Coolable stator assembly for a rotary machine

Claim 2

In a gas turbine engine of the type having an annular flow path for working medium gases, an engine case extending circumferentially about the working medium flow path, a coolable stator assembly which includes an outer air seal spaced radially inwardly from the engine case leaving a cavity for cooling air therebetween and a means for supporting the outer air seal from the case about the working medium flow path, the improvement which comprises: a coolable stator assembly which includes an outer air seal formed of an array of arcuate segments, at least one of said segments having a passage for cooling air which extends through the segment and which is in flow communication with said cavity; and a means for supporting the outer air seal which includes a support extending inwardly of the engine to engage the outer air seal, the support having at least one passage in flow communication with said passage in the outer air seal for metering the flow of cooling air which is radially oriented for directing cooling air radially inward through the support toward the arcuate seal segment to radially impinge the cooling air on the arcuate seal segment.

Claim 3

The coolable stator assembly of claim 1 wherein the arcuate seal segment has a circumferentially extending hook which adapts the seal segment to engage the support and wherein the passage in the seal segment is a slot which extends through the hook to interrupt the circumferential continuity of the hook.

Claim 4

The coolable stator assembly of claim 1 wherein the arcuate seal segment has a circumferentially extending hook which adapts the seal segment to engage the support and wherein the passage in the seal segment extends through the hook.

Claim 5

The coolable stator assembly of claim 3 wherein the arcuate seal segment has a circumferentially extending edge, the hook extends from the arcuate seal segment at a first location spaced axially from the edge leaving an edge region therebetween and wherein each passage in the support has a discharge opening for cooling air at a second axial location which is radially outward of the edge region.

Claim 6

The stator assembly as claimed in claim 4 wherein the passages in the hook are slots extending through the hook and wherein the support has a plurality of holes in flow communication with the slots in said hook.

Claim 7

The stator assembly as claimed in claim 5 wherein a first seal member extends outwardly of the hook to direct the cooling air inwardly through the slots toward the holes in the support and a second seal member engages the arcuate seal segment at an axial location between the first axial location and the second axial location and engages the support at an axial location between the first axial location and the second axial location to direct the flow of cooling air outwardly through the slots toward the holes in the support.

Claim 8

The stator assembly as claimed in claim 6 wherein the support has a flange which engages the hook of the seal segment and which is spaced radially from the arcuate segment leaving a cavity therebetween across which cooling air is flowed before being impinged on the edge region and through which cooling air is flowed after impingement on the outer air seal to provide convective cooling to the flange and to the edge region.

Claim 9

For a gas turbine engine having an annular flow path for hot working medium gases disposed about an axis A e and an engine case which extends circumferentially about the working medium flow path, a stator assembly which comprises: an outer air seal which is spaced radially from the engine case leaving a first cavity for cooling air therebetween and which is formed of an array of arcuate seal segments extending circumferentially about the working medium flow path, each seal segment having a plate having an edge which extends circumferentially about the plate and a sealing surface which extends axially from the edge and which bounds the working medium flow path, a hook attached to the plate which has a first section extending outward from the plate and a second section extending axially from the first section in the direction of the edge and spaced radially from the plate leaving a circumferentially extending groove therebetween; and a support which extends inwardly from the engine case to engage the hook of the seal segment, the support having a flange which extends into the groove formed by the hook and the seal plate to engage the seal segment, the flange being spaced radially from the seal plate leaving a second cavity therebetween, being spaced axially from the first section of the hook leaving a third cavity therebetween and being spaced axially from the second section of the hook leaving a fourth cavity therebetween; wherein each hook has a plurality of slots, spaced circumferentially one from the other which extend axially through the hook to interrupt the circumferential continuity of the hook and to place the first cavity in flow communication with the fourth cavity, wherein a first seal member extends between the support and the second section of the hook to block the flow of cooling air along a flow path outwardly of the hook into the fourth cavity, and a second seal member disposed in the third cavity extends between the seal segment and the support to block the leakage of cooling air into the second cavity along a flow path between the seal segment and the support, and wherein each support has a plurality of passages outwardly of and aligned with the edge region that are in flow communication with the second cavity and in flow communication through said slot with the first cavity for cooling air for directing cooling air in the radial direction toward the edge region.

Claim 10

For a gas turbine engine having an annular flow path for hot working medium gases disposed about an axis A e and an engine case which extends circumferentially about the working medium flow path, a stator assembly which comprises: an outer air seal which is spaced radially from the engine case leaving a first cavity for cooling air therebetween and which is formed of an array of arcuate seal segments extending circumferentially about the working medium flow path, each seal segment having a plate having an edge which extends circumferentially about the plate and a sealing surface which extends axially from the edge and which bounds the working medium flow path, a hook attached to the plate which has a first section extending outward from the plate and a second section extending axially from the first section in the direction of the edge and spaced radially from the plate leaving a circumferentially extending groove therebetween; and a support which extends inwardly from the engine case to engage the hook of the seal segment, the support having a flange which extends into the groove formed by the hook and the seal plate to engage the seal segment, the flange being spaced radially from the seal plate leaving a second cavity therebetween, being spaced axially from the first section of the hook leaving a third cavity therebetween and being spaced axially from the second section of the hook leaving a fourth cavity therebetween; wherein each hook has a plurality of slots, spaced circumferentially one from the other which extend axially through the hook to interrupt the circumferential continuity of the hook and to place the first cavity in flow communication with the fourth cavity, wherein a first seal member extends between the support and the second section of the hook to block the flow of cooling air along a flow path outwardly of the hook into the fourth cavity, and a second seal member disposed in the third cavity extends between the seal segment and the support to block the leakage of cooling air into the second cavity along a flow path between the seal segment and the support, and wherein each support has a plurality of passages outwardly of and aligned with the edge region that are in flow communication with the second cavity and in flow communication through said slot with the first cavity for cooling air for directing cooling air in the radial direction toward the edge region.

Claim 11

The stator assembly as claimed in claim 8 wherein said passages in said support meter the flow of cooling and radially direct cooling air across the second cavity such that the cooling air impinges on the edge region of the seal plate.

Claim 12

The stator assembly as set forth in claim 9 wherein at least one passage in the support is aligned with a slot in the hook such that cooling air is flowed directly from the first cavity to the passage in the support through the slot.

Claim 15

The method for cooling the stator assembly of claim 11 wherein the stator assembly has an upstream edge region and a downstream edge region and the stator assembly includes an impingement plate which extends between the end regions; wherein the step of radially impinging the cooling air against the outer air seal at a first location includes the step of flowing the cooling air through the impingment plate to impinge against the outer air seal at a first location between the edge regions; and, wherein the step of radially impinging the cooling air against the outer air seal at a second location includes the step of impinging the cooling air against one of said edge regions.

Claim 16

The method for cooling a stator assembly of claim 11 wherein the outer air seal includes an outwardly extending hook for engaging the support structure and wherein the step of flowing the cooling air through the outer air seal includes the step of flowihg the cooling air through the hook.