Coated member, coating material, and method of manufacturing coated member

Patent metadata

Field	Value
Publication number	US-11059751-B2
Application number	US-201615549516-A
Country	US
Kind code	B2
Filing date	Feb 9, 2016
Priority date	Feb 9, 2015
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

A coated member includes a heat-shielding coating layer made of a zirconia-dispersed silicate in which ytterbia-stabilized zirconia is precipitated as a dispersed phase in a matrix phase which is any one of a rare earth disilicate, a rare earth monosilicate, and a mixed phase of the rare earth disilicate and the rare earth monosilicate. The rare earth disilicate is a (Y 1-a [Ln 1 ] a ) 2 Si 2 O 7 solid solution wherein Ln 1 is any one of Sc, Yb, and Lu, or a (Y 1-c [Ln 2 ] c ) 2 Si 2 O 7 solid solution wherein Ln 2 is any one of Nd, Sm, Eu, and Gd. The rare earth monosilicate is Y 2 SiO 5 , [Ln 1 ′] 2 SiO 5 , a (Y 1-b [Ln 1 ′]b) 2 SiO 5 solid solution wherein Ln 1 ′ is any one of Sc, Yb, and Lu, or a (Y 1-d [Ln 2 ′] d ) 2 SiO 5 solid solution wherein Ln 2 ′ is any one of Nd, Sm, Eu, and Gd.

First claim

The invention claimed is:

1. A method of manufacturing a coated member, the method comprising:
forming a heat-shielding coating layer on a substrate by spraying particles onto the substrate made of a silicon-based ceramic or a ceramic fiber-reinforced ceramic matrix composite, the particles being obtained by mixing any one of rare earth disilicate powder, rare earth monosilicate powder and mixed powder of the rare earth disilicate powder and the rare earth monosilicate powder with ytterbia-stabilized zirconia powder containing ytterbia in a content of 8 wt % or more and 27 wt % or less and diffusion heat-treating the obtained mixed powder at a temperature of 1300° C. or more and 1700° C. or less,
wherein the rare earth disilicate powder is made a (Y 1-a [Ln 1 ] a ) 2 Si 2 O 7 solid solution (here, Ln 1 is any one of Sc, Yb, and Lu, a is 0.05 or more and less than 1 when Ln 1 is Sc, and a is 0.2 or more and less than 1 when Ln 1 is Yb or Lu, and
the rare earth monosilicate powder is made of a (Y 1-b [Ln 1 ′] b ) 2 SiO 5 solid solution (here, Ln 1 ′ is any one of Sc, Yb, and Lu, and 0<b≤0.5).

2. The method of claim 1 , wherein the substrate is made of an oxide-based ceramic fiber-reinforced oxide-based ceramic matrix composite or a SiC fiber-reinforced SiC matrix composite.

3. The method of claim 2 , wherein the oxide-based ceramic fiber-reinforced oxide-based ceramic matrix composite is an Al 2 O 3 fiber-reinforced Al 2 O 3 matrix composite.

4. The method of claim 1 , wherein an addition amount of the ytterbia-stabilized zirconia in the particles is 50 vol % or more and 90 vol % or less.

5. The method of claim 1 , wherein any one of the rare earth disilicate powder, the rare earth monosilicate powder, and the mixed powder thereof is mixed with the ytterbia-stabilized zirconia at a mixing ratio at which a difference in thermal expansion coefficient between the substrate and the heat-shielding coating layer is less than 3×10 −6 /K.

6. A method of manufacturing a coated member, the method comprising:
forming a heat-shielding coating layer on a substrate by spraying particles onto the substrate made of a silicon-based ceramic or a ceramic fiber-reinforced ceramic matrix composite, the particles being obtained by mixing any one of rare earth disilicate powder, rare earth monosilicate powder and mixed powder of the rare earth disilicate powder and the rare earth monosilicate powder with ytterbia-stabilized zirconia powder containing ytterbia in a content of 8 wt % or more and 27 wt % or less and diffusion heat-treating the obtained mixed powder at a temperature of 1300° C. or more and 1700° C. or less,
wherein the rare earth disilicate powder is made of any one of a (Y 1-c [Ln 2 ] c ) 2 Si 2 O 7 solid solution (here, Ln 2 is any one of Nd, Sm, Eu, and Gd, c is 0.1 or more and less than 1 when Ln 2 is Nd, Sm, or Eu, and c is 0.2 or more and less than 1 when Ln 2 is Gd, and
the rare earth monosilicate powder is made of a (Y 1-d [Ln 2 ′] d ) 2 SiO 5 solid solution (here, Ln 2 ′ is any one of Nd, Sm, Eu, and Gd, and 0<d≤0.5).

7. The method of claim 6 , wherein the substrate is made of an oxide-based ceramic fiber-reinforced oxide-based ceramic matrix composite or a SiC fiber-reinforced SiC matrix composite.

8. The method of claim 7 , wherein the oxide-based ceramic fiber-reinforced oxide-based ceramic matrix composite is an Al 2 O 3 fiber-reinforced Al 2 O 3 matrix composite.

9. The method of claim 6 , wherein an addition amount of the ytterbia-stabilized zirconia in the particles is 50 vol % or more and 90 vol % or less.

10. The method of claim 6 , wherein any one of the rare earth disilicate powder, the rare earth monosilicate powder, and the mixed powder thereof is mixed with the ytterbia-stabilized zirconia at a mixing ratio at which a difference in thermal expansion coefficient between the substrate and the heat-shielding coating layer is less than 3×10 −6 /K.

Assignees

• Mitsubishi Heavy Ind Aero Engines Ltd

Inventors

• Matsumoto Mineaki
• Kurimura Takayuki
• Nishikawa kosuke
• Hanada Tadayuki

Classifications

• C04B2235/3224

  Rare earth oxide or oxide forming salts thereof, e.g. scandium oxide · CPC title

• C04B35/10

  based on aluminium oxide · CPC title

• C04B35/62675

  characterised by the treatment temperature · CPC title

• C04B2235/3246

  Stabilised zirconias, e.g. YSZ or cerium stabilised zirconia · CPC title

• F05D2300/15

  Rare earth metals, i.e. Sc, Y, lanthanides · CPC title