BR112013023875A2 - método para o retroencaixe de uma turbina de vapor com fluxo duplo - Google Patents

método para o retroencaixe de uma turbina de vapor com fluxo duplo

Info

Publication number
BR112013023875A2
BR112013023875A2 BR112013023875A BR112013023875A BR112013023875A2 BR 112013023875 A2 BR112013023875 A2 BR 112013023875A2 BR 112013023875 A BR112013023875 A BR 112013023875A BR 112013023875 A BR112013023875 A BR 112013023875A BR 112013023875 A2 BR112013023875 A2 BR 112013023875A2
Authority
BR
Brazil
Prior art keywords
rotor
steam turbine
new
retrofitting
providing
Prior art date
Application number
BR112013023875A
Other languages
English (en)
Other versions
BR112013023875A8 (pt
Inventor
Andrew Martin Diesch
David Lloyd Bell
David Paul Blatchford
Suyog Sidram Ghodake
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=44627042&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=BR112013023875(A2) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Alstom Technology Ltd filed Critical Alstom Technology Ltd
Publication of BR112013023875A2 publication Critical patent/BR112013023875A2/pt
Publication of BR112013023875A8 publication Critical patent/BR112013023875A8/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
    • 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
    • F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
    • F01D3/02—Machines or engines with axial-thrust balancing effected by working-fluid characterised by having one fluid flow in one axial direction and another fluid flow in the opposite direction
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
    • F01D3/04—Machines or engines with axial-thrust balancing effected by working-fluid axial thrust being compensated by thrust-balancing dummy piston or the like
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005—Repairing methods or devices
    • 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
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

resumo patente de invenção: "método para o retroencaixe de uma turbina de vapor com fluxo duplo". a presente invenção refere-se a um método para o retroencaixe de uma turbina de vapor com fluxo duplo (1), o qual compreende: abrir um envoltório externo (21) da turbina de vapor (1), remover os transportadores de lâmina (5, 6) e as lâminas de estator (7, 8), remover o envoltório interno (11a) com correia interna (11b), remover o rotor com fluxo duplo (2) e as lâminas de rotor (3, 4). desse modo, o método compreende as etapas adicionais para prover um novo rotor de fluxo único (23) e novas lâminas de rotor (24) diferentes das lâminas de rotor (3, 4) conectadas ao rotor com fluxo duplo (2), prover balanceadores conectados ao rotor de fluxo único (23) para equilibrar a propulsão axial, prover novos transportadores de lâmina de estator (28) e novas lâminas de estator (29) diferentes das lâminas de estator (7, 8) associadas ao rotor com fluxo duplo (2), prover um novo envoltório interno (31a) com correia interna (31b), prover uma passagem (30) entre o envoltório interno (31a) e o envoltório externo (21), fechar o envoltório externo (21).
BR112013023875A 2011-03-18 2011-06-06 Método para o retroencaixe de uma turbina de vapor com fluxo duplo BR112013023875A8 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IN758DE2011 2011-03-18
PCT/EP2011/059245 WO2012126533A1 (en) 2011-03-18 2011-06-06 Method for retrofitting a double flow steam turbine

Publications (2)

Publication Number Publication Date
BR112013023875A2 true BR112013023875A2 (pt) 2016-12-13
BR112013023875A8 BR112013023875A8 (pt) 2018-04-03

Family

ID=44627042

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013023875A BR112013023875A8 (pt) 2011-03-18 2011-06-06 Método para o retroencaixe de uma turbina de vapor com fluxo duplo

Country Status (11)

Country Link
US (1) US9242316B2 (pt)
EP (1) EP2686521B1 (pt)
KR (1) KR101509439B1 (pt)
CN (1) CN103429849B (pt)
AU (1) AU2011362770B2 (pt)
BR (1) BR112013023875A8 (pt)
CA (1) CA2830059C (pt)
ES (1) ES2534296T3 (pt)
MX (1) MX337848B (pt)
WO (1) WO2012126533A1 (pt)
ZA (1) ZA201306687B (pt)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140119910A1 (en) * 2012-10-29 2014-05-01 General Electric Company Turbine exhaust hood and related method
US11225913B2 (en) * 2015-02-19 2022-01-18 Raytheon Technologies Corporation Method of providing turbine engines with different thrust ratings
CN110017174A (zh) * 2018-01-10 2019-07-16 长兴永能动力科技有限公司 一种并联双头分别排气式向心涡轮
CN112412548B (zh) * 2020-11-23 2021-12-31 东方电气集团东方汽轮机有限公司 一种汽轮机变工况下轴向推力的调整系统及其使用方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH499012A (de) * 1968-12-03 1970-11-15 Siemens Ag Anordnung zur axial festen und radial beweglichen Lagerung von Turbinengehäuseteilen
US4362464A (en) * 1980-08-22 1982-12-07 Westinghouse Electric Corp. Turbine cylinder-seal system
US5110256A (en) 1991-02-11 1992-05-05 Westinghouse Electric Corp. Methods and apparatus for attaching a flow guide to a steam turbine for retrofit of longer rotational blades
DE19700899A1 (de) * 1997-01-14 1998-07-23 Siemens Ag Dampfturbine
US6752589B2 (en) * 2002-10-15 2004-06-22 General Electric Company Method and apparatus for retrofitting a steam turbine and a retrofitted steam turbine
EP1624155A1 (de) * 2004-08-02 2006-02-08 Siemens Aktiengesellschaft Dampfturbine und Verfahren zum Betrieb einer Dampfturbine
BRPI0822015A2 (pt) * 2008-04-08 2015-07-21 Eriksson Dev And Innovation Ab Método para a conservação de um motor de turbina a gás para um motor de turbina com uma dispositivo de turbina de gás e vapor combinados, palheta de rotor de turbina, palheta de estator de turbina, dispositivo de turbina e método para regular um motor de turbina.

Also Published As

Publication number Publication date
ES2534296T3 (es) 2015-04-21
KR101509439B1 (ko) 2015-04-07
CA2830059C (en) 2015-08-04
CN103429849A (zh) 2013-12-04
AU2011362770B2 (en) 2015-06-11
KR20130135964A (ko) 2013-12-11
US20140013598A1 (en) 2014-01-16
US9242316B2 (en) 2016-01-26
MX337848B (es) 2016-03-22
EP2686521A1 (en) 2014-01-22
WO2012126533A1 (en) 2012-09-27
CA2830059A1 (en) 2012-09-27
CN103429849B (zh) 2015-08-12
MX2013010350A (es) 2014-03-27
EP2686521B1 (en) 2015-01-14
AU2011362770A1 (en) 2013-10-03
BR112013023875A8 (pt) 2018-04-03
ZA201306687B (en) 2014-11-26

Similar Documents

Publication Publication Date Title
BR112013023875A2 (pt) método para o retroencaixe de uma turbina de vapor com fluxo duplo
WO2013165515A3 (en) Gas turbine engine with fan-tied inducer section
BRPI0911341A2 (pt) rotor de compressor de uma turbomáquina e turbomáquina, tal como um turborreator ou um turbopropulsor de avião.
BR112016027042A8 (pt) pá de turbina de turbomáquina, meios de moldagem para a fabricação de uma pá, turbina de turbomáquina e turbomáquina
BR112015013455A2 (pt) máquina de rotação elétrica
WO2012064575A3 (en) Exhaust-gas turbocharger
EP2535519A3 (en) A retention device for a rotating blade
BR112012011535A2 (pt) montagem de uma agb em uma carcaça intermediária para um compartimento de ventilador de turbojato
WO2010106337A3 (en) Turbine assembly
FR2982635B1 (fr) Roue a aubes pour une turbomachine
BR112012020163A2 (pt) unidade de estator e tampa sinterizada e regulador de eixo de eixo de excêntricos.
BRPI0911686A2 (pt) rotor de compressor de uma turbomáquina e turbomáquina, tal como um turborreator ou um turbopropulsor de avião
IN2015MN00039A (pt)
CO6761363A2 (es) Masa de chocolate
BR112014012875A2 (pt) roda dentada para um estágio de roda dentada reta isenta de folga
BR112012028905A2 (pt) elemento aerodinâmico para uma nacela de aeronave e nacela de aeronave
BR112016024618A2 (pt) ?lâmina para uma turbina de turbomáquina de aeronave, turbina de turbomáquina de aeronave e turbomáquina de aeronave?
BR112015009250A2 (pt) conjunto de rotor de turbina
BR112013011988A2 (pt) separadora centrífuga, e, elemento de zona de alimentação para montagem em um corpo de núcleo de um transportador helicoidal
BR112015004983A2 (pt) rotor para turbomáquina de fluxo axial e porca dupla para conectar dois elementos de tirante
WO2011128551A3 (fr) Dispositif redresseur pour turbomachine
WO2016118208A3 (en) Turbopump machine with isolated cooling passage discharge
WO2013189943A3 (en) Centrifugal compressor impeller cooling
GB2498321A (en) Set of rotor discs for a turbomachine
WO2014186016A3 (en) Tie shaft flow trip

Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH (CH)

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 7A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]