초록 ▼

A platform is provided for use between adjacent fan blades joined to a rotor disk to provide an inner flowpath boundary. The platform includes: a metallic arcuate body with opposed forward and aft ends and opposed lateral edges; and a pair of frangible wings that extend from the lateral edges latera

A platform is provided for use between adjacent fan blades joined to a rotor disk to provide an inner flowpath boundary. The platform includes: a metallic arcuate body with opposed forward and aft ends and opposed lateral edges; and a pair of frangible wings that extend from the lateral edges laterally and radially beyond the body.

대표청구항 ▼

1. A fan rotor assembly comprising: a rotor including an annular array of dovetail slots;an array of blades each having a dovetail engaged in one of the dovetail slots of the rotor, and an airfoil extending radially outward from the dovetail wherein a plurality of spaces are present between adjacent

1. A fan rotor assembly comprising: a rotor including an annular array of dovetail slots;an array of blades each having a dovetail engaged in one of the dovetail slots of the rotor, and an airfoil extending radially outward from the dovetail wherein a plurality of spaces are present between adjacent ones of the fan blades;an array of platforms disposed in the spaces between adjacent fan blades, each platform comprising:a metallic arcuate body with opposed forward and aft ends and opposed lateral edges; anda pair of frangible wings that extend from the lateral edges laterally and radially outwards away from the rotor beyond the body towards the fan blades, wherein a gap is present between each lateral edge of each of the platforms and the adjacent fan blade. 2. The rotor assembly of claim 1 wherein the body and the wings form part of a unitary member. 3. The rotor assembly of claim 1 wherein one of the lateral edges has a concave curvature and the other lateral edge has a convex curvature. 4. The rotor assembly of claim 1 wherein one of the wings has a concave curvature and the other wings has a convex curvature. 5. The rotor assembly of claim 1 wherein a lean angle between each wing and an outer surface of the body is less than 90 degrees. 6. The rotor assembly of claim 1 wherein a ratio of the thickness at the tip of each wing to the thickness of the root of each wing is less than one. 7. The rotor assembly of claim 1 wherein a radial length of each wing is substantially larger than the size of the gap. 8. The rotor assembly of claim 1 further comprising a resilient seal member disposed between a tip of the each of the wings and the adjacent fan blade. 9. The rotor assembly of claim 1 wherein each platform is mounted to the rotor through a forward mounting flange extending axially outward from a forward end of the platform and an aft mounting flange extending axially outward from an aft end of the platform.