Oxidation resistant bond coat layers, processes for coating articles, and their coated articles

Patent metadata

Field	Value
Publication number	US-11459650-B2
Application number	US-201715789393-A
Country	US
Kind code	B2
Filing date	Oct 20, 2017
Priority date	Oct 20, 2017
Publication date	Oct 4, 2022
Grant date	Oct 4, 2022

Abstract

A coated article including an article having a surface; an oxidation resistant bond coat layer deposited on the surface, the oxidation resistant bond coat layer comprising a healing silica matrix and at least one oxygen scavenger forming a metal silicide network dispersed within the healing silica matrix; and a top coat layer disposed upon the oxidation resistant bond coat layer, whereby the oxidation resistant bond coat layer is operable to seal a crack in the top coat layer.

First claim

What is claimed is:

1. A process for applying an oxidation resistant bond coat layer to an article, comprising:
forming a slurry consisting of components of: one or multiple silicide and boride powders, silica-containing matrix constituents, a viscosity modifier and a liquid medium, wherein the silica-containing matrix constituents consist of at least one of the following: silica, silicon oxycarbide (SiOC), aluminosilicate, borosilicate, and glass, wherein the components of the slurry are present such that the slurry consists of:
at least 10% to up to 70% by volume of the slurry of at least one silica based material with glass phases having a viscosity of 100 to 10,000,000 poise at a temperature of 1,292° F. (700° C.) to 3,272° F. (1800° C.),
at least 30% to up to 90% by volume of the slurry of at least one oxygen scavenger selected from the group consisting of at least one silicide of molybdenum, chromium, titanium, hafnium, zirconium, yttrium, and mixtures thereof, and a boride of at least one of the following: molybdenum, tantalum, chromium, titanium, hafnium, zirconium, yttrium and mixtures thereof,
wherein the viscosity modifier is selected from the group consisting of a mullite, a hafnium oxide, a zirconium oxide, or combination thereof;

coating an article with the slurry to form a slurry coated article;
subjecting the slurry coated article to a first heat treatment in an inert atmosphere at a temperature below 2190° F. (1200° C.), wherein during the first heat treatment, healing silica matrix from any one of the silica-based material with glass phases or the silica-containing matrix surrounds the at least one oxygen scavenger; and
subjecting the slurry coated article to a second heat treatment subsequent to the first heat treatment in air at 2372° F.-3002° F. (1,300° C.-1,650° C.) to form a metal silicide network in the healing silica matrix to form an oxidation resistant bond coat layer on a surface of the article, wherein the healing silica matrix protects the oxygen scavenger from oxidation during the second heat treatment; and
applying a top coat layer onto the oxidation resistant bond coat layer.

2. The process as recited in claim 1 , wherein the top coat layer comprises at least one of the following: refractory oxide material, rare earth oxides, mixed rare earth and refractory metal oxides, alkaline earth oxides, rare earth silicates, refractory metal silicates, mixed metal silicates, borosilicates, aluminum silicates, or mixtures thereof.

3. The process as recited in claim 1 , wherein the refractory oxide material is selected from the group consisting of TaxOy (where x=1 to 3 and y=1 to 5), NbxOy (where x=1 to 3 and y=1 to 5), MgO, CaO, SrO, BaO, SiO2, HfO2, TiO2, ZrO2, Al2O3, Y2O3, La2O3, rare earth oxides, yttrium silicate, hafnium silicate, ytterbium silicate and mixtures thereof.

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Tang Xia
• Jarmon David C
• Beals James T
• Jackson R Wesley
• Sheedy Paul

Classifications

• F05D2230/90

  Coating; Surface treatment · CPC title

• C23C24/08

  by application of heat or pressure and heat (C23C24/04 takes precedence) · CPC title

• F05D2300/2261

  of silicon · CPC title

• F05D2220/80

  in supersonic vehicles excluding hypersonic vehicles or ram, scram or rocket propulsion · CPC title

• F01D5/284

  Selection of ceramic materials · CPC title