摘要:
A method of coating a metal substrate (17) such as the components in second and third stages of gas turbine engines in order to increase the oxidation and corrosion resistance of the metal substrate (17) under high temperature operating conditions, the method including the steps of forming a powdered mixture of a high-melt superalloy or MCrAIY component (14), where M comprises Fe, Ni and/or Co, and a low-melt component (15) containing about 2-5 wt.% silicon, boron or hafnium, applying the powdered mixture to the surface of the metal substrate (17) at room temperature using an atomized spray to form a uniform surface coating, and then heating the coated substrate surface under vacuum conditions to a temperature in the range of about 1900°F to 2275°F to obtain a uniform coating composition (19) providing oxidation resistance to the underlying substrate.
摘要:
A method of coating a metal substrate (17) such as the components in second and third stages of gas turbine engines in order to increase the oxidation and corrosion resistance of the metal substrate (17) under high temperature operating conditions, the method including the steps of forming a powdered mixture of a high-melt superalloy or MCrAIY component (14), where M comprises Fe, Ni and/or Co, and a low-melt component (15) containing about 2-5 wt.% silicon, boron or hafnium, applying the powdered mixture to the surface of the metal substrate (17) at room temperature using an atomized spray to form a uniform surface coating, and then heating the coated substrate surface under vacuum conditions to a temperature in the range of about 1900°F to 2275°F to obtain a uniform coating composition (19) providing oxidation resistance to the underlying substrate.
摘要:
A method of coating a metal substrate (17) such as the components in second and third stages of gas turbine engines in order to increase the oxidation and corrosion resistance of the metal substrate (17) under high temperature operating conditions, the method including the steps of forming a powdered mixture of a high-melt superalloy or MCrAIY component (14), where M comprises Fe, Ni and/or Co, and a low-melt component (15) containing about 2-5 wt.% silicon, boron or hafnium, applying the powdered mixture to the surface of the metal substrate (17) at room temperature using an atomized spray to form a uniform surface coating, and then heating the coated substrate surface under vacuum conditions to a temperature in the range of about 1900°F to 2275°F to obtain a uniform coating composition (19) providing oxidation resistance to the underlying substrate.
摘要:
Improved compositions are described for the protection of gas turbine parts at elevated temperatures. The compositions are of the MCrAlY type, wherein M is selected from nickel, or a combination of nickel with cobalt, iron, or combinations thereof. The compositions further comprise ruthenium, rhenium, or a combination thereof, a Group 4 metal (e.g., hafnium, zirconium, titanium), and can further include silicon and/or germanium, where the composition results in improved aluminum diffusion properties. Also disclosed herein are articles comprising the composition.
摘要:
A process (10) for repairing a metal component (102) includes sintering (12) a mixture comprising particles of a coating composition and particles of a brazing alloy to form a composite preform (200); disposing (14) the composite preform (200) on an uncoated surface of the metal component (102); and heating (16) the preform (200) to a temperature effective to form a brazed joint between the composite preform (200) and the metal component (102).