US20080260529A1 - Turbine Nozzle Support Device and Steam Turbine - Google Patents

Turbine Nozzle Support Device and Steam Turbine Download PDF

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Publication number
US20080260529A1
US20080260529A1 US11/631,335 US63133505A US2008260529A1 US 20080260529 A1 US20080260529 A1 US 20080260529A1 US 63133505 A US63133505 A US 63133505A US 2008260529 A1 US2008260529 A1 US 2008260529A1
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Prior art keywords
turbine
cylinder
nozzle holder
disposed
steam
Prior art date
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Abandoned
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US11/631,335
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English (en)
Inventor
Hiroshi Kawakami
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Toshiba Corp
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Toshiba Corp
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Assigned to KABUSHIKI KAISHA TOSHIBA reassignment KABUSHIKI KAISHA TOSHIBA ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: KAWAKAMI, HIROSHI
Publication of US20080260529A1 publication Critical patent/US20080260529A1/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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/025—Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations
    • 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
    • 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
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • 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
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation

Definitions

  • the present invention relates to a turbine nozzle (stationary blade) holder for a steam turbine and a steam turbine which include the holder, and particularly relates to a turbine nozzle holder having a structure for supporting the turbine nozzle and fixing a turbine casing.
  • a steam turbine has turbine stages, each including turbine movable blades (turbine buckets) and turbine nozzles (stationary blades) paired with the turbine movable blades.
  • the turbine movable blades are disposed circumferentially around a turbine rotor (rotating shaft) inside a turbine casing.
  • the turbine nozzles are disposed upstream of the turbine movable blades in the circumferential direction of the turbine rotor.
  • the turbine nozzles (stationary blades) are held between inner and outer nozzle diaphragm rings.
  • the outer nozzle diaphragm ring is supported by the turbine casing so as to fix the turbine nozzles inside the casing.
  • a support structure is used in which turbine nozzles of turbine pressure stages are supported by a single holder, called a turbine nozzle holder, which is supported by a turbine casing.
  • FIG. 11 is a sectional view of the upper half part of the known turbine nozzle holder.
  • a turbine nozzle holder 57 includes a cylinder 56 extending axially substantially in parallel with a turbine rotor 52 and a support flange 58 engaged with a turbine casing 51 to support the cylinder 56 .
  • An outer nozzle diaphragm ring is engaged with grooves provided in an inner surface of the cylinder 56 .
  • the number of grooves corresponds to the number of nozzle plates 53 supported (four grooves in the example of FIG. 11 ).
  • the cylinder 56 has a separate structure including two semicylindrical portions for ease of assembly. These semicylindrical portions are mechanically joined at joint portions, such as flanges, disposed along separate surfaces by means of bolts, for example.
  • the turbine nozzle holder 57 having the structure described above is engaged and supported at a relatively upstream position on the turbine casing 51 for easy assembling, for example, for easy positioning of the support flange 58 and the turbine casing 51 .
  • a high-temperature, high-pressure steam passing through pressure stages 55 in the turbine nozzle holder 57 feeds a torque to movable blades 54 and flows toward the downstream side while decreasing in pressure and temperature.
  • the upstream side of a space defined between the turbine casing 51 and the turbine nozzle holder 57 (outside the cylinder 56 ) is filled with the high-pressure steam to be supplied to the turbine stages while the downstream side of the space is filled with the low-pressure steam that has lost its pressure after passing through all stages.
  • the support flange 58 also serves as a pressure barrier to prevent communication between the steams with different pressures.
  • FIG. 12 shows pressure distribution inside and outside the turbine nozzle holder 57 and on the front and rear sides of the support flange 58 .
  • a curve indicated by the dotted line P 1 represents the pressure distribution of the steam passing through the pressure stages inside the turbine nozzle holder 57 . This curve shows that the pressure decreases gradually as the steam passes through the pressure stages.
  • the solid line P 2 a represents the pressure of an atmosphere 59 upstream of the support flange 58 , which also serves as a pressure barrier.
  • the solid line P 2 b represents the pressure of an atmosphere 60 downstream of the support flange 58 .
  • the hatched parts represent pressures applied to the turbine nozzle holder 57 (cylinder 56 ) as a result of a pressure difference between the inside and outside of the turbine nozzle holder 57 .
  • the pressure outside the cylinder 56 is larger than the pressure inside the cylinder 56 , and thus, the cylinder 56 receives an external pressure.
  • the pressure inside the cylinder 56 is larger than the pressure outside the cylinder 56 , and thus, the cylinder 56 receives an internal pressure.
  • the turbine nozzle holder 57 is required to support a net internal pressure because the hatched area A 2 is much larger than the hatched area A 1 .
  • An example of a steam turbine includes a turbine nozzle holder supported on a casing by a pressure difference between the upstream and downstream sides of the turbine nozzle holder (for example, see Japanese Unexamined Patent Application Publication No. 10-103009).
  • the turbine nozzle holder is supported by fitting or engaging a rib protruding from an inner surface of the turbine casing to a groove provided on an outer circumferential portion of the turbine nozzle holder.
  • a side surface of the groove of the turbine nozzle holder is pressed against and fixed to a side surface of the rib of the turbine casing by a thrust force resulting from a pressure difference between the front and rear sides of the rib.
  • the turbine nozzle holder 57 involves several matters to be solved, including leakage of steam passing through the cylinder (i.e., through the stages).
  • the turbine nozzle holder 57 (cylinder 56 ) constantly supports an internal pressure. This pressure is generally supported by the fastening bolts attached to the joint portions point flanges) provided along the joint surfaces of the cylinder 56 , which has a separate structure.
  • the temperature of the fastening bolts reaches substantially the same temperature as that of the steam passing through the turbine stages.
  • the steam temperature reaches about 600° C. After extended operation, therefore, the fastening bolts undergo gradual creep deformation. Such fastening bolts fail to maintain the initial fastening force and thus cause steam leakage.
  • the turbine nozzle holder 57 becomes longer in the axial direction if the number of the turbine nozzles 53 supported by the turbine nozzle holder 57 is increased. In that case, a uniform fastening force is difficult to achieve over the entire joint surfaces of the cylinder 56 because of complicated factors, including the creep deformation of the fastening bolts, the thermal expansion and the deformation of the turbine nozzle holder 57 due to the temperature distribution thereof, the pressure distribution of the steam passing through the turbine stages 55 , and the number of fastening bolts. As a result, the turbine nozzle holder 57 cannot avoid slight steam leakage.
  • One of the possible measures to avoid such leakage is to increase the diameter of the fastening bolts or the area of the joint portions joint flanges) of the cylinder 56 .
  • Such measures contribute to an increase in the size of the turbine nozzle holder 57 and thus to an increase in the volume of the turbine casing 51 . This undesirably causes problems such as increases in the cost and installation area of the steam turbine.
  • An object of the present invention is to eliminate the defects of the known art described above by providing a turbine nozzle holder having joint portions (joint flanges) closely fastened without depending on the fastening force of fastening bolts to reduce steam leakage and achieve uniform rigidity in a circumferential direction and by providing a steam turbine including the holder.
  • a turbine nozzle holder for a steam turbine which includes a turbine casing, a turbine rotor disposed in the turbine casing, a plurality of turbine stages, a cylinder substantially coaxial with the turbine casing, and a fixing partition plate having an outer edge fixed to the turbine casing and an inner edge fixed to an outer circumferential portion of the cylinder, wherein the turbine stages each includes turbine movable blades disposed circumferentially around the turbine rotor and turbine nozzles paired with the turbine movable blades and disposed upstream of the turbine movable blades.
  • the turbine nozzles of the turbine stages are arranged inside the cylinder in an axial direction and are engaged with and fixed to the cylinder.
  • the fixing partition is disposed downstream of the center of the cylinder in the axial direction to separate an upstream atmosphere and a downstream atmosphere with respect to the partition plate.
  • the cylinder may be separated in two portions in the axial direction, and the turbine nozzle holder further includes joint flanges disposed along opposing separate surfaces and fastening bolts fastening the joint flanges.
  • the turbine nozzle holder may further include dummy flanges protruding from the outer circumferential portion of the cylinder in addition to the joint flanges disposed along the separate surfaces.
  • the dummy flanges may be preferably regularly arranged between the two joint flanges disposed on the cylinder.
  • the dummy flanges are preferably regularly arranged at intervals of 45° or 60° between the two joint flanges disposed on the cylinder.
  • the dummy flanges preferably have substantially the same shape as the joint flanges.
  • the cylinder preferably may have a cross-sectional shape symmetrical with respect to the axis thereof.
  • a steam turbine comprising a turbine casing, a turbine rotor disposed in the turbine casing, a plurality of turbine stages, a cylinder substantially coaxial with the turbine casing, and a fixing partition plate having an outer edge fixed to the turbine casing and an inner edge fixed to an outer circumferential portion of the cylinder, wherein the turbine stages each includes turbine movable blades disposed circumferentially around the turbine rotor and turbine nozzles paired with the turbine movable blades and disposed upstream of the turbine movable blades, the turbine nozzles of the turbine stages are arranged inside the cylinder in an axial direction and are engaged with and fixed to the cylinder, and the fixing partition plate is disposed downstream of the center of the cylinder in the axial direction to separate an upstream atmosphere and a downstream atmosphere with respect to the partition plate.
  • the size or number of fastening bolts used to fasten the separate surfaces can be reduced, and the separate surfaces are firmly fastened by a steam pressure difference between the inside and outside of the turbine nozzle holder.
  • the turbine nozzle holder and the steam turbine can therefore reduce leakage of steam passing through the stages to further enhance the internal efficiency of the turbine.
  • FIG. 1 is a schematic partial sectional view of a turbine nozzle holder and a steam turbine according to a first embodiment of the present invention.
  • FIG. 2 is a graph showing pressure distribution inside and outside the turbine nozzle holder according to the first embodiment of the present invention.
  • FIG. 3A is a front vertical sectional view of a known turbine nozzle holder and steam turbine for comparison with the turbine nozzle holder and the steam turbine according to the present invention.
  • FIG. 3B is a front vertical sectional view of the turbine nozzle holder and the steam turbine according to the present invention.
  • FIG. 4 is a schematic sectional view of a turbine nozzle holder according to a modification of the first embodiment of the present invention.
  • FIG. 5 is a schematic sectional view of a turbine nozzle holder according to a second embodiment of the present invention.
  • FIG. 6 is a sectional view taken along line VI-VI of FIG. 5 .
  • FIG. 7 is a sectional view of a turbine nozzle holder having no dummy flanges and a steam turbine.
  • FIG. 8 is a sectional view of a turbine nozzle holder having dummy flanges and a steam turbine.
  • FIG. 9 is a schematic sectional view of a turbine nozzle holder and a steam turbine according to a modification of the second embodiment of the present invention.
  • FIG. 10 is a schematic sectional view of a turbine nozzle holder and a steam turbine according to another modification of the second embodiment of the present invention.
  • FIG. 11 is a schematic partial sectional view of a known turbine nozzle holder and steam turbine.
  • FIG. 12 is a graph showing pressure distribution inside and outside the known turbine nozzle holder.
  • FIG. 13 is a schematic axial sectional view of a steam turbine according to the present invention, and a circled portion thereof corresponds to the view of FIG. 1 in an enlarged scale.
  • FIG. 13 is a schematic longitudinal sectional view of the steam turbine according to this embodiment.
  • the steam turbine generally includes three pressure sections of a high-pressure turbine, an intermediate pressure turbine, and a low-pressure turbine. Among the three pressure sections, FIG. 13 illustrates the high-pressure turbine section and the intermediate pressure turbine section.
  • the high-pressure turbine and the intermediate pressure turbine are integrally provided inside a single turbine casing 1 among the pressure sections of the steam turbine.
  • the high-pressure turbine and the intermediate pressure turbine each have turbine stages 5 , each including turbine movable blades (buckets) 3 and turbine nozzles (stationary blades) 4 paired with the turbine movable blades 3 .
  • the turbine movable blades 3 are disposed circumferentially around a turbine rotor (rotating shaft) 2 .
  • the turbine nozzles 4 are disposed upstream of the turbine movable blades 3 in the circumferential direction of the turbine rotor 2 .
  • reference numerals 1 ′ to 14 ′ denote the individual stages of the high-pressure turbine.
  • a main steam flows in the order of the stages 1 ′ to 14 ′ to rotate the movable blades before being discharged.
  • Reference numerals 15 ′ to 22 ′ denote the individual stages of the intermediate pressure turbine.
  • a boiler not shown, reheats the steam discharged from the high-pressure turbine, and the reheated steam flows in the order of the stages 15 ′ to 22 ′ to rotate the movable blades before being discharged.
  • the turbine nozzles 4 of, for example, the turbine stages of the intermediate pressure turbine are held between inner and outer nozzle diaphragm rings.
  • the outer nozzle diaphragm ring is supported by the turbine casing 1 to fix the turbine nozzles inside the casing 1 .
  • the high-pressure turbine has a support structure, particularly on the downstream side thereof, in which the turbine nozzles 4 of the turbine stages are supported by a single holder, called a turbine nozzle holder, which is supported by the turbine casing 1 .
  • FIG. 1 is a schematic diagram of the turbine nozzle holder according to the first embodiment of the present invention, showing an enlarged view of the circled portion of the steam turbine shown in FIG. 13 .
  • FIG. 1 illustrates the upper half of the turbine nozzle holder and the steam turbine along a horizontal plane in the axial direction.
  • the steam turbine includes the pressure sections (generally, a high-pressure section, an intermediate pressure section, and/or a low-pressure section). These pressure sections each has the turbine stages 5 inside the turbine casing 1 , each including the turbine movable blades 4 and the turbine nozzles (stationary blades) 3 paired with the turbine movable blades 4 .
  • the turbine movable blades 4 are disposed circumferentially around the turbine rotor (rotating shaft) 2 .
  • the turbine nozzles are disposed upstream of the turbine movable blades 4 in the circumferential direction of the turbine rotor 2 .
  • a turbine nozzle holder 7 includes a cylinder 6 extending axially substantially in parallel with the turbine rotor 2 and a fixing partition 8 engaged with the turbine casing 1 so as to support the cylinder 6 .
  • the fixing partition 8 also serves to divide the atmosphere of a space defined between the turbine casing 1 and the cylinder 6 into an upstream atmosphere 9 and a downstream atmosphere 10 .
  • Grooves (not shown) for engagement with the turbine nozzles 3 are formed in an inner surface of the cylinder 6 . The number of grooves corresponds to the number of the turbine nozzles 3 supported (four grooves in the example of FIG. 1 ).
  • a high-temperature and high-pressure steam passes through the stages 5 from the upstream side to the downstream side in the axial direction of the steam turbine (that is, in the direction from right (IN) to left (EX) in FIG. 1 and from 1 ′ to 14 ′ in FIG. 13 ).
  • the movable blades convert the energy of the steam into rotational energy as the steam passes through the stages 5 .
  • the steam itself is discharged from the steam turbine with decreased pressure and temperature.
  • the fixing partition 8 is engaged with the turbine casing 1 so as to fix and, support the turbine nozzle holder 7 .
  • the fixing partition 8 is positioned downstream of the central position C of the turbine nozzle holder 7 (cylinder 6 ) in the axial direction (a position corresponding to a length of L/2 where L is the full length of the turbine nozzle holder 7 ). More specifically, as shown in FIG. 1 , a rear joint end 11 of a portion of the fixing partition 8 joined to the cylinder 6 on the downstream side is positioned downstream of the central position C of the turbine nozzle holder 7 (cylinder 6 ) in the axial direction.
  • FIG. 2 shows a graph representing internal and external steam pressures applied to the turbine nozzle holder 7 with the fixing partition 8 disposed at the position described above.
  • a curve indicated by the dotted line P 1 represents the pressure distribution of the steam passing through the stages inside the turbine nozzle holder 7 . This curve shows the fact that the pressure decreases gradually as the steam passes through the stages.
  • the solid lines P 2 a and P 2 b represent the pressures of the upstream atmosphere 9 and the downstream atmosphere 10 , respectively, separated by the fixing partition 8 (rear joint end 11 ) inside the space defined between the turbine casing 1 and the cylinder 6 .
  • the hatched portions represent pressures applied to the turbine nozzle holder 7 (cylinder 6 ) as a result of a pressure difference between the inside and outside of the turbine nozzle holder 7 .
  • the net external pressure applied to the turbine nozzle holder 7 eliminates the need to use fasteners, such as bolts, for fastening the separate structure of the turbine nozzle holder 7 if the separate surfaces are accurately aligned.
  • FIG. 3B The embodiment based on the mechanism described above is specifically illustrated in FIG. 3B , where the cylinder 6 of the turbine nozzle holder 7 is separated in two parts along a horizontal plane HL in the axial direction.
  • This structure does not require, for example, flanges or fastening bolts.
  • FIG. 3A illustrates a known turbine nozzle holder 57 including a cylinder 56 having the same diameter as that of the cylinder 6 of the turbine nozzle holder 7 according to this embodiment.
  • the cylinder 56 has joint flanges 63 a and 63 b and fastening bolts 64 along the horizontal separating plane HL.
  • a comparison of the turbine nozzle holders 7 and 57 clearly shows that the turbine casing 51 requires a diameter larger than the turbine casing 1 according to this embodiment because the turbine casing 51 accommodates the joint flanges 63 a and 63 b and the fastening bolts 64 .
  • the external pressure is smaller than the internal pressure in the example of FIG. 3A , while the external pressure is larger than the internal pressure in the example of FIG. 3B .
  • the rear joint end 11 of the fixing partition 8 is positioned on the downstream side of the central position C of the turbine nozzle holder 7 in the axial direction so that the external pressure applied to the turbine nozzle holder 7 is larger than the internal pressure applied thereto.
  • This structure eliminates the need to use flanges or fastening bolts for the separate structure of the turbine nozzle holder and, because of no fastening bolts used, prevents steam leakage from the separate surfaces due to the creep deformation of bolts after extended exposure to elevated temperature.
  • the steam turbine can therefore constantly maintain the high internal efficiency over an extended period of time.
  • the cylinder 6 of the turbine nozzle holder 7 has a separate structure, that is, separated in two parts along the horizontal plane HL in the axial direction, and no flanges or fastening bolts are provided along the separate surfaces.
  • the external-pressure region (the length of the portion of the cylinder 6 upstream of the rear joint end 11 ) does not necessarily have a sufficient area.
  • steam leakage may be possible from the separate surfaces of the cylinder 6 on the downstream side of the rear joint end 11 , at which the cylinder 6 receives an internal pressure, depending on steam conditions.
  • a combination of joint flanges and fastening bolts may be optionally used to prevent leakage as in the known art.
  • fixed joint flanges may be coupled to each other with fastening bolts so as to prevent the misalignment of the separate surfaces of the cylinder 6 due to, for example, the steam vibration.
  • the sizes, diameters, and numbers of joint flanges and the fastening bolts used may be reduced relative to those of the known art.
  • FIG. 4 is a schematic sectional view of a turbine nozzle holder and a steam turbine according to a modification of the first embodiment of the present invention, in which the same components as those used in the first embodiment are indicated by the same reference numerals.
  • the fixing partition 8 is engaged with the turbine casing 1 to fix and support the turbine nozzle holder 7 .
  • the fixing partition 8 is largely shifted from the central position C of the turbine nozzle holder 7 (cylinder 6 ) in the axial direction (i.e., a position corresponding to a length of L/2 where L is the full length of the turbine nozzle holder 7 ) to the downstream side (to the left in FIG. 4 , for example, to a position corresponding to a length of 3L/4 where L is the full length of the turbine nozzle holder 7 ).
  • the fixing partition 8 is disposed at such a position, the area of the hatched portion A 1 on the upstream side of the fixing partition 8 (rear joint end 11 ) in FIG. 2 is significantly increased, and the area of the downstream hatched portion A 2 is decreased accordingly.
  • the turbine nozzle holder 7 receives a net external pressure larger than that of the first embodiment. As in the first embodiment, therefore, the net external pressure eliminates the need to use joint flanges or fastening bolts for preventing the leakage.
  • the rear joint end 11 of the fixing partition 8 is largely shifted from the central position C of the turbine nozzle holder 7 in the axial direction to the downstream side so that the external pressure applied to the turbine nozzle holder 7 is larger than the internal pressure applied thereto.
  • This structure eliminates the need to use flanges or fastening bolts for the separate structure of the turbine nozzle holder and, because of no fastening bolts used, reduces the steam leakage from the separate surfaces due to the creep deformation of the bolts after the extended exposure to elevated temperature.
  • the steam turbine can therefore constantly maintain high internal efficiency over an extended period of time.
  • the position of the fixing partition 8 relative to the turbine nozzle holder 7 is specifically determined according to, for example, the steam conditions and operating conditions of the steam turbine used and the number of turbine nozzles supported by the turbine nozzle holder 7 .
  • joint flanges and fastening bolts may be used to prevent misalignment of the separate surfaces due to, for example, the steam vibration.
  • FIGS. 5 and 6 are sectional views of a turbine nozzle holder and a steam turbine according to a second embodiment of the present invention.
  • the turbine nozzles 3 are engaged with and supported by the cylinder 6
  • the turbine nozzle holder 7 has joint flanges 13 a and 13 b and dummy flanges 15 disposed on the outer circumferential portion of the cylinder 6 along the separate surfaces thereof.
  • FIGS. 7 and 8 are views for explaining the effect of the dummy flange 15 of the steam turbine, graphically showing the amount of deformation.
  • FIG. 7 is a sectional view of a known steam turbine including a turbine nozzle holder having no dummy flanges.
  • FIG. 8 is a sectional view of the steam turbine including the turbine nozzle holder 7 having the dummy flanges according to the second embodiment.
  • the cylinder 6 shown in FIG. 8 has the same diameter as that shown in FIG. 7 .
  • the joint flanges 13 a and 13 b are firmly fastened with the fastening bolts 14 .
  • an internal pressure tends to expand the cylinder 6 by exerting a uniform force on the entire cylinder 6 in directions in which the diameter thereof uniformly increases, that is, perpendicularly to the inner circumferential surface of the cylinder 6 .
  • the joint flanges 13 a and 13 b restrain deformation of the cylinder 6 in the direction along the joint surfaces (HL line).
  • Portions of the cylinder 6 around the joint flanges 13 a and 13 b have a rigidity higher than other portions because of the thickness of the joint flanges and the fastening force of the fastening bolts. Accordingly, the internal pressure deforms a less rigid portion more significantly, for example, in the vertical direction of FIG. 7 . As a result, the entire cylinder 6 can be deformed to an oval shape.
  • the dummy flanges 15 which have substantially the same shape as the joint flanges 13 a and 13 b , are provided on the less rigid portion to ensure the rigidity thereof, thus realizing the substantially uniform amount of deformation.
  • the cylinder 6 shown in FIG. 7 is less rigid and more susceptible to the deformation in the vertical direction and is more rigid and less susceptible to the deformation in the horizontal direction, as indicated by the bidirectional arrows.
  • the cylinder 6 shown in FIG. 8 is more rigid and less susceptible to the deformation in both directions.
  • This embodiment is based on the phenomenon mentioned above, and as shown in FIG. 6 , specifically, the cylinder 6 is separated along the horizontal plane HL in the axial direction, and the joint flanges 13 a and 13 b and the fastening bolts 14 are provided along the separate surfaces.
  • the dummy flanges 15 are provided at the positions farthest away from the joint flanges 13 a and 13 b so as to further enhance the rigidity of the turbine nozzle holder 7 (cylinder 6 ).
  • the turbine nozzle holder 7 including the cylinder 6 having the dummy flanges 15 can be used for a steam turbine, as shown in FIG. 5 .
  • Gaps 16 a between seal fins 16 disposed at the leading ends of the movable blades 4 and gaps 17 a between seal fins 17 disposed inside the turbine nozzles 4 can be uniformly maintained irrespective of the operating conditions of the steam turbine (the extent of variations in pressure difference between the inside and outside of the turbine nozzle holder).
  • the turbine nozzle holder 7 has the dummy flanges 15 in addition to the joint flanges 13 a and 13 b to achieve and realize the rigidity sufficient to substantially uniformly maintain the distances of the gaps 16 a between the seal fins 16 disposed at the leading ends of the movable blades 4 and the gaps 17 a between the seal fins 17 disposed inside the turbine nozzles 3 .
  • the turbine nozzle holder 7 can therefore reduce the steam leakage through the seal fins 16 of the movable blades 4 and the seal fins 17 of the turbine nozzles 3 to enhance the internal efficiency of the turbine.
  • the dummy flanges 15 may have any other shape that allows the cylinder 6 to be deformed uniformly. Such a shape may be determined by analyzing the deformation of the turbine nozzle holder 7 (cylinder 6 ).
  • the dummy flanges 15 are not necessarily provided over the full length of the turbine nozzle holder 7 (cylinder 6 ) in the axial direction, and may be only partially provided thereon with consideration given to the amount of the deformation in the longitudinal direction.
  • the turbine nozzle holder 7 (cylinder 6 ) is separated along the horizontal plane HL in the axial direction with the joint flanges 13 a and 13 b disposed along the separate surfaces in this embodiment, the turbine nozzle holder 7 (cylinder 6 ) may also be separated along a vertical plane (perpendicular to the horizontal plane in the axial direction).
  • FIGS. 9 and 10 are schematic views of turbine nozzle holders and steam turbines according to modifications of the second embodiment of the present invention.
  • the turbine nozzle holder 7 includes the joint flanges 13 a and 13 b and the fastening bolts 14 along the separate surfaces in the horizontal plane HL in the axial direction and dummy flanges 15 a , 15 b , 15 c , . . . regularly arranged at intervals of 45° from the horizontal plane HL.
  • the turbine nozzle holder 7 includes the dummy flanges 15 a , 15 b , 15 c , . . . in addition to the joint flanges 13 a and 13 b and the fastening bolts 14 .
  • the dummy flanges 15 a , 15 b , 15 c , . . . are regularly arranged at intervals of 45° from the horizontal plane HL to further reduce the amount of the deformation due to, for example, a pressure difference between the inside and outside of the turbine nozzle holder 7 .
  • the turbine nozzle holder 7 can therefore inhibit the steam leakage through, for example, the seal fins of the movable blades and the turbine nozzles so that the steam turbine can maintain high internal efficiency.
  • the turbine nozzle holder 7 is separated along a vertical cross section VL in the axial direction.
  • the joint flanges 13 a and 13 b and the fastening bolts 14 are disposed along the separate surfaces of the turbine nozzle holder 7 .
  • the dummy flanges 15 a , 15 b , 15 c , . . . are regularly arranged at intervals of 60° from the vertical cross section VL.
  • any other structure may be used in which the dummy flanges 15 a , 15 b , 15 c . . . are arranged so that the entire cross-sectional shape of the turbine nozzle holder 7 (cylinder 6 ) is symmetrical with respect to the axis of the cylinder 6 .

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
US11/631,335 2004-06-30 2005-06-29 Turbine Nozzle Support Device and Steam Turbine Abandoned US20080260529A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2004-192692 2004-06-30
JP2004192692A JP2006016976A (ja) 2004-06-30 2004-06-30 タービンノズル支持装置および蒸気タービン
PCT/JP2005/011908 WO2006003911A1 (ja) 2004-06-30 2005-06-29 タービンノズル支持装置および蒸気タービン

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CN101010488A (zh) 2007-08-01
JP2006016976A (ja) 2006-01-19
EP1793092A4 (en) 2009-09-02
KR20070033012A (ko) 2007-03-23
WO2006003911A1 (ja) 2006-01-12
EP1793092A1 (en) 2007-06-06

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