Embodiments of the invention relate to brush seals for sealing a gap between a high pressure and a low pressure area.
The use of brush seals for sealing gaps, such as those found in gas turbine engines, is known in the art. For example, in gas turbine engines brush seals are often utilized to minimize leakage of fluids at circumferential gaps, such as between a machine housing and a rotor, around a rotary shaft of the engine, and between two spaces having different fluid pressure within the engine. The fluid pressure within the system, which may be either liquid or gas, is greater than the discharge pressure (the pressure outside the area of the engine housing, toward which the fluid will tend to leak), thus creating a pressure differential in the system. As used herein, the system pressure side of the brush seal is referred to as the high pressure side, while the discharge pressure side of the brush seal is referred to as the low pressure side.
Conventional brush seals include a bristle pack which is traditionally flexible and includes a plurality of bristles for sealing the gap, the bristles having a free end for contacting one component, such as the rotor. Circular brush seals have been utilized in gas turbine engine applications to minimize leakage and increase engine fuel efficiency. Conventional brush seals are made from metallic fibers, which are typically cobalt or nickel-base high temperature superalloy wire products suitable for elevated temperature operation.
Because brush seals are contacting seals where bristle tips establish sealing contacts against the rotor surface, their applications are generally limited to surface speeds of less than about 1200 ft/sec and temperatures below about 1500° F. and usually below about 1200-1300° F. At extremely high surface speeds and temperatures, metallic brush seals have been found to suffer from excessive wear resulting from bristle tip melting. There are many areas in existing gas turbine engines, such as balance piston and other secondary flow areas near the gas path where surface speed and temperature conditions are typically beyond the capabilities of conventional metallic brush seals. As such, these locations are generally sealed by large-gap labyrinth seals which have been found to have high levels of leakage during use as compared to contacting seals such as carbon seals and metallic brush seals. Rotating intershaft seals, for both co-rotating and counter-rotating shafts, for example in advanced military aircraft engines, are also generally labyrinth type seals.
Metallic brush seals are also traditionally not used for sealing buffer air near the bearing cavity. Buffer air is used to seal the bearing lubricant by pressurizing the buffer air higher than that of bearing lubricating oil pressure. Metallic brush seals are not used because of metallic debris could reach the interface between the bearing elements (e.g., balls, pins, etc.) and races causing bearing and rotor damage and possibly failure. Again, current seals used at these locations are generally high-leakage labyrinth seals. Higher leakage for bearing oil seals is not desirable because of contamination of downstream components and cabin air that can be introduced through the leak path. Appropriate carbon seals have not yet been developed for such applications because of their fragile characteristics and low damage tolerance.
Large diameter main shaft bearing oil seals for large aircraft engines or land based turbo machinery are also typically labyrinth seals with large clearances that lead to oil contamination. In these applications large diameter carbon seals are expensive and metallic brush seals are not suitable.
Although there have been developments in creating non-metallic brush seals, the use of polymeric or ceramic material to replace the metallic bristles has met with many design challenges due, in part, to the difficulty in handling and fabricating brush seals from such material. Typically ceramic or polymeric fibers are very thin, averaging in the range of about 2-3 μm in diameter. Fibers that are this thin have not traditionally been considered suitable for fabricating bristle strips. For example, the flexibility of the fibers can make it difficult to machine the inner diameter (ID) of the brush seal to the required tolerances.
Therefore, there exists a need for a contacting seal that minimizes leakage as compared to traditional labyrinth type seals and which can operate under higher temperatures and/or higher speeds than existing metallic brush seals and which can be readily fabricated.
In accordance with one embodiment of the present invention, there is provided a contacting brush seal including a plurality of fibers fabricated from non-metallic materials, the fibers being twisted or braided together substantially along their length (L). The fibers may be particularly made from ceramic or polymeric materials, and in one embodiment are more particularly fabricated from NOMEX®, a synthetic aromatic polyamide polymer, manufactured by DuPont for high temperature applications. The non-metallic ceramic brush seals disclosed herein have melting points much higher than those of nickel and cobalt base superalloys and, therefore, should prevent the tips from melting under most conditions. In addition, brush seals made from softer high strength polymeric fibers with moderate (about 500-700° F.) temperature capability, may also be used for high performance bearings such as counter-rotating bearing cavities of advanced gas turbine engines.
In accordance with one embodiment, a brush seal includes a plurality of metallic bristles and a support member that mechanically captures the plurality of metallic bristles. In one arrangement, the support member includes a pair of relatively rigid front and back plates and a pair of relatively flexible front and back plates, the plurality of metallic bristles, such as formed as a flexible bristle pack, being disposed between the front and back plates. The support member provides a level of rigidity to the flexible fiber pack. In one arrangement, the support member is configured to hold the flexible fiber pack in an axially inclined position such that the flexible fiber pack is coned either toward a low pressure area or a high pressure area in a brush seal system.
In one arrangement, a brush seal includes a plurality of metallic bristles having a bristle length and a support member constructed and arranged to support the plurality of metallic bristles. The support member includes at least one flexible plate extending at least substantially along the bristle length of the plurality of bristles.
In one arrangement, a brush seal system includes a contact rotor and a rotatable shaft, the contact rotor and the rotatable shaft defining a space therebetween. The brush seal system also includes a brush seal disposed between the contact rotor and the rotatable shaft to divide the pathway into a high pressure side and a low pressure side. The brush seal includes a plurality of metallic bristles having a bristle length and a support member constructed and arranged to support the plurality of metallic bristles. The support member has at least one flexible plate extending at least substantially along the bristle length of the plurality of bristles.
In one arrangement, a brush seal includes a plurality of brush seal members having a brush seal member length and a support member constructed and arranged to support the plurality of brush seal members. The support member includes at least one flexible plate extending at least substantially along the brush seal member length of the plurality of brush seal members. The plurality of brush seal members is configured as a brush seal pack. The support member is constructed and arranged to mount to a base and to orient the brush seal pack in an axially inclined position relative to the base.
It should be understood that the drawings are provided for the purpose of illustration only and are not intended to define the limits of the invention. The present invention is not limited to the precise arrangements and instrumentalities shown in the drawings and the drawings are not necessarily to scale, emphasis instead being placed upon illustrating the principles disclosed herein.
Referring initially to
In the case where the brush seal members 12 are formed as ceramic or polymeric fibers, the ceramic or polymeric fibers are preferably twisted or braided, as illustrated in
In one embodiment, NOMEX®, can be selected for brush seal fabrication because the NOMEX® fibers are generally made into strong fabrics for applications where thermal and flame resistant properties are essential. NOMEX® is the high temperature version of KEVLAR® which is as strong as or stronger than high strength steel. Other general properties of NOMEX® include: 1.) usable in wide range of temperatures from −196° C. to over 300° C.; 2.) broad compatibility with industrially used oils, resins, adhesives and refrigerants; 3.) chemical resistance to acids, alkalis and solvents; 4.) non-toxic; 5.) self-extinguishing; 6.) does not support combustion; and 7.) does not drip or melt when heated or burned.
In one embodiment, Nextel™ can be selected for brush seal fabrication. Nextel™ fibers are very thin, in the range of about 25 μm to 0.001″ in diameter, and have a low modulus of elasticity. In this embodiment, the fibers are twisted as shown in
The thinner and more flexible front and back plates, 30, 32 located near an inner diameter (ID) of the brush seal 10, protect the brush seal members 12 from damage during installation, aid in holding the brush member pack 17 together, and minimize its flaring. The flexible plates 30, 32 help to control axial and radial displacements of the brush seal members 12 by supporting the brush member pack 17 against pressure and centrifugal forces within a brush seal system (e.g., engine). The front plate 30 may be fabricated from a thin metallic strip which is configured to contact the brush member pack 17 when the brush seal system builds up pressure. Thus, the front plate 30 acts as a flow deflector minimizing brush seal members blow-down on a rotating surface, such as the rotor 26, causing excessive brush member wear. The flexible back plate 32 may also be made from a metallic sheet stock. However, the thickness of the flexible back plate 32 may be greater than the front plate thickness 30. The relatively thicker back plate 32 is designed to support the brush member pack 17 under pressure.
The flexible front and back plates 30, 32 may also be divided into segments 21 by radial slots 20 as shown in
The flexible plates 30, 32 can extend a predetermined length 38 of the brush seal members 12 so as to expose only a brush seal members tip area 22, and protect the brush seal members 12 from being damaged during installation and/or mishandling. The brush seal 10 may be attached to the rotating shaft 24 at a first end can contact the rotor 26 at a second end with the rotating shaft 24 and the rotor 26 configured to rotate in relatively opposing directions. For a rotating seal, the stresses in the brush seal members 12 resulting from the centrifugal force are minimized as the brush member pack 17 is supported by flexible metallic back plate segment 21. The metallic segments 21 are designed to withstand the maximum bending stress due to centrifugal force. By securing the brush member pack 17 between axially inclined (e.g., coned) front and back plates 30, 32 in the direction of the fluid flow, the front plate 30 can control brush memberpack 17 displacement and can minimize stresses in the brush member pack 17.
An order of magnitude value of the maximum bending stress induced in a rotating flexible metallic segment is estimated in the following example. The following example is provided for purposes of illustration only and is not intended to limit the scope of the present invention.
Assuming that the flexible back plate 32 is made from age hardened Inco 718 (density=0.295 lbm/(in)3 and Y.S=130,000 psi); the size of each finger segment 21 is:
width=1.0″, length=0.25″ and thickness=0.05″,
mass of each finger=1.0×0.25×0.05×0.295 lbm=0.0037 lbm
and at the center of mass of each finger segment 21,
surface speed=500 ft/sec
radius=0.5 ft;
centrifugal force (Fcf) acting radially outward on each finger segment 21 is given by:
If the cant angle of the finger segments 21 with respect to a vertical plane=10°, the bending force (Fn) acting normally through the center of mass of each finger 21 is:
F
n
=F
cf Sin 10°=1850×0.174=322 lbs.
[Note: The Fcf will vary along the length of the finger segment 21 and it needs to be integrated for a more accurate estimate]
Therefore, the maximum bending stress (σmax) generated at the surface of each finger segment 21 is:
where,
This stress is well below the yield stress of Inco 718. The rest of the rigid structure of the rotating seal can easily be optimized to maintain stresses below the yield stress. For design optimization, detailed Finite Element Analysis (FEA) of the entire structure may be performed.
It will be appreciated that the braided ceramic brush seals, as disclosed herein, can operate effectively at relatively high temperatures (above about 1500° F.) and at high surface speeds (exceeding about 1000 ft/sec) while being capable of being manufactured using standard automatic and low-cost brush strip manufacturing process. Controlled bending of the flexible plates 30, 32 and the brush member pack 17 also aid in controlling seal radial clearance or interference throughout the operating cycle of the bush seal system.
It will be understood that various modifications may be made to the embodiments disclosed herein. Therefore, the above description should not be construed as limiting, but merely as exemplifications of preferred embodiments. Those skilled in the art will envision other modifications within the scope, spirit and intent of the invention.
For example, although the fibers are illustrated as twisted in
As indicated above with respect to
As indicated above with respect to
As indicated above with respect to
The present application is a continuation-in-part of U.S. Utility application Ser. No. 11/121,872, filed May 4, 2005, entitled “Non-metallic Brush Seals,” which claims the benefit of U.S. Provisional Application No. 60/567,905 filed May 4, 2004. The entire content of the above applications is incorporated by reference herein.
Number | Date | Country | |
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60567905 | May 2004 | US |
Number | Date | Country | |
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Parent | 11121872 | May 2005 | US |
Child | 11787301 | US |