초록 ▼

A method is provided for damping vibrations in a turbine. The method includes performing structural dynamics analysis on the turbine to determine at least one area of high vibrational stress on the turbine, and performing thermal analysis of the turbine to determine at least an approximated maximum

A method is provided for damping vibrations in a turbine. The method includes performing structural dynamics analysis on the turbine to determine at least one area of high vibrational stress on the turbine, and performing thermal analysis of the turbine to determine at least an approximated maximum operating temperature at the area of high vibrational stress. Additionally, the method includes utilizing hysteresis damping to dampen operational vibrations. The hysteresis damping includes selecting a shape memory alloy (SMA) having a martensitic-to-austenite transformation temperature substantially similar to the approximate maximum operating temperature of the component at the area of high vibrational stress, and disposing the selected SMA on the turbine on the related area of high vibratory stress.

대표청구항 ▼

1. A method for damping vibrations in a turbine engine during operation, wherein said method comprises:determining at least one area of high vibratory stress on a component of the turbine engine;determining at least an approximate maximum operating temperature at the area of high vibratory stress;di

1. A method for damping vibrations in a turbine engine during operation, wherein said method comprises:determining at least one area of high vibratory stress on a component of the turbine engine;determining at least an approximate maximum operating temperature at the area of high vibratory stress;disposing a shape memory alloy (SMA) on a surface of the component at the area of high vibratory stress such that the SMA is an integral part of the surface; andutilizing hysteresis damping to dampen vibrations at the area of high vibratory stress based on the approximate maximum operating temperature. 2. The method of claim 1, wherein determining at least one area of high vibratory stress comprises performing structural dynamics analysis on the component. 3. The method of claim 1, wherein determining the approximate maximum operating temperature comprises performing thermal analysis of the component during operation. 4. The method of claim 1, wherein utilizing hysteresis damping comprises selecting the SMA to have a martensitic-to-austenite transformation temperature substantially similar to the approximate maximum operating temperature of the component at the area of high vibratory stress. 5. The method of claim 1, wherein disposing the selected SMA comprises applying the SMA to the area of high vibratory stress using physical vapor deposition. 6. The method of claim 1, wherein disposing the selected SMA comprises brazing the SMA to the area of high vibratory stress. 7. The method of claim 1, wherein disposing the selected SMA comprises thermally spraying a SMA coating on the area of high vibratory stress. 8. The method of claim 1, wherein disposing the selected SMA comprises at least one of welding the SMA to the area of high vibratory stress and mechanically attaching the SMA to the area of high vibratory stress. 9. A turbine engine resistive to vibratory damage during operation, said turbine engine comprising:a housing;a disk rotatably mounted within said housing;at least one blade connected to said disk, at least one of said disk and said blade having at least one area susceptible to high vibratory stress during operation of said engine; anda shape memory alloy (SMA) disposed on a surface of said blade or said disk at said area of high vibratory stress such that the SMA is an integral part of said surface, the SMA for dissipating vibrational energy in said turbine engine, wherein the dissipation of vibrational energy is a result of hysteresis loops generated by the SMA. 10. The engine of claim 9, wherein said area of high vibratory stress has at least an approximate maximum operating temperature. 11. The engine of claim 10, wherein said SMA has a martensitic-to-austenite transformation temperature. 12. The engine of claim 11, wherein said martensitic-to-austenite transformation temperature of said SMA is substantially similar to the approximated maximum operating temperature of said area of high vibratory stress. 13. The engine of claim 9, wherein said SMA is disposed on said blade using physical vapor disposition. 14. The engine of claim 9, wherein said SMA is disposed on said blade by brazing the SMA to the area of high vibratory stress. 15. The engine of claim 9, wherein said SMA is disposed on said blade by thermally spraying the SMA on the area of high vibratory stress. 16. The engine of claim 9, wherein said SMA is disposed on said blade by at least one of welding the SMA to the area of high vibratory stress and mechanically attaching the SMA to the area of high vibratory stress. 17. A method for damping vibrations in a turbine during operation, wherein said method comprises:performing thermal analysis of the turbine to determine at least an approximate maximum operating temperature;selecting a shape memory alloy (SMA) having a martensitic-to-austenite transformation temperature substantially similar to the approximate maximum operating temperature of the turbine;disposing the SMA on a surface of a component of the turbin e at a location on the component of high vibratory stress such that the SMA is an integral part of the surface; andutilizing hysteresis damping to dampen operational vibrations in the turbine independent from a determination of a resonant frequency of vibration in the turbine. 18. The method of claim 17, wherein disposing the SMA comprises at least one of:applying the SMA to the turbine using physical vapor deposition;applying the SMA to the turbine using thermal spray cladding;brazing the SMA to the turbine;welding the SMA to the turbine; andmechanically attaching the SMA to the turbine.