Method for simultaneously protecting carbon-containing components against catalytic oxidation and high temperature non-catalytic oxidation
Coated articles ( 19 ) that comprise components, made of carbon fiber or carbon-carbon composites which may be configured, for example, as aircraft landing system brake discs. The components ( 10 ) are coated with a system that includes a phosphorus-containing undercoating ( 11 ) having a specified formulation and a boron-containing overcoating ( 12 ) having specified formulation. The coated articles of the invention, e.g., aircraft brake discs, are protected against catalytic oxidation when the article is subjected to temperatures of 800° C. (1472° F.) or greater. Also, a method of protecting a component made of a carbon fiber or carbon-carbon composite simultaneously against catalytic oxidation (e.g., catalyzed by de-icer compositions) and high temperature non-catalytic oxidation.
1. A method of protecting a component made of carbon fiber or carbon-carbon composite simultaneously against catalytic oxidation and high temperature non-catalytic oxidation, which method comprises:
covering said composite with an undercoating comprising ions formed from 10-80 wt % H 2 O, 20-70 wt % H 3 PO 4 , 0.1-25 wt % alkali metal mono-, di-, or tri-basic phosphate, 0-2 wt % B 2 O 3 , and 0-25 wt % MnHPO 4 .1.6H 2 O, 0-30 wt % AlPO 4 , and 0-10 wt % Zn 3 (PO 4 ) 2 , provided that at least one of AlPO 4 , MnHPO 4 .1.6H 2 O, and Zn 3 (PO 4 ) 2 is present, said undercoating having a thickness of approximately 1-10 mil, and subsequently
covering the undercoating with a boron-containing glass overcoating comprising boron nitride, said overcoating having a thickness of approximately 1-10 mil.
2. The method of claim 1 , wherein the catalytic oxidation is oxidation that is catalyzed by potassium acetate.
3. The method of claim 1 , wherein said component is configured as an aircraft landing system brake disc.
4. The method of claim 1 , wherein said phosphorus-containing undercoating comprises ions formed from 20-50 wt % H 2 O, 30-55 wt % H 3 PO 4 , 0-15 wt % MnHPO 4 .1.6H 2 O, 2-15 wt % AlPO 4 , 0.5-2 wt % B 2 O 3 , 1-7 wt % Zn 3 (PO 4 ) 2 , and 10-20 wt % KH 2 PO 4 .
5. The method of claim 1 , wherein said boron-containing glass overcoating also comprises boron carbide and/or elemental boron.
6. The method of claim 5 , wherein the formulation used to make the boron-containing glass overcoating comprises ions formed from 20-60 wt % H 2 O, 25-50 wt % H 3 PO 4 , 2-20 wt % alkali metal hydroxide, 1-10 wt % alkali or alkaline earth metal mono-, di-, or tri-basic phosphate, 1-10 wt % boron nitride, and one or both of 1-10 wt % elemental boron and/or 1-10 wt % boron carbide.
7. The method of claim 1 , wherein the undercoating is annealed to the carbon composite at a temperature in the range of 250-900° C. (482-1652° F.).
8. The method of claim 1 , wherein the glass overcoating is annealed to the undercoating at a temperature in the range of 250-650° C. (482-1202° F.).
9. A method of protecting a component made of carbon fiber or carbon-carbon composite simultaneously against catalytic oxidation and high temperature non-catalytic oxidation, which method comprises:
covering said composite with an undercoating comprising ions formed from 10-80 wt % H 2 O, 20-70 wt % H 3 PO 4 , 0.1-25 wt % alkali metal mono-, di-, or tri-basic phosphate, 0-2 wt % B 2 O 3 , and 0-25 wt % MnHPO 4 .1.6H 2 O, 0-30 wt % AlPO 4 , and 0-10 wt % Zn 3 (PO 4 ) 2 , provided that at least one of AlPO 4 , MnHPO 4 .1.6H 2 O, and Zn 3 (PO 4 ) 2 is present, said undercoating having a thickness of approximately 1-10 mil, and subsequently
covering the undercoating with a boron-containing glass overcoating comprising boron nitride, said overcoating a thickness of approximately 1-10 mil and subsequently
subjecting the undercoated and overcoated component to potassium acetate under oxidation conditions,
wherein said component is protected simultaneously against catalytic oxidation and high temperature non-catalytic oxidation.