NO975814L - Aksialturbin for en turbolader - Google Patents

Aksialturbin for en turbolader

Info

Publication number
NO975814L
NO975814L NO975814A NO975814A NO975814L NO 975814 L NO975814 L NO 975814L NO 975814 A NO975814 A NO 975814A NO 975814 A NO975814 A NO 975814A NO 975814 L NO975814 L NO 975814L
Authority
NO
Norway
Prior art keywords
nozzle
distance
point
turbocharger
axial turbine
Prior art date
Application number
NO975814A
Other languages
English (en)
Other versions
NO975814D0 (no
Inventor
Dominique Bochud
Markus Kohling
Jean Yves Werro
Original Assignee
Asea Brown Boveri
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 Asea Brown Boveri filed Critical Asea Brown Boveri
Publication of NO975814D0 publication Critical patent/NO975814D0/no
Publication of NO975814L publication Critical patent/NO975814L/no

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
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/04Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially axially
    • 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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/16Other safety measures for, or other control of, pumps
    • 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
    • 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
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/30Preventing corrosion or unwanted deposits in gas-swept spaces
    • 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
    • F05D2200/00Mathematical features
    • F05D2200/10Basic functions
    • F05D2200/13Product

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)

Abstract

Oppfinnelsens oppgave er å tilveiebringe en renseanordning for dyseringen og løpeskovlene av en turboladers aksialturbin, hvormed det oppnås en forbedret rensevirkning. Ifølge oppfinnelsen oppnås dette ved at renseanordningen består av bare en dyse (21, 44) med i det minste en innsprøytningsåpning (24) samt en rensemiddeltilførsel (23). Innsprøyt- ningsåpningen (24) er anordnet på et vilkårlig punkt (38) av en tenkt sirkelflate (34) , som på sin side defineres av et på en avstand (a) oppstrøms av den indre husvegg (11) anordnet midtpunkt (33) samt ved en diameter (dj . Midtpunktet (33) ligger på en i avstanden (a) til den indre husvegg (11) utformet, tenkt parallellflate (35). Avstanden (a) tilsvarer den med en prosentsats pj (5%^?! ^.30%) multiplisert midlere diameter av dyseringen (8) . Midtpunktet (33) ligger på et krysningspunkt (36) mellom parallell- flaten (35) og den strømlinje (17) som skjærer denne rettvinklet. Diameteren (dk) av sirkelflåten (34) er likeledes avhengig av dyseringens (8) midlere dia- meter, som multipliseres med en prosentsats p2 (0% Sp2^:6%) . Dysens (21, 44) innsprøytningsåpning (24) er i det minste innrettet tilnærmet parallelt med tangentialplanet (37).
NO975814A 1996-12-11 1997-12-10 Aksialturbin for en turbolader NO975814L (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19651318A DE19651318A1 (de) 1996-12-11 1996-12-11 Axialturbine eines Turboladers

Publications (2)

Publication Number Publication Date
NO975814D0 NO975814D0 (no) 1997-12-10
NO975814L true NO975814L (no) 1998-06-12

Family

ID=7814253

Family Applications (1)

Application Number Title Priority Date Filing Date
NO975814A NO975814L (no) 1996-12-11 1997-12-10 Aksialturbin for en turbolader

Country Status (9)

Country Link
US (1) US5938402A (no)
EP (1) EP0848150B1 (no)
JP (1) JP2929534B2 (no)
KR (1) KR100473472B1 (no)
CN (1) CN1089408C (no)
CZ (1) CZ292033B6 (no)
DE (2) DE19651318A1 (no)
NO (1) NO975814L (no)
PL (1) PL323551A1 (no)

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US6311704B1 (en) * 2000-03-03 2001-11-06 Hydrochem Industrial Services Methods and apparatus for chemically cleaning turbines
US8475636B2 (en) * 2008-11-07 2013-07-02 Novellus Systems, Inc. Method and apparatus for electroplating
US6712080B1 (en) * 2002-02-15 2004-03-30 The United States Of America As Represented By The Secretary Of The Army Flushing system for removing lubricant coking in gas turbine bearings
US6883527B2 (en) * 2002-07-24 2005-04-26 General Electric Company Method for robotically cleaning compressor blading of a turbine
SE522132C2 (sv) * 2002-12-13 2004-01-13 Gas Turbine Efficiency Ab Förfarande för rengöring av en stationär gasturbinenhet under drift
DE10355105A1 (de) * 2003-11-24 2005-06-02 Abb Turbo Systems Ag Reinigungsvorrichtung
US7703286B2 (en) * 2006-09-22 2010-04-27 Pratt & Whitney Canada Corp. Internal fuel manifold and fuel fairing interface
EP1627993A1 (de) * 2004-08-16 2006-02-22 ABB Turbo Systems AG Reinigungsvorrichtung für eine Abgasturbine
US7721546B2 (en) 2005-01-14 2010-05-25 Pratt & Whitney Canada Corp. Gas turbine internal manifold mounting arrangement
US20060156733A1 (en) * 2005-01-14 2006-07-20 Pratt & Whitney Canada Corp. Integral heater for fuel conveying member
US7540157B2 (en) 2005-06-14 2009-06-02 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
FI120211B (fi) * 2005-06-14 2009-07-31 Waertsilae Finland Oy Turbokompressorin turpiiniyksikkö ja menetelmä turbokompressorin turpiiniyksikön karstoittumisen estämiseksi
DE102005027890B4 (de) 2005-06-16 2007-05-03 Man Diesel Se Abgasturbolader für eine Brennkraftmaschine
DE102005028296B4 (de) * 2005-06-18 2007-03-29 Man Diesel Se Abgasturbolader für eine Brennkraftmaschine
EP1754862A1 (de) * 2005-08-17 2007-02-21 ABB Turbo Systems AG Verdichter, Verdichterrad, Reinigungsaufsatz und Abgasturbolader
FI117804B (fi) 2005-09-16 2007-02-28 Waertsilae Finland Oy Järjestely ja menetelmä turbokompressorilla varustetun mäntämoottorin yhteydessä
JP4650233B2 (ja) * 2005-11-24 2011-03-16 株式会社Ihi 過給機
ATE556276T1 (de) 2006-04-24 2012-05-15 Ebm Papst St Georgen Gmbh & Co Anordnung mit einem lüfter
US8353166B2 (en) 2006-08-18 2013-01-15 Pratt & Whitney Canada Corp. Gas turbine combustor and fuel manifold mounting arrangement
US20080053096A1 (en) * 2006-08-31 2008-03-06 Pratt & Whitney Canada Corp. Fuel injection system and method of assembly
US8033113B2 (en) * 2006-08-31 2011-10-11 Pratt & Whitney Canada Corp. Fuel injection system for a gas turbine engine
US7743612B2 (en) * 2006-09-22 2010-06-29 Pratt & Whitney Canada Corp. Internal fuel manifold and fuel inlet connection
US7926286B2 (en) * 2006-09-26 2011-04-19 Pratt & Whitney Canada Corp. Heat shield for a fuel manifold
US8171738B2 (en) * 2006-10-24 2012-05-08 Pratt & Whitney Canada Corp. Gas turbine internal manifold mounting arrangement
EP1972758A1 (de) * 2007-03-19 2008-09-24 ABB Turbo Systems AG Turbinenreinigung
DE502008000748D1 (de) * 2007-03-27 2010-07-15 Abb Turbo Systems Ag Reinigungsvorrichtung
US7856825B2 (en) * 2007-05-16 2010-12-28 Pratt & Whitney Canada Corp. Redundant mounting system for an internal fuel manifold
US8051664B2 (en) 2007-07-23 2011-11-08 Pratt & Whitney Canada Corp. Pre-loaded internal fuel manifold support
EP2071151A1 (en) * 2007-12-12 2009-06-17 Siemens Aktiengesellschaft Method for cleaning turbine blades under operation conditions, corresponding turbine and turbocharger
US8020381B2 (en) * 2007-12-18 2011-09-20 Detroit Diesel Corporation Method for determining necessity of multiple vane cleaning procedures
EP2116696A1 (en) 2008-05-07 2009-11-11 Napier Turbochargers Limited Method for cleaning a component of a turbocharger under operating conditions and turbine of a turbocharger
EP2123864A1 (de) * 2008-05-23 2009-11-25 ABB Turbo Systems AG Verdichterreinigung
US8303243B2 (en) * 2009-01-15 2012-11-06 Pratt & Whitney Canada Corp. Turbine wash port for a gas turbine engine
WO2010085494A1 (en) * 2009-01-20 2010-07-29 Williams International Co., L.L.C. Turbocharger with turbine nozzle cartridge
US8245952B2 (en) * 2009-02-20 2012-08-21 Pratt & Whitney Canada Corp. Compressor wash nozzle integrated in an inlet case strut
DE102011080596A1 (de) 2011-08-08 2013-02-14 Abb Turbo Systems Ag Anordnung für ein Leiten eines Abgases in einer axial angeströmten Abgasturbine
DE102011082089A1 (de) * 2011-09-02 2013-03-07 Abb Turbo Systems Ag Reinigungsvorrichtung einer Abgasturbine
DE102012211950A1 (de) 2012-07-09 2014-05-08 Abb Turbo Systems Ag Abgasturbine
EP2722495B1 (de) 2012-10-17 2015-03-11 ABB Turbo Systems AG Gaseintrittsgehäuse und zugehörige Abgasturbine
EP2781699B1 (de) * 2013-03-19 2018-05-02 ABB Turbo Systems AG Reinigungsvorrichtung einer Abgasturbine
US9951647B2 (en) * 2015-12-17 2018-04-24 General Electric Company System and method for in situ cleaning of internal components of a gas turbine engine and a related plug assembly
US10858990B2 (en) * 2016-10-07 2020-12-08 Dma Tech S.À R.L. Internal combustion steam engine
DE102017114608A1 (de) * 2017-06-30 2019-01-03 Man Diesel & Turbo Se Turbinenzuströmgehäuse einer Axialturbine eines Turboladers
CN109469548B (zh) * 2018-12-05 2024-07-19 神通科技集团股份有限公司 一种进气歧管除尘装置
CN112081654B (zh) * 2020-09-22 2021-03-19 广州雷易科技有限公司 一种汽车涡轮增压器
JP2023123967A (ja) 2022-02-25 2023-09-06 三菱重工コンプレッサ株式会社 弁装置、及び弁蓋

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Also Published As

Publication number Publication date
DE19651318A1 (de) 1998-06-18
KR19980063939A (ko) 1998-10-07
CZ292033B6 (cs) 2003-07-16
KR100473472B1 (ko) 2005-03-16
US5938402A (en) 1999-08-17
NO975814D0 (no) 1997-12-10
PL323551A1 (en) 1998-06-22
DE59711615D1 (de) 2004-06-17
CN1191276A (zh) 1998-08-26
JPH10176540A (ja) 1998-06-30
EP0848150A2 (de) 1998-06-17
JP2929534B2 (ja) 1999-08-03
EP0848150B1 (de) 2004-05-12
CN1089408C (zh) 2002-08-21
CZ393697A3 (cs) 1998-06-17
EP0848150A3 (de) 2000-03-22

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