The invention relates to sealing structures between a rotating component and a static component typically found in turbomachinery and, more particularly, to a compliant-plate seal arrangement including staggered shingles that are effective in reducing axial leakage.
Dynamic sealing between a rotor (e.g., rotating shaft) and a stator (e.g., static shell, casing or housing) is an important concern in turbomachinery. Several methods of sealing have been proposed in the past. In particular, sealing based on flexible members has been utilized including seals described as leaf seals, brush seals, finger seals, shim seals, etc.
A brush seal is comprised of tightly packed generally cylindrical bristles that are effective in preventing leakage because of their staggered arrangement. The bristles have a low radial stiffness that allows them to move out of the way in the event of a rotor excursion while maintaining a tight clearance during steady state operation. Brush seals, however, are effective only up to a certain pressure differential across the seal. Because of the generally cylindrical geometry of the bristles, the brush seals tend to have a low stiffness in the axial direction, which limits the maximum operable pressure differential to generally less than 1000 psi. Radial and axial directions in this context are defined with respect to the turbo-machine axis.
To overcome this problem, leaf seals have been proposed that include a plate-like geometry with higher axial stiffness and therefore the capability of handling large pressure differentials. Axial leakage, however, remains a problem due to the leaf seal geometry. That is, with reference to
In an exemplary embodiment of the invention, a shaft seal reduces leakage between a rotating shaft and a stator. The shaft seal includes a plurality of compliant-plate members attached to the stator in facing relation, the compliant-plate members defining a sealing ring between the stator and the rotating shaft. Each of the compliant-plate members includes a plurality of shingles, wherein adjacent compliant-plate members are disposed relative to each other such that the shingles are at least partially staggered in a direction of axial leakage. This preferred embodiment of compliant-plate seals is also referred to as a shingle seal.
In another exemplary embodiment of the invention, a method of manufacturing a shaft seal for reducing leakage between a rotating shaft and a stator includes the steps of (a) providing a plurality of compliant-plate members, each including a plurality of shingles; (b) attaching the plurality of compliant-plate members to the stator in facing relation, the compliant-plate members defining a sealing ring between the stator and the rotating shaft; and (c) positioning adjacent compliant-plate members relative to each other such that the shingles are at least partially staggered in a direction of axial leakage.
In a conventional leaf seal, because the leaves are packed tightly at the tips and loosely at the roots, leakage from high pressure side to low pressure side entering the leaf pack tends to flow/expand radially outwards, then flows axially, and finally converges as it exits the leaf pack. The compliant-plate seal described herein significantly reduces the above-mentioned axial leakage with structure that is geometrically and functionally a hybrid between a conventional compliant-plate seal and a conventional brush seal. The geometric configuration of the compliant-plate seal described herein, also known as a shingle seal, is such that it retains the low leakage attributes of the brush seal owing to a staggered arrangement of shingles, as well as the high pressure-differential capability of conventional leaf seals owing to the plate shaped shingle members.
With reference to
The exemplary shingle seal described herein includes at least two kinds of compliant-plate members 16A, 16B as shown in
The shingles 18 are preferably rectangular in the circumferential view as shown in
In the conventional leaf seal as shown in
The compliant-plate members 16 and therefore the shingles 18 may not be straight or of uniform thickness as seen in the axial view, but rather could be curved or tapered.
The compliant-plates 16 may be coated or surface-treated with special materials to achieve one or more of the following objectives: minimize friction, wear and heat generation during relative sliding, act as diffusion barrier during manufacturing, allow high temperature operation, and improve seal life. The surface of the rotor, which is in close proximity to the compliant-plate tips may also be coated for the above or other reasons. Common coating methods include Physical Vapor Deposition, thermal spray and galvanic deposition, to name a few. Coating materials include, but are not limited to, Titanium Nitride, Zirconium Nitride, NickelChrome-ChromeCarbide along with solid lubricants, Nickel, etc.
Each compliant-plate and/or shingle may have additional features at the root to enable assembly steps such as, but not limited to, alignment, fixturing and spacing. A typical example is a T-shape feature 23 at the compliant-plate root shown in
Additionally, there may be provided further vertical features such as rings 36, attached to the static shell 15 or housing 14, seen in the circumferential view in
Referring to
An alternative option for fabricating the compliant-plate members is illustrated in
Additionally, the strip material 22 may incorporate the T-shaped section 23, as shown in
An additional de-burring step can be included between the punching and folding steps, where the continuous unfolded strip may be made to pass between emery papers or similar de-burring devices. A single machine can be designed or configured to continuously perform all the above manufacturing steps in series.
As part of the punching process, dimples of controlled depth may be formed on the strip material in the seal root area so as to provide any necessary spacing between the members. Other spacing features such as controlled thickness coating may also be incorporated.
The described methods provide fabrication processes that allow integral multiples of the compliant-plate effective thickness at the seal root. Other practical manufacturing methods, one of which is described below, may be conceived that can allow fractional overlap (as seen in the axial view) or non-integral multiples of the compliant-plate effective thickness at the seal root.
Still another alternative method of shingle seal fabrication utilizes a conventional leaf seal that may be cut vertically into several parallel segments of varying thickness using wire EDM or the like along cutting lines 38 shown in
The shingle seal described herein is geometrically and functionally a hybrid between a conventional leaf seal and a conventional brush seal. The geometric configuration of the described shingle seal is such that it retains the low leakage attributes of the brush seal owing to a staggered arrangement of shingles as well as the high pressure differential capacity of leaf seals owing to the plate shaped shingles.
While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiments, it is to be understood that the invention is not to be limited to the disclosed embodiments, 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 |
---|---|---|---|
4526509 | Gay, Jr. et al. | Jul 1985 | A |
4811961 | Williams | Mar 1989 | A |
5031922 | Heydrich | Jul 1991 | A |
5135237 | Flower | Aug 1992 | A |
5749584 | Skinner et al. | May 1998 | A |
5755445 | Arora | May 1998 | A |
5941685 | Bagepalli et al. | Aug 1999 | A |
5961125 | Wolfe et al. | Oct 1999 | A |
5961280 | Turnquist et al. | Oct 1999 | A |
5971400 | Turnquist et al. | Oct 1999 | A |
6027121 | Cromer et al. | Feb 2000 | A |
6030175 | Bagepalli et al. | Feb 2000 | A |
6045134 | Turnquist et al. | Apr 2000 | A |
6053699 | Turnquist et al. | Apr 2000 | A |
6079945 | Wolfe et al. | Jun 2000 | A |
6105966 | Turnquist et al. | Aug 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 |
6139019 | Dinc et al. | Oct 2000 | A |
6168162 | Reluzco et al. | Jan 2001 | B1 |
6196550 | Arora et al. | Mar 2001 | B1 |
6220602 | Webster et al. | Apr 2001 | B1 |
6250640 | Wolfe et al. | Jun 2001 | B1 |
6250641 | Dinc et al. | Jun 2001 | B1 |
6257586 | Skinner et al. | Jul 2001 | B1 |
6260269 | Turnquist et al. | Jul 2001 | B1 |
6261057 | Turnquist et al. | Jul 2001 | B1 |
6267381 | Wright | Jul 2001 | B1 |
6286211 | Turnquist et al. | Sep 2001 | B1 |
6308958 | Turnquist et al. | Oct 2001 | B1 |
6331006 | Baily et al. | Dec 2001 | B1 |
6343792 | Shinohara et al. | Feb 2002 | B1 |
6364316 | Arora | Apr 2002 | B1 |
6367806 | Turnquist et al. | Apr 2002 | B1 |
6428009 | Justak | Aug 2002 | B2 |
6431827 | Wolfe et al. | Aug 2002 | B1 |
6435513 | Skinner et al. | Aug 2002 | B2 |
6439844 | Turnquist et al. | Aug 2002 | B1 |
6460857 | Turnquist et al. | Oct 2002 | B1 |
6553639 | Hobbs et al. | Apr 2003 | B2 |
6644667 | Grondahl | Nov 2003 | B2 |
6685427 | Dhar et al. | Feb 2004 | B1 |
6733014 | Inoue | May 2004 | B2 |
6764078 | Inoue | Jul 2004 | B2 |
6786487 | Dinc et al. | Sep 2004 | B2 |
6786488 | Laurello et al. | Sep 2004 | B2 |
6790001 | Turnquist et al. | Sep 2004 | B2 |
6854735 | Sarshar et al. | Feb 2005 | B2 |
6860484 | Urlichs | Mar 2005 | B2 |
6874788 | Kono | Apr 2005 | B2 |
6935631 | Inoue | Aug 2005 | B2 |
6976680 | Uehara et al. | Dec 2005 | B2 |
7066468 | Uehara et al. | Jun 2006 | B2 |
7159872 | Nicholson et al. | Jan 2007 | B2 |
7201378 | Kono | Apr 2007 | B2 |
7419164 | Awtar et al. | Sep 2008 | B2 |
20010030397 | Beichl | Oct 2001 | A1 |
20020117806 | Grondahl | Aug 2002 | A1 |
20030042682 | Inoue | Mar 2003 | A1 |
20030062684 | Inoue | Apr 2003 | A1 |
20030062685 | Inoue | Apr 2003 | A1 |
20030062686 | Uehara et al. | Apr 2003 | A1 |
20040150165 | Grondahl | Aug 2004 | A1 |
20040256810 | Nakano et al. | Dec 2004 | A1 |
20050194745 | Hogg | Sep 2005 | A1 |
20060033285 | Nishimoto et al. | Feb 2006 | A1 |
20060208427 | Wright et al. | Sep 2006 | A1 |
20060210392 | Enderby | Sep 2006 | A1 |
20080061513 | Awtar et al. | Mar 2008 | A1 |
Number | Date | Country |
---|---|---|
0 391 676 | Oct 1990 | EP |
1 298 368 | Apr 2003 | EP |
1 302 708 | Apr 2003 | EP |
0 933 567 | Nov 2006 | EP |
1 479 952 | Jan 2007 | EP |
Number | Date | Country | |
---|---|---|---|
20080061513 A1 | Mar 2008 | US |