IP Library Granted Patent US 7,396,592
Granted Patent B2
US 7,396,592 · App. 11/953,491 · Granted Jul 8, 2008

Target for vaporizing under an electron beam, a method of fabricating it, a thermal barrier and a coating obtained from a target, and a mechanical part including such a coating

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Quick Facts
Patent No.
US 7,396,592
App. No.
11/953,491
Granted
Jul 8, 2008
Kind
B2
Abstract

The invention relates to a composite target in the form of a bar made of ceramic powders and designed to be evaporated under an electron beam, the target comprising zirconia and at least one zirconia stabilizer. In characteristic manner, said target is wherein said zirconia stabilizer is at a molar content lying in the range 2% to 30% and wherein said zirconia is formed by more than 90% of a monoclinic phase. The invention is applicable to fabricating a ceramic thermal barrier of low thermal conductivity and high thermomechanical strength formed by evaporation under an electron beam.

Claims (20)

1. A ceramic thermal barrier of low thermal conductivity and high thermomechanical strength, comprising:

a composite target in the form of a bar made of ceramic powders, the target comprising zirconia and at least one zirconia stabilizer, said zirconia stabilizer being included at a molar content lying in a range of 2% to 30%, wherein

after sintering of the target, said zirconia in the target contains more than 90% of a monoclinic phase,

the barrier is formed by evaporating the composite target under an electron beam, and

the barrier is deposited on a substrate made of superalloy.

2. A ceramic coating composition, comprising:

a bonding underlayer;

a first ceramic layer based on yttrified zirconia having a molar content of yttrium oxide lying in the range 4% to 12%; and

a second ceramic layer formed by a thermal barrier of low thermal conductivity and high thermomechanical strength, including

a composite target in the form of a bar made of ceramic powders, the target comprising zirconia and at least one zirconia stabilizer, said zirconia stabilizer being included at a molar content lying in a range of 2% to 30%, wherein after sintering of the target, said zirconia in the target contains more than 90% of a monoclinic phase, the barrier is formed by evaporating the composite target under an electron beam, and the barrier is deposited on a substrate made of superalloy,

wherein said first ceramic layer is situated between said bonding underlayer and said second ceramic layer.

3. A mechanical part made of superalloy, comprising:

a ceramic coating including a thermal barrier obtained from a composite target in the form of a bar made of ceramic powders, the target comprising zirconia and at least one zirconia stabilizer, said zirconia stabilizer being included at a molar content lying in a range of 2% to 30%, wherein

after sintering of the target, said zirconia in the target contains more than 90% of a monoclinic phase,

the barrier is formed by evaporating the composite target under an electron beam.

4. A superalloy mechanical part according to claim 3 , further including a bonding underlayer on which said ceramic coating is deposited.

5. A superalloy mechanical part according to claim 4 , wherein said bonding underlayer is constituted by an alloy suitable for forming a protective alumina layer by oxidation.

6. A superalloy mechanical part according to claim 4 , wherein said bonding underlayer is constituted by an alloy of the MCrAlY type, where M is a metal selected from the group consisting of nickel, cobalt, iron, and mixtures of these metals.

7. A superalloy mechanical part according to claim 4 , wherein said bonding underlayer is constituted by a nickel aluminide optionally containing a metal selected from the group consisting of platinum, chromium, palladium, ruthenium, iridium, osmium, rhodium, or a mixture of these metals, and/or a reactive element selected from the group consisting of zirconium, hafnium, and yttrium.

8. A superalloy mechanical part according to claim 3 , wherein said ceramic coating further includes, on said underlayer, a ceramic layer based on yttrified zirconia having a molar content of yttrium oxide lying in the range 4% to 12%.

Assignments (4)
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 →
MERGER Recorded May 17, 2018
From: SNECMA SERVICES SA (A/K/A SNECMA SERVICES)
To: SNECMA
Reel/Frame 045829/0954 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →