Method of forming an abrasive coating on a fan blade tip
A novel method of depositing grit particles onto a fan blade tip coating is provided. The method enhances grit capture by presenting a softened coating surface for the impinging particles. The softened surface is achieved without high substrate temperatures that could degrade the base metal properties in the fan blade. An auxiliary heat source is used to establish a locally heated and softened surface where the grit deposition takes place. The softened surface greatly increases the probability of grit capture.
1. A method of forming an abrasive coating on a rotating turbomachine component, the rotating turbomachine component comprising an airfoil section and a tip, the airfoil section and the tip having an aluminum or aluminum alloy substrate, the rotating turbomachine component designed to rotate within an abradable liner made of an abradable material, the method comprising the steps of:
providing a feedstock consisting of aluminum powder;
heating the aluminum powder until the aluminum powder is molten;
spraying the molten aluminum powder onto the substrate of the tip with a plasma spray gun to form a coating consisting of aluminum, wherein the plasma spray gun has an axis of rotation and an axis of powder injection substantially perpendicular to the axis of rotation; and
depositing grit particles onto the coating while maintaining a temperature of the coating within a desired range by controlling deposition rate parameters; wherein
the deposition rate parameters include an aluminum powder feed rate of 20 g/min to 120 g/min, a traverse rate of the plasma spray gun of 1200 inches per minute to 20 inches per minute, a traverse direction substantially parallel to the axis of powder injection, and a spray plume area.
2. The method of claim 1 wherein the aluminum powder feed rate is between about 30 g/min and 60 g/min.
3. The method of claim 1 wherein the traverse rate of the plasma spray gun is between about 900 inches per minute and about 500 inches per minute.
4. The method of claim 1 wherein the aluminum powder is heated by introducing the powder into the plasma plume emanating from the plasma spray gun.
5. The method of claim 4 wherein before the depositing step the grit particles are introduced into a plasma jet stream downstream from the plasma plume so the grit particles do not melt.
6. The method of claim 1 wherein the rotating turbomachine component is a fan blade.
7. The method of claim 1 wherein during the spraying step the traverse rate of the plasma spray gun is varied.
8. The method of claim 1 wherein during the spraying step the plasma spray gun is directed along a spray path.
9. The method of claim 8 wherein the spray path is varied to increase spray path spacing.
10. The method of claim 8 wherein the spray path is varied to increase or decrease spray overlap.
11. The method of claim 1 wherein the plasma spray gun has an axis of rotation and wherein, during the spraying step, the plasma spray gun is rotated about its axis of rotation.
12. The method of claim 1 wherein the plasma spray gun has an axis of rotation and wherein, during the spraying step, the axis of rotation changes.
13. A method of forming an abrasive coating on a fan blade, the fan blade comprising an airfoil section and a tip, the airfoil section and tip having an aluminum or aluminum alloy substrate, the fan blade mounted to a hub and configured to rotate within a fan case assembly, the fan case assembly comprising an abradable liner made of an abradable material, the method comprising the steps of:
providing a feedstock consisting of aluminum powder;
heating the aluminum powder until the aluminum powder is molten;
spraying the molten aluminum powder onto the substrate of the fan blade tip with a plasma spray gun to form a matrix coating consisting of aluminum, wherein the plasma spray gun has an axis of rotation and an axis of powder injection substantially perpendicular to the axis of rotation; and
depositing grit particles onto the matrix coating while maintaining a temperature of the matrix coating within a desired range by controlling deposition rate parameters;
wherein the deposition rate parameters include an aluminum powder feed rate of 20 g/min to 120 g/min, a traverse rate of the plasma spray gun of 1200 inches per minute to 20 inches per minute, a traverse direction substantially parallel to the axis of powder injection, and a spray plume area.
14. The method of claim 13 wherein the grit particles are harder than the abradable material in the abradable liner.
15. The method of claim 14 wherein the abradable liner comprises epoxy bonded glass micro-balloons.
16. A method of forming an abrasive coating on a rotating turbomachine component, the rotating turbomachine component comprising an airfoil section and a tip, the airfoil section and the tip having an aluminum or aluminum alloy substrate, the rotating turbomachine component designed to rotate within an abradable liner made of an abradable material, the method comprising the steps of:
providing a feedstock consisting of aluminum powder;
heating the aluminum powder until the aluminum powder is molten;
spraying the molten aluminum powder onto the substrate of the tip with a plasma spray gun to form a coating consisting of aluminum, wherein the plasma spray gun has an axis of rotation and an axis of powder injection substantially perpendicular to the axis of rotation; and
depositing grit particles onto the coating while maintaining a temperature of the coating within a desired range by controlling deposition rate parameters; wherein
the deposition rate parameters include an aluminum powder feed rate of 30 g/min to 60 g/min, a traverse rate of the plasma spray gun of 900 inches per minute to 500 inches per minute, a traverse direction substantially parallel to the axis of powder injection, and a spray plume area.