US20150252681A1 - Modular turbomachine inner and outer casings with multi-stage steam extraction sites - Google Patents

Modular turbomachine inner and outer casings with multi-stage steam extraction sites Download PDF

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Publication number
US20150252681A1
US20150252681A1 US14/197,720 US201414197720A US2015252681A1 US 20150252681 A1 US20150252681 A1 US 20150252681A1 US 201414197720 A US201414197720 A US 201414197720A US 2015252681 A1 US2015252681 A1 US 2015252681A1
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United States
Prior art keywords
casing
inner shell
access region
outer shell
turbomachine
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Abandoned
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US14/197,720
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English (en)
Inventor
Dayananda Thukra Kotian
Jeyaruban Selliah Amirtharajah
Stephen Roger Swan
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General Electric Co
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General Electric Co
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Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US14/197,720 priority Critical patent/US20150252681A1/en
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: KOTIAN, DAYANANDA THUKRA, AMIRTHARAJAH, JEYARUBAN SELLIAH, SWAN, STEPHEN ROGER
Priority to JP2015037509A priority patent/JP2015169208A/ja
Priority to DE102015103044.6A priority patent/DE102015103044A1/de
Priority to CN201520127236.1U priority patent/CN205101051U/zh
Publication of US20150252681A1 publication Critical patent/US20150252681A1/en
Abandoned legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/32—Collecting of condensation water; Drainage ; Removing solid particles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/31—Application in turbines in steam turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/61—Assembly methods using limited numbers of standard modules which can be adapted by machining
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making

Definitions

  • the subject matter disclosed herein relates generally to steam turbines. More specifically, the disclosure provided herein relates to inner and outer casings within steam turbines.
  • Turbomachine casings may be tapped in order to extract high pressure fluid circulating within and the high pressure fluid may be used for many different applications which may include powering an adjacent machine or heating water prior to its being used as steam.
  • the location of fluid extraction from the turbomachine casing may be chosen based on characteristics of the high pressure fluid at such a location, i.e., fluid that is extracted through a port in an upstream stage of the turbomachine will have higher pressure than fluid that is extracted from a downstream stage. Also, the site of extraction of the fluid affects the operation of the turbomachine itself.
  • fluid extraction location is determined prior to casting of the turbomachine casing, and as discussed above, the location of extraction is chosen based on desired fluid characteristics of the fluid and/or based on the effect that such an extraction will have on the operation of the turbomachine.
  • a steam turbomachine casing intermediate structure includes an inner shell having an external surface, wherein a material of the inner shell defines an inner shell cavity, and wherein the material of the inner shell defines an opening for allowing fluid from a steam path of the turbomachine to enter the inner shell cavity, and an outer shell having an internal surface, the internal surface of the outer shell and the external surface of the inner shell defining at least one closed chamber extending in an axial direction of the steam turbomachine, the inner shell having a first access region adjacent the at least one closed chamber, the first access region including a plurality of inner shell axial locations, wherein at least one of the plurality of inner shell axial locations is selectable to be machined to create an exhaust slot for allowing fluid to exit the inner shell cavity and enter the at least one closed chamber, and wherein a structural integrity of the casing is uniform regardless of which of the inner shell axial locations is selected to be machined, the
  • a first aspect provides a steam turbomachine casing intermediate structure comprising: an inner shell having an external surface, wherein a material of the inner shell defines an inner shell cavity, and wherein the material of the inner shell defines an opening for allowing fluid from a steam path of the turbo machine to enter the inner shell cavity; and an outer shell having an internal surface, the internal surface of the outer shell and the external surface of the inner shell defining at least one closed chamber extending in an axial direction of the steam turbomachine, the inner shell having a first access region adjacent the at least one closed chamber, the first access region including a plurality of inner shell axial locations, wherein at least one of the plurality of inner shell axial locations is selectable to be machined to create an exhaust slot for allowing fluid to exit the inner shell cavity and enter the at least one closed chamber, and wherein a structural integrity of the casing is uniform regardless of which of the inner shell axial locations is selected to be machined, the outer shell having a second access region adjacent the at least one closed chamber, the second access region including a plurality of outer
  • a second aspect provides a steam turbomachine casing intermediate structure comprising: at least one shell casing defining at least one cavity and having a plurality of pre-formed extraction opening sites selectable for use, wherein a structural integrity of the at least one shell casing is uniform regardless of which of the plurality of pre-formed extraction opening sites is selected for use.
  • a third aspect provides a method of fabricating a turbomachine casing structure, the method comprising: forming a casing inner shell having an external surface, wherein a material of the casing inner shell defines an inner shell cavity and a fluid opening for allowing fluid from a turbomachine steam path to enter the inner shell cavity; and forming a casing outer shell having an internal surface such that the internal surface of the outer shell and the external surface of the inner shell define at least one closed chamber extending in an axial direction of the steam turbomachine; forming, in the casing inner shell, a first access region adjacent the at least one closed chamber, the first access region including a plurality of inner shell axial locations, wherein at least one of the plurality of inner shell axial locations is selectable to be machined to create an exhaust slot for allowing fluid to exit the inner shell cavity and enter the at least one closed chamber, and wherein a structural integrity of the casing is uniform regardless of which of the inner shell axial locations is selected to be machined; and forming, in the casing outer shell,
  • FIG. 1 illustrates a cross sectional view of an apparatus according to embodiments of the invention.
  • FIG. 2 illustrates a cross-sectional view of an apparatus according to embodiments of the invention.
  • FIG. 3 illustrates a cross-sectional view of an apparatus according to embodiments of the invention.
  • FIG. 4 shows an illustrative environment according to embodiments of the invention.
  • FIG. 5 shows illustrative processes that may be performed in methods according to embodiments of the invention.
  • FIG. 6 shows illustrative processes that may be performed in methods according to embodiments of the invention.
  • FIG. 7 shows an illustrative process that may be performed in methods according to embodiments of the invention.
  • the subject matter disclosed herein relates generally to steam turbines. More specifically, the disclosure provided herein relates to inner and outer casings within steam turbines.
  • turbomachine casing intermediate structures As indicated herein, illustrative embodiments of turbomachine casing intermediate structures and methods of their manufacture are disclosed. Embodiments described herein include turbomachine intermediate structures having many different possible fluid extraction locations which may be selected to be machined after desired characteristics of extractable fluid are known. Intermediate structures may be produced in order to be adapted at a later date. That is a casing intermediate structure may be produced with a plurality of locations for potential steam extraction, however none of such steam extraction locations are machined to define fluid extraction ports or openings in an intermediate structure. Intermediate structures are useful because a single, modular design may be modified in many different ways, after design characteristics are known.
  • FIG. 1 a cross sectional view of an apparatus according to embodiments of the invention is shown.
  • FIG. 1 illustrates casing intermediate structure 100 having inner shell 110 .
  • Inner shell 110 is designed to encase a plurality of stages 130 of steam turbomachine 10 and to enclose part of a steam path from steam inlet 140 to a steam extraction location such as slot 150 or 250 , the latter described below with respect to FIG. 2 .
  • Inner shell 110 has an external surface 115 .
  • the material of inner shell 110 defines an inner shell cavity 155 and an opening such as exhaust slot 150 .
  • Exhaust slot 150 is machined into one of a plurality of inner shell axial locations 175 . Exhaust slot 150 , in axial location 175 allows fluid to exit steam path 130 and enter inner shell cavity 155 .
  • Inner shell cavity 155 may be cast at the time of creation of inner shell 110 , in some embodiments. It is understood that, according to embodiments, the inner shell cavity 155 is entirely contained within the inner shell 110 .
  • Intermediate structure 100 also includes outer shell 120 .
  • Outer shell 120 is illustrated surrounding inner shell 110 and having an internal surface 125 . Internal surface 125 of outer shell 120 and external surface 115 of inner shell 110 define at least one closed chamber 160 extending in an axial direction A of the steam turbomachine 10 .
  • Inner shell 110 has a first access region 170 adjacent the at least one closed chamber 160 .
  • First access region 170 includes a plurality of inner shell axial locations 175 , (inner shell axial locations 175 shown in FIG. 3 ).
  • At least one axial location 175 of the plurality of inner shell axial locations 175 is selectable to be machined to create exhaust slot 150 .
  • Inner shell axial locations 175 are sections of inner shell 120 which may be machined for extraction of fluid from an adjacent closed chamber 160 .
  • inner shell axial locations 175 may, as a whole, define an elongated shape, extending in an axial direction A of turbomachine 10 .
  • Inner shell axial locations 175 may be located in inner shell 110 , contiguous to one another; that is, there may be no distinct separation between two adjacent inner shell axial locations 175 .
  • Inner shell axial locations 175 define potentially machinable areas of inner shell 120 for creation of fluid extraction.
  • exhaust slot 150 by machining a selected inner shell axial location 175 is performed while maintaining a structural integrity of casing intermediate structure 100 , and the structural integrity remains uniform regardless of which of the inner shell axial locations 175 is selected to be machined.
  • slot and “opening” are used to differentiate between the ports through the inner and outer casings, 110 and 120 , respectively; no other differences between “slot” and “opening” need be inferred.
  • inner shell 110 with the plurality of machinable axial locations 175 allows for a designer to select fluid extraction locations when desired characteristics of extracted fluid are known.
  • an inner shell axial location 175 adjacent an upstream stage of a turbomachine 10 may be machined in order to extract high pressure fluid, if a designer determines that high pressure fluid is desired for a particular industrial purpose.
  • fluid may be extracted from inner shell axial locations adjacent other stages of turbomachine 10 according to the needs of the designer and the pressure or other characteristics of the fluid within such stages, such characteristics may include, but are not limited to moisture content or temperature.
  • outer shell 120 includes a second access region 180 adjacent at least one closed chamber 160
  • second access region 180 includes a plurality of outer shell axial locations 185 (shown in FIG. 3 ).
  • Outer shell axial locations 185 are locations which may be machined to create a fluid extraction port, e.g. an opening 190 , from closed chamber 160 .
  • at least one of the plurality of outer shell axial locations 185 is selectable to be machined to create an exhaust opening 190 fluidly connected with the at least one closed chamber 160 through outer shell 120 .
  • the creation of the exhaust opening 190 by machining is performed while maintaining the structural integrity of the casing 100 and the structural integrity remains uniform regardless of which of the outer shell axial locations 185 is selected to be machined.
  • Inner shell 110 and outer shell 120 may be formed by casting using at least one of steel, nickel, chromium or alloys thereof, e.g., ferritic steel, ferritic-martensitic steel, austenitic stainless steel, 2.25 Cr-1 Mo steel, 1-2 CrMo steel, etc. Other materials may be used as known by those skilled in the art.
  • the casting of the shells maybe performed using molds.
  • the inner and outer shells 110 , 120 respectively, may be created at the same time, using the same mold, or they may be created separately, using different sets of molds.
  • the at least one closed chamber 160 may be created as follows. First, internal surface 125 of outer shell 120 and external surface 115 of inner shell 110 may be defined by at least one mold.
  • molten metal may be poured into a mold, or molds, as appropriate.
  • a core may be inserted into the mold(s) in order to create the surfaces defining at least one chamber 160 .
  • Such a core may comprise sand which is inserted into the mold space prior to the pouring of the molten metal.
  • the core is removed, creating the at least one chamber 160 .
  • the chamber may need to be cleaned of any debris, e.g., remaining sand.
  • the casting process described enables accessibility for cleaning of the chamber 160 after solidification of metal casting and core removal.
  • FIG. 2 a cross-sectional view of an apparatus according to embodiments is shown.
  • FIG. 2 illustrates an embodiment having inner shell 110 including first and second axial sections, 117 and 119 , respectively.
  • FIG. 2 illustrates options for embodiments according to aspects.
  • steam extraction exhaust slot 250 may be in a position different from steam extraction exhaust slot 150 , as illustrated in FIG. 2 .
  • inner shell 110 may include separate first and second axial sections 117 and 119 , the axial sections 117 and 119 are shaped complementary to one another, with a 360 degree fit 135 , acting as a dividing wall or support between axial sections 117 , 119 .
  • first and second axial sections 117 and 119 of inner shell 110 at least one first stage 132 may be supported on first axial section 117
  • at least one second stage 134 may be supported on second axial section 119 as illustrated in FIG. 2 .
  • the first and second stages, 132 and 134 are stationary stages of turbomachine 10 . Such stationary stages may include, but are not limited to nozzle stages.
  • Exhaust slots 150 and 250 shown in FIGS. 1 and 2 , respectively, allow extraction of a high pressure fluid from inner shell 110 at a steam extraction location, such as slot 150 or 250 , proximate a selected stage 130 , (selected stage not specifically shown) of steam turbomachine 10 , the steam extraction location, such as slot 150 or 250 , being related to a fluid characteristic of the fluid within steam turbomachine 10 in operation.
  • fluid such as steam may be released via slots 150 adjacent various stages 130 .
  • the outer shell may be machined to allow for extraction of fluid upstream of the 360 degree fit 135 and second axial section 119 may not be machined (opened) to allow for fluid extraction therefrom.
  • the outer casing 120 may be machined to allow for fluid extraction downstream of 360 degree fit 135 and in such embodiments, second axial section 119 lies adjacent a closed chamber 160 designed specific to that particular stage.
  • inner shell cavity 155 may be sealed by a closure, such as plate 176 .
  • a closure such as plate 176 .
  • Such closure may be accomplished using now-known or later-developed fabrication techniques, including, e.g., welding, or casting of plate 176 .
  • Exhaust slot 150 in axial location 175 may be machined by access through steam path 130 directly, in embodiments using multiple inner shells 110 .
  • opening 175 may be created by machining plate 176 to allow fluid flow from closed chamber 160 .
  • Such procedures may for example be performed in embodiments having single or multiple inner shell casing sections.
  • the fluid characteristic may be a characteristic of steam.
  • Such a characteristic may include, but are not limited to: pressure, moisture content (wetness), temperature, flow rate.
  • steam may be released via steam extraction location, such as slot 150 or 250 proximate a selected stage 130 of the turbomachine 10 .
  • this steam (or fluid) may be used for an industrial process or it may be sent to a boiler feed water heater to alter (e.g., to increase) cycle efficiency.
  • one of a plurality of axial locations 175 may be selected to be machined in order to allow for extraction of fluid, from exhaust opening 190 proximate a relatively upstream stage of the steam turbine, in order to allow extraction of a relatively high pressure fluid from the at least one closed chamber 160 proximate a selected stage of the turbomachine 10 .
  • exhaust slot 150 may be selected in order to extract fluid from an exhaust opening 190 proximate a relatively downstream stage of the previously mentioned upstream stage in order to extract a lower pressure fluid.
  • the location of fluid extraction may determine the fluid characteristics of the extracted fluid.
  • FIG. 3 illustrates a cross-sectional view of an apparatus according to embodiments.
  • FIG. 3 illustrates an embodiment where first and second access regions 170 and 180 , respectively, each have a uniform thickness T 1 , T 2 respectively, different from a thickness of the inner shell 110 adjacent first access region 170 and different from a thickness of the outer shell 120 adjacent second access region 180 .
  • first access region 170 has a thickness T 1 that is less than half a thickness of a remainder of inner shell 110 .
  • second access region 180 has a thickness T 2 that is less than half a thickness of a remainder of the outer shell 120 .
  • FIG. 3 further illustrates an embodiment where internal surface 125 of outer shell 120 and external surface 115 of inner shell 110 define at least two closed chambers 160 extending in an axial direction A of the steam turbomachine 10 . While only two chambers 160 are illustrated in FIG. 3 , any number of closed chambers 160 may be created. It should be noted that the intermediate structures described herein, are designed to allow for fluid extraction at any of a number of locations 175 , but actual extraction at a plurality of locations within the same turbomachine is not necessary according to all embodiments of the invention.
  • a steam turbomachine intermediate structure may have at least one shell casing having a plurality of pre-formed extraction opening sites selectable for use, wherein a structural integrity of the at least one shell casing is uniform, regardless of which of the plurality of pre-formed extraction opening sites is selected for use.
  • the at least one shell casing according to this embodiment is analogous to the inner and outer shell casings, 110 and 120 , described herein above with respect to FIGS. 1-3 .
  • the pre-formed extraction opening sites according to such embodiments are analogous to inner shell axial locations 175 and outer shell axial locations 185 described herein above with respect to FIGS. 1 and 3 , respectively.
  • an extraction opening may be selected to be used based on the location of the opening. That is, an opening may be selected because it is adjacent a relatively upstream stage in the steam turbo machine and because a designer desires to access high pressure steam for use in an industrial process. Likewise, an extraction opening may be selected due to its proximity to a relatively downstream stage because a designer chooses to access steam from the turbomachine having a different fluid characteristic than steam from an upstream stage. For non-limiting example a designer may need relatively high moisture content (wet) steam or relatively low temperature steam for an industrial purpose and therefore the designer may use an extraction opening appropriate for this desired industrial purpose.
  • wet moisture content
  • the at least one casing may be an inner casing having first and second axial sections 117 and 119 , as described above with respect to FIG. 2 .
  • the pre-formed extraction opening site may selected for use based on one or more fluid characteristics of a fluid within the steam turbomachine during operation, adjacent the selected opening site. Such fluid characteristics are described herein and will not be repeated here, for the sake of brevity.
  • FIG. 4 illustrates an environment according to embodiments of the invention.
  • System 300 includes a dynamoelectric machine 305 and a steam turbomachine 10 coupled with the dynamoelectric machine 305 .
  • Steam turbomachine 10 as illustrated includes steam turbomachine casing intermediate structure 100 as described above with respect to FIGS. 1-3 , and such description will not be repeated for the sake of brevity.
  • Some embodiments of the invention include a gas turbine 320 fluidly connected with generator 340 , as illustrated in FIG. 4 .
  • Embodiments may further include heat recovery steam generator (HRSG) 330 fluidly coupled with the gas turbomachine 320 and the steam turbomachine 10 , as illustrated in FIG. 4 .
  • Embodiments of the invention may also include generator 340 operationally connected with gas turbine 320 or alternatively with steam turbomachine 10 (such connection is not shown in FIG. 4 ).
  • HRSG heat recovery steam generator
  • FIG. 5 illustrates processes in a method of fabricating a turbomachine casing structure according to embodiments of the invention.
  • Process P 100 is illustrated in FIG. 5 and includes, forming a casing inner shell having an external surface, wherein a material of the casing inner shell defines an inner shell cavity and a fluid opening for allowing fluid from a turbomachine steam path to enter the inner shell cavity.
  • Process P 110 may be performed concurrently with, or after process P 100 and includes forming a casing outer shell having an internal surface such that the internal surface of the outer shell and the external surface of the inner shell define at least one closed chamber extending in an axial direction of the steam turbomachine. It should be understood that the timing of performance of processes P 100 and P 110 may not be affect the method as a whole.
  • Processes P 100 and P 110 may include casting as describe above which will not be repeated for the sake of brevity.
  • Optional Process P 115 shown in FIG. 6 , includes forming a casing inner shell and the forming of the casing outer shell such that the outer surface of the casing inner shell and the inner surface of the casing outer shell define at least two closed chambers extending in an axial direction of the steam turbomachine. According to embodiments, optional process P 115 may be performed in lieu of processes P 100 and P 110 , or process P 115 may be performed as an embellishment to processes P 100 and P 110 .
  • process P 120 includes forming, in the casing inner shell, a first access region adjacent the at least one closed chamber, the first access region including a plurality of inner shell axial locations.
  • the first access region may be formed of casing material of a different thickness than adjacent casing material.
  • the first access region may be cast of steel having a thickness half of the thickness of the steel that makes up the inner casing adjacent to the first access region.
  • each of the plurality axial locations within the inner shell is selectable to be machined to create an exhaust slot for allowing fluid to exit the inner shell cavity and enter the at least one closed chamber.
  • an exhaust slot may be located to allow high pressure fluid, such as steam, to flow from the inner shell and into one or more of the closed chambers. Any machining performed to create an exhaust slot maintains the structural integrity of the casing uniformly, regardless of which of the inner shell axial locations may be selected to be machined.
  • the forming of the first access region may include forming the first access region to have a uniform thickness, different from a thickness of the inner shell adjacent the first access region. Also according to aspects the forming of the first access region may include forming the first access region to have a thickness less than half a thickness of the remainder of the inner shell.
  • the inner shell casing may be formed using optional process P 124 , which is illustrated in FIG. 7 .
  • Optional process P 124 includes forming the casing inner shell by forming a first axial section and forming a second axial section, the second axial section being separate from and complementary to the first axial section.
  • process P 125 includes forming, in the casing outer shell, a second access region adjacent the at least one closed chamber, the second access region including a plurality of outer shell axial locations, wherein at least one of the plurality of outer shell axial location is selectable to be machined to create an exhaust opening fluidly connected with the at least one closed chamber through the outer shell and wherein the structural integrity of the casing is uniform regardless of which of the outer shell axial locations is selected to be machined.
  • the forming of the second access region may include forming the second access region to have a uniform thickness, different from a thickness of the outer shell adjacent the second access region.
  • the forming of the second access region may include forming the second access region to have a thickness less than half a thickness of a remainder of the outer shell.
  • FIG. 5 shows optional processes P 130 and P 140 .
  • Optional process P 130 includes machining a first slot through the first access region, wherein a location of the first slot is based upon a performance characteristic of the turbomachine.
  • Optional process P 140 includes machining a first opening in the second access region, the first opening extending through the outer shell. Such locations and associated performance characteristics where discussed above with respect FIG. 1 and will not be repeated for the sake of brevity.
  • Optional processes P 150 and P 160 are illustrated in FIG. 6 ; optional processed P 150 and P 160 may be performed after optional process P 115 .
  • Optional process P 150 includes machining a second slot through the first access region into a second of the at least two closed chambers while maintaining the structural integrity of the casing, a location of the second slot being based upon a performance characteristics of the turbomachine
  • Optional process P 150 may be performed, for example in cases where a designer may desire two outputs from a steam turbine and where the designer desires fluid having different characteristics to perform different functions. For example a designer may desire fluid of relatively high pressure for some industrial process and therefore the designer may locate a first slot adjacent an upstream stage of a steam turbomachine.
  • the designer may also desire lower pressure fluid to operate a different industrial application, and the designer may locate a second slot adjacent a stage downstream of the first slot to attain such relatively lower pressure fluid. While two slots located adjacent different stages are discussed, embodiments of the invention may include any number of slots, located adjacent the same or different stages of a steam turbomachine without deviating from the spirit of the invention.
  • Optional process P 160 includes machining a second opening in the second access region adjacent the second of the at least two closed chambers while maintaining the structural integrity of the casing, the second opening extending through the outer shell.
  • a second opening may allow a designer to access fluid from a second location to be used for a second industrial purpose.
  • the slots and openings described herein are not necessarily intended to remain open or to constantly allow release of fluid. Such openings and slots may be capped, and/or valves may be used to allow for release of fluid only when desired.
  • Optional processes P 150 and P 160 may be performed subsequent to process P 115 , in which a plurality of closed chambers is defined.
  • the terms “axial” and/or “axially” refer to the relative position/direction of objects along axis A, which is substantially parallel with the long axis of a conduit at a pipe crossing.
  • the terms “radial” and/or “radially” refer to the relative position/direction of objects along radius (r), which is substantially perpendicular with axis A and intersects axis A at only one location.
  • the terms “circumferential” and/or “circumferentially” refer to the relative position/direction of objects along a circumference which surrounds axis A but does not intersect the axis A at any location.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
US14/197,720 2014-03-05 2014-03-05 Modular turbomachine inner and outer casings with multi-stage steam extraction sites Abandoned US20150252681A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US14/197,720 US20150252681A1 (en) 2014-03-05 2014-03-05 Modular turbomachine inner and outer casings with multi-stage steam extraction sites
JP2015037509A JP2015169208A (ja) 2014-03-05 2015-02-27 多段抽気箇所を有するモジュール式ターボ機械内部及び外部ケーシング
DE102015103044.6A DE102015103044A1 (de) 2014-03-05 2015-03-03 Modulares inneres und äußeres Turbomaschinengehäuse mit Mehrstufen-Dampfentnahmestellen
CN201520127236.1U CN205101051U (zh) 2014-03-05 2015-03-05 蒸汽涡轮机壳体中间结构

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US14/197,720 US20150252681A1 (en) 2014-03-05 2014-03-05 Modular turbomachine inner and outer casings with multi-stage steam extraction sites

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3734025A1 (de) * 2019-04-30 2020-11-04 Siemens Aktiengesellschaft Dampfturbine mit standardisiertem gehäuse
EP3744952A1 (de) * 2019-05-31 2020-12-02 Siemens Aktiengesellschaft Gehäuseanordnung für fluidtechnische ausrüstung

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US5351478A (en) * 1992-05-29 1994-10-04 General Electric Company Compressor casing assembly
US20110247333A1 (en) * 2010-04-13 2011-10-13 General Electric Company Double flow low-pressure steam turbine
US8662831B2 (en) * 2009-12-23 2014-03-04 General Electric Company Diaphragm shell structures for turbine engines

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5351478A (en) * 1992-05-29 1994-10-04 General Electric Company Compressor casing assembly
US8662831B2 (en) * 2009-12-23 2014-03-04 General Electric Company Diaphragm shell structures for turbine engines
US20110247333A1 (en) * 2010-04-13 2011-10-13 General Electric Company Double flow low-pressure steam turbine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3734025A1 (de) * 2019-04-30 2020-11-04 Siemens Aktiengesellschaft Dampfturbine mit standardisiertem gehäuse
EP3744952A1 (de) * 2019-05-31 2020-12-02 Siemens Aktiengesellschaft Gehäuseanordnung für fluidtechnische ausrüstung
WO2020239997A1 (en) * 2019-05-31 2020-12-03 Siemens Aktiengesellschaft Customisable casing arrangement for steam turbine

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CN205101051U (zh) 2016-03-23
JP2015169208A (ja) 2015-09-28

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