NO975814L - Aksialturbin for en turbolader - Google Patents
Aksialturbin for en turboladerInfo
- 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
Links
- 238000004140 cleaning Methods 0.000 abstract 3
- 238000002347 injection Methods 0.000 abstract 2
- 239000007924 injection Substances 0.000 abstract 2
- 239000012459 cleaning agent Substances 0.000 abstract 1
- 230000001419 dependent effect Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
- 238000011144 upstream manufacturing Methods 0.000 abstract 1
Classifications
-
- 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
- F01D25/002—Cleaning of turbomachines
-
- 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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-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
- F01D1/04—Non-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
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/16—Other safety measures for, or other control of, pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/04—Cleaning of, preventing corrosion or erosion in, or preventing unwanted deposits in, combustion engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/10—Gas-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
- F02C6/12—Turbochargers, i.e. plants for augmenting mechanical power output of internal-combustion piston engines by increase of charge pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, 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
- F02C7/30—Preventing corrosion or unwanted deposits in gas-swept spaces
-
- 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
- F05D2200/00—Mathematical features
- F05D2200/10—Basic functions
- F05D2200/13—Product
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).
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) |
Families Citing this family (47)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6394108B1 (en) * | 1999-06-29 | 2002-05-28 | John Jeffrey Butler | Inside out gas turbine cleaning method |
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 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3623668A (en) * | 1968-03-04 | 1971-11-30 | Gen Electric | Wash manifold |
US3913845A (en) * | 1972-12-31 | 1975-10-21 | Ishikawajima Harima Heavy Ind | Multihole fuel injection nozzle |
US4196020A (en) * | 1978-11-15 | 1980-04-01 | Avco Corporation | Removable wash spray apparatus for gas turbine engine |
JPS59190428A (ja) * | 1983-04-12 | 1984-10-29 | Mitsubishi Heavy Ind Ltd | ガスタ−ビン車室の洗浄方法 |
US4548040A (en) * | 1984-05-11 | 1985-10-22 | Elliott Turbomachinery Company, Inc. | Method and apparatus for determining when to initiate cleaning of turbocharger turbine blades |
SU1214222A1 (ru) * | 1984-10-08 | 1986-02-28 | Центральный научно-исследовательский и проектно-конструкторский институт профилактики пневмокониозов и техники безопасности | Плоскофакельный распылитель |
JPS61195383U (no) * | 1985-05-28 | 1986-12-05 | ||
JPS6216737U (no) * | 1985-07-16 | 1987-01-31 | ||
DE3526343A1 (de) * | 1985-07-23 | 1987-02-05 | Proizv Ob Turbomotornyj Z Im K | Axialgasturbine |
DE3724385A1 (de) * | 1987-07-23 | 1989-02-02 | Man B & W Diesel Gmbh | Abgasturbolader mit vorrichtung zum abscheiden von festkoerpern |
SU1667939A1 (ru) * | 1989-02-03 | 1991-08-07 | Московский Полиграфический Институт | Струйный распределитель |
US5065945A (en) * | 1990-04-03 | 1991-11-19 | Spraying Systems Co. | Multiple head spray nozzle assembly with common supply manifold |
US5385014A (en) * | 1992-09-11 | 1995-01-31 | Aeronautical Accessories, Inc. | Valve and method of valve use while washing a compressor in an aircraft engine |
-
1996
- 1996-12-11 DE DE19651318A patent/DE19651318A1/de not_active Withdrawn
-
1997
- 1997-11-13 DE DE59711615T patent/DE59711615D1/de not_active Expired - Lifetime
- 1997-11-13 EP EP97810868A patent/EP0848150B1/de not_active Expired - Lifetime
- 1997-12-05 US US08/986,241 patent/US5938402A/en not_active Expired - Lifetime
- 1997-12-05 CZ CZ19973936A patent/CZ292033B6/cs not_active IP Right Cessation
- 1997-12-05 PL PL97323551A patent/PL323551A1/xx unknown
- 1997-12-09 JP JP9338741A patent/JP2929534B2/ja not_active Expired - Lifetime
- 1997-12-09 KR KR1019970067057A patent/KR100473472B1/ko not_active IP Right Cessation
- 1997-12-10 NO NO975814A patent/NO975814L/no unknown
- 1997-12-11 CN CN97114376A patent/CN1089408C/zh not_active Expired - Lifetime
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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