Airfoils with vibration damping system
View Patent ↗The disclosure relates to adjacently mounted circumferentially distributed turbo machine airfoils with a vibration damping system. Each adjacent pair of airfoils includes a fixing and receiving portion, extending between the paired adjacent airfoils, each with a face that are proximal (e.g., in contact with) each other. Vibration can be suppressed by the fixing and receiving portions each having a received magnet fixingly installed therein and a non-magnetic conducting plate therebetween. Each magnet has a pole that faces the pole of the other magnet in between which the non-magnetic conducting plate is located and in which eddy currents can be induced by the relative movement of the magnets due to vibration.
1. A vibration damping system for adjacently mounted circumferential distributed turbo machine airfoils, the system comprising:
a first fixing and receiving portion, configured to extend from a first airfoil to an end defining a first face;
a second fixing and receiving portion configured to extend towards the first fixing and receiving portion to establish an end defining a second face proximal with the first face of the first fixing and receiving portion;
a first magnet, fixed in the first fixing and receiving portion and arranged such that a pole faces towards the first face of the first fixing and receiving portion;
a first non-magnetic conducting plate mounted between the first face and the first magnet; and
a second magnet, fixed in the second fixing and receiving portion and arranged such that a pole which faces the second face is aligned with, and separated by a separation distance from the pole of the first magnet.
2. The vibration damping system of claim 1 wherein the poles of the first and second magnets which face one another have opposite polarities.
3. The vibration damping system of claim 2 , wherein the first magnet and the second magnet are separated by a distance of between 1 mm and 5 mm.
4. The vibration damping system of claim 3 , wherein the second fixing and receiving portion has a second non-magnetic conducting plate mounted between the second magnet and the second face, wherein the first non-magnetic conducting plate and the second non-magnetic conducting plate are made of a material with an electrical conductivity of greater than 35×10 6 S·m −1 measured at 20° C.
5. The vibration damping system of claim 2 , wherein the second fixing and receiving portion has a second non-magnetic conducting plate mounted between the second magnet and the second face, wherein the first non-magnetic conducting plate and the second non-magnetic conducting plate are made of a material with an electrical conductivity of greater than 35×10 6 S·m −1 measured at 20° C.
6. The vibration damping system of claim 1 wherein the second fixing and receiving portion has a second non-magnetic conducting plate mounted between the second magnet and the second face.
7. The vibration damping system of claim 6 , wherein the first non-magnetic conducting plate and the second non-magnetic conducting plate are made of a material with an electrical conductivity of greater than 35×10 6 S·m −1 measured at 20° C.
8. The vibration damping system of claim 6 , wherein the first magnet and the second magnet are separated by a distance of between 1 mm and 5 mm.
9. The vibration damping system of claim 6 , wherein the first non-magnetic conducting plate and the second non-magnetic conducting plate are made of a material with an electrical conductivity of greater than 35×10 6 S·m −1 measured at 20° C.
10. The vibration damping system of claim 1 , wherein the first magnet and the second magnet are separated by a distance of between 1 mm and 5 mm.
11. The vibration damping system of claim 10 , wherein the second fixing and receiving portion has a second non-magnetic conducting plate mounted between the second magnet and the second face, wherein the first non-magnetic conducting plate and the second non-magnetic conducting plate are made of a material with an electrical conductivity of greater than 35×10 6 S·m −1 measured at 20° C.
12. The vibration damping system of claim 1 , wherein the first face and the second face are in contact with one another.
13. A turbo machine comprising:
a first airfoil and a second airfoil; and
a vibration damping system which includes:
a first fixing and receiving portion, configured to extend from within the first airfoil to an end defining a first face;
a second fixing and receiving portion configured to extend from within the second airfoil towards the first fixing and receiving portion to establish an end defining a second face proximal with the first face of the first fixing and receiving portion;
a first magnet, fixed in the first fixing and receiving portion and arranged such that a pole faces towards the first face of the first fixing and receiving portion;
a first non-magnetic conducting plate mounted between the first face and the first magnet; and
a second magnet, fixed in the second fixing and receiving portion and arranged such that a pole which faces the second face is aligned with, and separated by a separation distance from the pole of the first magnet.
14. The vibration damping system of claim 13 , wherein the first face and the second face are in contact with one another.