Patent Application
20140321993
The present application relates generally to seals for use with rotary machines and more particularly relates to a compliant and an abradable labyrinth sealing system having an elliptical shape for use with a rotary machine such as a rotary compressor and the like.
In a rotary machine, one or more seal generally extend along an interface between the rotating and the stationary components. For example, compressors, turbines, and the like may have one or more seals at the interface between a series of rotating blades or buckets disposed within a casing or a vane. These seals are intended to preserve a pressure differential across the rotating components between upstream and downstream sides thereof. A smaller clearance dimension at the seal generally increases the performance of the seal and the efficiency of the overall rotary machine by limiting the leakage thereacross.
The seals and the components thereof, however, may be subject to relatively high temperatures, thermal gradients, and thermal expansion and contraction during various operational stages of the rotary machine such as during start-up and during other types of transient operations. Typically, the seal includes an extra clearance dimension to reduce the likelihood of contact and damage between the rotating and the stationary components during such transient operations. This extra clearance dimension, however, also may reduce the performance and efficiency of the seal and the overall rotary machine because of the leakage flow across the seal. Fluid leakage between the rotor and the casing may lower the efficiency of the compressor and hence lead to increased fuel costs.
There is thus a desire for an improved sealing system for a rotary machine such as a compressor and the like that reduces leakage therethrough while maintaining adequate clearance during transient operations as well as during steady state operating conditions. Such reduced leakage should improve overall efficiency while preventing damage to the components herein.
One embodiment of the invention is directed to an elliptical sealing system for use with a rotor and a stator housing of a rotary machine. The elliptical sealing system includes a plurality of sealing segments; and an abradable coating having a uniform thickness disposed on each of the plurality of sealing segments, such that the plurality of sealing segments with the abradable coating disposed thereon has a substantially elliptical shape under all conditions when the rotor rotates and the rotor remains stationary.
Another embodiment of the invention is directed to a rotary machine. The rotary machine includes a stator housing, a rotor including a plurality of teeth mounted thereon. The rotary machine further includes a first semielliptical sealing segment and a second semielliptical sealing segment mechanically coupled to each other at about a 3 o'clock position and about a 9 o'clock position. Each of the first semielliptical sealing segment and the second semielliptical sealing segment includes an abradable coating of a uniform thickness disposed thereon. The first semielliptical sealing segment and the second semielliptical sealing segment with the abradable coating disposed thereon have an elliptical shape under all conditions when the rotor rotates and the rotor remains stationary. The abradable coating has an interference engagement with the plurality of teeth at about a 12 o'clock position and at about a 6 o'clock position, and the abradable coating has a line on line engagement with the plurality of teeth at about the 3 o'clock position and at about the 9 o'clock position
These and other features, aspects, and advantages of the present invention will become better understood when the following detailed description is read with reference to the accompanying drawings, in which like characters represent like parts throughout the drawings, wherein:
The present disclosure may be best understood with reference to the figures and detailed description set forth herein. Various embodiments are discussed below with reference to the figures. However, those skilled in the art will readily appreciate that the detailed description given herein with respect to these figures is just for explanatory purposes as the system extends beyond the described embodiments.
Approximating language, as used herein throughout the specification and claims, may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about”, and “substantially” is not to be limited to the precise value specified. Here and throughout the specification and claims, range limitations may be combined and/or interchanged; such ranges are identified and include all the sub-ranges contained therein unless context or language indicates otherwise.
In the following specification and the claims, the singular forms “a”, “an” and “the” include plural referents unless the context clearly dictates otherwise. As used herein, the term “or” is not meant to be exclusive and refers to at least one of the referenced components being present and includes instances in which a combination of the referenced components may be present, unless the context clearly dictates otherwise.
As used herein, the terms “may” and “may be” indicate a possibility of an occurrence within a set of circumstances; a possession of a specified property, characteristic or function; and/or qualify another verb by expressing one or more of an ability, capability, or possibility associated with the qualified verb. Accordingly, usage of “may” and “may be” indicates that a modified term is apparently appropriate, capable, or suitable for an indicated capacity, function, or usage, while taking into account that in some circumstances, the modified term may sometimes not be appropriate, capable, or suitable.
The gas turbine engine 10 may use natural gas, various types of syngas, and/or other types of fuels. The gas turbine engine 10 may be one of any number of different gas turbine engines offered by General Electric Company of Schenectady, N.Y. and the like. The gas turbine engine 10 may have other configurations and may use other types of components. Other types of gas turbine engines also may be used herein. Multiple gas turbine engines 10, other types of turbines, and other types of power generation equipment also may be used herein together. Other types of rotary machines also may be used herein.
Gas leakage out of the gas path or into the gas path of the gas turbine engine 10 from an area of higher pressure to an area of lower pressure generally is undesirable. As described above, gas path leakage in the compressor 15 and/or in the turbine 40 may lower the efficiency of the overall gas turbine engine 10 and lead to increased fuel costs. The gas turbine engine 10 therefore may include a sealing system 50 provided in the compressor 15 and/or the turbine 40. The sealing system 50 facilitates a minimum clearance between the stationary components and the rotating components therein. As a result, fluid leakage through these components may be minimized so as to enhance overall efficiency.
The abradable coating 170 may include an alloy of cobalt, nickel, chromium, aluminum, yttrium, hexagonal boron nitride, and polymers such as polyesters, polyimides, or the like. Alternatively, the abradable coating 170 may include nickel, chromium, aluminum, and clay (bentonite). Further, the abradable coating 170 may include nickel, graphite, and stainless steel. Furthermore, the abradable coating 170 may include nickel, chromium, iron, aluminum, boron and nitrogen. Furthermore, the abradable coating 170 may also include non-metallic materials (e.g., polytetrafluoroethylene applied by electrostatic powder coating process or polytetrafluoroethylene filled synthetic mica which may be attached by a mechanical device). The abradable coating 170 may use any desired material in any desired size, shape, and/or orientation.
As depicted in
The shapes of the first semielliptical sealing segment 270 and the second semielliptical sealing segment 280 are such that when coupled to each other, the coupling joints 273 and 274 define a major axis 250 of the elliptical shape of the sealing system 140. In one embodiment, the length of the major axis 250 is substantially equal to the outside diameter of the rotor 120 defined by the plurality of teeth mounted on the outer surface of the rotor 120. Further, as depicted in
A center of the stator housing 130 is hereinafter also referred to as a statoric center 115 which is represented by + symbol. In one embodiment of the invention, the rotor 120 and the elliptical sealing system 140 are assembled such that the rotoric center 114 and the statoric center 115 are centrally aligned. Further, in one embodiment of the invention, the rotor 120 and the elliptical sealing system 140 are assembled such that the abradable coating 170 has an interference engagement with the teeth of the rotor 120 at about the 12 o'clock position and at about the 6 o'clock position, and the abradable coating 170 has a line on line engagement with the teeth at about the 3 o'clock position and at about the 9 o'clock position. The term “line on line arrangement” as used herein refers to providing no engagement between the abradable coating 170 and the teeth at the 3 o'clock and the 9 o'clock positions such that no end gap is introduced at the 3 o'clock and the 9 o'clock positions. Such line on line engagement is achieved by designing the rotary machine such that the major axis 250 of the elliptical sealing system 140 is substantially equal to the outside diameter of the rotor 120 defined by the teeth.
Once assembled, the gas turbine engine 10 may be operated for about a few seconds or minutes (hereinafter also referred to as an initial period of rotation). For example, when operated at a certain speed (e.g., at about 4500 rpm) during the initial period of rotation, the rotor journal may be lifted-up into the rotor bearing from its initial position. Consequently, the rotor 120 also lifts-up and the teeth of the rotor 120. The teeth in turn abrade the abradable coating 170 defining an elliptical groove (at times herein referred to as a path) in the abradable coating 170. In one embodiment of the invention, the teeth of the rotor 120 abrade the abradable coating 170 at about the 12 o'clock position and at bout the 6 o'clock position. More particularly, due to the upward lift of the rotor 120, the teeth abrade more material at about the 12 o'clock position than at about the 6 o'clock position. Further, since the line on line arrangement is provided at about the 3 o'clock position and at bout the 9 o'clock position, and due to the upward lift of the rotor 120, no material is abraded from the abradable coating 170 at about the 3 o'clock position and at about the 9 o'clock position. Therefore, before the gas turbine engine 10 is implemented for a real-time application/operation the elliptical path has already been cut/defined in-to the abradable coating 170.
The elliptical sealing system 140 may be positioned between the rotor 120 and the stator housing 130. The elliptical sealing system 140 may be configured to control the leakage of the fluid therethrough without damaging the components thereof. Although described herein in the context of the compressor, the elliptical sealing system 140 may be used with any type of rotary machine, including steam turbines, gas turbines, and the like.
The elliptical sealing system 140 may include a retractable packing ring 150 positioned within a slot 160 of the stator housing 130. As noted previously, a packing ring such as the packing ring 150 in its entirety is formed by the first semielliptical sealing segment 270 and the second semielliptical sealing segment 280. In the cross-sectional view of
A plurality of biasing members 180 such as springs 190 may be disposed between the packing ring 150 and the stator housing 130. The biasing members 180 may include leaf springs, coil springs, helical springs, hydraulic springs, pneumatic springs, stacked washers, and the like. The biasing members 180 may be configured to bias the packing ring 150 towards the rotor 120. In this example, the biasing members 180 may be positioned at about a 12 o'clock position and about a 6 o'clock position. Other positions may be used herein. Any number or type of biasing members 180 may be used herein. Other configurations and other components may be used herein.
The rotor 120 also may include a plurality teeth 200 (represented by the area 113 in the axial view of
Various advantages that may be realized in the practice of some embodiments of the invention include, but are not limited to, improved leakage sealing, improved reliability, and improved efficiency of the rotary machine. For example, by only using the two sealing segments, such as, the first semielliptical sealing segment 270 and the second semielliptical sealing segment 280, no additional end gap leakage may be introduced through the elliptical sealing system 140. As noted previously, the traditional designs include a use of more than two sealing segments. In stark contrast, embodiments of the present invention utilize only the two sealing segments. Also, the coupling joints 273 and 274 are made at the positions (e.g., at about the 3 o'clock position and at about the 9 o'clock position, respectively) where an effect of a force caused by the lifting of the rotor 120 during rotation is minimum. Consequently, the possibility of displacement and/or bending/twisting of the first semielliptical sealing segment 270 and the second semielliptical sealing segment 280 may be substantially eliminated. This also results in improved reliability/lifetime of the rotary machine. Moreover, as the displacement and/or the bending/twisting of the first semielliptical sealing segment 270 and the second semielliptical sealing segment 280 may be substantially eliminated, any additional leakage that may have resulted due to the lifting of the rotor 120 is effectively eliminated. Likewise, the use of the biasing members 180 at about the 12 o'clock position and about at the 6 o'clock position generally force the elliptical sealing system 140 towards the teeth of the rotor 120 for contact therewith. Such an adaptive action by the biasing members 180 also eliminates the leakage. Reduction/elimination of the leakage leads to an improvement in the efficiency of the rotary machine.
It will be appreciated that variants of the above disclosed and other features and functions, or alternatives thereof, may be combined to create many other different systems or applications. Various unanticipated alternatives, modifications, variations, or improvements therein may be subsequently made by those skilled in the art and are also intended to be encompassed by the following claims.
This application is a continuation-in-part of U.S. application Ser. No. 12/986,226 filed on Jan. 7, 2011, the entire contents of which are hereby incorporated by reference.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 12986226 | Jan 2011 | US |
| Child | 14330183 | US |
