US 5,400,586 A · Self-accommodating brush seal for gas turbine combustor

Abstract

The gas turbine includes a combustor 10 having a transition piece 18 with its exit end spaced from a first-stage nozzle 22. A brush seal 26 seals about the space between the transition piece and first-stage nozzle. The brush seal includes a sealing cap 28 supported by one of the transition piece and the first-stage nozzle and having a portion 38 overlying the other of the transition piece and first-stage nozzle. A seal ring 30 is secured to the other of the transition piece and the first-stage nozzle and carries bristles 32 projecting therefrom for engagement with the overlying portion 38 of the sealing cap 28 to seal the gap between the transition piece and the first-stage nozzle. In one form, the side face portions of the bristles of the bristle pack form the seal by engaging against a planar sealing surface.

Claims14

Dependent claims

A gas turbine comprising:

a first-stage nozzle;
a combustor having a transition piece for flowing hot gases of combustion from said combustor to said first-stage nozzle, said transition piece being spaced from said first-stage nozzle;
a brush seal between said transition piece and said first-stage nozzle, sealing the space therebetween, said brush seal including a sealing cap and a sealing surface, said brush seal further including a brush seal mount carrying a plurality of elongated brush bristles projecting outwardly from said mount and lying in a plane, said sealing surface and certain of said bristles extending substantially in a plane parallel to the plane of said bristles such that side face portions of said certain bristles register with and engage said sealing surface throughout substantially the entirety of the free length of the certain bristles in registration with the sealing surface to form said seal.

A gas turbine comprising:

a first-stage nozzle;
a combustor having a transition piece for flowing hot gases of combustion from said combustor to said first-stage nozzle, said transition piece being spaced from said first-stage nozzle;
a brush seal between said transition piece and said first-stage nozzle sealing the space therebetween, said brush seal including a brush seal mount and a sealing surface, said brush seal mount carrying a plurality of elongated brush bristles projecting from said mount and lying in a plane, said sealing surface and certain of said bristles extending substantially in a plane parallel to the plane of said bristles such that side face portions of said certain bristles register with and engage said sealing surface throughout substantially the entirety of the free length of the certain bristles in registration with the sealing surface to form said seal.

Dependencies are inferred from the claim text.

Self-accommodating brush seal for gas turbine combustor

Life of this patent

Self-accommodating brush seal for gas turbine combustor

Life of this patent

Abstract

Claims14