Methods of repairing a thermal barrier coating of a gas turbine component and the resulting components
US-2021025592-A1 · Jan 28, 2021 · US
US11913383B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11913383-B2 |
| Application number | US-202017615895-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 12, 2020 |
| Priority date | Jul 2, 2019 |
| Publication date | Feb 27, 2024 |
| Grant date | Feb 27, 2024 |
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The present invention provides a thermal barrier coated component, monitoring or evaluation of the soundness of which is able to be adequately carried out on the basis of the thermal boundary conditions that are detected by a sensor. A thermal barrier coated component according to the present invention comprises: a base material; a first bond coat layer that is a metal bonding layer formed on the base material; a sensor unit that comprises a sensor and a conductive wire, which are formed on the first bond coat layer; a second bond coat layer that is formed on the first bond coat layer so as to cover at least the sensor unit, while having a surface roughness higher than that of the first bond coat layer; and a top coat layer that is formed on the second bond coat layer.
Opening claim text (preview).
The invention claimed is: 1. A thermal barrier coated component comprising: a base material; a first bond coat layer that is a metal bonding layer formed on the base material; a sensor unit disposed on the first bond coat layer and including a sensor and a conductive wire; a second bond coat layer that is formed on the first bond coat layer so as to cover at least the sensor unit such that the sensor is arranged between the first bond coat layer and the second bond coat layer, wherein the second bond coat layer has a surface roughness higher than that of the first bond coat layer; and a top coat layer that is formed on the second bond coat layer. 2. The thermal barrier coated component according to claim 1 , wherein the second bond coat layer includes more pores than the first bond coat layer. 3. The thermal barrier coated component according to claim 2 , wherein the first bond coat layer has a porosity of 0% by volume or more and 5.0% by volume or less, and the second bond coat layer has a porosity of 0.1% by volume or more and 10.0% by volume or less. 4. The thermal barrier coated component according to claim 1 , wherein the sensor is any one of a thermocouple sensor, a heat flux sensor, a strain sensor, and a sensor that detects a crack generated in the first bond coat layer, the second bond coat layer, and the top coat layer. 5. The thermal barrier coated component according to claim 1 , wherein the second bond coat layer is thinner than the first bond coat layer. 6. A method for producing a thermal barrier coated component, comprising: forming a first bond coat layer, which is a metal bonding layer, on a base material; disposing a sensor unit including a sensor and a conductive wire on the first bond coat layer; forming a second bond coat layer having a surface roughness higher than that of the first bond coat layer on the first bond coat layer so as to cover at least the sensor unit such that the sensor is arranged between the first bond coat layer and the second bond coat layer; and forming a top coat layer on the second bond coat layer. 7. The method for producing a thermal barrier coated component according to claim 6 , wherein in the forming of the first bond coat layer, the first bond coat layer is formed by either a high velocity oxygen fuel spraying or a low pressure plasma spraying, and in the forming of the second bond coat layer, the second bond coat layer is formed by an atmospheric plasma spraying. 8. The method for producing a thermal barrier coated component according to claim 6 , wherein the disposing of the sensor unit includes drawing the sensor on the first bond coat layer by spraying.
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