IP Library Granted Patent US 7,374,821
Granted Patent B2
US 7,374,821 · App. 10/911,598 · Granted May 20, 2008

Thermal barrier composition and a ceramic coating having such a composition

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Quick Facts
Patent No.
US 7,374,821
App. No.
10/911,598
Granted
May 20, 2008
Kind
B2
Abstract

The invention relates to a ceramic thermal barrier composition of low conductivity and high high-temperature strength. In characteristic manner, the composition comprises a zirconia base, at least one trivalent oxide enabling the zirconia to be stabilized and enabling the thermal conductivity of the zirconia to be reduced in optimum manner, and at least one pentavalent oxide enabling the content of oxygen vacancies to be reduced so as to make it substantially equal to that of a partially stabilized zirconia. Preferably, said trivalent oxide is present with a molar content constituted by a first portion enabling the zirconia to be stabilized partially and a second portion which introduces point defects into the lattice said pentavalent oxide is present with a molar concentration equal to said molar concentration of said second portion of the trivalent oxide. The invention is applicable to making a superalloy machine part having a ceramic coating with said composition, and possibly also a bonding underlayer.

Claims (16)

1. A thermal barrier composition of low thermal conductivity and of high high-temperature strength, made of ceramic, the composition comprising a zirconia base, at least one trivalent oxide enabling the zirconia to be stabilized, and enabling the thermal conductivity of the zirconia to be reduced in optimum manner, and at least one pentavalent oxide enabling the content of oxygen vacancies to be reduced so as to make it substantially equal to that of the partially stabilized zirconia, said trivalent oxide being selected from the group consisting of: erbium oxide, europium oxide, praseodymium oxide, terbium oxide, holmium oxide, and mixtures thereof.

2. A thermal barrier composition according to claim 1 , wherein said trivalent oxide is present at a molar concentration constituted by a first portion enabling the zirconia to be stabilized partially, and by a second portion which introduces point defects into the lattice, and wherein said pentavalent oxide is present at a molar concentration equal to said molar concentration of said second portion of the trivalent oxide.

3. A thermal barrier composition according to claim 1 , wherein said pentavalent oxide is selected from the group consisting of niobium oxide, tantalum oxide, and mixtures thereof.

4. A thermal barrier composition according to claim 1 , wherein said trivalent oxide is present at a molar concentration lying in the range 4% to 30%.

5. A thermal barrier composition according to claim 1 , wherein said pentavalent oxide is present at a molar concentration lying in the range 2% to 20%.

6. A thermal barrier composition according to claim 1 , wherein the difference between the molar concentration of the trivalent oxide and the molar concentration of the pentavalent oxide lies in the range 4% to 12%.

7. A superalloy machine part including a ceramic coating having a composition according to claim 1 .

8. A superalloy machine part according to claim 7 , further including a bonding underlayer on which said ceramic coating is deposited.

9. A superalloy machine part according to claim 8 , wherein said bonding underlayer is constituted by an alloy suitable for forming a protective alumina layer by oxidation.

10. A superalloy machine part according to claim 9 , wherein said bonding underlayer is constituted by an alloy of the MCrAlY type, where M is a metal selected from nickel, cobalt, iron, or a mixture of said metals.

11. A superalloy machine part according to claim 9 , wherein said bonding underlayer is constituted by a nickel aluminide optionally containing a metal selected from platinum, chromium, palladium, ruthenium, iridium, osmion, rhodium, or a mixture of these metals, and/or a reactive element selected from zirconium, hafnium, and yttrium.

12. A superalloy machine part according to claim 8 , said ceramic coating further comprising, on said underlayer, a ceramic layer based on yttrium-containing zirconia, having a molar content of yttrium oxide lying in the range 4% to 12%.

13. A ceramic coating comprising a bonding underlayer, a first ceramic layer based on yttrium-containing zirconia having a molar content of yttrium oxide lying in the range 4% to 12%, and a second ceramic layer presenting a composition according to claim 1 , said first ceramic layer being situated between said bonding underlayer and said second ceramic layer.

14. A thermal barrier composition according to claim 1 , wherein said pentavalent oxide is present at a molar concentration lying in the range of 4% to 12%.

15. A thermal barrier composition according to claim 1 , wherein said pentavalent oxide is present at a molar concentration lying in the range of 3% to 10%.

16. A thermal barrier composition according to claim 1 , wherein the difference between the molar concentration of the trivalent oxide is substantially equal to 4%.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →