Fan blades with abrasive tips
A fan blade for a gas turbine engine is disclosed. The disclosed fan blade includes an airfoil having a leading edge, a trailing edge, a convex side, a concave side and a distal tip. The leading edge, trailing edge, convex side and concave side of the airfoil is at least partially coated with an erosion resistant coating. The distal tip of the airfoil is coated with a bonded abrasive coating. The bonded abrasive coating engages the abradable coating disposed on the fan liner and, because of its low thermal conductivity, reduces heat transfer to the distal tip of the fan blade. The reduction in heat transfer to the distal tip of the fan blade preserves the integrity of erosion resistant coatings that may be applied to the body or the airfoil of the fan blade.
1. A fan blade comprising: an airfoil including a distal tip that extends between a concave side and a convex side, the distal tip coated with a bonded abrasive coating, the concave side including an erosion resistant coating, the convex side abutting the bonded abrasive coating, the bonded abrasive coating having a bonding material that is coated with more than one layer of abrasive particulate, the distal tip of the airfoil being connected to a leading edge, a trailing edge, the concave side, and the convex side, and the bonded abrasive coating being rounded at portions in which the bonded abrasive coating extends from the distal tip onto portions of the leading edge, trailing edge, concave side and convex side of the airfoil to define a raised portion of the bonded abrasive coating sized to promote a reduction in temperature of the distal tip when the bonded abrasive coating contacts an abradable coating disposed upon a liner for a fan section of a gas turbine engine.
2. The fan blade of claim 1 , wherein the bonding material includes at least one material selected from a group consisting of: epoxy, polyimide, polyurethane, cyanoacrylate, acrylic and combinations thereof.
3. The fan blade of claim 1 , wherein the erosion resistant coating is a polyurethane.
4. The fan blade of claim 1 , wherein the abrasive particulate includes at least one abrasive material selected from the group consisting of zirconia, alumina, silica, cubic boron nitride (CBN), a metal alloy and mixtures thereof.
5. The fan blade of claim 1 , wherein the bonded abrasive coating is coated onto the distal tip with a thickness ranging from about 4 to about 25 mils.
6. The fan blade of claim 1 , wherein the distal tip of the airfoil is connected to the leading edge, the trailing edge, the concave side, and the convex side, the bonded abrasive coating extends from the distal tip onto portions of the leading edge, trailing edge, concave side and convex side of the airfoil.
7. The fan blade of claim 1 , wherein the bonded abrasive coating includes a bonding layer disposed on the distal tip and a layer of abrasive particles disposed on the bonding layer opposite the distal tip.
8. The fan blade of claim 1 , wherein the bonded abrasive coating includes a bonding layer disposed on top of a layer of abrasive particles that are disposed on the distal tip.
9. A fan blade comprising:
an airfoil including a leading edge, a trailing edge, a convex side, a concave side and a distal tip, the leading edge, the trailing edge, the convex side, the concave side, and the distal tip being at least partially coated with an erosion resistant coating, the distal tip of the airfoil coated with a bonded abrasive coating that is disposed on the concave side and convex side and abuts the erosion resistant coating that extends around to the concave side and the convex side, the bonded abrasive coating increasing in thickness as the bonded abrasive coating extends from at least one of the concave side and the convex side towards a mid-portion of the distal tip, the midportion having a raised middle portion that is arranged to wear faster than a remainder of the mid-portion, the bonded abrasive coating decreasing In thickness as the bonded abrasive coating extends from the mid-portion towards the other of at least one of the concave side and the convex side, the raised middle portion promoting a localized abrasive contact with an abradable coating disposed upon a liner for a fan section of a gas turbine engine to substantially evenly share work associated with reducing a thickness of the abradable coating with adjacent fan blades, wherein the bonded abrasive coating is rounded as it extends from the concave side to the convex side.
10. The fan blade of claim 9 , wherein the bonded abrasive coating includes at least one material selected from the group consisting of: epoxy, polyimide, polyurethane, cyanoacrylate, acrylic and combinations thereof.
11. The fan blade of claim 9 , wherein the bonded abrasive coating includes at least one abrasive material selected from the group consisting of zirconia, alumina, silica, cubic boron nitride (CBN), a metal alloy and mixtures thereof.
12. The fan blade of claim 9 , wherein the bonded abrasive coating extends from the distal tip onto portions of the leading edge, trailing edge, concave side and convex side of the airfoil.
13. The fan blade of claim 12 , wherein the bonded abrasive coating is rounded as it extends from the distal tip onto portions of the leading edge and trailing edge of the airfoil.