US2023082214A1PendingUtilityA1

Coating method, coating layer, and turbine shroud

Assignee: MITSUBISHI HEAVY IND AERO ENGINES LTDPriority: Sep 8, 2016Filed: Nov 16, 2022Published: Mar 16, 2023
Est. expirySep 8, 2036(~10.1 yrs left)· nominal 20-yr term from priority
Y02T50/60C04B 35/80C04B 41/009C04B 41/52C23C 4/02C04B 2111/00405F05D 2250/63F05D 2300/6033C04B 41/87C04B 41/5031F05D 2240/11F05D 2300/2118F01D 11/122C04B 41/89F01D 5/28
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Claims

Abstract

A coating method includes depositing a slurry including a coarsely particulate ceramic and a finely particulate ceramic on a base material configured with an oxide-based ceramics matrix composite such that a proportion of coarse particles decreases towards a surface of the base material; forming a bond coating by performing a heat treatment on the base material on which the slurry has been deposited; and forming a top coating by thermally spraying a ceramic onto the bond coating. The oxide-based ceramics matrix composite is an alumina silica type oxide-based ceramics matrix composite. The coarsely particulate ceramic and the finely particulate ceramic are alumina-based powder.

Claims

exact text as granted — not AI-modified
1 . A coating film comprising:
 a bond coating obtained by baking a coating material including a coarsely particulate ceramic and a finely particulate ceramic on a base material configured with an oxide-based ceramics matrix composite such that a proportion of coarse particles decreases towards a surface of the base material; and   a top coating formed by thermally spraying a ceramic onto the bond coating,   wherein the oxide-based ceramics matrix composite is an alumina silica type oxide-based ceramics matrix composite, and   the coarsely particulate ceramic and the finely particulate ceramic are alumina-based powder.   
     
     
         2 . The coating film according to  claim 1 , wherein the bond coating includes
 a first bond coating obtained by baking a first coating material in which the coarsely particulate ceramic and the finely particulate ceramic are mixed at a first proportion which has been preset, and   a second bond coating obtained by baking a second coating material in which the coarsely particulate ceramic and the finely particulate ceramic are mixed at a second proportion having a proportion of coarse particles, which is lower than that in the first proportion, on a surface of the first bond coating.   
     
     
         3 . A turbine shroud in which the coating film according to  claim 1  is provided on an inner surface. 
     
     
         4 . A coating film comprising:
 a bond coating obtained by baking a coating material including a coarsely particulate ceramic and a finely particulate ceramic on a base material configured with an oxide-based ceramics matrix composite such that a proportion of coarse particles decreases towards a surface of the base material; and   a top coating formed by thermally spraying a ceramic onto the bond coating,   wherein the oxide-based ceramics matrix composite is a pure alumina type oxide-based ceramics matrix composite, and   the coarsely particulate ceramic and the finely particulate ceramic are alumina-based powder and zirconia-based powder.   
     
     
         5 . The coating film according to  claim 4 , wherein the bond coating includes
 a first bond coating obtained by baking a first coating material in which the coarsely particulate ceramic and the finely particulate ceramic are mixed at a first proportion which has been preset, and   a second bond coating obtained by baking a second coating material in which the coarsely particulate ceramic and the finely particulate ceramic are mixed at a second proportion having a proportion of coarse particles, which is lower than that in the first proportion, on a surface of the first bond coating.   
     
     
         6 . A turbine shroud in which the coating film according  claim 4  is provided on an inner surface. 
     
     
         7 . A coating film comprising:
 a bond coating obtained by baking a coating material including a coarsely particulate ceramic and a finely particulate ceramic on a base material configured with an oxide-based ceramics matrix composite such that a proportion of coarse particles decreases towards a surface of the base material; and   a top coating formed by thermally spraying a ceramic onto the bond coating,   wherein the top coating is a zirconia abradable top coating.   
     
     
         8 . The coating film according to  claim 7 , wherein the bond coating includes
 a first bond coating obtained by baking a first coating material in which the coarsely particulate ceramic and the finely particulate ceramic are mixed at a first proportion which has been preset, and   a second bond coating obtained by baking a second coating material in which the coarsely particulate ceramic and the finely particulate ceramic are mixed at a second proportion having a proportion of coarse particles, which is lower than that in the first proportion, on a surface of the first bond coating.   
     
     
         9 . A turbine shroud in which the coating film according  claim 7  is provided on an inner surface.

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