Fan blade with filled pocket
A fan of a gas turbine engine includes a plurality of fan blades secured to a rotor, each of the plurality of fan blades having an airfoil secured to the rotor at one end, wherein the airfoil comprises pockets filled with an elastomeric composite.
1. A fan of a gas turbine engine, comprising: a plurality of fan blades secured to a rotor, each of the plurality of fan blades having an airfoil secured to the rotor at one end, wherein the airfoil comprises pockets filled with an elastomeric composite and an erosion coating disposed on the elastomeric composite; and
wherein each of the pockets have a width at the bottom of the pocket that is larger than the width of the pocket near an airfoil surface.
2. The fan as in claim 1 , wherein the elastomeric composite comprises a silicone rubber.
3. The fan as in claim 1 , wherein the elastomeric composite comprises an elastomer and glass microspheres.
4. The fan as in claim 3 , wherein the microspheres are present in an amount of 10 to 30% by weight, based on the total weight of the elastomeric composite.
5. The fan as in claim 1 , wherein the pockets are located on the convex side of the airfoil.
6. The fan as in claim 1 , wherein the pockets are located on the concave side of the airfoil.
7. The fan as in claim 1 , wherein the pockets are located on the convex and concave sides of the airfoil.
8. The fan as in claim 1 , wherein the pockets are bordered by ribs having a height sufficient to form part of a final surface.
9. A method of making a fan blade having filled pockets comprising:
forging a fan blade;
heat treating the fan blade;
machining the fan blade to form pockets and ribs;
shot peening the pockets and ribs;
preparing surfaces of the pockets and ribs for bonding;
applying a primer to the prepared surfaces;
filling the pockets with an elastomeric composite.
10. The method of claim 9 , wherein preparing surfaces comprises etching, grit blasting, or laser cleaning.
11. The method of claim 9 , wherein the primer comprises a silicon rubber and the elastomeric composite comprises a silicon rubber.
12. The method of claim 9 , wherein the elastomeric composite comprises an elastomer and glass microspheres.
13. The method of claim 12 , wherein the elastomer is a thermoset and the method further comprises curing the thermoset.
14. The method of claim 9 , further comprising applying an erosion coating to the elastomeric composite.
15. The method of claim 9 , further comprising sanding the elastomeric composite.
16. A gas turbine engine, comprising: a fan, comprising; a plurality of fan blades secured to a rotor, each of the plurality of fan blades having an airfoil secured to the rotor at one end wherein the airfoil comprises pockets filled with an elastomeric composite, wherein each of the pockets have a width at the bottom of the pocket that is larger than the width of the pocket near an airfoil surface; a compressor; a combustor; and a turbine, wherein an erosion coating is disposed on the elastomeric composite.
17. The gas turbine engine as in claim 16 , wherein the elastomeric composite comprises an elastomer and glass microspheres.
18. The fan as in claim 16 , wherein the pockets are bordered by ribs having a height sufficient to form part of a final surface.