ES2014630A6 - Sistema y metodo para vigilar la holgura entre una pluralidad de segmentos de envuelta ade alabe y una parte estacionaria de una turbina. - Google Patents

Sistema y metodo para vigilar la holgura entre una pluralidad de segmentos de envuelta ade alabe y una parte estacionaria de una turbina.

Info

Publication number
ES2014630A6
ES2014630A6 ES8901749A ES8901749A ES2014630A6 ES 2014630 A6 ES2014630 A6 ES 2014630A6 ES 8901749 A ES8901749 A ES 8901749A ES 8901749 A ES8901749 A ES 8901749A ES 2014630 A6 ES2014630 A6 ES 2014630A6
Authority
ES
Spain
Prior art keywords
clearance
shroud
steam turbine
turbine shroud
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.)
Expired - Lifetime
Application number
ES8901749A
Other languages
English (en)
Inventor
Robert Lee Osborne
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 ES2014630A6 publication Critical patent/ES2014630A6/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/14Measuring arrangements characterised by the use of electric or magnetic techniques for measuring distance or clearance between spaced objects or spaced apertures
    • 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
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)

Abstract

SISTEMA Y METODO PARA VIGILAR LA HOLGURA ENTRE UNA PLURALIDAD DE SEGMENTOS DE ENVUELTA DE ALABE Y UNA PARTE ESTACIONARIA DE UNA TURBINA, QUE COMPRENDEN UNA PLURALIDAD DE PERCEPTORES PARA EFECTUAR VARIAS MEDICIONES DE LA HOLGURA ENTRE LA PARTE ESTACIONARIA DE LA TURBINA Y LOS SEGMENTOS DE ENVUELTA EN CADA FILA DE ALABES DE TURBINA. LAS MEDICIONES SON PROMEDIADAS POR UN MICROORDENADOR PARA OBTENER UN VALOR MEDIO DE LA HOLGURA PARA CADA SEGMENTO DE ENVUELTA. EL MICROORDENADOR ANALIZA ENTONCES LOS VALORES DE HOLGURA MEDIA PARA CADA SEGMENTO DE ENVUELTA, PARA DETERMINAR SI, Y CUANDO, LA HOLGURA ENTRE UN SEGMENTO DE ENVUELTA Y LA PARTE ESTACIONARIA DE LA TURBINA ESTA PROXIMA A UN VALOR CRITICO. SE GENERA ENTONCES UNA RESPUESTA DE SALIDA AL ANALISIS ANTERIOR PARA SEÑALAR UNA CONDICION CRITICA.
ES8901749A 1988-05-27 1989-05-24 Sistema y metodo para vigilar la holgura entre una pluralidad de segmentos de envuelta ade alabe y una parte estacionaria de una turbina. Expired - Lifetime ES2014630A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/199,633 US4876505A (en) 1988-05-27 1988-05-27 Apparatus and method for monitoring steam turbine shroud clearance

Publications (1)

Publication Number Publication Date
ES2014630A6 true ES2014630A6 (es) 1990-07-16

Family

ID=22738377

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8901749A Expired - Lifetime ES2014630A6 (es) 1988-05-27 1989-05-24 Sistema y metodo para vigilar la holgura entre una pluralidad de segmentos de envuelta ade alabe y una parte estacionaria de una turbina.

Country Status (7)

Country Link
US (1) US4876505A (es)
JP (1) JP2736345B2 (es)
KR (1) KR0121796B1 (es)
CN (1) CN1020781C (es)
CA (1) CA1329846C (es)
ES (1) ES2014630A6 (es)
IT (1) IT1233528B (es)

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US7025559B2 (en) * 2004-06-04 2006-04-11 General Electric Company Methods and systems for operating rotary machines
DE602005022462D1 (de) * 2004-09-20 2010-09-02 Ltb4 Sweden Ab Stabilisiertes leukotrien b4 (ltb4) pharmazeutikum
US7075296B2 (en) * 2004-11-09 2006-07-11 Siemens Power Generation, Inc. Inspection carriage for turbine blades
US7722310B2 (en) * 2004-12-17 2010-05-25 General Electric Company System and method for measuring clearance between two objects
US7333913B2 (en) * 2005-06-27 2008-02-19 General Electric Company Clearance measurement system and method of operation
US7455495B2 (en) * 2005-08-16 2008-11-25 United Technologies Corporation Systems and methods for monitoring thermal growth and controlling clearances, and maintaining health of turbo machinery applications
GB0621620D0 (en) * 2006-10-31 2006-12-06 Rolls Royce Plc A sensor
CN100437015C (zh) * 2006-11-10 2008-11-26 东北电力大学 汽轮机通流间隙变化在线监测方法
US7762153B2 (en) * 2007-05-31 2010-07-27 General Electric Company Method and systems for measuring blade deformation in turbines
US20090142194A1 (en) * 2007-11-30 2009-06-04 General Electric Company Method and systems for measuring blade deformation in turbines
US8593296B2 (en) * 2010-10-19 2013-11-26 General Electric Company System and method for turbine bucket tip shroud deflection measurement
US8684669B2 (en) 2011-02-15 2014-04-01 Siemens Energy, Inc. Turbine tip clearance measurement
EP2505779B1 (en) * 2011-03-28 2018-05-23 General Electric Company Method and system for inspecting blade tip clearance
US9037434B2 (en) * 2012-01-03 2015-05-19 General Electric Company Method and apparatus for obtaining discrete axial clearance data using radial clearance sensors
US9400171B2 (en) 2012-04-05 2016-07-26 Siemens Energy, Inc. Optical wear monitoring
US9395171B2 (en) 2012-11-05 2016-07-19 Siemens Energy, Inc. Capacitive sensor with orthogonal fields
WO2014162767A1 (ja) * 2013-04-03 2014-10-09 三菱重工業株式会社 回転機械
EP2806110A1 (de) * 2013-05-22 2014-11-26 MTU Aero Engines GmbH Turbomaschinenstufe und Verfahren zum Ermitteln eines Dichtungsspalts einer solchen Turbomaschinenstufe
EP2821593A1 (en) 2013-07-04 2015-01-07 Alstom Technology Ltd Method and apparatus for controlling a steam turbine axial clearance
US9476318B2 (en) 2013-09-03 2016-10-25 General Electric Company Systems and methods to monitor a rotating component
US20150075265A1 (en) * 2013-09-17 2015-03-19 General Electric Company Measurement device and method for evaluating turbomachine clearances
KR101608130B1 (ko) 2014-01-14 2016-03-31 두산중공업 주식회사 블레이드 팁 간극 조절 수단을 구비한 가스 터빈 및 그 제어방법
GB2523474A (en) * 2014-02-19 2015-08-26 Vibrosystm Inc Real time monitoring of rotor or stator shape change for rotating machines
EP3141706A1 (en) 2015-09-09 2017-03-15 General Electric Technology GmbH Steam turbine stage measurement system and a method therefor
CN105317471A (zh) * 2015-11-26 2016-02-10 华电电力科学研究院 汽轮机汽封间隙调整方法
CN105484807B (zh) * 2016-01-27 2017-02-22 国家电投集团河南电力检修工程有限公司 汽轮机汽封间隙精密高效调整工艺系统
CN115223313B (zh) * 2022-07-15 2023-06-20 天津成成电气设备有限公司 一种配电柜监控预警方法、装置、电子设备及介质

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Also Published As

Publication number Publication date
CN1038333A (zh) 1989-12-27
JP2736345B2 (ja) 1998-04-02
CN1020781C (zh) 1993-05-19
CA1329846C (en) 1994-05-24
IT1233528B (it) 1992-04-03
KR0121796B1 (ko) 1997-11-19
IT8941607A0 (it) 1989-05-26
JPH0223205A (ja) 1990-01-25
KR890017519A (ko) 1989-12-16
US4876505A (en) 1989-10-24

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19980401