Aluminum based abradable material with reduced metal transfer to blades
A turbomachine has a seal which mates to a plurality of airfoils. The seal is formed from an abradable aluminum based material having a plurality of hard phase particles embedded therein and having a melting point higher than a melting point of the melting point of the abradable coating matrix alloy.
1. A turbo-machine comprising:
a seal mating to a plurality of airfoils; and
said seal being formed from an abradable aluminum based material having a plurality of hard phase particles embedded therein and having a melting point higher than the melting point of the abradable coating matrix alloy, wherein said abradable aluminum based material is characterized by the absence of any solid lubricant in the aluminum based material.
2. The turbo-machine of claim 1 , wherein said abradable aluminum based material contains from 40 to 60 vol % aluminum.
3. The turbo-machine of claim 1 , wherein said abradable aluminum based material comprises an aluminum-silicon based alloy.
4. The turbo-machine of claim 1 , wherein said airfoils have tips, and said hard phase particles in the abradable material facilitate the removal of any material transferred from the seal to the tips.
5. The turbo-machine of claim 1 , wherein the hard phase particles have an average diameter in the range of from 1.0 micron to 45 microns.
6. The turbo-machine of claim 1 , wherein the hard phase particles have an average diameter in the range of from 5.0 microns to 45 microns.
7. The turbo-machine of claim 1 , wherein the hard phase particles have an average diameter in the range of from 5.0 microns to 20 microns.
8. The turbo-machine of claim 1 , wherein the hard phase particles are present in an amount sufficient to raise an effective surface melting point of a matrix material of the abradable aluminum base material to a temperature higher than a melting point of the matrix material during a rub event.
9. The turbo-machine of claim 1 , wherein the hard phase particles are present in an amount of less than 10 vol % of the abradable aluminum based material.
10. The turbo-machine of claim 1 , wherein the hard phase particles are present in an amount in the range of from 0.1 to 5.0 vol %.
11. The turbo-machine of claim 1 , wherein the hard phase particles are present in an amount in the range of from 1.0 to 5.0 vol %.
12. The turbo-machine of claim 1 , wherein the seal is an outer air seal.
13. A seal material comprising an abradable aluminum based material containing from 40 to 60 vol % aluminum and having a plurality of hard phase particles embedded therein and said hard phase particles being present in an amount less than 10 vol % of the aluminum based material.
14. The seal material of claim 13 , wherein said hard phase particles are present in an amount in the range of from 0.1 to 5.0 vol %.
15. The seal material of claim 13 , wherein said hard phase particles are present in an amount in the range of from 1.0 to 5.0 vol %.
16. The seal material of claim 13 , wherein said hard phase particles are present in an amount which is sufficient to remove transferred matrix material from airfoil tips.
17. The seal material of claim 13 , wherein the hard phase particles have a particle size in the range of from 1.0 to 45 microns.
18. The seal material of claim 13 , wherein said hard phase particles have a particle size in the range of from 5.0 to 45 microns.
19. The seal material of claim 13 , wherein said hard phase particles have a particle size in the range of from 5.0 to 20 microns.
20. The seal material of claim 13 , wherein said hard phase particles are selected from the group consisting of alumina, hard oxides, nitrides, carbides, intermetallics, and combinations thereof.