ES2012654A6 - Barreras de flujo en cierres de laberinto para mejorar la estabilidad de rotores de turbinas de vapor. - Google Patents

Barreras de flujo en cierres de laberinto para mejorar la estabilidad de rotores de turbinas de vapor.

Info

Publication number
ES2012654A6
ES2012654A6 ES8900557A ES8900557A ES2012654A6 ES 2012654 A6 ES2012654 A6 ES 2012654A6 ES 8900557 A ES8900557 A ES 8900557A ES 8900557 A ES8900557 A ES 8900557A ES 2012654 A6 ES2012654 A6 ES 2012654A6
Authority
ES
Spain
Prior art keywords
labyrinth seals
swirl
preventing
flow
improve rotor
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.)
Expired - Lifetime
Application number
ES8900557A
Other languages
English (en)
Inventor
Albert F Lebreton
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of ES2012654A6 publication Critical patent/ES2012654A6/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/20Specially-shaped blade tips to seal space between tips and stator
    • 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
    • F16J15/44Free-space packings
    • F16J15/441Free-space packings with floating ring
    • F16J15/442Free-space packings with floating ring segmented

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)

Abstract

UN CIERRE DE LABERINTO PARA UNA TURBINA DE VAPOR QUE TIENE UN TRAMO ESTACIONARIO (18) DE FORMA ANULAR A TRAVES DEL CUAL PASA POR ZONAS CON PRESION DIFERENCIAL UN ARBOL GIRATORIO (10), COMPRENDE BARRERAS DE FLUJO (26) SITUADAS PERPENDICULARMENTE CON RESPECTO A UNA PLURALIDAD DE DIENTES ANULARES (20) ESPACIADOS, QUE SE EXTIENDEN RADIALMENTE HACIA ADENTRO DESDE EL TRAMO ESTACIONARIO (18) HACIA EL ARBOL (10) DE FORMA QUE BLOQUEAN EL FLUJO CIRCUNFERENCIAL DE VAPOR, EVITANDO ASI QUE SE INDUZCA TURBULENCIA.
ES8900557A 1988-02-18 1989-02-16 Barreras de flujo en cierres de laberinto para mejorar la estabilidad de rotores de turbinas de vapor. Expired - Lifetime ES2012654A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/157,552 US4979755A (en) 1988-02-18 1988-02-18 Flow dams in labyrinth seals to improve rotor stability

Publications (1)

Publication Number Publication Date
ES2012654A6 true ES2012654A6 (es) 1990-04-01

Family

ID=22564235

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8900557A Expired - Lifetime ES2012654A6 (es) 1988-02-18 1989-02-16 Barreras de flujo en cierres de laberinto para mejorar la estabilidad de rotores de turbinas de vapor.

Country Status (7)

Country Link
US (1) US4979755A (es)
JP (1) JP2877827B2 (es)
KR (1) KR960004212B1 (es)
CN (1) CN1015484B (es)
CA (1) CA1317613C (es)
ES (1) ES2012654A6 (es)
IT (1) IT1233535B (es)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5197281A (en) * 1990-04-03 1993-03-30 General Electric Company Interstage seal arrangement for airfoil stages of turbine engine counterrotating rotors
US5080556A (en) * 1990-09-28 1992-01-14 General Electric Company Thermal seal for a gas turbine spacer disc
US5211535A (en) * 1991-12-30 1993-05-18 General Electric Company Labyrinth seals for gas turbine engine
US5707064A (en) * 1993-01-08 1998-01-13 The Texas A&M University System Modulated pressure damper seal
CA2152789C (en) * 1993-01-08 2003-07-29 Richard R. Shultz Pressure damper seals
US5794942A (en) * 1993-01-08 1998-08-18 The Texas A&M University System Modulated pressure damper seals
US5439347A (en) * 1994-08-31 1995-08-08 Brandon; Ronald E. Turbine tip seal damage protection means
US5599026A (en) * 1995-09-06 1997-02-04 Innovative Technology, L.L.C. Turbine seal with sealing strip and rubbing strip
US5961279A (en) * 1996-05-31 1999-10-05 Atlantic Richfield Company Turbine power plant having minimal-contact brush seal augmented labyrinth seal
US6273426B1 (en) * 1999-07-22 2001-08-14 Avaya Technology Corp. Hydrodynamic seal and a method for providing the same
US6226975B1 (en) 1999-09-14 2001-05-08 Steven G. Ingistov Turbine power plant having a floating brush seal
US6612809B2 (en) * 2001-11-28 2003-09-02 General Electric Company Thermally compliant discourager seal
CN1294340C (zh) * 2002-10-30 2007-01-10 东方汽轮机厂 铁素体镶齿汽封圈加工方法
WO2004113770A2 (en) * 2003-06-20 2004-12-29 Elliott Company Swirl-reversal abradable labyrinth seal
JP2007521442A (ja) * 2003-08-26 2007-08-02 ゼネラル・エレクトリック・カンパニイ 回転機械用シールキャリヤおよび改装方法
US7004475B2 (en) * 2003-09-26 2006-02-28 Siemens Westinghouse Power Corporation Flow dam design for labyrinth seals to promote rotor stability
US20070120329A1 (en) * 2005-11-29 2007-05-31 Chevrette Richard J Apparatus and method for steam turbine variable clearance packing
US7631879B2 (en) * 2006-06-21 2009-12-15 General Electric Company “L” butt gap seal between segments in seal assemblies
EP2249066A1 (en) * 2009-05-07 2010-11-10 Siemens Aktiengesellschaft Sealing apparatus and method for steam turbines
US9074486B2 (en) * 2011-01-31 2015-07-07 General Electric Company Method and apparatus for labyrinth seal packing ring
DE102013003401A1 (de) * 2013-02-28 2014-08-28 Klinger Ag Flachdichtung für Flanschverbindungen
US10100672B2 (en) * 2013-03-08 2018-10-16 United Technologies Corporation Fluid-cooled seal arrangement for a gas turbine engine
US9574453B2 (en) * 2014-01-02 2017-02-21 General Electric Company Steam turbine and methods of assembling the same
CN105673862A (zh) * 2016-03-24 2016-06-15 国家电网公司 周向刷式挡片气封
JP7029339B2 (ja) * 2018-04-04 2022-03-03 株式会社東芝 シール装置
CN112610287A (zh) * 2020-12-29 2021-04-06 中国神华能源股份有限公司国华电力分公司 一种高压汽轮机叶顶汽封结构

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4370094A (en) * 1974-03-21 1983-01-25 Maschinenfabrik Augsburg-Nurnberg Aktiengesellschaft Method of and device for avoiding rotor instability to enhance dynamic power limit of turbines and compressors
US4273510A (en) * 1974-03-21 1981-06-16 Maschinenfabrik Augsburg-Nunberg Aktiengesellschaft Method of and device for avoiding rotor instability to enhance dynamic power limit of turbines and compressors
US4114059A (en) * 1976-09-03 1978-09-12 Westinghouse Electric Corp. Grooved visco seal for stationary discharge chamber of water-cooled turbine generator
US4257617A (en) * 1978-11-06 1981-03-24 Carrier Corporation Shaft seal assembly
JPS5838666A (ja) * 1981-08-31 1983-03-07 Mitsubishi Electric Corp 正極性ア−ク溶接装置
US4436311A (en) * 1982-04-20 1984-03-13 Brandon Ronald E Segmented labyrinth-type shaft sealing system for fluid turbines
US4420161A (en) * 1982-05-10 1983-12-13 General Electric Company Rotor stabilizing labyrinth seals for steam turbines
JPS59505A (ja) * 1982-06-28 1984-01-05 Toshiba Corp 蒸気タ−ビン

Also Published As

Publication number Publication date
CN1015484B (zh) 1992-02-12
CA1317613C (en) 1993-05-11
KR890013311A (ko) 1989-09-22
KR960004212B1 (ko) 1996-03-28
CN1035544A (zh) 1989-09-13
US4979755A (en) 1990-12-25
JP2877827B2 (ja) 1999-04-05
IT1233535B (it) 1992-04-03
JPH01247702A (ja) 1989-10-03
IT8941521A0 (it) 1989-02-15

Similar Documents

Publication Publication Date Title
ES2012654A6 (es) Barreras de flujo en cierres de laberinto para mejorar la estabilidad de rotores de turbinas de vapor.
SE8008936L (sv) Turbinledskovelupphengning for gasturbinmotorer
GB1410658A (en) Turbomachinery rotors
EP0940562A3 (en) Gas turbine
GB1523668A (en) Turbomachinery stator assembly
ES8401567A1 (es) Perfeccionamientos en una turbina de vapor con admision axial.
GB1291302A (en) Improvements in bladed rotor assemblies
GB1306575A (en) Segmented seal assembly for axial flow turbines
GB1484936A (en) Gas turbine engines
MY101134A (en) Centrifugal seal.
GB1241358A (en) Static seal structure
GB1109457A (en) Segmented diaphragm assembly for turbines
GB1125920A (en) Turbomachine rotors
KR900018507A (ko) 터빈 베인 보호판 밀봉 시스템
GB1344221A (en) Vane rings
ES2046932A1 (es) Guia totalmente flotante de flujo de admision para turbinas de vapor de baja presion de flujo doble.
KR900006639A (ko) 축류 증기 터어빈
FR2324873A1 (fr) Perfectionnements aux flasques de rotors de turbomachines
GB847242A (en) Improvements in or relating to radial flow gas turbines
ES2005730A6 (es) Bomba de canales laterales.
GB1385666A (en) Sealing of vaned assemblies of gas turbine engines
GB1058759A (en) Improvements in or relating to the bladed diaphragms of turbines
GB1534660A (en) Sealing arrangement in a gas turbine
GB1236366A (en) Elastic fluid machine
GB1524969A (en) Stator vane assembly

Legal Events

Date Code Title Description
SA6 Expiration date (snapshot 920101)

Free format text: 2009-02-16

FD1A Patent lapsed

Effective date: 19980504