Variable area turbine

Claim 2

In a gas turbine engine of the type having an inner shroud and an outer shroud which radially bound a flow path for the working medium gases in the engine, a variable area nozzle including a cantilevered guide vane which is rotatable and has an airfoil section overhanging a portion of the outer shroud, wherein the improvement comprises: means for controlling the radial clearance between the overhung vane and the opposing outer shroud including a bearing cartridge having a cylindrical bushing which axially and radially positions the rotatable vane, an annular ring which extends circumferentially about the engine and which is attached to the bearing cartridge, and means for attaching the outer shroud to the annular ring to axially and radially position the outer shroud thereby fixing the radial position of said shroud with respect to said rotatable vane.

Claim 3

The invention according to claim 1 wherein the outer shroud is segmented.

Claim 4

The invention according to claim 1 wherein the guide vane has a plurality of orifices leading to a hollow cavity therein and the bearing cartridge has one or more apertures through which cooling air is flowable to the cavity and further including a locating pin which extends through the annular ring to engage the cartridge at a preferred orientation wherein the vane orifices and the cartridge apertures are in substantial alignment to minimize aerodynamic losses in the cooling air flowing to the cavity.

Claim 5

The invention according to claim 1 wherein the rotatable vane is cantilevered radially inward from the bearing cartridge.

Claim 6

The invention according to claim 4 wherein the cartridge includes a cylindrical bushing.

Claim 7

The invention according to claim 5 wherein the bushing cartridge is fabricated from a carbonaceous material.

Claim 8

The invention according to claim 1 wherein the annular ring includes an upstream segment and a downstream segment and wherein the downstream segment is adapted to support each bearing cartridge under axial pressure loads exerted by the working medium gases on the rotatable vane mounted therein.

Claim 9

The invention according to claim 7 further including a combustion chamber located upstream of the rotatable vanes and wherein the upstream segment of the annular ring is adapted to radially support the downstream end of the combustion chamber.

Claim 10

In the turbine section of a gas turbine engine of the type having a variable area nozzle including a plurality of rotatable guide vanes which are cantilevered across the flow path for the working medium gases from a bearing cartridge, the improvement which comprises: an inner engine case spaced radially inward of the flow path for the working medium gases; an inner shroud which is attached to the inner engine case and radially opposes the tips of the cantilevered guide vanes; a double wall outer engine case which is spaced radially outward of the flow path for the working medium gases and includes an outer wall from which the bearing cartridges extend and an inner wall having an annular ring affixed to a radially inward portion of the cartridges, the thermal response of the double wall case being closely matched to the thermal response of the inner case to control the radial clearance between the cantilevered vanes and the opposing inner shroud.

Claim 11

In the turbine section of a gas turbine engine of the type having a variable area nozzle including a plurality of rotatable guide vanes which are cantilevered across the flow path for the working medium gases from a bearing cartridge, the improvement which comprises: an inner engine case spaced radially inward of the flow path for the working medium gases; an inner shroud which is attached to the inner engine case and radially opposes the tips of the cantilevered guide vanes; a double wall outer engine case which is spaced radially outward of the flow path for the working medium gases and includes an outer wall from which the bearing cartridges extend and an inner wall having an annular ring affixed to a radially inward portion of the cartridges, the thermal response of the double wall case being closely matched to the thermal response of the inner case to control the radial clearance between the cantilevered vanes and the opposing inner shroud.

Claim 12

The invention according to claim 9 which further includes an outer shroud held in radial position relative to the cartridge by the annular ring and wherein the vanes each have a downstream portion which overhangs the outer shroud and is held in relative radial position thereto by the respective bearing cartridge to control the clearance between the overhung portion of the vane and the outer shroud.