Fan frame
AssigneeUnited Technologies Corporation
InventorsJennifer Grudnoski, John DiTomasso, Akwetee E. Watkins, Jody M. Grosso
Life of this patent
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Abstract
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.
Claims7
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.
Dependencies are inferred from the claim text.