The present invention relates to seals in turbines and turbo-machinery for sealing between stationary and rotary components and particularly relates to a combination of a brush seal and flexible beams for enhanced sealing capability
Current state-of-the art seals for turbines and turbo-machinery include brush seals and leaf seals. The construction of both are very complex and labor intensive, hence driving cost. For example, the individual bristles of brush seals are not modular. Rather, they are laid in by hand to form a bristle pack at a certain diameter. Specialized tooling is also required for brush seals of different diameters. This becomes a particular problem where brush seals are used in steam turbines which have a substantial number of stages e.g., 40-50 stages of different diameters and even additional and varying diameters depending upon seal location. Thus a very large number of differently sized seals would be required at substantial cost. Certain of these problems in brush seals have been addressed e.g. by offering brush seals in flexible strips in an effort to avoid tooling issues. However, such seals are often limited in their pressure drop capacity. Accordingly there is a need for seals between stationary and rotary components in turbines and turbo-machinery affording a modular seal construction with little or no dependency on diameter specific tooling, enhanced pressure capabilities and stiffness over conventional brush seals and the elimination of diameter specific tooling in most cases.
In a preferred embodiment of the present invention, there is provided a pressure seal for a flow path comprising: a pair of plates spaced from and extending generally parallel to one another and extending in spaced generally parallel planes; a brush seal between the plates extending in a plane between and generally parallel to planes containing the plates and including a plurality of bristles having tips extending beyond margins of the plates; and a first set of a plurality of beams stacked one against the other between one of the plates and the brush seal, the beams extending beyond the margins of the plates and in a plane generally parallel to the planes containing the plates and the brush seal and terminating short of the bristle tips.
In a further preferred embodiment of the present invention, there is provided a pressure seal in a flow path comprising a pair of plates spaced from one another carried by a stationary component and extending toward a rotary component; a brush seal between the plates carried by the stationary component and including a plurality of bristles extending generally toward and for engagement with the rotary component; and a first set of a plurality of beams stacked one against the other in the circumferential direction of the pressure seal and carried by the stationary component between one of the plates and the bristles, the beams extending generally toward and terminating short of the rotary component.
a) is a cross-section of a brush bristle taken from
Referring to the drawings particularly to
The seal 10 includes a fence or front plate 16, for example on the high pressure side of the seal, a first set of a plurality of beams 18 described below, a plurality of bristles 20 forming a bristle pack 22, a second set of beams 24 on the downstream side of the seal and a back plate 26. Shims 30 and 32 are interposed between the first set of beams 18 and the bristles 22 and the bristles 22 and the second set of beams 24, respectively. The individual bristles 20 forming the bristle pack 22 may be formed in a conventional manner with proximal ends of the bristles secured to a plate or a weldment 26. The individual bristles are typically 5 mils or less in diameter (see the round cross-sectional shape in
The first and second sets of beams 18 and 24 respectively are formed substantially identically to one another and a description of one set constitutes a description of the other set. The beams are preferably formed to have a rectilinear or square cross section. As illustrated in
The beams 18 and 24 may extend from their proximal ends to their distal ends at angles corresponding to the angle of the bristles at each circumferential location or they may extend at greater or lesser angles relative to the bristles and at different angles relative to one another. The distal ends of the beams also terminate short of the surface of the rotary component as illustrated in
It will also be appreciated that the front fence 16 and back plate 26 may be formed in strips i.e., plates which are not machined. Thus, the front fence 16 and back plate 26 may be readily and inexpensively formed to varying diameters as necessary and desired. The assembly of the front fence, back plate, beams, shims and bristle pack may be readily formed to varying diameters by a bending operation without special tooling for each diameter. Further, the beams, while flexible, provide a certain stiffness which enables the beams to take up most of the pressure difference across the seal. The bristles of the bristle pack provide the necessary flexibility for rotor stability as well as a fine sealing capability. The spaces between adjacent beams as well as the spaces between the distal ends of the beams and the surface of the rotor provide a bypass flow about the beams whereby most of the pressure drop is taken up by the beams and the remaining pressure drop is taken up by the bristles.
Referring to
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
Number | Name | Date | Kind |
---|---|---|---|
5106104 | Atkinson et al. | Apr 1992 | A |
5201530 | Kelch et al. | Apr 1993 | A |
5474306 | Bagepalli et al. | Dec 1995 | A |
5480165 | Flower | Jan 1996 | A |
5568931 | Tseng et al. | Oct 1996 | A |
5704760 | Bouchard et al. | Jan 1998 | A |
5749584 | Skinner et al. | May 1998 | A |
6010132 | Bagepalli | Jan 2000 | A |
6027121 | Cromer et al. | Feb 2000 | A |
6042119 | Bagepalli et al. | Mar 2000 | A |
6045134 | Turnquist et al. | Apr 2000 | A |
6105967 | Turnquist et al. | Aug 2000 | A |
6131910 | Bagepalli et al. | Oct 2000 | A |
6131911 | Cromer et al. | Oct 2000 | A |
6139018 | Cromer et al. | Oct 2000 | A |
6168162 | Reluzco et al. | Jan 2001 | B1 |
6173958 | Dinc et al. | Jan 2001 | B1 |
6250640 | Wolfe et al. | Jun 2001 | B1 |
6257586 | Skinner | Jul 2001 | B1 |
6290232 | Reluzco | Sep 2001 | B1 |
6308957 | Wright | Oct 2001 | B1 |
6331006 | Baily et al. | Dec 2001 | B1 |
6390476 | Tong et al. | May 2002 | B1 |
6431827 | Wolfe et al. | Aug 2002 | B1 |
6435513 | Skinner | Aug 2002 | B2 |
6464230 | Tong et al. | Oct 2002 | B1 |
6527274 | Herron et al. | Mar 2003 | B2 |
6550777 | Turnquist et al. | Apr 2003 | B2 |
6589012 | Burnett et al. | Jul 2003 | B2 |
6619669 | Zhuo et al. | Sep 2003 | B2 |
6648334 | Inoue | Nov 2003 | B2 |
6669203 | Mortzheim | Dec 2003 | B1 |
6669443 | Burnett et al. | Dec 2003 | B2 |
6790001 | Turnquist et al. | Sep 2004 | B2 |
6805356 | Inoue | Oct 2004 | B2 |
6827350 | Walcott et al. | Dec 2004 | B2 |
Number | Date | Country | |
---|---|---|---|
20070063448 A1 | Mar 2007 | US |