Coating Repair for Ceramic Matrix Composite (CMC) Substrates
US-2021171409-A1 · Jun 10, 2021 · US
US2024084703A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2024084703-A1 |
| Application number | US-202318239532-A |
| Country | US |
| Kind code | A1 |
| Filing date | Aug 29, 2023 |
| Priority date | Sep 8, 2022 |
| Publication date | Mar 14, 2024 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
Methods for repairing a thermal barrier coating deposited on a component with localized spallation of the thermal barrier coating includes depositing a primer slurry on a thermally grown oxide of the component exposed by the localized spallation, depositing a ceramic slurry on the primer slurry, and heating the primer slurry and the ceramic slurry. The primer slurry includes a primer that includes at least one of a metal and a metal oxide. The ceramic slurry includes a ceramic material, a ceramic slurry binder material, and a ceramic slurry fluid carrier. Heating the primer slurry and the ceramic slurry forms a first chemical bond between the primer and the thermally grown oxide and a second chemical bond between the primer and the ceramic material.
Opening claim text (preview).
What is claimed is: 1 . A method for repairing a thermal barrier coating deposited on a component with localized spallation of the thermal barrier coating, comprising: depositing a primer slurry on a thermally grown oxide of the component exposed by the localized spallation, the primer slurry comprising a primer that includes at least one of a metal and a metal oxide; depositing a ceramic slurry on the primer slurry, the ceramic slurry comprising a ceramic material, a ceramic slurry binder material, and a ceramic slurry fluid carrier; and heating the primer slurry and the ceramic slurry to form a first chemical bond between the primer and the thermally grown oxide and a second chemical bond between the primer and the ceramic material. 2 . The method of claim 1 , wherein the ceramic material comprises yttria-stabilized zirconia particles. 3 . The method of claim 1 , wherein the ceramic slurry binder material is silicone based. 4 . The method of claim 1 , wherein the primer includes an organometallic precursor-derived metal oxide. 5 . The method of claim 1 , wherein the primer comprises Si. 6 . The method of claim 1 , wherein the primer comprises SiO 2 . 7 . The method of claim 1 , wherein the primer comprises MgO. 8 . The method of claim 1 , wherein the primer comprises Al. 9 . The method of claim 1 , wherein the primer comprises Cr 2 O 3 . 10 . The method of claim 1 , wherein the primer comprises Al 2 O 3 . 11 . The method of claim 1 , wherein the primer slurry comprises a primer slurry binder material having a different composition than the ceramic slurry binder material. 12 . The method of claim 1 , wherein the primer slurry comprises a first primer slurry and a second primer slurry having a different composition than the first primer slurry. 13 . The method of claim 12 , wherein the first primer slurry has a higher concentration of primer than the second primer slurry. 14 . The method of claim 1 , wherein: the heating the primer slurry and the ceramic slurry forms a primer layer comprising the primer and a repair thermal barrier coating comprising the ceramic material; the first chemical bond bonds the primer layer to the thermally grown oxide and the second chemical bond bonds the primer layer to the repair thermal barrier coating; and the primer layer has a thickness between 0.1 and 4 mils. 15 . The method of claim 14 , wherein the primer layer has a thermal expansion coefficient between 4 PPM/K and 10 PPM/K. 16 . The method of claim 14 , wherein a thickness of the primer layer is between 0.2 and 0.6 mils. 17 . The method of claim 1 , wherein the method is performed on wing. 18 . A material system for in-situ repair of a thermal barrier coating deposited on a component with localized spallation of the thermal barrier coating, comprising: a primer slurry comprising a primer chemically for bonding to a thermally grown oxide of the component exposed by the localized spallation, wherein the primer includes at least one of a metal and a metal oxide; and a ceramic slurry comprising a ceramic material, a binder material, and a fluid carrier, wherein the ceramic material is chemically for bonding to the primer and comprises yttria-stabilized zirconia particles. 19 . The material system of claim 18 , wherein the primer includes a metal and an oxide of the same metal. 20 . The material system of claim 18 , wherein the primer includes Ti.
Thermal properties, e.g. thermal expansion coefficient · CPC title
Stabilised zirconias, e.g. YSZ or cerium stabilised zirconia · CPC title
Coating not provided for in groups C23C2/00 - C23C24/00 · CPC title
characterised by the material treated · CPC title
Multiple coating or impregnating {multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation} · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.