초록 ▼

A high velocity oxygen fuel thermal spray powder comprising a superalloy having the formula MCrAlY--X, wherein M is at least one metal taken from the group consisting of nickel, cobalt, and iron; X is at least one reactive element taken from the group consisting of hafnium, rhenium, lanthanum, and t

A high velocity oxygen fuel thermal spray powder comprising a superalloy having the formula MCrAlY--X, wherein M is at least one metal taken from the group consisting of nickel, cobalt, and iron; X is at least one reactive element taken from the group consisting of hafnium, rhenium, lanthanum, and tantalum; and yttrium is present in levels greater than 1% by weight of the total composition and up to about 6% by weight of the total composition. In addition, the powder may be blended with an agglomeration of M'CrAlY and a ceramic, wherein M' is at least one metal taken from the group consisting of nickel, cobalt, and iron. The invention offers improved high temperature oxidation, corrosion and creep resistance.

대표청구항 ▼

1. A method of applying a thermal barrier coating to an object comprising the steps of: (a) providing a thermal spray powder composition comprising a superalloy having the formula M--Cr--Al--Y--X, wherein M is at least one metal taken from the group consisting of nickel, cobalt, and iron; X i

1. A method of applying a thermal barrier coating to an object comprising the steps of: (a) providing a thermal spray powder composition comprising a superalloy having the formula M--Cr--Al--Y--X, wherein M is at least one metal taken from the group consisting of nickel, cobalt, and iron; X is at least one reactive element; and yttrium is present in levels from about 4% by weight of the total composition to about 6% by weight of the total composition; and (b) applying the powder to the object using high velocity oxygen fuel spraying. 2. The method of claim 1, wherein chromium is present in levels of 20-35% by weight of the total thermal spray powder composition. 3. The method of claim 2, wherein aluminum is present in levels of 5-15% by weight of the total thermal spray powder composition. 4. The method of claim 1, wherein said at least one reactive element is taken from the group consisting of hafnium, rhenium, lanthanum, and tantalum. 5. The method of claim 4, wherein said at least one reactive element is present in levels of 2-10% by weight of the total thermal spray powder composition. 6. The method of claim 1, wherein said at least one reactive element is present in levels of 2-10% by weight of the total thermal spray powder composition. 7. The method of claim 1, wherein yttrium is present in levels of about 4% by weight of the total thermal spray powder composition. 8. A method of applying a thermal barrier coating to an object comprising the steps of: (a) providing a thermal spray powder composition comprising (i) a first superalloy having the formula M--Cr--Al--Y--X, wherein M is at least one metal taken from the group consisting of nickel, cobalt, and iron; X is at least one reactive element; and yttrium is present in levels greater than 1% by weight of the first superalloy to about 6% by weight of the first superalloy, and (ii) an agglomeration of a second superalloy having the formula M'--Cr--Al--Y, and a ceramic, wherein M' is at least one metal taken from the group consisting of nickel, cobalt and iron; and (b) applying the powder to the object using high velocity oxygen fuel spraying. 9. The method in claim 8, wherein said ceramic is taken from the group consisting of alumina, yttria, and garnet. 10. The method in claim 8, wherein said ceramic is present in a level of 15% by weight of the agglomeration. 11. The method in claim 8, wherein said ceramic is present in levels of 3-15% by weight of the thermal spray powder composition. 12. The method in claim 8, wherein said ceramic is present in levels of 4.5-7.5% by weight of the total thermal spray powder composition. 13. The method in claim 8, wherein said agglomeration is present in levels of 30-50% by weight of the total thermal spray powder composition. 14. The method in claim 8, wherein the yttrium of the first superalloy is present in levels from about 1.5% by weight of the first superalloy to about 5.5% by weight of the first superalloy. 15. The method in claim 8, wherein the yttrium of the first superalloy is present in levels of about 4% by weight of the first superalloy.