in a metal which is in liquid state at the operation temperature where damping is desired, wherein the solid particles have a melting point above 2000° C. 24. A rotating element for a turbine machine, comprising: a root;an airfoil;a tip shroud; anda vibration damper for damping vibrations of the element during operation of the machine, wherein the vibration damper comprises a closed cavity in a body of the element, said closed cavity including a movable solid damping body and a damping medium, and wherein the closed cavity, the movable solid damping body, and the damping medium are arranged in a lengthwise center of the airfoil, and said damping medium comprising a metal which at rest is in a cool state being a solid, and during start-up, the metal liquefies and is in a liquid state at an operation temperature where damping is desired, andthe damping medium is a dispersion of solid particles in the metal which is in the liquid state at the operation temperature where damping is desired, wherein the solid particles have a melting point above 800° C.
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이 특허에 인용된 특허 (5)
Bagley Ronald L. ; Hollkamp Joseph J. ; Gordon Robert W., Centrifugal pendulum absorber for engine blades.
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