초록 ▼

A foil thrust bearing forms the primary rotating interface for a film riding face seal. This face seal includes a spring system that will allow the entire assembly to translate axially relative to a static attachment. The complete assembly will form a hybrid foil/film riding face seal that shows muc

A foil thrust bearing forms the primary rotating interface for a film riding face seal. This face seal includes a spring system that will allow the entire assembly to translate axially relative to a static attachment. The complete assembly will form a hybrid foil/film riding face seal that shows much promise at being sufficiently flexible to enable operation in a gas turbine engine. The seal includes a flexible top plate having a non-flat surface under its working conditions, and a spring support system to allow the top plate to accommodate axial excursions and out-of-flat distortions.

대표청구항 ▼

The invention claimed is: 1. In a gas riding annular face seal for mounting between a first structure and an adjacent second structure so that the annular face seal separates a first region from a second region, at least one of the structures being rotatable relative to the other, the improvement c

The invention claimed is: 1. In a gas riding annular face seal for mounting between a first structure and an adjacent second structure so that the annular face seal separates a first region from a second region, at least one of the structures being rotatable relative to the other, the improvement comprising: the face seal comprises a flexible annular top plate for mounting on such first structure; the top plate having an undulate face surface, at least when such structures are rotating relative to each other, for generating a riding gas film between the top plate and such second structure, the top plate (a) being sufficiently flexible to be compliant to out-of-flat distortions between the first and second relatively rotating structures, and (b) having a plurality of sector plates on the face surface; a support spring system for rendering the top plate compliant to out-of-flat distortions and axial excursions between the rotating structures while maintaining the riding gas film; and a seal ring positioned between the top plate and the structure on which the face seal is mounted to establish a barrier to gas flow across the face seal, whereby the face seal is able to maintain a pressure differential between the first and second regions. 2. The face seal of claim 1 wherein the seal ring is secured to the top plate. 3. The face seal of claim 2 wherein the first structure is a stationary structure and the second structure is rotatable. 4. The face seal of claim 1 wherein the seal ring comprises a labyrinth seal. 5. The face seal of claim 1 wherein the support spring system comprises a primary spring system for accommodating out-of-flat distortions, and a secondary spring system for accommodating axial excursions. 6. The face seal of claim 5 wherein the support spring system comprises a support plate having two sides, wherein the primary spring system is on one side of the support plate, and the secondary spring system is on the other side of the support plate from the primary spring system. 7. The face seal of claim 6 wherein the primary spring system is between the top plate and the support plate. 8. The face seal of claim 5 wherein the top plate comprises a low-friction, low-wear surface. 9. The face seal of any one of claims 1, 2, 4 or 5 wherein the plurality of sector plates on the face surface overlap each other to provide an undulate surface even when neither of such first and second structures are rotating. 10. The face seal of claim 9 wherein the sector plates are hingedly attached to the top plate. 11. The face seal of claim 1 wherein the top plate is flat when at rest, and wherein the seal is configured to allow the top plate to deform into a non-flat configuration when such structures are rotating relative to each other. 12. The face seal of any one of claims 1, 2, 4 or 5 wherein the plurality of sector plates on the face surface are spaced from one another to define grooves between them to provide an undulate surface even when neither of such first and second structures are rotating. 13. The face seal of any one of claims 1, 2, 4 or 5 wherein the seal is mounted on such first structure adjacent to such second structure, and the first structure is a stationary structure and the second structure is rotatable. 14. The face seal of any one of claims 1, 2, 4 or 5 wherein the seal is mounted on such first structure adjacent to such second structure, and the first structure is rotatable. 15. In a gas riding annular face seal for mounting between a first structure and an adjacent second structure so that the annular face seal separates a first region from a second region, at least one of the structures being rotatable relative to the other, the improvement comprising: the face seal comprises a flexible annular top plate for mounting on such first structure, and a seal ring positioned to seal the face seal against gas flow across the face seal; the top plate having an undulate face surface, at least when such structures are rotating relative to each other, for generating a riding gas film between the top plate and such second structure, the top plate (a) being sufficiently flexible to be compliant to out-of-flat distortions between the first and second relatively rotating structures, and (b) having a plurality of sector plates on the face surface; and a support spring system for rendering the top plate compliant to out-of-flat distortions and axial excursions between the rotating structures while maintaining the riding gas film, the support spring system comprising a primary spring system for accommodating out-of-flat distortions, and a secondary spring system for accommodating axial excursions; and a case which is dimensioned and configured for being sealingly mounted onto such first structure, and within which the top plate, the primary spring system, and the secondary spring system are mounted, and wherein the seal ring establishes a seal between the top plate and the case, whereby the face seal is able to maintain a pressure differential between the first and second regions. 16. A method for maintaining a pressure differential across a gas riding annular face seal mounted between a first structure and an adjacent second structure to separate a first region containing gas at a first pressure from a second region containing gas at a second pressure which is different from the first pressure, the face seal comprising (a) a flexible annular top plate mounted on a first structure which is adjacent to a second structure, at least one of the structures being rotatable relative to the other; the top plate having an undulate face surface, at least when the structures are rotating relative to each other, for generating a riding gas film between the top plate and the second structure, the top plate (i) being sufficiently flexible to be compliant to out-of-flat distortions between the first and second relatively rotating structures, and (ii) having a plurality of sector plates on the face surface; (c) a support spring system for rendering the top plate compliant to out-of-flat distortions and axial excursions between the rotating structures while maintaining the riding gas film; and (d) a seal ring positioned between the top plate and the structure on which the face seal is mounted to establish a baffler to gas flow across the face seal, whereby the face seal is able to maintain a pressure differential between the first and second regions, the method comprising: rotating at least one of the first and second structures relative to each other at a rate at least sufficient to establish and maintain the riding gas film. 17. The method of claim 16 comprising maintaining the first structure stationary and rotating the second structure.