ES2159349T3 - Procedimiento y dispositivo para la limpieza en humedo de los anillos de toberas de una turbina de turbocompresor de gases de escape. - Google Patents

Procedimiento y dispositivo para la limpieza en humedo de los anillos de toberas de una turbina de turbocompresor de gases de escape.

Info

Publication number
ES2159349T3
ES2159349T3 ES96810822T ES96810822T ES2159349T3 ES 2159349 T3 ES2159349 T3 ES 2159349T3 ES 96810822 T ES96810822 T ES 96810822T ES 96810822 T ES96810822 T ES 96810822T ES 2159349 T3 ES2159349 T3 ES 2159349T3
Authority
ES
Spain
Prior art keywords
turbine
housing
exhaust gas
running wheel
turbocompresor
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
ES96810822T
Other languages
English (en)
Inventor
Andre Beck
Dieter Haberle
Johann Kronthaler
Gavin John Menzies
Dirk Dr Telschow
Jonas Zumbrunn
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.)
Accelleron Industries AG
Original Assignee
ABB Turbo Systems AG
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 ABB Turbo Systems AG filed Critical ABB Turbo Systems AG
Application granted granted Critical
Publication of ES2159349T3 publication Critical patent/ES2159349T3/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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/002Cleaning of turbomachines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B77/00Component parts, details or accessories, not otherwise provided for
    • F02B77/04Cleaning of, preventing corrosion or erosion in, or preventing unwanted deposits in, combustion engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/10Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant
    • F02C6/12Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)

Abstract

EL OBJETIVO DE LA INVENCION ES CONSEGUIR UN PROCEDIMIENTO PARA LIMPIEZA HUMEDA DEL ANILLO DE TOBERAS DE TURBINAS DE TURBOCOMPRESOR, CON EL CUAL A PESAR DE LA UTILIZACION DE CANTIDAD DE AGUA REDUCIDA SE CONSIGUE UN EFECTO DE LIMPIEZA MEJORADO. PUEDE REDUCIRSE ADEMAS LA POTENCIA DEL MOTOR DE COMBUSTION INTERNA DESDE EL PRINCIPIO DEL PROCESO DE LIMPIEZA EN UNA CANTIDAD MENOR QUE LA CONOCIDA HASTA AHORA Y DEBE ELEVARSE POR TANTO LA SEGURIDAD DE FUNCIONAMIENTO DEL TURBOCOMPRESOR. DE ACUERDO CON LA INVENCION ESTO SE CONSIGUE DE TAL MODO, QUE DESPUES DE LA DETERMINACION DE LA NECESIDAD DE LIMPIEZA SE DISPARA UN CICLO DE LIMPIEZA QUE SE DESARROLLA DE FORMA AUTOMATICA, DONDE EL AGUA (37) SE INYECTA MULTIPLES VECES EN UN TIEMPO CORTO EN LA ZONA DELANTERA DEL ANILLO (7) DE TOBERAS Y SE MANTIENE UNA PAUSA DE INYECCION ENTRE LOS PROCESOS DE INYECCION PARA CALENTAMIENTO DE NUEVO DEL ANILLO (7) DE TOBERAS.
ES96810822T 1995-12-29 1996-11-25 Procedimiento y dispositivo para la limpieza en humedo de los anillos de toberas de una turbina de turbocompresor de gases de escape. Expired - Lifetime ES2159349T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19549142A DE19549142A1 (de) 1995-12-29 1995-12-29 Verfahren und Vorrichtung zur Nassreinigung des Düsenrings einer Abgasturbolader-Turbine

Publications (1)

Publication Number Publication Date
ES2159349T3 true ES2159349T3 (es) 2001-10-01

Family

ID=7781644

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96810822T Expired - Lifetime ES2159349T3 (es) 1995-12-29 1996-11-25 Procedimiento y dispositivo para la limpieza en humedo de los anillos de toberas de una turbina de turbocompresor de gases de escape.

Country Status (13)

Country Link
US (1) US5944483A (es)
EP (1) EP0781897B1 (es)
JP (1) JP3051352B2 (es)
KR (1) KR100354689B1 (es)
CN (1) CN1079895C (es)
AT (1) ATE201481T1 (es)
CZ (1) CZ290308B6 (es)
DE (2) DE19549142A1 (es)
DK (1) DK0781897T3 (es)
ES (1) ES2159349T3 (es)
NO (1) NO312166B1 (es)
PL (1) PL182202B1 (es)
RU (1) RU2178531C2 (es)

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US8858720B2 (en) * 2008-12-09 2014-10-14 Chevron Belgium Nv Method for cleaning deposits from turbocharger and supercharger compressors
US8303243B2 (en) * 2009-01-15 2012-11-06 Pratt & Whitney Canada Corp. Turbine wash port for a gas turbine engine
US8245952B2 (en) * 2009-02-20 2012-08-21 Pratt & Whitney Canada Corp. Compressor wash nozzle integrated in an inlet case strut
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US8602721B2 (en) 2009-12-02 2013-12-10 Wartsila Finland Oy Method of operating turbocharged piston engine
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Also Published As

Publication number Publication date
NO965423L (no) 1997-06-30
KR100354689B1 (ko) 2002-11-18
PL317600A1 (en) 1997-07-07
EP0781897A3 (de) 1999-04-21
EP0781897A2 (de) 1997-07-02
EP0781897B1 (de) 2001-05-23
PL182202B1 (pl) 2001-11-30
ATE201481T1 (de) 2001-06-15
CN1079895C (zh) 2002-02-27
DK0781897T3 (da) 2001-09-10
RU2178531C2 (ru) 2002-01-20
JP3051352B2 (ja) 2000-06-12
US5944483A (en) 1999-08-31
NO965423D0 (no) 1996-12-17
JPH09222025A (ja) 1997-08-26
DE59606953D1 (de) 2001-06-28
DE19549142A1 (de) 1997-07-03
NO312166B1 (no) 2002-04-02
CN1157370A (zh) 1997-08-20
CZ373996A3 (en) 1997-08-13
CZ290308B6 (cs) 2002-07-17
KR970044598A (ko) 1997-07-26

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