Variable area turbine

Claim 2

In a gas turbine engine having a flow path for working medium gases extending through the engine and including a variable area nozzle comprising a plurality of rotatable guide vanes disposed between the inner engine case and the outer engine case, means attached to the outer case for cantilevering free of radial restraint said guide vanes from the outer case to support the vanes under axial loads exerted by the working medium gases on the vanes and means attached to the inner case for radially restraining the vanes under radial pressure loads exerted by the working medium gases on the vanes.

Claim 3

In a gas turbine engine having a flow path for working medium gases extending through the engine, a variable area nozzle disposed across the flow path and comprising: an outer engine case located radially outward of the flow path for the working medium gases; an inner engine case located radially inward of the flow path for the working medium gases; an inner shroud which is affixed to the inner case and includes a bore extending therethrough; an outer shroud which is spaced apart radially from the inner shroud to form a portion of the flow path and which has a cylindrical socket radially aligned with the bore of the inner shroud; a bearing cartridge extending radially inward from the outer case; a rotatable guide vane having a stem which engages the bearing cartridge, a cylindrical platform which is interposed within the socket of the outer shroud, an airfoil section extending across the flow path for the working medium gases and a post which penetrates the bore of the inner shroud; and attaching means affixed to the vane post for positioning the vane airfoil section radially with respect to the inner shroud while permitting the vane to reposition axially and circumferentially with respect to the inner shroud.

Claim 4

In a gas turbine engine having a flow path for working medium gases extending through the engine, a variable area nozzle disposed across the flow path and comprising: an outer engine case located radially outward of the flow path for the working medium gases; an inner engine case located radially inward of the flow path for the working medium gases; an inner shroud which is affixed to the inner case and includes a bore extending therethrough; an outer shroud which is spaced apart radially from the inner shroud to form a portion of the flow path and which has a cylindrical socket radially aligned with the bore of the inner shroud; a bearing cartridge extending radially inward from the outer case; a rotatable guide vane having a stem which engages the bearing cartridge, a cylindrical platform which is interposed within the socket of the outer shroud, an airfoil section extending across the flow path for the working medium gases and a post which penetrates the bore of the inner shroud; and attaching means affixed to the vane post for positioning the vane airfoil section radially with respect to the inner shroud while permitting the vane to reposition axially and circumferentially with respect to the inner shroud.

Claim 5

The invention according to claim 2 wherein the bearing cartridge includes an inner cylindrical bushing and an outer cylindrical bushing which are positioned in coaxial alignment with the vane stem by a bearing housing.

Claim 6

The invention according to claim 2 wherein the inner shroud has at least one cooling air cavity and wherein cooling air is flowable to the cavity through a plate having a plurality of orifices therein.

Claim 7

The invention according to claim 2 wherein the said inner shroud is segmented.

Claim 8

The invention according to claim 2 wherein said outer shroud is segmented.

Claim 9

The invention according to claim 2 wherein the inner shroud contains a washer housing having a thrust washer mounted therein wherein the washer is positioned in concentric relationship to the bore of the inner shroud and wherein the washer is adapted to receive the radial pressure load exerted by the working medium gases on said rotatable vane during operation of the engine.

Claim 10

The invention according to claim 7 which further includes a bearing seat disposed between said attaching means and the thrust washer wherein the bearing seat has a planar surface which opposes the thrust washer.

Claim 11

The invention according to claim 8 which further includes a spherical bearing disposed between the bearing seat and the attaching means wherein the bearing has a convex spherical surface and where the seat has a concave spherical surface which opposes the convex spherical surface of the bearing.

Claim 12

The invention according to claim 2 wherein said attaching means is a positioning nut which is adjustable on the vane post to selectively adjust the clearance between the vane airfoil section and the inner shroud.

Claim 13

The invention according to claim 10 which further includes in contact with the vane post a finger spring which is adapted to adjust the vane radially outward to maintain the clearance between the vane airfoil section and the inner shroud.

Claim 14

The invention according to claim 7 wherein the washer housing has a plurality of pedestals which support the housing in relationship to the inner shroud to thermally isolate the thrust washer in the housing from the inner shroud.

Claim 15

The invention according to claim 7 wherein the thrust washer is manufactured from a carbonaceous material.

Claim 16

The invention according to claim 3 wherein the inner cylindrical bushing and outer cylindrical bushing of the bearing cartridge are fabricated from a carbonaceous material.

Claim 17

In a gas turbine engine having a flow path for working medium gases extending through the engine and including a variable area nozzle disposed across the flow path comprising a plurality of rotatable guide vanes which are cantilevered from the outer engine case and are radially opposed at their inner tips by an inner shroud, a method for controlling the radial clearance between the vane tips and the inner shroud comprising the step of: affixing each vane to the inner shroud in a manner imposing radial restraint against the pressure load of the working medium gases on the vane while permitting the vane tip to reposition axially and circumferentially with respect to the inner shroud.

Claim 18

In a gas turbine engine having a flow path for working medium gases extending through the engine and including a variable area nozzle disposed across the flow path comprising a plurality of rotatable guide vanes which are cantilevered from the outer engine case and are radially opposed at their inner tips by an inner shroud, a method for controlling the radial clearance between the vane tips and the inner shroud comprising the step of: affixing each vane to the inner shroud in a manner imposing radial restraint against the pressure load of the working medium gases on the vane while permitting the vane tip to reposition axially and circumferentially with respect to the inner shroud.

Claim 19

The method according to claim 15 wherein a positioning nut which is adjustable to vary the clearance between the vane and the inner shroud affixes the vane to the inner shroud.