US20070081892A1 - Steam turbine exhaust diffuser - Google Patents

Steam turbine exhaust diffuser Download PDF

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Publication number
US20070081892A1
US20070081892A1 US11/243,974 US24397405A US2007081892A1 US 20070081892 A1 US20070081892 A1 US 20070081892A1 US 24397405 A US24397405 A US 24397405A US 2007081892 A1 US2007081892 A1 US 2007081892A1
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United States
Prior art keywords
steam
volute
flow path
exhaust
turbine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US11/243,974
Inventor
Edward Sharrow
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US11/243,974 priority Critical patent/US20070081892A1/en
Assigned to GENERAL ELECTRIC COMPANY reassignment GENERAL ELECTRIC COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SHARROW, EDWARD
Priority to CNA2006101420320A priority patent/CN1944962A/en
Priority to EP06255126A priority patent/EP1772595A3/en
Priority to JP2006273597A priority patent/JP2007100701A/en
Publication of US20070081892A1 publication Critical patent/US20070081892A1/en
Abandoned legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30Exhaust heads, chambers, or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28Supporting or mounting arrangements, e.g. for turbine casing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/31Application in turbines in steam turbines

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

An axial flow steam turbine includes an exhaust diffuser in the form of a volute for diffusing the exhaust steam and turning the exhaust steam from a generally axial flow direction to a generally radial direction. The volute exit may be at the bottom or to one side of the steam turbine. The volute and casing are independently mounted relative to one another on a foundation with a flexible joint therebetween.

Description

  • The present invention relates to steam turbines and particularly relates to an exhaust diffuser in the shape of a volute.
  • BACKGROUND OF THE INVENTION
  • In prior steam turbines, the inner case of the steam turbine, for example a double flow down exhaust unit has an encompassing exhaust hood split vertically and extending along opposite sides and ends of the turbine. This large box-like structure houses the entire low pressure section of the turbine. The exhaust steam outlet from the turbine is generally conically shaped and the steam exhaust is redirected from a generally axial extending flow direction to a flow direction 90° relative to the axial flow direction. This 90° flow direction may be in any plane, downwardly, upwardly or transversely. Thus the prior exhaust hoods for steam turbines constitute a large rectilinear structure at the exit end of the conical section for turning and diffusing the steam flow at right angles. The steam flow path was thus tortuous resulting in losses and adverse pressure drop. It will also be appreciated that access to various parts of the turbine, for example, the bearing for maintenance purposes was difficult in that it necessitated the removal of the upper half of the exhaust hood. Further, it will be appreciated that the exhaust hood in conventional steam turbines typically supports the inner casing of the turbine and the associated steam path parts such as diaphragms and the like. Accordingly, there has been found a need to provide a new geometry to improve exhaust steam pressure recovery and overall performance of the turbine.
  • BRIEF DESCRIPTION OF THE INVENTION
  • In a preferred embodiment of the invention, there is provided an axial flow steam turbine flow path comprising: a rotor and a casing defining the axial steam flow path; and an exhaust diffuser for the turbine including a volute for diffusing the exhaust steam and turning the exhaust steam from a generally axial flow direction to a generally transverse and tangential direction.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a fragmentary schematic illustration of half of a double flow down exhaust steam turbine according to the prior art.
  • FIG. 2 is a fragmentary side cross-sectional view of a steam turbine illustrating an exhaust diffuser having a volute configuration; and
  • FIGS. 3 and 4 are axial end views of two embodiments of volutes which may be employed to receive the exhaust steam from the steam turbine.
  • DETAILED DESCRIPTION OF THE INVENTION
  • Referring now to the drawings, particularly to FIG. 1 there is illustrated a portion of a steam turbine, generally designated 10, including a rotor 12 mounting a plurality of turbine buckets 14. An inner casing 16 is also illustrated mounting a plurality of diaphragms 18. A centrally disposed generally radial steam inlet 20 applies steam to each of the turbine buckets and stator blades on opposite axial sides of the turbine to drive the rotor. The stator vanes of the diaphragms 18 and the axially adjacent buckets 14 form the various stages of the turbine forming a flow path and it will be appreciated that the steam is exhausted from the final stage of the turbine for flow into a condenser not shown.
  • Also illustrated in FIG. 1 is an outer exhaust hood 22 which surrounds and supports the inner casing of the turbine as well as other parts such as the bearings. In the illustration of FIG. 1, the turbine includes steam guides 24 for guiding the steam exhausting from the turbine into an outlet 26 for flow to one or more condensers. With the use of an exhaust hood supporting the turbine, bearings and ancillary parts, the exhaust steam path is tortuous and subject to pressure losses with consequent reduction in performance and efficiency.
  • Referring now to FIG. 2, there is illustrated an aspect of the present invention wherein like reference numerals as in FIG. 1 are applied to like parts preceded by the numeral 1. As illustrated, the exhaust hood 22 of the prior art is completely eliminated in favor of a volute diffuser 40. The diffuser 40 includes a diffusing conical section 42 coupled to the inner casing 116 by a flexible joint 44. The volute 40 has an axis parallel to the axis of rotation of the rotor 112. The axis of volute 40 is generally perpendicular to the direction of the general spiral flow about the axis and through the volute. Consequently, the exhaust steam flowing substantially in an axial direction from the final stage of the turbine flows into the volute 40 where it changes its flow direction by about 90°. Additionally, by using the volute 40, the geometry of the volute enables the steam to expand reducing its pressure. The volute 40 also guides the diffused steam through an outlet 46 coupled to one or more condensers, not shown. As illustrated in FIG. 3, the volute 40 includes an internal passage 48 which increases in cross-sectional area in a direction toward the outlet 46 thereby diffusing the exhaust steam. It will be appreciated that the exit or outlet 46 need not be a down exhaust but can be a side or upwardly directed exhaust. In either configuration, a single volute can exhaust a single flow steam turbine or a pair of volutes may exhaust steam from double flow steam turbines. In FIG. 4, a double walled volute is illustrated having a divider wall 50 forming a pair of diffuser exit passages.
  • Apart from the increased performance due to the diffusion of the steam in a volute on the steam exhaust side of the turbine, there are additional advantages. For example, the exhaust hood in prior conventional steam turbines is entirely eliminated and there is no longer a need to support the inner casing and associated steam path parts, such as diaphragms from the exhaust hood. Cost reduction is also realized because an exhaust hood is no longer used to enclose the inner casing. Also the overall dimensions of the turbine are reduced. Steam guides previously necessary are also entirely eliminated. Importantly, the inner casing and the volute of the turbine are each supported directly from the foundation of the turbine. To facilitate this, a flexible connection 44 (FIG. 2) is provided between the inner casing and the volute 40. The flexible connection may be of many different types such as an expansion bellows to allow for differential thermal expansion. Further, the previously utilized exhaust hood is no longer necessary for the support of the turbine bearings. As illustrated in FIG. 2, the bearings 54 may be supported on stanchions 56 in turn directly supported by the foundation of the turbine. Thus, the stanchions provide a rigid support for the bearings with improved turbine reliability as a result. The volute may be formed of a composite material, steel plate or pipe, structural steel, fiber-reinforced plastic or any combination of these materials to obtain the required structural integrity and desired steam flow diffusion characteristics.
  • While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.

Claims (7)

1. An axial flow steam turbine flow path comprising:
a rotor and a casing defining the axial steam flow path; and
an exhaust diffuser for the turbine including a volute for diffusing the exhaust steam and turning the exhaust steam from a generally axial flow direction to a generally transverse and tangential direction.
2. A flow path according to claim 1 wherein said volute has an axis generally parallel to an axis of the flow path.
3. A flow path according to claim 1 wherein said exhaust diffuser and said casing are independently mounted relative to one another on a foundation.
4. A flow path according to claim 1 including a flexible joint between said exhaust diffuser and said casing.
5. A flow path according to claim 1 wherein said volute has an axis generally parallel to an axis of the flow path, said volute terminating in an outlet facing in a downward, upward or transverse direction.
6. A flow path according to claim 1 wherein said volute has an axis generally parallel to an axis of the flow path, said exhaust diffuser and said casing being independently mounted relative to one another on a foundation.
7. A flow path according to claim 6 including a flexible joint between said exhaust diffuser and said casing.
US11/243,974 2005-10-06 2005-10-06 Steam turbine exhaust diffuser Abandoned US20070081892A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US11/243,974 US20070081892A1 (en) 2005-10-06 2005-10-06 Steam turbine exhaust diffuser
CNA2006101420320A CN1944962A (en) 2005-10-06 2006-09-30 Steam turbine exhaust diffuser
EP06255126A EP1772595A3 (en) 2005-10-06 2006-10-04 Steam turbine exhaust diffuser
JP2006273597A JP2007100701A (en) 2005-10-06 2006-10-05 Steam turbine exhaust diffuser

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/243,974 US20070081892A1 (en) 2005-10-06 2005-10-06 Steam turbine exhaust diffuser

Publications (1)

Publication Number Publication Date
US20070081892A1 true US20070081892A1 (en) 2007-04-12

Family

ID=37395898

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/243,974 Abandoned US20070081892A1 (en) 2005-10-06 2005-10-06 Steam turbine exhaust diffuser

Country Status (4)

Country Link
US (1) US20070081892A1 (en)
EP (1) EP1772595A3 (en)
JP (1) JP2007100701A (en)
CN (1) CN1944962A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080286099A1 (en) * 2007-05-17 2008-11-20 General Electric Company Steam turbine exhaust hood and method of fabricating the same
US20090191052A1 (en) * 2004-07-02 2009-07-30 Brian Haller Exhaust Gas Diffuser Wall Contouring
US20100162705A1 (en) * 2008-12-30 2010-07-01 Sharrow Edward J Methods, systems and/or apparatus relating to steam turbine exhaust diffusers
US20100251716A1 (en) * 2009-04-07 2010-10-07 General Electric Company Cooled exhaust hood plates for reduced exhaust loss
US20100303620A1 (en) * 2009-05-28 2010-12-02 General Electric Company Corrugated hood for low pressure steam turbine
US20100303619A1 (en) * 2009-05-28 2010-12-02 General Electric Company Shaped and stiffened lower exhaust hood sidewalls
US20110176917A1 (en) * 2004-07-02 2011-07-21 Brian Haller Exhaust Gas Diffuser Wall Contouring
US20120207595A1 (en) * 2011-02-11 2012-08-16 Alstom Technology Ltd Exhaust device for a steam turbine module
US20130094956A1 (en) * 2011-10-14 2013-04-18 General Electric Company Asymmetric butterfly plate for steam turbine exhaust hood
US8662821B2 (en) 2010-12-29 2014-03-04 General Electric Company Removable steam inlet assembly for steam turbine
US8668450B2 (en) 2010-12-29 2014-03-11 General Electric Company Removable upper steam guide segment for steam turbine
US9057287B2 (en) 2011-08-30 2015-06-16 General Electric Company Butterfly plate for a steam turbine exhaust hood
US20150267565A1 (en) * 2012-10-22 2015-09-24 Nuovo Pignone Srl Exhaust gas collector and gas turbine

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2295732A1 (en) * 2009-09-14 2011-03-16 Alstom Technology Ltd Axial turbine and method for discharging a flow from an axial turbine
CN102588016A (en) * 2011-01-05 2012-07-18 南阳汉冶特钢有限公司 Volute type symmetrical discharger
CN102434233B (en) * 2011-12-09 2014-05-28 青岛捷能汽轮机集团股份有限公司 Exhaust steam cylinder of miniature steam turbine
US20140119910A1 (en) * 2012-10-29 2014-05-01 General Electric Company Turbine exhaust hood and related method
EP3129608A1 (en) * 2014-04-10 2017-02-15 Siemens Aktiengesellschaft Gas turbine exhaust system

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1269998A (en) * 1915-02-01 1918-06-18 Westinghouse Electric & Mfg Co Steam-turbine.
US1781108A (en) * 1928-12-12 1930-11-11 Worthington Pump & Mach Corp Exhaust connection for condensers
US1814629A (en) * 1928-10-12 1931-07-14 Westinghouse Electric & Mfg Co Elastic fluid turbine
US2047501A (en) * 1934-05-03 1936-07-14 Spontan Ab Steam or gas turbine
US2781057A (en) * 1953-03-06 1957-02-12 Power Jets Res & Dev Ltd Turbine outlet ducting
US2840342A (en) * 1953-03-17 1958-06-24 David H Silvern Turbine exhaust
US4390319A (en) * 1979-09-25 1983-06-28 Garkusha Anatoly V Turbine exhaust hood
US5104286A (en) * 1991-02-08 1992-04-14 Westinghouse Electric Corp. Recirculation seal for a gas turbine exhaust diffuser
US6134876A (en) * 1997-11-26 2000-10-24 General Electric Company Gas turbine engine with exhaust expander and compressor
US6419448B1 (en) * 2000-03-20 2002-07-16 Jerzy A. Owczarek Flow by-pass system for use in steam turbine exhaust hoods

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB105933A (en) * 1916-02-04 1917-05-04 Karl Baumann Improvements in or relating to Steam Turbines.
US4961310A (en) * 1989-07-03 1990-10-09 General Electric Company Single shaft combined cycle turbine

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1269998A (en) * 1915-02-01 1918-06-18 Westinghouse Electric & Mfg Co Steam-turbine.
US1814629A (en) * 1928-10-12 1931-07-14 Westinghouse Electric & Mfg Co Elastic fluid turbine
US1781108A (en) * 1928-12-12 1930-11-11 Worthington Pump & Mach Corp Exhaust connection for condensers
US2047501A (en) * 1934-05-03 1936-07-14 Spontan Ab Steam or gas turbine
US2781057A (en) * 1953-03-06 1957-02-12 Power Jets Res & Dev Ltd Turbine outlet ducting
US2840342A (en) * 1953-03-17 1958-06-24 David H Silvern Turbine exhaust
US4390319A (en) * 1979-09-25 1983-06-28 Garkusha Anatoly V Turbine exhaust hood
US5104286A (en) * 1991-02-08 1992-04-14 Westinghouse Electric Corp. Recirculation seal for a gas turbine exhaust diffuser
US6134876A (en) * 1997-11-26 2000-10-24 General Electric Company Gas turbine engine with exhaust expander and compressor
US6419448B1 (en) * 2000-03-20 2002-07-16 Jerzy A. Owczarek Flow by-pass system for use in steam turbine exhaust hoods

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110176917A1 (en) * 2004-07-02 2011-07-21 Brian Haller Exhaust Gas Diffuser Wall Contouring
US20090191052A1 (en) * 2004-07-02 2009-07-30 Brian Haller Exhaust Gas Diffuser Wall Contouring
US7895840B2 (en) * 2004-07-02 2011-03-01 Siemens Aktiengesellschaft Exhaust gas diffuser wall contouring
US7785068B2 (en) * 2007-05-17 2010-08-31 General Electric Company Steam turbine exhaust hood and method of fabricating the same
US20080286099A1 (en) * 2007-05-17 2008-11-20 General Electric Company Steam turbine exhaust hood and method of fabricating the same
US20100162705A1 (en) * 2008-12-30 2010-07-01 Sharrow Edward J Methods, systems and/or apparatus relating to steam turbine exhaust diffusers
US20100251716A1 (en) * 2009-04-07 2010-10-07 General Electric Company Cooled exhaust hood plates for reduced exhaust loss
US8161749B2 (en) 2009-04-07 2012-04-24 General Electric Company Cooled exhaust hood plates for reduced exhaust loss
US8221054B2 (en) 2009-05-28 2012-07-17 General Electric Company Corrugated hood for low pressure steam turbine
US20100303619A1 (en) * 2009-05-28 2010-12-02 General Electric Company Shaped and stiffened lower exhaust hood sidewalls
US20100303620A1 (en) * 2009-05-28 2010-12-02 General Electric Company Corrugated hood for low pressure steam turbine
US8221053B2 (en) 2009-05-28 2012-07-17 General Electric Company Shaped and stiffened lower exhaust hood sidewalls
US8662821B2 (en) 2010-12-29 2014-03-04 General Electric Company Removable steam inlet assembly for steam turbine
US8668450B2 (en) 2010-12-29 2014-03-11 General Electric Company Removable upper steam guide segment for steam turbine
US20120207595A1 (en) * 2011-02-11 2012-08-16 Alstom Technology Ltd Exhaust device for a steam turbine module
US9243516B2 (en) * 2011-02-11 2016-01-26 Alstom Technology Ltd Exhaust device for a steam turbine module
US9057287B2 (en) 2011-08-30 2015-06-16 General Electric Company Butterfly plate for a steam turbine exhaust hood
RU2603227C2 (en) * 2011-08-30 2016-11-27 Дженерал Электрик Компани Rotary plate
US20130094956A1 (en) * 2011-10-14 2013-04-18 General Electric Company Asymmetric butterfly plate for steam turbine exhaust hood
US9062568B2 (en) * 2011-10-14 2015-06-23 General Electric Company Asymmetric butterfly plate for steam turbine exhaust hood
US20150267565A1 (en) * 2012-10-22 2015-09-24 Nuovo Pignone Srl Exhaust gas collector and gas turbine

Also Published As

Publication number Publication date
CN1944962A (en) 2007-04-11
JP2007100701A (en) 2007-04-19
EP1772595A3 (en) 2009-02-25
EP1772595A2 (en) 2007-04-11

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Legal Events

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AS Assignment

Owner name: GENERAL ELECTRIC COMPANY, NEW YORK

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SHARROW, EDWARD;REEL/FRAME:017076/0784

Effective date: 20051004

STCB Information on status: application discontinuation

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