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A coated fan rotor blade and method for coating a fan rotor blade. The coated fan rotor blade includes a fan rotor blade; and a coating disposed on said fan rotor blade. The coating comprises a binder; and a filler made up of a plurality of particles. The filler material is incorporated into the bin

A coated fan rotor blade and method for coating a fan rotor blade. The coated fan rotor blade includes a fan rotor blade; and a coating disposed on said fan rotor blade. The coating comprises a binder; and a filler made up of a plurality of particles. The filler material is incorporated into the binder material, and the particles in the filler interact to produce vibrational damping. In particular, the coating includes small, dense, flattened particles or plates that are incorporated into a thin layer of visco-elastic material, such as rubber, silicone, fluoro-elastomer, or urethane and bonded to the surface of the rotor blade to provide damping of high frequency excitation.

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What is claimed is: 1. A coated fan rotor blade comprising: a fan rotor blade; and a coating disposed on said fan rotor blade comprising: a binder; and a filler made up of a plurality of particles, the particles being configured to provide interaction between the plurality of particles; wherein th

What is claimed is: 1. A coated fan rotor blade comprising: a fan rotor blade; and a coating disposed on said fan rotor blade comprising: a binder; and a filler made up of a plurality of particles, the particles being configured to provide interaction between the plurality of particles; wherein the filler material is incorporated into the binder material, and the particles interact to produce vibrational damping; and wherein the binder and filler are configured to withstand temperature exposures from about-65�� F. to about 450�� F. at high rotational speeds. 2. The coated fan rotor blade of claim 1, wherein the particles have an elongated geometry. 3. The coated fan rotor blade of claim 2, wherein the aspect ratios for the area to thickness aspect ratios for the particles is from about 100:1 to about 1000:1. 4. The coated fan rotor blade of claim 1, wherein the particles are selected from the group consisting of metallic particles, carbon particles, graphite particles, silicate particles and combinations thereof. 5. The coated fan rotor blade of claim 1, wherein the binder is visco-elastic. 6. The coated fan rotor blade of claim 5, wherein the binder is selected from the group consisting of rubber, silicon, fluoro-elastomer and urethane. 7. The coated fan rotor blade of claim 6, wherein the fan rotor blade is a single-piece structure. 8. The coated fan rotor blade of claim 7, wherein the single-piece structure is a blisk rotor. 9. A method for damping vibration of a fan rotor blade comprising: providing a fan rotor blade; applying a coating composition to a surface of the fan rotor blade, the composition comprising a binder material and a filler material; wherein the filler material is a plurality of particles, the particles being configured to provide interaction between the plurality of particles, the particles interacting to produce vibrational damping; and wherein the binder and filler are configured to withstand temperature exposures from about-65�� F. to about 450�� F. at high rotational speeds. 10. The method of claim 9, wherein the coating includes molding the composition onto the substrate. 11. The method of claim 9, wherein the coating includes spraying the composition onto the substrate. 12. The method of claim 9, wherein the coating includes bonding sheets of material to the substrate. 13. The method of claim 9, wherein the particles have an elongated geometry. 14. The method of claim 13, wherein the aspect ratios for the area to thickness aspect ratios for the particles is from about 100:1 to about 1000:1. 15. The method of claim 9, wherein the particles are selected from the group consisting of metallic particles, carbon particles, graphite particles, silicate particles and combinations thereof. 16. The method of claim 9, wherein the binder material is visco-elastic. 17. The method of claim 9, wherein the fan rotor blade is a one-piece structure. 18. The method of claim 17, wherein the one-piece structure is a blisk rotor.