IN2014DN07620A - - Google Patents

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Publication number
IN2014DN07620A
IN2014DN07620A IN7620DEN2014A IN2014DN07620A IN 2014DN07620 A IN2014DN07620 A IN 2014DN07620A IN 7620DEN2014 A IN7620DEN2014 A IN 7620DEN2014A IN 2014DN07620 A IN2014DN07620 A IN 2014DN07620A
Authority
IN
India
Prior art keywords
exhaust hood
bulkhead
flanges
gasket
radially
Prior art date
Application number
Inventor
Julien Roge
Jerome Lamaque
Xavier Laurent
Original Assignee
Alstom Technology Ltd
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 Alstom Technology Ltd filed Critical Alstom Technology Ltd
Publication of IN2014DN07620A publication Critical patent/IN2014DN07620A/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • 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
    • 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
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/02Sealings between relatively-stationary surfaces
    • F16J15/021Sealings between relatively-stationary surfaces with elastic packing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/55Seals
    • F05D2240/57Leaf seals
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/02Sealings between relatively-stationary surfaces

Landscapes

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

Abstract

A seal arrangement is installed between confronting co-planar portions of a low pressure steam turbine exhaust hood (2) and a circular bulkhead (16) that forms part of an exhaust duct structure (lOB) of a steam turbine module (I). The seal arrangement forms a vacuum seal between the interior and exterior of the exhaust hood and comprises a flexible gasket (18) in the form of an annular diaphragm. This diaphragm has a radially inner circumferential portion (30) that seals with the bulkhead (16), a radially outer circumferential portion (32) that seals with the exhaust hood (2), and a radially median resilient portion (34). Sealing is achieved by providing radially inner and outer clamping flanges (36, 38) operative to sealingly clamp inner and outer circumferential portions (30, 32) of the gasket (18) to the bulkhead (16) and the exhaust hood (2) respectively. To enable quick access to the interior of the exhaust hood (2), the clamping flanges comprise upper and lower halves and the upper part of the gasket (18) is sealed to the upper parts of the exhaust hood (2AU) and the bulkhead (16U) by an arrangement of flanges (36, 38) and counter-flanges (40, 42), the counter-flanges being releasably secured to outside surfaces of the exhaust hood and the bulkhead.
IN7620DEN2014 2012-03-20 2013-03-19 IN2014DN07620A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP12290096 2012-03-20
PCT/EP2013/055676 WO2013139782A1 (en) 2012-03-20 2013-03-19 Low pressure steam turbine seal arrangement

Publications (1)

Publication Number Publication Date
IN2014DN07620A true IN2014DN07620A (en) 2015-05-15

Family

ID=47891752

Family Applications (1)

Application Number Title Priority Date Filing Date
IN7620DEN2014 IN2014DN07620A (en) 2012-03-20 2013-03-19

Country Status (6)

Country Link
US (1) US9291068B2 (en)
EP (1) EP2828487B1 (en)
CN (1) CN104204415B (en)
IN (1) IN2014DN07620A (en)
RU (1) RU2624086C2 (en)
WO (1) WO2013139782A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10113560B2 (en) * 2013-06-20 2018-10-30 Mitsubishi Hitachi Power Systems, Ltd. Gas guiding device and facility including the same
DE102014224419A1 (en) * 2014-11-28 2016-06-02 Siemens Aktiengesellschaft Turbine housing arrangement, in particular with an outer housing part and a Abdampfgehäusenteil a steam turbine, and use thereof
US10451362B2 (en) 2016-10-14 2019-10-22 Dana Canada Corporation Heat exchanger having bypass seal with retention clip
JP6694837B2 (en) * 2017-02-27 2020-05-20 三菱日立パワーシステムズ株式会社 Steam turbine
US10392967B2 (en) * 2017-11-13 2019-08-27 General Electric Company Compliant seal component and associated method
US10570781B2 (en) * 2018-03-15 2020-02-25 General Electric Technology Gmbh Connection system for condenser and steam turbine and methods of assembling the same
FR3080144B1 (en) * 2018-04-12 2020-03-20 Safran Aircraft Engines DEVICE FOR MASKING AN INTERIOR SURROUNDING OF A TURBOMACHINE DISC
RU196772U1 (en) * 2020-01-21 2020-03-16 Акционерное общество "Уральский турбинный завод" Sealing the cylinder bodies of the steam turbine
CN111608747B (en) * 2020-04-07 2022-05-10 东方电气集团东方汽轮机有限公司 Short-span steam turbine rotor supporting structure and steam turbine rotor support mounting method
KR20230127497A (en) * 2022-02-25 2023-09-01 두산에너빌리티 주식회사 Air inlet manifold and gas turbine including the same

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3313517A (en) * 1965-04-01 1967-04-11 Worthington Corp Gas expander turbines for power recovery use with jet type, hot gas generators
DK128331B (en) * 1968-01-22 1974-04-08 Bbc Brown Boveri & Cie Waste steam house for the low pressure part of a steam turbine.
DE2200447A1 (en) * 1971-01-13 1972-12-07 Creusot Loire Low-pressure turbine sections of steam turbines
FR2651276B1 (en) * 1989-08-28 1991-10-25 Alsthom Gec CONCRETE CONDENSER FOR TURBINE WITH AXIAL EXHAUST AND TURBINE PROVIDED WITH SUCH A CONDENSER.
US5104286A (en) * 1991-02-08 1992-04-14 Westinghouse Electric Corp. Recirculation seal for a gas turbine exhaust diffuser
DE19523923C2 (en) * 1995-06-30 2003-09-18 Alstom Low-pressure steam turbine
GB2335470B (en) * 1998-03-18 2002-02-13 Rolls Royce Plc A seal
JP4088368B2 (en) * 1998-06-04 2008-05-21 三菱重工業株式会社 Gland deformation prevention structure of low-pressure steam turbine
RU23315U1 (en) * 2002-01-08 2002-06-10 Акционерное общество открытого типа "Ленинградский Металлический завод" END SEAL OF LOW PRESSURE CYLINDER FOR STEAM TURBINE
JP2006312885A (en) * 2005-05-06 2006-11-16 Mitsubishi Heavy Ind Ltd Structure of low pressure steam turbine
JP4991600B2 (en) * 2008-02-29 2012-08-01 株式会社東芝 Steam turbine
US8359866B2 (en) * 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
CN103635707B (en) * 2011-04-05 2016-05-11 蒂森克虏伯罗特艾德有限公司 Oil lubrication anti-friction bearing

Also Published As

Publication number Publication date
WO2013139782A1 (en) 2013-09-26
EP2828487B1 (en) 2017-12-06
RU2014142064A (en) 2016-05-20
US20150001814A1 (en) 2015-01-01
EP2828487A1 (en) 2015-01-28
CN104204415B (en) 2016-11-16
RU2624086C2 (en) 2017-06-30
CN104204415A (en) 2014-12-10
US9291068B2 (en) 2016-03-22

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