Seal means for a gas turbine engine

Claim 2

In a gas turbine engine of the type having a flowpath for hot working medium gases which is circumscribed by an engine case and having a flowpath for cooling air disposed between the flowpath for working medium gases and the engine case, and further including first and second elements extending from the engine case across the flowpath for cooling air, wherein the improvement comprises: means inwardly of the engine case extending between said first and second elements and extending to define a flowpath for pressurized cooling air between said means and the engine case, said means having a first side in heat transfer communication with the hot working medium gases and a second side in gas communication with the pressurized cooling air wherein said means is adapted to develop a sealing force against said first element and said second element in response to the flow of pressurized cooling air and by elongating in operative response to the flow of hot working medium gases in the working medium flowpath.

Claim 3

The invention as claimed in claim 1 wherein the means for defining a flowpath for cooling air has a center section in close proximity to the hot working medium flowpath which elongates in operative response to the flow of hot working medium gases in the working medium flowpath.

Claim 4

In a gas turbine engine of the type having a flowpath for hot working medium gases which is circumscribed by an engine case and having a flowpath for cooling air disposed between the flowpath for working medium gases and the engine case, and further including first and second elements extending from the engine case across the flowpath for cooling air, wherein the improvement comprises: means inwardly of the engine case extending between said first and second elements and extending to define a flowpath for cooling air between said means and the engine case, said means having a center section in close proximity to the hot working medium flowpath, a first leg extending outwardly from the center section to slidably engage said first element, and a second leg spaced axially from said first leg, the second leg extending outwardly to slidably engage said second element, wherein the center section adapts the means to develop a sealing force by elongating which causes the first leg and the second leg to exert a sealing force against the first element and the second element in operative response to the flow of hot working medium gases in the hot working medium flowpath and wherein the slidable engagement between the seal means and both the first and second elements adapts the means to provide sealing and accommodate differences in radial growth between the seal means and the adjacent elements.

Claim 5

In a gas turbine engine of the type having a flowpath for hot working medium gases which is circumscribed by an engine case and having a flowpath for cooling air disposed between the flowpath for working medium gases and the engine case, and further including first and second elements extending from the engine case across the flowpath for cooling air, wherein the improvement comprises: means inwardly of the engine case extending between said first and second elements and extending to define a flowpath for cooling air between said means and the engine case, said means having a center section in close proximity to the hot working medium flowpath, a first leg extending outwardly from the center section to slidably engage said first element, and a second leg spaced axially from said first leg, the second leg extending outwardly to slidably engage said second element, wherein the center section adapts the means to develop a sealing force by elongating which causes the first leg and the second leg to exert a sealing force against the first element and the second element in operative response to the flow of hot working medium gases in the hot working medium flowpath and wherein the slidable engagement between the seal means and both the first and second elements adapts the means to provide sealing and accommodate differences in radial growth between the seal means and the adjacent elements.

Claim 6

The invention as claimed in claim 3 which further includes a spline-type connection joining the first leg to the first element.

Claim 7

The invention as claimed in claim 3 wherein the first element has an outwardly facing surface and the second element has an inwardly facing surface and wherein the means for defining a flowpath for cooling air is trapped radially between the outwardly facing surface on the first element and the inwardly facing surface on the second element.

Claim 8

The invention as claimed in claim 4 or claim 5 wherein the second leg has a portion extending in a substantially radial direction from the center section and wherein the second leg bears against the second element a sufficient distance from the center section to enable the seal means to flexibly engage the second element to accommodate elongation of the center section.