Assembly forming a gasket for a turbomachine, comprising a brush seal
An assembly forming a gasket for a turbomachine, includes a brush seal made of a plurality of sealing elastic bristles surrounding a core, a retaining ring including a recess to at least partly accommodate the brush seal, and a bearing cover, placed in contact with the brush seal to hold it in position against the retaining ring, the brush seal being located between the retaining ring and the bearing cover.
1. A method of forming an assembly forming a gasket for a turbomachine, comprising:
providing a brush seal made of a plurality of sealing elastic bristles surrounding a core, and a retaining ring comprising a recess;
fixing the retaining ring to a support element of a turbomachine stator part;
inserting the brush seal in the recess of the retaining ring;
placing a bearing cover in contact with the brush seal to hold the brush seal in position against the retaining ring, the brush seal being located between the retaining ring and the bearing cover; and
machining an inner diameter of the bristles of the brush seal, after assembling the bearing cover on the retaining ring, such that the brush seal is adapted to meet sealing requirements,
wherein the retaining ring includes a fixing leg for fixing the retaining ring to the support element of the turbomachine stator part, the fixing leg forming a substantially linear extension of the retaining ring from a portion of the retaining ring in contact with the brush seal, a free end of the fixing leg being above an upper end of the bearing cover.
2. The method according to claim 1 , wherein the recess of the retaining ring has a cylindrical shape to fit closely a shape of a toroidal area of the brush seal and to hold the brush seal in position.
3. The method according to claim 1 , wherein the bearing cover comprises a first planar bearing portion, placed in contact with the bristles of the brush seal outside a toroidal area of the brush seal.
4. The method according to claim 1 , wherein the bearing cover comprises a second bearing portion, placed in contact with the bristles of the brush seal at the toroidal area of the brush seal and having a cylindrical shape to fit closely a shape of the toroidal area of the brush seal.
5. The method according to claim 1 , wherein the bearing cover is fixed to the retaining ring by welding or crimping.
6. The method according to claim 1 , wherein a portion of the retaining ring abuts a first side of the bristles, and a portion of the bearing cover abuts a second side of the bristles.
7. An assembly forming a gasket for a turbomachine, comprising:
a brush seal made of a plurality of sealing elastic bristles surrounding a core,
a retaining ring comprising a recess to at least partly accommodate the brush seal, and
a bearing cover, placed in contact with the brush seal to hold the brush seal in position against the retaining ring, the brush seal being located between the retaining ring and the bearing cover,
wherein an inner diameter of the bristles of the brush seal is machined after assembling the bearing cover on the retaining ring so as to be adapted to sealing requirements,
wherein the assembly can be assembled and disassembled on the turbomachine, and
wherein the retaining ring comprises a fixing leg for fixing the retaining ring to a support element of a turbomachine stator part, the fixing leg forming a substantially linear extension of the retaining ring from a portion of the retaining ring in contact with the brush seal, a free end of the fixing leg being above an upper end of the bearing cover.
8. The assembly forming a gasket according to claim 7 , wherein the recess of the retaining ring has a cylindrical shape to fit closely a shape of a toroidal area of the brush seal, at least partly accommodated in the recess, and to hold the brush seal in position.
9. The assembly forming a gasket according to claim 7 , wherein the bearing cover comprises a first planar bearing portion, placed in contact with the bristles of the brush seal outside a toroidal area of the brush seal.
10. The assembly forming a gasket according to claim 7 , wherein the bearing cover comprises a second bearing portion, placed in contact with the bristles of the brush seal at a toroidal area of the brush seal and having a cylindrical shape to fit closely a shape of the toroidal area of the brush seal.
11. The assembly forming a gasket according to claim 7 , wherein the bearing cover is fixed to the retaining ring by welding or crimping.
12. The assembly forming a gasket according to claim 7 , wherein a portion of the retaining ring abuts a first side of the bristles, and a portion of the bearing cover abuts a second side of the bristles.
13. An assembly forming a gasket for a turbomachine, comprising:
a brush seal made of a plurality of sealing elastic bristles surrounding a core,
a retaining ring comprising a recess to at least partly accommodate the brush seal, and a fixing leg extending linearly from a portion of the retaining ring in contact with the brush seal in an opposite direction of the bristles of the brush seal, and
a bearing cover, placed in contact with the brush seal to hold the brush seal in position against the retaining ring, the brush seal being located between the retaining ring and the bearing cover,
wherein the brush seal is free of plastic deformation when being held in position against the retaining ring by the bearing cover,
wherein a rigidity of the retaining ring is higher than a rigidity of the brush seal,
wherein an inner diameter of the bristles of the brush seal is machined after assembling the bearing cover on the retaining ring so as to be adapted to sealing requirements,
wherein the assembly can be assembled and disassembled on the turbomachine, and
wherein the retaining ring comprises a fixing leg for fixing the retaining ring to a support element of a turbomachine stator part, the fixing leg forming a substantially linear extension of the retaining ring from a portion of the retaining ring in contact with the brush seal, a free end of the fixing leg being above an upper end of the bearing cover.
14. A turbomachine stator part, comprising:
an assembly forming a gasket according to claim 7 , and
a support element on which the retaining ring of the assembly forming a gasket is fixed.
15. The turbomachine stator part according to claim 14 , further comprising an elastic return member placed between the support element and the bearing cover of the assembly forming a gasket to intensify contact between the bristles of the brush seal and the retaining ring.
16. A turbomachine comprising an assembly forming a gasket according to claim 7 .
17. A turbomachine comprising a turbomachine stator part according to claim 14 .
18. A method for assembling an assembly forming a gasket according to claim 7 on a turbomachine stator part, comprising the only step of fixing the retaining ring of the assembly forming a gasket to a support element of the stator part.