EP3263851B1 - Turbine assembly - Google Patents

Turbine assembly Download PDF

Info

Publication number
EP3263851B1
EP3263851B1 EP16177535.8A EP16177535A EP3263851B1 EP 3263851 B1 EP3263851 B1 EP 3263851B1 EP 16177535 A EP16177535 A EP 16177535A EP 3263851 B1 EP3263851 B1 EP 3263851B1
Authority
EP
European Patent Office
Prior art keywords
casing
turbine
nozzle valve
blade carrier
valve casing
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.)
Active
Application number
EP16177535.8A
Other languages
German (de)
French (fr)
Other versions
EP3263851A1 (en
Inventor
Libor Chroboczek
Peter Jankura
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Priority to EP16177535.8A priority Critical patent/EP3263851B1/en
Priority to PCT/EP2017/062745 priority patent/WO2018001651A1/en
Publication of EP3263851A1 publication Critical patent/EP3263851A1/en
Application granted granted Critical
Publication of EP3263851B1 publication Critical patent/EP3263851B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • F01D25/243—Flange connections; Bolting arrangements
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • 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

Definitions

  • the present invention relates to a turbine assembly, in particular to a steam turbine assembly. More particularly the present invention relates to a turbine assembly, for example a steam turbine assembly, including an outer turbine casing, a nozzle valve casing and a stator blade carrier.
  • a flow of steam is channelled, through a plurality of nozzle blades, towards a plurality of turbine stage which transform the energy from the hot steam into work for powering one or more devices which converts power, for example including a generator in a power generation application.
  • Each stage of the turbine includes a row of stator blades which channel the hot steam into a corresponding row of rotor blades.
  • the stator blades extend radially inwardly from stator components of the turbine.
  • the rotor blades extend radially outwardly from a rotor of the turbine.
  • the flowing and the expansion of the steam through the turbine stages cause the rotation of the rotor blades and of the rotor itself around its axis.
  • the rotation of the rotor is the source of work which is usable as output for powering one or more devices which converts power.
  • the outer turbine casing of a steam turbine has an axis of symmetry, which is normally coincident with the axis of rotation of the rotor, and is constituted by a lower part and an upper part joined together by means of joining bolts at a splitting plane.
  • the splitting plane is typically horizontally disposed.
  • the turbine further comprises a nozzle valve casing and a stator blade carrier, which are fixed to the outer turbine casing for supporting, respectively, the plurality of nozzle blades and the plurality of stator blades.
  • the outer turbine casing, the nozzle valve casing and the stator blade carrier comprise respective lower half portions and upper half portions joined together at the horizontal splitting plane.
  • the nozzle valve casing and the stator blade carrier are fixed to the casing in such a way that:
  • GB 2076065 discloses a turbine according to the preamble of claim 1.
  • a turbine comprising:
  • the above described turbine may be a steam turbine.
  • stator blade carrier no coupling between the stator blade carrier and the casing.
  • the stator blade carrier is in contact only with the nozzle valve casing, which is interposed between the casing and the stator blade carrier.
  • the nozzle valve casing and the stator blade carrier are distinct components, the stator comprising at least a fixing connection between the nozzle valve casing and the stator blade carrier.
  • the fixing connection may include a plurality of bolts or a welding.
  • the nozzle valve casing and the stator blade carrier are integrated in a single component.
  • the nozzle valve casing and the stator blade carrier may be obtained through casting of a single component.
  • this permits to avoid the use of connecting means between the nozzle valve casing and the stator blade carrier.
  • the casing comprises at least two seats to which the nozzle valve casing is coupled, for example by a forced coupling.
  • this permits to further improve the stiffness and strength of the stator assembly and to further facilitate the assembly of the with the nozzle valve casing and of the stator blade carrier to the outer turbine casing.
  • FIG. 1 shows an example of a steam turbine 1 in a vertical sectional view.
  • the steam turbine 1 comprises an outer casing 12 and rotor 13, having a common axis of symmetry Y, also coincident with the rotational axis of the rotor 13.
  • Both the turbine outer casing 12 and the rotor 13 are partially represented in Fig. 1 .
  • the terms axial, radial and circumferential are made with reference to the rotational axis Y of the rotor 13.
  • the rotor 13 comprises a plurality of rows of rotor blades 19.
  • the rotor blades 19 extend radially outwardly from the rotor 13 of the steam turbine 1.
  • the rotor blades 19 are regularly distributed around the rotational axis Y.
  • the outer turbine casing 12 is constituted by a first lower portion and a second upper portion (only the latter is represented in the attached figures).
  • Each of the lower and upper portions of the casing 12 extends circumferentially for angle of 180° around the rotational axis Y and are joined together, by means of joining bolts (not represented in the attached figures), at an intermediate horizontal splitting plane (in the attached figures the dot-dashed line Y also represent the trace of the horizontal splitting plane).
  • the outer casing 12 comprises an external surface 12a, towards the external environment, an internal surface 12b towards the rotational axis Y.
  • the outer casing 12 extends radially between a first axial end 11a and a second axial end 11b. Inside the casing, steam flows mainly according to an axial direction oriented from the first axial end 11a towards second axial end 11b.
  • the terms upstream and downstream refer to the flow direction of the steam flow through the casing 12 of the turbine 1, unless otherwise stated.
  • the turbine 1 further comprises a nozzle valve casing 14 for supporting a plurality of nozzle blades 16. Through the nozzle blades 16, the flow of steam is channelled towards a plurality of stages of the steam turbine 1.
  • Each stage of the steam turbine 1 comprises a row of stator blades 18 which channel the hot steam into a corresponding row of the rotor blades 19.
  • the plurality of nozzle blades 16 are connected to the nozzle valve casing 14 by means of a nozzle ring 26.
  • the nozzle ring 26 is radially supported by a wheel 27 fixed to the rotor 13.
  • the plurality nozzle blades 16, the nozzle ring 26 and the connections between the nozzle ring 26 and the nozzle valve casing 14 and between the nozzle ring 26 and the wheel 27 are not described in further detail, as they are conventional and do not form specific part of the present invention.
  • the nozzle valve casing 14 is fixed to the outer casing 12. For the fixing of the nozzle valve casing 14 to the casing 12, at least one seat in the casing is provided.
  • a first upstream seat 23 is provided as a circumferential cylindrical groove to be coupled, for example by means of a forced coupling, to a correspondent cylindrical surface 14a of the nozzle valve casing 14.
  • a second downstream seat 24, axially adjacent to the first upstream seat 23, is provided as a circumferential surface at the radial end of an annular protrusion 34 extending radially inward from the internal surface 12b of the casing 12 towards the rotational axis Y.
  • the second downstream seat 24 is coupled, for example by means of a forced coupling, to a correspondent circumferential surface 14b of the nozzle valve casing 14.
  • the turbine 1 further comprises a stator blade carrier 22 supporting the plurality of stator blades 18.
  • the stator blades 18 are distributed into a plurality of rows of stator blades 18, one for each of the stages of the steam turbine 1.
  • the stator blades 18 extend radially inwardly from the stator blade carrier 22 and are regularly distributed around the rotational axis Y.
  • a row of stator blades 18 are axially upstream a corresponding row of rotor blades 19.
  • the stator blade carrier 22 is supported by the nozzle valve casing 14.
  • the nozzle valve casing 14 is interposed between the casing 12 and the stator blade carrier 22 in such a way that the casing 12 and the stator blade carrier 22 are separated from each other, i.e.
  • the nozzle valve casing 14 and the stator blade carrier 22 are connected in series between the casing 12 and the stator blades 18.
  • the nozzle valve casing 14 and the stator blade carrier 22 are distinct components.
  • the turbine 1 comprises a plurality of bolts, parallel to the rotational axis Y and circumferentially distributed around the rotational axis Y.
  • the length of the bolts 25 are long enough to assure the connection between the nozzle valve casing 14 and the stator blade carrier 22 and are considerably shorter than in other known-in-the-art application where bolts are provided to couple the stator blade carrier 22 to the nozzle valve casing 14 and at the same time to the casing 12 of the turbine. According to other embodiments of the present invention (not represented in the attached figures), other fixing connections may be provided between the stator blade carrier 22 and the nozzle valve casing 14, for example a welding.
  • the nozzle valve casing 14 and the stator blade carrier 22 are integrated in a single component 15.
  • such single component may be obtained through casting.
  • the stator blade carrier 22 is identified as the portion of the single component 15 which is downstream of the nozzle valve casing 14 and of the annular protrusion 34.
  • it is essential that the stator blade carrier 22 has not direct connection to the outer casing 12 of the turbine 1.

Description

    Field of invention
  • The present invention relates to a turbine assembly, in particular to a steam turbine assembly. More particularly the present invention relates to a turbine assembly, for example a steam turbine assembly, including an outer turbine casing, a nozzle valve casing and a stator blade carrier.
    • Art Background
  • In a steam turbine a flow of steam is channelled, through a plurality of nozzle blades, towards a plurality of turbine stage which transform the energy from the hot steam into work for powering one or more devices which converts power, for example including a generator in a power generation application.
  • Each stage of the turbine includes a row of stator blades which channel the hot steam into a corresponding row of rotor blades. The stator blades extend radially inwardly from stator components of the turbine. The rotor blades extend radially outwardly from a rotor of the turbine. The flowing and the expansion of the steam through the turbine stages cause the rotation of the rotor blades and of the rotor itself around its axis. The rotation of the rotor is the source of work which is usable as output for powering one or more devices which converts power.
  • The outer turbine casing of a steam turbine has an axis of symmetry, which is normally coincident with the axis of rotation of the rotor, and is constituted by a lower part and an upper part joined together by means of joining bolts at a splitting plane. In operation the splitting plane is typically horizontally disposed.
  • The turbine further comprises a nozzle valve casing and a stator blade carrier, which are fixed to the outer turbine casing for supporting, respectively, the plurality of nozzle blades and the plurality of stator blades.
  • The outer turbine casing, the nozzle valve casing and the stator blade carrier comprise respective lower half portions and upper half portions joined together at the horizontal splitting plane.
  • According to known technical solutions, the nozzle valve casing and the stator blade carrier are fixed to the casing in such a way that:
    • the nozzle valve casing is coupled to at least a seat provided in the outer turbine casing.
    • the stator blade carrier is attached to the nozzle valve casing, by means of a plurality of coupling bolts distributed around the central axis of symmetry of the rotor, and is also coupled to at least a second seat provided in the outer turbine casing.
  • Such solution is not considered optimal, as it exhibits some drawbacks, including:
    • a not satisfactory level of stiffness for the casing assembly,
    • a not satisfactory level of strength for the casing assembly ,
    • excessive length of the coupling bolts, which are needed to couple together the stator blade carrier and the nozzle valve casing. This implies an excessive length of the respective coupling holes provided in the stator blade carrier and a consequent weakening of the structure of the stator blade carrier.
  • It is therefore desirable to provide a new design for a turbine where the coupling between the casing, the nozzle valve casing and the stator blade carrier limits or removes the above mentioned drawbacks. GB 2076065 discloses a turbine according to the preamble of claim 1.
    • Summary of the Invention
  • It may be an object of the present invention to provide a turbine, in particular a steam turbine, having a higher level of stiffness, with respect to the existing turbine solutions.
  • It may be another object of the present invention to provide a a turbine, in particular a steam turbine, having a higher level of strength, with respect to the existing turbine solutions.
  • It may be a further object of the present invention to provide a turbine, in particular a steam turbine, where the extension of the coupling between the stator blade carrier and the nozzle valve casing is minimized.
  • In order to achieve the objects defined above, a turbine is provided in accordance to the independent claim. The dependent claims describe advantageous developments and modifications of the invention.
  • According to an aspect of the present invention, a turbine is provided. The turbine comprises:
    • a casing,
    • a plurality of nozzle blades,
    • a plurality of stator blades,
    • a nozzle valve casing supporting the plurality of nozzle blades, the nozzle valve casing being fixed to the casing,
    • a stator blade carrier supporting the plurality of stator blades, the stator blade carrier being supported by the nozzle valve casing.
    The casing comprises at least one seat to which the nozzle valve casing is coupled, the nozzle valve casing being interposed between the casing and the stator blade carrier in such a way that the casing and the stator blade carrier are separated from each other.
  • More particularly, the above described turbine may be a steam turbine.
  • According to the present invention no coupling between the stator blade carrier and the casing are provided. The stator blade carrier is in contact only with the nozzle valve casing, which is interposed between the casing and the stator blade carrier. This implies a plurality of advantages, with respect to known stators, including:
    • easier assembly of the with the nozzle valve casing and of the stator blade carrier to the stator,
    • higher stiffness of the stator assembly,
    • higher strength of the stator assembly,
    • improvement of the design of the flow channel in the direction of steam flow, i.e. from nozzle ring to stator blades,
    • decreasing of cost for the manufacturing process.
  • According to an exemplary embodiment of the present invention, the nozzle valve casing and the stator blade carrier are distinct components, the stator comprising at least a fixing connection between the nozzle valve casing and the stator blade carrier.
    In particular, the fixing connection may include a plurality of bolts or a welding.
    Advantageously, this allows, with respect to known stators mean term, an easier manufacturing process of the nozzle valve casing and of the stator blade carrier.
  • According to another exemplary embodiment of the present invention, the nozzle valve casing and the stator blade carrier are integrated in a single component.
    In particular, the nozzle valve casing and the stator blade carrier may be obtained through casting of a single component.
    Advantageously, this permits to avoid the use of connecting means between the nozzle valve casing and the stator blade carrier.
  • According to a further exemplary embodiment of the present invention, the casing comprises at least two seats to which the nozzle valve casing is coupled, for example by a forced coupling.
    Advantageously, this permits to further improve the stiffness and strength of the stator assembly and to further facilitate the assembly of the with the nozzle valve casing and of the stator blade carrier to the outer turbine casing.
    • Brief Description of the Drawings
  • The aspects defined above and further aspects of the present invention are apparent from the examples of embodiment to be described hereinafter and are explained with reference to the examples of embodiment. The invention will be described in more detail hereinafter with reference to examples of embodiment, but to which the invention is not limited.
    • Fig. 1 is a partial sectional view of a first embodiment of a steam turbine according to the present invention,
    • FIG. 2 is a partial sectional view of a second embodiment of a steam turbine according to the present invention.
    Detailed Description
  • Hereinafter, above-mentioned and other features of the present invention are described in details. A plurality of embodiments is described with reference to the drawings, wherein the same reference numerals are used to refer to the same elements throughout. The illustrated embodiments are intended to explain, and not to limit the invention.
  • FIG. 1 shows an example of a steam turbine 1 in a vertical sectional view.
    The steam turbine 1 comprises an outer casing 12 and rotor 13, having a common axis of symmetry Y, also coincident with the rotational axis of the rotor 13. Both the turbine outer casing 12 and the rotor 13 are partially represented in Fig. 1.
    In the following, the terms axial, radial and circumferential are made with reference to the rotational axis Y of the rotor 13.
  • The rotor 13 comprises a plurality of rows of rotor blades 19. The rotor blades 19 extend radially outwardly from the rotor 13 of the steam turbine 1. In each row, which corresponds to a respective stage of the steam turbine 1, the rotor blades 19 are regularly distributed around the rotational axis Y.
    The outer turbine casing 12 is constituted by a first lower portion and a second upper portion (only the latter is represented in the attached figures). Each of the lower and upper portions of the casing 12 extends circumferentially for angle of 180° around the rotational axis Y and are joined together, by means of joining bolts (not represented in the attached figures), at an intermediate horizontal splitting plane (in the attached figures the dot-dashed line Y also represent the trace of the horizontal splitting plane).
    The outer casing 12 comprises an external surface 12a, towards the external environment, an internal surface 12b towards the rotational axis Y.
  • In the representation of FIG. 1 , the outer casing 12 extends radially between a first axial end 11a and a second axial end 11b. Inside the casing, steam flows mainly according to an axial direction oriented from the first axial end 11a towards second axial end 11b.
    In the following, the terms upstream and downstream refer to the flow direction of the steam flow through the casing 12 of the turbine 1, unless otherwise stated.
    The turbine 1 further comprises a nozzle valve casing 14 for supporting a plurality of nozzle blades 16. Through the nozzle blades 16, the flow of steam is channelled towards a plurality of stages of the steam turbine 1. Each stage of the steam turbine 1 comprises a row of stator blades 18 which channel the hot steam into a corresponding row of the rotor blades 19.
    The plurality of nozzle blades 16 are connected to the nozzle valve casing 14 by means of a nozzle ring 26. The nozzle ring 26 is radially supported by a wheel 27 fixed to the rotor 13. The plurality nozzle blades 16, the nozzle ring 26 and the connections between the nozzle ring 26 and the nozzle valve casing 14 and between the nozzle ring 26 and the wheel 27 are not described in further detail, as they are conventional and do not form specific part of the present invention.
    The nozzle valve casing 14 is fixed to the outer casing 12. For the fixing of the nozzle valve casing 14 to the casing 12, at least one seat in the casing is provided.
    With reference to the embodiments in attached figures, two seats 23, 24 are provided on the internal surface 12b of the casing 12 for fixing the nozzle valve casing 14 to the casing 12. A first upstream seat 23 is provided as a circumferential cylindrical groove to be coupled, for example by means of a forced coupling, to a correspondent cylindrical surface 14a of the nozzle valve casing 14. A second downstream seat 24, axially adjacent to the first upstream seat 23, is provided as a circumferential surface at the radial end of an annular protrusion 34 extending radially inward from the internal surface 12b of the casing 12 towards the rotational axis Y. The second downstream seat 24 is coupled, for example by means of a forced coupling, to a correspondent circumferential surface 14b of the nozzle valve casing 14. The turbine 1 further comprises a stator blade carrier 22 supporting the plurality of stator blades 18.
    The stator blades 18 are distributed into a plurality of rows of stator blades 18, one for each of the stages of the steam turbine 1. The stator blades 18 extend radially inwardly from the stator blade carrier 22 and are regularly distributed around the rotational axis Y. In each stage of the steam turbine 1, a row of stator blades 18 are axially upstream a corresponding row of rotor blades 19.
    The stator blade carrier 22 is supported by the nozzle valve casing 14. The nozzle valve casing 14 is interposed between the casing 12 and the stator blade carrier 22 in such a way that the casing 12 and the stator blade carrier 22 are separated from each other, i.e. no seat is provided in the casing 12 for coupling with the stator blade carrier 22.
    In other words, according to the present invention, the nozzle valve casing 14 and the stator blade carrier 22 are connected in series between the casing 12 and the stator blades 18.
    With reference to the embodiment of FIG. 1 , the nozzle valve casing 14 and the stator blade carrier 22 are distinct components. The turbine 1 comprises a plurality of bolts, parallel to the rotational axis Y and circumferentially distributed around the rotational axis Y. The length of the bolts 25 are long enough to assure the connection between the nozzle valve casing 14 and the stator blade carrier 22 and are considerably shorter than in other known-in-the-art application where bolts are provided to couple the stator blade carrier 22 to the nozzle valve casing 14 and at the same time to the casing 12 of the turbine.
    According to other embodiments of the present invention (not represented in the attached figures), other fixing connections may be provided between the stator blade carrier 22 and the nozzle valve casing 14, for example a welding.
  • With reference to the embodiment of FIG. 2 , the nozzle valve casing 14 and the stator blade carrier 22 are integrated in a single component 15. According to a possible embodiment of the present invention, such single component may be obtained through casting. Such a solution permits to avoid the use of the bolts 25 of the embodiment of FIG. 1 . In this embodiment, the stator blade carrier 22 is identified as the portion of the single component 15 which is downstream of the nozzle valve casing 14 and of the annular protrusion 34.
    In any case, in all the embodiments of the present invention, it is essential that the stator blade carrier 22 has not direct connection to the outer casing 12 of the turbine 1.

Claims (8)

  1. A turbine (1) comprising:
    - a casing (12),
    - a plurality of nozzle blades (16),
    - a plurality of stator blades (18),
    - a nozzle valve casing (14) supporting the plurality of nozzle blades (16), the nozzle valve casing (14) being fixed to the casing (12),
    - a stator blade carrier (22) supporting the plurality of stator blades (18), the stator blade carrier (22) being supported by the nozzle valve casing (14),
    wherein the casing (12) comprises at least one seat (23, 24) to which the nozzle valve casing (14) is coupled, characterized in having the nozzle valve casing (14) being interposed between the casing (12) and the stator blade carrier (22) in such a way that the casing (12) and the stator blade carrier (22) are separated from each other.
  2. The turbine (1) according to claim 1, wherein the nozzle valve casing (14) and the stator blade carrier (22) are distinct components, the turbine (1) comprising at least a fixing connection (25) between the nozzle valve casing (14) and the stator blade carrier (22).
  3. The turbine (1) according to claim 2, wherein the fixing connection (25) includes at least a bolt.
  4. The turbine (1) according to claim 2 or 3, wherein the fixing connection (25) includes at least a welding.
  5. The turbine (1) according to claim 1, wherein the nozzle valve casing (14) and the stator blade carrier (22) are integrated in a single component.
  6. The turbine (1) according to claim 5, wherein the nozzle valve casing (14) and the stator blade carrier (22) are integrated in a single casted component (15).
  7. The turbine (1) according to any of the preceding claims, wherein the casing (12) comprises at least two seats (23, 24) to which the nozzle valve casing (14) is coupled.
  8. The turbine (1) according to any of the preceding claims, further comprising a nozzle valve ring (26) for connecting the plurality of nozzle blades (16) to the nozzle valve casing (14).
EP16177535.8A 2016-07-01 2016-07-01 Turbine assembly Active EP3263851B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP16177535.8A EP3263851B1 (en) 2016-07-01 2016-07-01 Turbine assembly
PCT/EP2017/062745 WO2018001651A1 (en) 2016-07-01 2017-05-26 Turbine assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP16177535.8A EP3263851B1 (en) 2016-07-01 2016-07-01 Turbine assembly

Publications (2)

Publication Number Publication Date
EP3263851A1 EP3263851A1 (en) 2018-01-03
EP3263851B1 true EP3263851B1 (en) 2018-10-17

Family

ID=56292604

Family Applications (1)

Application Number Title Priority Date Filing Date
EP16177535.8A Active EP3263851B1 (en) 2016-07-01 2016-07-01 Turbine assembly

Country Status (2)

Country Link
EP (1) EP3263851B1 (en)
WO (1) WO2018001651A1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2076065B (en) * 1980-05-20 1983-11-23 Forster Terence Owen Turbine
CN1119505C (en) * 1999-10-29 2003-08-27 三菱重工业株式会社 Steam turbine with improved outer shell cooling system
US9528392B2 (en) * 2013-05-10 2016-12-27 General Electric Company System for supporting a turbine nozzle

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
EP3263851A1 (en) 2018-01-03
WO2018001651A1 (en) 2018-01-04

Similar Documents

Publication Publication Date Title
CA2672096C (en) Fabricated itd-strut and vane ring for gas turbine engine
JP5748960B2 (en) Compressor diffuser
US8727719B2 (en) Annular flange for fastening a rotor or stator element in a turbomachine
US8348608B2 (en) Turbomachine rotor cooling
US9127559B2 (en) Diaphragm for turbomachines and method of manufacture
US20160195110A1 (en) Rotor for a thermal turbomachine
US10077662B2 (en) Rotor for a thermal turbomachine
CN101096919B (en) Turbo machine
RU2435038C2 (en) Steam turbine
JP7254472B2 (en) Steam turbine exhaust chamber, steam turbine, and method for replacing steam turbine
US9057278B2 (en) Turbine bucket including an integral rotation controlling feature
JP5965622B2 (en) Steam turbine singlet joint for margin stage nozzle with pinned or bolted inner ring
EP3263851B1 (en) Turbine assembly
KR102261350B1 (en) Methods and systems for securing turbine nozzles
JP7076943B2 (en) Combustor cap module and holding system for it
EP2576998B1 (en) Steam turbine assembly and method of assembling a steam turbine
JP2008051101A (en) Rotor for steam turbine, and turbine engine
US20130034445A1 (en) Turbine bucket having axially extending groove
US20130058779A1 (en) Turbine casing assembly mounting pin
US9194244B2 (en) Drum rotor dovetail component and related drum rotor system
US8864459B2 (en) Turbine casing assembly mounting pin
JP2019518903A (en) Turbine vane for turbine diaphragm and associated turbine diaphragm
JP4981416B2 (en) Stacked reaction steam turbine rotor assembly
US8801376B2 (en) Fabricated intermediate case with engine mounts
US8282349B2 (en) Steam turbine rotor and method of assembling the same

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN PUBLISHED

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20180205

RBV Designated contracting states (corrected)

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: GRANT OF PATENT IS INTENDED

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20180621

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602016006419

Country of ref document: DE

Ref country code: AT

Ref legal event code: REF

Ref document number: 1054278

Country of ref document: AT

Kind code of ref document: T

Effective date: 20181115

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20181017

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1054278

Country of ref document: AT

Kind code of ref document: T

Effective date: 20181017

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190217

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190117

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190117

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: RS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190118

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20190217

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602016006419

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

26N No opposition filed

Effective date: 20190718

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

REG Reference to a national code

Ref country code: BE

Ref legal event code: MM

Effective date: 20190731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190701

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20190701

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 602016006419

Country of ref document: DE

Owner name: SIEMENS ENERGY GLOBAL GMBH & CO. KG, DE

Free format text: FORMER OWNER: SIEMENS AKTIENGESELLSCHAFT, 80333 MUENCHEN, DE

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20200701

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20200701

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20160701

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20181017

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CZ

Payment date: 20230629

Year of fee payment: 8

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20230721

Year of fee payment: 8

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20230726

Year of fee payment: 8