초록 ▼

A fan frame (10) for a gas turbine is provided. The fan frame (10) has fan exit guide vanes (100) that are connected to an intermediate case (50) for structural support, and are constrained from movement in a radial direction by a first joint (110, 110a) and constrained from movement in an axial and

A fan frame (10) for a gas turbine is provided. The fan frame (10) has fan exit guide vanes (100) that are connected to an intermediate case (50) for structural support, and are constrained from movement in a radial direction by a first joint (110, 110a) and constrained from movement in an axial and radial direction by a second joint (120a, 110a). The intermediate case (50) provides structural integrity while reducing weight by providing struts (56, 95) with a width that increases in a direction away from a central bearing (55) as the thickness of the struts (56, 95) decreases.

대표청구항 ▼

What is claimed is: 1. A fan assembly for a gas turbine, the assembly comprising: one or more fan blades; and a fan frame having a fan exit case rear, a plurality of fan exit guide vanes and an intermediate case having a plurality of struts, wherein each of said plurality of fan exit guide vanes is

What is claimed is: 1. A fan assembly for a gas turbine, the assembly comprising: one or more fan blades; and a fan frame having a fan exit case rear, a plurality of fan exit guide vanes and an intermediate case having a plurality of struts, wherein each of said plurality of fan exit guide vanes is connected to said intermediate case by a forward joint and an aft joint, wherein, for each of said plurality of fan exit guide vanes, one of said forward joint and said aft joint constrains movement of said fan exit guide vane in a radial and an axial direction with respect to said intermediate case and the other of said forward joint and said aft joint constrains movement of said fan exit guide vane in said radial direction with respect to said intermediate case, and wherein each of said struts has a circumferential width that increases and an axial thickness that decreases as each strut extends towards one of said forward joint and said aft joint. 2. The assembly of claim 1, wherein said forward joint or said aft joint has mating surfaces with a dovetail. 3. The assembly of claim 2, wherein said mating surfaces with said dovetail are disposed with said forward joint or said aft joint that constrains movement of said fan exit guide vane in said radial and said axial directions. 4. The assembly of claim 1, wherein said aft joint further comprises a blind boss. 5. The assembly of claim 4, wherein said aft joint has mating surfaces with a dovetail. 6. The assembly of claim 5, wherein said aft joint constrains movement of said fan exit guide vane in said radial and said axial directions. 7. The assembly of claim 1, wherein said plurality of struts extend from a central bearing.