초록 ▼

A gas turbine engine includes alternating rows of rotary airfoils or blades and static airfoils or vanes. The vanes are made of a base metal, such as cobalt or nickel superalloy. If a crack forms in one of the vanes, a braze alloy is applied to the crack. The braze alloy is a powdered slurry. The br

A gas turbine engine includes alternating rows of rotary airfoils or blades and static airfoils or vanes. The vanes are made of a base metal, such as cobalt or nickel superalloy. If a crack forms in one of the vanes, a braze alloy is applied to the crack. The braze alloy is a powdered slurry. The braze alloy includes approximately 50 to 100% of a base material and approximately 0 to 50% of a braze material. The base material of the braze alloy has the same composition as the composition of the base metal of the vane. The airfoil is then exposed to microwaves which melt the braze alloy in preference to the base metal to repair the crack in the vane.

대표청구항 ▼

What is claimed is: 1. A method of repairing a crack in an airfoil and dimensionally restoring the airfoil, the method comprising the steps of: applying a braze alloy to a crack in an airfoil utilized in a gas turbine engine, wherein the airfoil is made of a base metal, the braze alloy includes a b

What is claimed is: 1. A method of repairing a crack in an airfoil and dimensionally restoring the airfoil, the method comprising the steps of: applying a braze alloy to a crack in an airfoil utilized in a gas turbine engine, wherein the airfoil is made of a base metal, the braze alloy includes a base material and a braze material, the base material has the same composition as the base metal, the braze alloy is composed of more than 50% of the base material and less than 50% of the braze material, and the airfoil is a single unitary component, wherein the base material is a cobalt superalloy and includes carbon, manganese, silicon, sulfur, chromium, nickel, tungsten, tantalum, titanium, zirconium, iron, boron, and cobalt, and the braze material includes carbon, chromium, nickel, boron, and cobalt; and exposing the airfoil to microwaves to melt the braze alloy and repair the crack in the airfoil. 2. The method as recited in claim 1 wherein the base material includes 0.00 to 0.80% carbon, 0.00 to 0.80% manganese, 0.00 to 0.80% silicon, 0.00 to 0.80% sulfur, 18.0 to 26.00% chromium, 8.00 to 12.00% nickel, 5.00 to 8.00% tungsten, 2.00 to 4.00% tantalum, 0.10 to 0.30% titanium, 0.00 to 0.60% zirconium, 0.00 to 2.50% iron, 0.00 to 0.0 1% boron and the balance is cobalt, and the braze material includes 0.00 to 4.50% carbon, 19.50 to 29.50% chromium, 34.50% to 45.50% nickel, 2.00 to 4.00% boron, and the balance is cobalt. 3. A method of repairing a crack in an airfoil and dimensionally restoring the airfoil, the method comprising the steps of: applying a braze alloy to a crack in an airfoil utilized in a gas turbine engine, wherein the airfoil is made of a base metal, the braze alloy includes a base material and a braze material, the base material has the same composition as the base metal, the braze alloy is composed of more than 50% of the base material and less than 50% of the braze material, and the airfoil is a single unitary component, wherein the base material is a nickel superalloy and includes carbon, manganese, silicon, phosphorus, sulfur, chromium, cobalt, tungsten, tantalum, aluminum, titanium, hafnium, molybdenum, boron, iron, columbium, copper, zirconium, lead, bismuth, selenium, tellurium, thallium, and nickel, and the braze material includes carbon, sulfur, phosphorus, copper, lead, bismuth, selenium, silicon, iron, zirconium, manganese, aluminum, hafnium, tungsten, boron, cobalt, chromium, and nickel; and exposing the airfoil to microwaves to melt the braze alloy and repair the crack in the airfoil. 4. The method as recited in claim 3 wherein the base material is a nickel superalloy and includes 0.00 to 0.27% carbon, 0.00 to 0.30% manganese, 0.00 to 0.30% silicon, 0.00 to 0.30% phosphorus, 0.00 to 0.30% sulfur, 8.00 to 12.00% chromium, 8.00 to 12.00% cobalt, 8.00 to 12.00% tungsten, 2.00 to 6.00% tantalum, 2.00 to 6.00% aluminum, 0.50 to 2.00% titanium, 0.50 to 2.00% hafnium, 0.50 to 2.00% molybdenum, 0.00 to 0.25% boron, 0.00 to 0.25% iron, 0.00 to 0.25% columbium, 0.00 to 0.25% copper, 0.00 to 0.25% zirconium, 0.00 to 0.25% lead, 0.00 to 0.25% bismuth, 0.00 to 0.25% selenium, 0.00 to 0.25% tellurium, 0.00 to 0.25% thallium and the balance of nickel, and the braze material includes 0.00 to 0.20% carbon, 0.00 to 0.20% sulfur, 0.00 to 0.20% phosphorus, 0.00 to 0.20% copper, 0.00 to 0.20% lead, 0.00 to 0.20% bismuth, 0.00 to 0.20% selenium, 0.00 to 0.20% silicon, 0.00 to 0.20% iron, 0.00 to 0.20% zirconium, 0.00 to 0.20% manganese, 0.00 to 2.50% aluminum, 0.00 to 2.50% hafnium, 2.00 to 5.00% tungsten, 2.00 to 5.00% boron, 7.00 to 11.00% cobalt, 7.00 to 11.00% chromium, and the balance is nickel. 5. A method of repairing a crack in an airfoil and dimensionally restoring the airfoil, the method comprising the steps of: applying a braze alloy to a crack in an airfoil utilized in a gas turbine engine, wherein the airfoil is made of a base metal, the braze alloy includes a base material and a braze material, the base material has the same composition as the base metal, the braze alloy is composed of more than 50% of the base material and less than 50% of the braze material, and the airfoil is a single unitary component, wherein the base material is a nickel superalloy and includes carbon, manganese, silicon, sulfur, aluminum, molybdenum, tantalum, columbium, chromium, titanium, zirconium, iron, cobalt, copper, lead, bismuth, boron, and a nickel cobalt mixture, and the braze material includes carbon, sulfur, phosphorus, copper, lead, bismuth, selenium, silicon, iron, zirconium, manganese, aluminum, hafnium, tungsten, boron, cobalt, chromium, and nickel; and exposing the airfoil to microwaves to melt the braze alloy and repair the crack in the airfoil. 6. The method as recited in claim 5 wherein the base material is a nickel superalloy and includes 0.00 to 0.35% carbon, 0.00 to 0.35% manganese, 0.00 to 0.35% silicon, 0.00 to 0.35% sulfur, 0.00 to 7.00% aluminum, 0.00 to 7.00% molybdenum, 0.00 to 7.00% tantalum, 0.00 to 7.00% columbium, 11.00 to 16.00% chromium, 0.00 to 1.50% titanium, 0.00 to 1.50% zirconium, 0.00 to 1.50% iron, 0.00 to 1.50% cobalt, 0.00 to 0.50% copper, 0.00 to 0.50% lead, 0.00 to 0.50% bismuth, 0.00 to 0.50% boron, and the balance is a nickel cobalt mixture, and the braze material includes 0.00 to 0.20% carbon, 0.00 to 0.20% sulfur, 0.00 to 0.20% phosphorus, 0.00 to 0.20% copper, 0.00 to 0.20% lead, 0.00 to 0.20% bismuth, 0.00 to 0.20% selenium, 0.00 to 0.20% silicon, 0.00 to 0.20% iron, 0.00 to 0.20% zirconium, 0.00 to 0.20% manganese, 0.00 to 2.50% aluminum, 0.00 to 2.50% hafnium, 2.00 to 5.00% tungsten, 2.00 to 5.00% boron, 7.00 to 11.00% cobalt, 7.00 to 11.00% chromium, and the balance is nickel; and exposing the airfoil to microwaves to melt the braze alloy and repair the crack in the airfoil.