Provided are a thermal barrier coating material and a member coated with thermal barrier that can suppress the separation when used at a high temperature, and have a high thermal barrier effect; a method for manufacturing the member coated with thermal barrier; a turbine member coated with the thermal barrier coating material; and a gas turbine. More specifically provided are a shield coating member comprising a heat-resistant substrate, a bond coat layer formed on the heat-resistant substrate, and a ceramic layer formed on the bond coat layer, wherein the ceramic layer comprises a ceramic represented by a general formula A 2 Zr 2 O 7 , wherein A denotes a rare earth element, and the ceramic layer has (a) a porosity of 1 to 30%, (b) cracks in a thickness direction in pitches of 5 to 100% the total thickness of layers other than the bond coat layer on the heat-resistant substrate, or (c) columnar crystals.

Claims

6 · 1 independent · depth 2

6 granted claims

›1.independentA member coated with thermal barrier comprising:na heat-resistant substrate,a bond coat layer formed on the heat-resistant substrate, anda ceramic lay…+5

Classifications

5 codes

IPC · International Patent Classification

Section H — Electricity

H01L23/06

USPC · US Patent Classification

257/703257/632257/E23.002257/641

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4.7 y

1,715 days filing → grant

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Examiner

Wai-Sing Louie

art unit 2814 · TC 2800

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Citations: 16 back · 0 forward

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1 priority documents

›Priority documents — 1

Type	Document	Date
related publication	US 20060151856 A1	13 Jul 2006

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