[go: up one dir, main page]

US20100284782A1 - Steam turbine, system, and method of operation - Google Patents

Steam turbine, system, and method of operation Download PDF

Info

Publication number
US20100284782A1
US20100284782A1 US12/436,114 US43611409A US2010284782A1 US 20100284782 A1 US20100284782 A1 US 20100284782A1 US 43611409 A US43611409 A US 43611409A US 2010284782 A1 US2010284782 A1 US 2010284782A1
Authority
US
United States
Prior art keywords
pressure
steam turbine
hpip
seal
section
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US12/436,114
Inventor
Nestor Hernandez Sanchez
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US12/436,114 priority Critical patent/US20100284782A1/en
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SANCHEZ, NESTOR HERNANDEZ
Priority to EP10161475A priority patent/EP2420650A3/en
Priority to JP2010104699A priority patent/JP2010261455A/en
Priority to RU2010117020/06A priority patent/RU2010117020A/en
Publication of US20100284782A1 publication Critical patent/US20100284782A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/003Preventing or minimising internal leakage of working-fluid, e.g. between stages by packing rings; Mechanical seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/28Arrangement of seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/31Application in turbines in steam turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/55Seals
    • F05D2240/56Brush seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/55Seals
    • F05D2240/57Leaf seals

Definitions

  • Embodiments of the invention relate generally to steam turbines, steam turbine systems, and methods for their operation and, more particularly, to high-pressure-intermediate-pressure (HPIP) steam turbine configurations having pressure drop-limited seals and exhibiting reduced mid-packing and/or end-packing leakage.
  • HPIP high-pressure-intermediate-pressure
  • HP high-pressure
  • IP intermediate-pressure
  • FIGS. 1A-B A schematic cross-sectional view typical of a known combined HPIP steam turbine is shown in FIGS. 1A-B .
  • the steam turbine 100 comprises an HP section 110 , an IP section 150 , and a mid-packing section 130 herebetween.
  • the HP section 110 includes a plurality of steampath stages 112 A-E.
  • the mid-packing section 130 includes a plurality of packing rings 140 A-E positioned along a length of a rotor 134 . Leakage is reduced by the proximity of packing teeth 136 of the rotor 134 to corresponding teeth of packing rings 140 A-E. Such proximity is shown more clearly in the detailed view of FIG. 1B . Steam flow is generally along path A, from the HP section 110 to the IP section 150 .
  • One embodiment of the invention provides combined high-pressure-intermediate-pressure (HPIP) steam turbine comprising: a high-pressure section; an intermediate-pressure section sharing a common rotor with the high-pressure section; at least one packing ring disposed along a length of the rotor and between the high-pressure section and the intermediate-pressure section; and at least one conduit having a first end disposed adjacent a packing ring and a second end disposed adjacent a steampath stage of the high-pressure section.
  • HPIP high-pressure-intermediate-pressure
  • HPIP high-pressure-intermediate-pressure
  • HPIP high-pressure-intermediate-pressure
  • FIG. 1 Another embodiment of the invention provides a separate high-pressure-intermediate-pressure (HPIP) steam turbine comprising: a high-pressure section; an intermediate-pressure section; a low-pressure section; at least one rotor engaging at least one of the high-pressure section, the intermediate-pressure section, or the low-pressure section; an end-packing region having at least one packing ring disposed along a length of the at least one rotor; and at least one conduit having a first end disposed adjacent the end-packing region and a second end disposed adjacent a steampath stage of the high-pressure section.
  • HPIP high-pressure-intermediate-pressure
  • Yet another embodiment of the invention provides a steam turbine system comprising: a high-pressure-intermediate-pressure (HPIP) steam turbine comprising: a high-pressure section; an intermediate-pressure section; at least one rotor engaging at least one of the high-pressure section and the intermediate-pressure section; at least one packing ring disposed along a length of the at least one rotor; and at least one conduit having a first end disposed adjacent a packing ring and a second end disposed adjacent a steampath stage of the high-pressure section; and a steam-generating apparatus for providing a quantity of steam to the steam turbine.
  • HPIP high-pressure-intermediate-pressure
  • Still another embodiment of the invention provides a method of reducing mid-packing leakage in a high-pressure-intermediate-pressure (HPIP) steam turbine, the method comprising: directing a quantity of steam between a steampath stage of a high-pressure section of the HPIP steam turbine and a mid-packing section of the HPIP steam turbine containing at least one packing ring.
  • HPIP high-pressure-intermediate-pressure
  • FIG. 1A shows a schematic cross-sectional view of a know combined high-pressure-intermediate-pressure (HPIP) steam turbine;
  • HPIP high-pressure-intermediate-pressure
  • FIG. 1B shows a detailed view of a portion of the HPIP steam turbine of FIG. 1A ;
  • FIG. 2 shows a schematic cross-sectional view of a combined HPIP steam turbine according to one embodiment of the invention.
  • FIG. 3 shows a schematic cross-sectional view of a packing ring containing a pressure drop-limited seal suitable for use in various embodiments of the invention.
  • FIG. 4 shows a schematic cross-sectional view of a separate HPIP steam turbine according to one embodiment of the invention.
  • FIG. 2 shows a schematic cross-sectional view of a combined high-pressure-intermediate-pressure (HPIP) steam turbine according to an embodiment of the invention.
  • the HPIP steam turbine 200 of FIG. 2 includes a high-pressure (HP) section 210 , an intermediate-pressure (IP) section 250 , and a mid-packing section 230 therebetween.
  • the mid-packing section 230 includes a rotor 234 disposed between the HP section 210 and the IP section 250 and a plurality of packing rings 240 A-C along its length.
  • FIG. 2 The embodiment of the invention shown in FIG. 2 , however, includes packing rings 240 A-C having pressure drop-limited seals (shown in FIG. 3 and described in greater detail below).
  • the use of pressure drop-limited seals is made possible by the inclusion of conduits or “leak-off lines” 260 , 262 , 264 between the mid-packing section 230 and steampath stages 212 A, 212 C, 212 E of the HP section 210 , through which a quantity of high-pressure steam may travel (e.g., along path B, through conduit 264 ). Steam flow through the conduits determines the pressure difference across the packing rings 240 A, 240 B, 240 C.
  • the conduit or leak-off line may be of any material capable of containing and permitting the movement of steam having a temperature and pressure found within the HP section.
  • Each conduit or leak-off line 264 includes a first end 264 A adjacent a packing ring 240 C and a second end 264 B adjacent a steampath stage 212 A of the HP section 210 .
  • first and second ends of the conduit or leak-off line are shown only with respect to conduit or leak-off line 264 . It should be understood, however, that other conduits or leak-off lines 260 , 262 would also include first and second ends.
  • the resulting pressure difference across the pressure drop-limited seal(s) may vary, depending, for example, on the number of conduits or leak-off lines employed.
  • the pressure difference across the seal should, however, be no greater than the maximum design pressure difference of the seal.
  • the maximum design pressure difference of typical brush seals for example, is between about 14.1 kg/cm 2 (about 200 p.s.i.) and about 21.1 kg/cm 2 (about 300 p.s.i.).
  • the pressure difference across the brush seal may be no greater than, and preferably less than, about 21.1 kg/cm 2 (about 300 p.s.i.), more preferably less than about 17.6 kg/cm 2 (about 250 p.s.i.), and still more preferably less than about 14.1 kg/cm 2 (about 200 p.s.i.).
  • Some embodiments of the invention may include as few as one conduit or leak-off line, while other embodiments of the invention, such as that shown in FIG. 2 , may contain a plurality of such conduits or leak-off lines.
  • some embodiments of the invention may include one packing ring having a pressure drop-limited seal while other embodiments of the invention may contain a plurality of such packing rings.
  • Other conventional packing rings such as those shown in FIGS. 1A-B ( 140 A-E) may also be employed in such embodiments.
  • the inclusion of a plurality of packing rings containing pressure drop-limited seals may confer an additional benefit in that it affords the ability to reduce the overall length of the rotor 234 through the use of fewer, more efficient packing rings (i.e., those containing pressure drop-limited seals).
  • fewer, more efficient packing rings i.e., those containing pressure drop-limited seals.
  • increasing the number of packing rings results in an increased bearing span (longer rotor), greater rotor flexibility, and larger radial clearances.
  • the use of fewer packing rings allows for a reduced bearing span (shorter rotor), less rotor flexibility, and smaller radial clearances.
  • FIG. 3 shows a schematic cross-sectional view of a packing ring 340 including a brush seal 342 , suitable for use in an embodiment of the invention, and as shown in FIG. 2 ( 240 A-C).
  • the brush seal 342 comprises a plurality of brushes 342 A radially oriented substantially perpendicular to a longitudinal axis of the rotor to be sealed against (not shown) and disposed between an HP block 342 B and an IP block 342 C.
  • the invention is not limited to the use of brush seals. Any pressure drop-limited seal may be employed, leaf seals being one additional example.
  • the pressure drop-limited seals useful in practicing the various embodiments of the invention include an element (e.g., brush, leaf, etc.) capable of movement in response to a pressure difference across the seal. For example, a brush of a brush seal bends or otherwise moves toward a side of the seal experiencing a lower pressure and away from a side of the seal experiencing a higher pressure. Leaves of a leaf seal move similarly in response to a pressure difference across the seal.
  • the packing ring 340 may further include teeth 344 , 346 , as are often found in known packing rings.
  • the reduction in mid-packing leakage effected by the brush seal or leaf seal may obviate the need or desirability for such teeth.
  • FIG. 4 shows a schematic cross-sectional view of a separate HPIP steam turbine 400 according to an embodiment of the invention.
  • the steam turbine 400 includes four end-packing sections 470 , 430 A, 430 B, 490 , one on either side of the HP section 410 , one adjacent the IP section 450 , and one adjacent a low-pressure (LP) section 452 .
  • LP low-pressure
  • the conduits 460 - 466 function similarly to those shown in FIG. 2 , permitting the flow of steam between the HP section 410 and the end-packing sections 470 , 430 A, 430 B, 490 .
  • packing rings 420 A-B, 440 A-B, 440 C-D, 480 A-B having a pressure drop-limited seal may be employed in each end-packing section 470 , 430 A, 430 B, 490 .
  • such packing rings may be employed in fewer than each end-packing section.
  • Steam turbine systems according to the invention may include a combined HPIP steam turbine or a separate HPIP steam turbine such as those described above and a steam-generating apparatus, such as a boiler, for providing a quantity of steam to such an HPIP steam turbine.
  • a steam-generating apparatus such as a boiler

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Devices (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)

Abstract

Embodiments of the invention relate generally to steam turbines, steam turbine systems, and methods for their operation and, more particularly, to high-pressure-intermediate-pressure (HPIP) steam turbine configurations having pressure drop-limited seals and exhibiting reduced mid-packing and/or end-packing leakage. One embodiment of the invention provides a combined high-pressure-intermediate-pressure (HPIP) steam turbine comprising: a high-pressure section; an intermediate-pressure section sharing a common rotor with the high-pressure section; at least one packing ring disposed along a length of the rotor and between the high-pressure section and the intermediate-pressure section; and at least one conduit having a first end disposed adjacent a packing ring and a second end disposed adjacent a steampath stage of the high-pressure section.

Description

    BACKGROUND OF THE INVENTION
  • Embodiments of the invention relate generally to steam turbines, steam turbine systems, and methods for their operation and, more particularly, to high-pressure-intermediate-pressure (HPIP) steam turbine configurations having pressure drop-limited seals and exhibiting reduced mid-packing and/or end-packing leakage.
  • All combined HPIP steam turbine configurations are susceptible to mid-packing leakage between the high-pressure (HP) section and the intermediate-pressure (IP) section. This mid-packing leakage is driven by a significant pressure ratio between the HP and IP sections (represented by arrow A in the drawings), as well as high operating temperatures in these areas. Typically, such leakage represents between 70% and 90% of the total leakage loss in the steam turbine. In separate HPIP sections, the highest leakages correspond to the high pressure drop and high temperature areas, which are the HP and IP inlet areas.
  • A schematic cross-sectional view typical of a known combined HPIP steam turbine is shown in FIGS. 1A-B. With reference to FIG. 1, the steam turbine 100 comprises an HP section 110, an IP section 150, and a mid-packing section 130 herebetween. The HP section 110 includes a plurality of steampath stages 112A-E. The mid-packing section 130 includes a plurality of packing rings 140A-E positioned along a length of a rotor 134. Leakage is reduced by the proximity of packing teeth 136 of the rotor 134 to corresponding teeth of packing rings 140A-E. Such proximity is shown more clearly in the detailed view of FIG. 1B. Steam flow is generally along path A, from the HP section 110 to the IP section 150.
  • One approach to reducing mid-packing leakage and improving overall turbine efficiency has been to increase the number of packing teeth 136 along rotor 134. This restricts flow, which would otherwise be expected to reduce leakage to some degree. However, the additional packing teeth require a greater bearing span, which in turn results in a more flexible rotor and necessarily larger radial clearances. These larger radial clearances increase leakage flow. As a result, little improvement is seen with respect to reduced mid-packing leakage or turbine efficiency.
  • Other sealing devices, such as those incorporating brush seals and leaf seals, provide small radial clearances and have been employed in other contexts. However, brush seals, leaf seals, and similar devices (referred to herein as pressure drop-limited seals) cannot be used where a large pressure difference is found across the seal. Typically, such pressure differences cannot be greater than about 21.1 kg/cm2 (about 300 p.s.i.) Pressures at the HP section of a typical HPIP steam turbine may be as high as 316 kg/cm2 (4500 p.s.i.), while pressures at the IP section are generally between 28.1 kg/cm2 (400 p.s.i.) and 35.2 kg/cm2 (500 p.s.i.). As a result, the pressure difference across each packing ring is too great for the use of pressure drop-limited seals such as brush seals or leaf seals.
  • BRIEF DESCRIPTION OF THE INVENTION
  • One embodiment of the invention provides combined high-pressure-intermediate-pressure (HPIP) steam turbine comprising: a high-pressure section; an intermediate-pressure section sharing a common rotor with the high-pressure section; at least one packing ring disposed along a length of the rotor and between the high-pressure section and the intermediate-pressure section; and at least one conduit having a first end disposed adjacent a packing ring and a second end disposed adjacent a steampath stage of the high-pressure section.
  • Another embodiment of the invention provides a separate high-pressure-intermediate-pressure (HPIP) steam turbine comprising: a high-pressure section; an intermediate-pressure section; a low-pressure section; at least one rotor engaging at least one of the high-pressure section, the intermediate-pressure section, or the low-pressure section; an end-packing region having at least one packing ring disposed along a length of the at least one rotor; and at least one conduit having a first end disposed adjacent the end-packing region and a second end disposed adjacent a steampath stage of the high-pressure section.
  • Yet another embodiment of the invention provides a steam turbine system comprising: a high-pressure-intermediate-pressure (HPIP) steam turbine comprising: a high-pressure section; an intermediate-pressure section; at least one rotor engaging at least one of the high-pressure section and the intermediate-pressure section; at least one packing ring disposed along a length of the at least one rotor; and at least one conduit having a first end disposed adjacent a packing ring and a second end disposed adjacent a steampath stage of the high-pressure section; and a steam-generating apparatus for providing a quantity of steam to the steam turbine.
  • Still another embodiment of the invention provides a method of reducing mid-packing leakage in a high-pressure-intermediate-pressure (HPIP) steam turbine, the method comprising: directing a quantity of steam between a steampath stage of a high-pressure section of the HPIP steam turbine and a mid-packing section of the HPIP steam turbine containing at least one packing ring.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • These and other features of this invention will be more readily understood from the following detailed description of the various aspects of the invention taken in conjunction with the accompanying drawings that depict various embodiments of the invention, in which:
  • FIG. 1A shows a schematic cross-sectional view of a know combined high-pressure-intermediate-pressure (HPIP) steam turbine;
  • FIG. 1B shows a detailed view of a portion of the HPIP steam turbine of FIG. 1A;
  • FIG. 2 shows a schematic cross-sectional view of a combined HPIP steam turbine according to one embodiment of the invention; and
  • FIG. 3 shows a schematic cross-sectional view of a packing ring containing a pressure drop-limited seal suitable for use in various embodiments of the invention; and
  • FIG. 4 shows a schematic cross-sectional view of a separate HPIP steam turbine according to one embodiment of the invention.
  • It is noted that the drawings of the invention are not to scale. The drawings are intended to depict only typical aspects of the invention, and therefore should not be considered as limiting the scope of the invention. In the drawings, like numbering represents like elements between the drawings.
  • DETAILED DESCRIPTION OF THE INVENTION
  • FIG. 2 shows a schematic cross-sectional view of a combined high-pressure-intermediate-pressure (HPIP) steam turbine according to an embodiment of the invention. As in known devices, such as that shown in FIG. 1A, the HPIP steam turbine 200 of FIG. 2 includes a high-pressure (HP) section 210, an intermediate-pressure (IP) section 250, and a mid-packing section 230 therebetween. The mid-packing section 230 includes a rotor 234 disposed between the HP section 210 and the IP section 250 and a plurality of packing rings 240A-C along its length.
  • The embodiment of the invention shown in FIG. 2, however, includes packing rings 240A-C having pressure drop-limited seals (shown in FIG. 3 and described in greater detail below). The use of pressure drop-limited seals is made possible by the inclusion of conduits or “leak-off lines” 260, 262, 264 between the mid-packing section 230 and steampath stages 212A, 212C, 212E of the HP section 210, through which a quantity of high-pressure steam may travel (e.g., along path B, through conduit 264). Steam flow through the conduits determines the pressure difference across the packing rings 240A, 240B, 240C.
  • The conduit or leak-off line may be of any material capable of containing and permitting the movement of steam having a temperature and pressure found within the HP section. Each conduit or leak-off line 264 includes a first end 264A adjacent a packing ring 240C and a second end 264B adjacent a steampath stage 212A of the HP section 210. (For the sake of simplicity, the first and second ends of the conduit or leak-off line are shown only with respect to conduit or leak-off line 264. It should be understood, however, that other conduits or leak-off lines 260, 262 would also include first and second ends.)
  • The resulting pressure difference across the pressure drop-limited seal(s) may vary, depending, for example, on the number of conduits or leak-off lines employed. The pressure difference across the seal should, however, be no greater than the maximum design pressure difference of the seal. The maximum design pressure difference of typical brush seals, for example, is between about 14.1 kg/cm2 (about 200 p.s.i.) and about 21.1 kg/cm2 (about 300 p.s.i.). In the case where a brush seal is used, therefore, the pressure difference across the brush seal may be no greater than, and preferably less than, about 21.1 kg/cm2 (about 300 p.s.i.), more preferably less than about 17.6 kg/cm2 (about 250 p.s.i.), and still more preferably less than about 14.1 kg/cm2 (about 200 p.s.i.).
  • Some embodiments of the invention may include as few as one conduit or leak-off line, while other embodiments of the invention, such as that shown in FIG. 2, may contain a plurality of such conduits or leak-off lines. In addition, some embodiments of the invention may include one packing ring having a pressure drop-limited seal while other embodiments of the invention may contain a plurality of such packing rings. For example, it may be possible, in some embodiments, to substantially reduce mid-packing leakage and/or improve turbine efficiency by the inclusion of a single packing ring having a pressure drop-limited seal, such as a brush seal, and a single conduit or leak-off line. Other conventional packing rings, such as those shown in FIGS. 1A-B (140A-E) may also be employed in such embodiments.
  • In other embodiments of the invention, the inclusion of a plurality of packing rings containing pressure drop-limited seals, while further reducing mid-packing leakage and/or improving turbine efficiency, may confer an additional benefit in that it affords the ability to reduce the overall length of the rotor 234 through the use of fewer, more efficient packing rings (i.e., those containing pressure drop-limited seals). As noted above, increasing the number of packing rings results in an increased bearing span (longer rotor), greater rotor flexibility, and larger radial clearances. Contrarily, the use of fewer packing rings, as embodiments of the invention make possible, allows for a reduced bearing span (shorter rotor), less rotor flexibility, and smaller radial clearances. Thus, while embodiments of the invention reduce mid-packing leakage and/or improve turbine efficiency through the use of packing rings having pressure drop-limited seals, the reduced bearing span made possible by the use of such packing rings may yield an additional reduction in mid-packing leakage and/or improvement in turbine efficiency.
  • FIG. 3 shows a schematic cross-sectional view of a packing ring 340 including a brush seal 342, suitable for use in an embodiment of the invention, and as shown in FIG. 2 (240A-C). The brush seal 342 comprises a plurality of brushes 342A radially oriented substantially perpendicular to a longitudinal axis of the rotor to be sealed against (not shown) and disposed between an HP block 342B and an IP block 342C.
  • As noted above, the invention is not limited to the use of brush seals. Any pressure drop-limited seal may be employed, leaf seals being one additional example. The pressure drop-limited seals useful in practicing the various embodiments of the invention include an element (e.g., brush, leaf, etc.) capable of movement in response to a pressure difference across the seal. For example, a brush of a brush seal bends or otherwise moves toward a side of the seal experiencing a lower pressure and away from a side of the seal experiencing a higher pressure. Leaves of a leaf seal move similarly in response to a pressure difference across the seal.
  • In some embodiments of the invention, the packing ring 340 may further include teeth 344, 346, as are often found in known packing rings. In other embodiments of the invention, the reduction in mid-packing leakage effected by the brush seal or leaf seal may obviate the need or desirability for such teeth.
  • FIG. 4 shows a schematic cross-sectional view of a separate HPIP steam turbine 400 according to an embodiment of the invention. Here, rather than a single mid-packing section between the HP section 410 and the IP section 450, the steam turbine 400 includes four end-packing sections 470, 430A, 430B, 490, one on either side of the HP section 410, one adjacent the IP section 450, and one adjacent a low-pressure (LP) section 452.
  • In the embodiment shown in FIG. 4, the conduits 460-466 function similarly to those shown in FIG. 2, permitting the flow of steam between the HP section 410 and the end-packing sections 470, 430A, 430B, 490. Thus, packing rings 420A-B, 440A-B, 440C-D, 480A-B having a pressure drop-limited seal may be employed in each end- packing section 470, 430A, 430B, 490. In other embodiments, such packing rings may be employed in fewer than each end-packing section.
  • Steam turbine systems according to the invention may include a combined HPIP steam turbine or a separate HPIP steam turbine such as those described above and a steam-generating apparatus, such as a boiler, for providing a quantity of steam to such an HPIP steam turbine. Other components of such a steam turbine system will be known to one skilled in the art.
  • This written description uses examples to disclose the invention, including the best mode, and also to enable any person skilled in the art to practice the invention, including making and using any devices or systems and performing any related or incorporated methods. The patentable scope of the invention is defined by the claims, and may include other examples that occur to those skilled in the art. Such other examples are intended to be within the scope of the claims if they have structural elements that do not differ from the literal language of the claims, or if they include equivalent structural elements with insubstantial differences from the literal language of the claims.

Claims (24)

1. A combined high-pressure-intermediate-pressure (HPIP) steam turbine comprising:
a high-pressure section;
an intermediate-pressure section sharing a common rotor with the high-pressure section;
at least one packing ring disposed along a length of the rotor and between the high-pressure section and the intermediate-pressure section; and
at least one conduit having a first end disposed adjacent a packing ring and a second end disposed adjacent a steampath stage of the high-pressure section.
2. The combined HPIP steam turbine of claim 1, wherein the at least one packing ring includes a pressure drop-limited seal.
3. The combined HPIP steam turbine of claim 2, wherein the pressure drop-limited seal includes an element adapted to move in response to a pressure difference across the pressure drop-limited seal.
4. The combined HPIP steam turbine of claim 2, wherein the first end of the at least one conduit is adjacent the at least one packing ring.
5. The combined HPIP steam turbine of claim 2, wherein the at least one conduit includes a plurality of conduits and a first end of each conduit is disposed adjacent a packing ring including a pressure drop-limited seal.
6. The combined HPIP steam turbine of claim 2, wherein the pressure drop-limited seal is selected from a group consisting of: a brush seal and a leaf seal.
7. The combined HPIP steam turbine of claim 6, wherein the pressure drop-limited seal is a brush seal.
8. The combined HPIP steam turbine of claim 2, wherein the at least one conduit is capable of moving a quantity of steam between the steampath stage and an area adjacent the packing ring.
9. The combined HPIP steam turbine of claim 8, wherein the quantity of steam is capable of reducing a pressure difference across the pressure drop-limited seal to less than a maximum design pressure difference for the seal.
10. A separate high-pressure-intermediate-pressure (HPIP) steam turbine comprising:
a high-pressure section;
an intermediate-pressure section;
a low-pressure section;
at least one rotor engaging at least one of the high-pressure section, the intermediate-pressure section, or the low-pressure section;
an end-packing region having at least one packing ring disposed along a length of the at least one rotor; and
at least one conduit having a first end disposed adjacent the end-packing region and a second end disposed adjacent a steampath stage of the high-pressure section.
11. The separate HPIP steam turbine of claim 10, wherein the at least one packing ring includes a pressure drop-limited seal.
12. The separate HPIP steam turbine of claim 11, wherein the pressure drop-limited seal includes an element adapted to move in response to a pressure difference across the pressure drop-limited seal.
13. The separate HPIP steam turbine of claim 11, wherein the first end of the at least one conduit is adjacent the at least one packing ring.
14. The separate HPIP steam turbine of claim 11, wherein the at least one conduit includes a plurality of conduits and a first end of each conduit is disposed adjacent a packing ring including a pressure drop-limited seal.
15. The separate HPIP steam turbine of claim 11, wherein the pressure drop-limited seal is selected from a group consisting of: a brush seal and a leaf seal.
16. The separate HPIP steam turbine of claim 15, wherein the pressure drop-limited seal is a brush seal.
17. The separate HPIP steam turbine of claim 11, wherein the at least one conduit is capable of moving a quantity of steam between the steampath section and the area adjacent the end-packing region.
18. The separate HPIP steam turbine of claim 17, wherein the quantity of steam is capable of reducing a pressure difference across the pressure drop-limited seal to less than a maximum design pressure difference for the seal.
19. A steam turbine system comprising:
a high-pressure-intermediate-pressure (HPIP) steam turbine comprising:
a high-pressure section;
an intermediate-pressure section;
at least one rotor engaging at least one of the high-pressure section and the intermediate-pressure section;
at least one packing ring disposed along a length of the at least one rotor; and
at least one conduit having a first end disposed adjacent a packing ring and a second end disposed adjacent a steampath stage of the high-pressure section; and
a steam-generating apparatus for providing a quantity of steam to the steam turbine.
20. The steam turbine system of claim 19, wherein the high-pressure section and the intermediate-pressure section share a common rotor.
21. The steam turbine system of claim 19, wherein the at least one packing ring includes a pressure drop-limited seal.
22. The steam turbine system of claim 21, wherein the pressure drop-limited seal includes an element adapted to move in response to a pressure difference across the pressure drop-limited seal.
23. A method of operating a high-pressure-intermediate-pressure (HPIP) steam turbine, the method comprising:
sealing against a rotor of the HPIP steam turbine using at least one packing ring having a pressure drop-limited seal; and
directing a quantity of steam between a steampath stage of a high-pressure section of the HPIP steam turbine and a mid-packing section of the HPIP steam turbine containing the at least one packing ring, such that a pressure difference across the pressure drop-limited seal is no greater than a maximum design pressure difference of the pressure drop-limited seal.
24. The method of claim 23, wherein the pressure drop-limited seal is selected from a group consisting of: a brush seal and a leaf seal.
US12/436,114 2009-05-05 2009-05-05 Steam turbine, system, and method of operation Abandoned US20100284782A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US12/436,114 US20100284782A1 (en) 2009-05-05 2009-05-05 Steam turbine, system, and method of operation
EP10161475A EP2420650A3 (en) 2009-05-05 2010-04-29 Steam turbine, system, and method of operation
JP2010104699A JP2010261455A (en) 2009-05-05 2010-04-30 Steam turbine, steam turbine system, and method for operation thereof
RU2010117020/06A RU2010117020A (en) 2009-05-05 2010-04-30 COMBINED STEAM TURBINE HIGH PRESSURE - MIDDLE PRESSURE AND SEPARATE STEAM TURBINE HIGH PRESSURE - MIDDLE PRESSURE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/436,114 US20100284782A1 (en) 2009-05-05 2009-05-05 Steam turbine, system, and method of operation

Publications (1)

Publication Number Publication Date
US20100284782A1 true US20100284782A1 (en) 2010-11-11

Family

ID=43062399

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/436,114 Abandoned US20100284782A1 (en) 2009-05-05 2009-05-05 Steam turbine, system, and method of operation

Country Status (4)

Country Link
US (1) US20100284782A1 (en)
EP (1) EP2420650A3 (en)
JP (1) JP2010261455A (en)
RU (1) RU2010117020A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130064638A1 (en) * 2011-09-08 2013-03-14 Moorthi Subramaniyan Boundary Layer Blowing Using Steam Seal Leakage Flow
US20130272872A1 (en) * 2012-04-13 2013-10-17 General Electric Company Shaft sealing system for steam turbines

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017216558A1 (en) * 2017-09-19 2019-03-21 Siemens Aktiengesellschaft Steam turbine with shaft seal arrangement
JP6917291B2 (en) * 2017-12-15 2021-08-11 株式会社荏原製作所 Non-contact annular seal, centrifugal pump, impeller ring, and casing ring

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3604206A (en) * 1968-07-31 1971-09-14 Gen Electric Shaft-sealing system for nuclear turbines
US4193603A (en) * 1978-12-21 1980-03-18 Carrier Corporation Sealing system for a turbomachine
US5971400A (en) * 1998-08-10 1999-10-26 General Electric Company Seal assembly and rotary machine containing such seal assembly
US6572115B1 (en) * 2001-12-21 2003-06-03 General Electric Company Actuating seal for a rotary machine and method of retrofitting
US7549834B2 (en) * 2006-06-19 2009-06-23 General Electric Company Actuation pressure control for adjustable seals in turbomachinery

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1041059B (en) * 1957-08-05 1958-10-16 Licentia Gmbh Circuit of the stuffing box steam collecting line of a multi-housing steam turbine
DE1401440A1 (en) * 1961-01-03 1968-10-24 Licentia Gmbh Device for the automatic control of the working medium passage in the sealing steam lines for the stuffing boxes of multi-housing steam or gas turbines
GB2393766A (en) * 2002-10-03 2004-04-07 Alstom A sealing arrangement for a turbine
EP1961921A1 (en) * 2007-02-26 2008-08-27 Siemens Aktiengesellschaft Seal for a turbo engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3604206A (en) * 1968-07-31 1971-09-14 Gen Electric Shaft-sealing system for nuclear turbines
US4193603A (en) * 1978-12-21 1980-03-18 Carrier Corporation Sealing system for a turbomachine
US5971400A (en) * 1998-08-10 1999-10-26 General Electric Company Seal assembly and rotary machine containing such seal assembly
US6572115B1 (en) * 2001-12-21 2003-06-03 General Electric Company Actuating seal for a rotary machine and method of retrofitting
US7549834B2 (en) * 2006-06-19 2009-06-23 General Electric Company Actuation pressure control for adjustable seals in turbomachinery

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130064638A1 (en) * 2011-09-08 2013-03-14 Moorthi Subramaniyan Boundary Layer Blowing Using Steam Seal Leakage Flow
US20130272872A1 (en) * 2012-04-13 2013-10-17 General Electric Company Shaft sealing system for steam turbines
US9540942B2 (en) * 2012-04-13 2017-01-10 General Electric Company Shaft sealing system for steam turbines

Also Published As

Publication number Publication date
JP2010261455A (en) 2010-11-18
EP2420650A3 (en) 2012-03-21
RU2010117020A (en) 2011-11-10
EP2420650A2 (en) 2012-02-22

Similar Documents

Publication Publication Date Title
US20120027582A1 (en) Floating packing ring assembly
US20110164965A1 (en) Steam turbine stationary component seal
JP2008008490A (en) Seal assembly provided with l-shaped butt gap seal between segments and rotary machine
EP1384856A3 (en) Endface gap sealing of steam turbine packing seal segments and retrofitting thereof
US8932001B2 (en) Systems, methods, and apparatus for a labyrinth seal
US20130283818A1 (en) Convolution seal for transition duct in turbine system
JP2010106830A (en) Pressure activated flow path seal for steam turbine
US20100284782A1 (en) Steam turbine, system, and method of operation
EP1387043A3 (en) Sealing for steam turbine diaphragm and methods of retrofitting
CN104632290A (en) Rotary machine secondary sealing assembly and method of assembling the same
US9347333B2 (en) Brush ring seal
US20110285090A1 (en) Seal assembly including plateau and concave portion in mating surface for seal tooth in turbine
ATE483891T1 (en) FLOW MACHINE, ESPECIALLY GAS TURBINE
US8181967B2 (en) Variable clearance packing ring
EP2650485B1 (en) Shaft sealing system for steam turbines
US20200088058A1 (en) Backside seal for steam turbine gland system
US6997677B2 (en) Method and apparatus for rotating machine main fit seal
US20100021283A1 (en) System and method for providing supercritical cooling steam into a wheelspace of a turbine
JP4413732B2 (en) Steam turbine plant
US10844748B2 (en) Inner casing for steam turbine engine
US2524724A (en) Turbine apparatus
US8490981B2 (en) Brush seal
US8926273B2 (en) Steam turbine with single shell casing, drum rotor, and individual nozzle rings
US20150118042A1 (en) Method and system for providing sealing in gas turbines
US10006303B2 (en) Contra-flow strips, contra-flow seal segments, and methods for inhibiting leakage

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION