BRPI0704032A - turbina de geometria variável - Google Patents

turbina de geometria variável

Info

Publication number
BRPI0704032A
BRPI0704032A BRPI0704032-6A BRPI0704032A BRPI0704032A BR PI0704032 A BRPI0704032 A BR PI0704032A BR PI0704032 A BRPI0704032 A BR PI0704032A BR PI0704032 A BRPI0704032 A BR PI0704032A
Authority
BR
Brazil
Prior art keywords
turbine
variable geometry
nozzle
wall
turbine rotor
Prior art date
Application number
BRPI0704032-6A
Other languages
English (en)
Inventor
Juerg Spuler
Original Assignee
Iveco Motorenforschung 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 Iveco Motorenforschung Ag filed Critical Iveco Motorenforschung Ag
Publication of BRPI0704032A publication Critical patent/BRPI0704032A/pt

Links

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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/143—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path the shiftable member being a wall, or part thereof of a radial diffuser
    • 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
    • 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
    • F05D2220/40—Application in turbochargers
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/14—Two-dimensional elliptical
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/16—Two-dimensional parabolic
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/19—Two-dimensional machined; miscellaneous
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/19—Two-dimensional machined; miscellaneous
    • F05D2250/192—Two-dimensional machined; miscellaneous bevelled
    • 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
    • F05D2250/00—Geometry
    • F05D2250/10—Two-dimensional
    • F05D2250/19—Two-dimensional machined; miscellaneous
    • F05D2250/193—Two-dimensional machined; miscellaneous milled
    • 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
    • F05D2250/00—Geometry
    • F05D2250/60—Structure; Surface texture
    • F05D2250/62—Structure; Surface texture smooth or fine
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • 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
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise

Landscapes

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

Abstract

TURBINA DE GEOMETRIA VARIáVEL A turbina de geometria variável, especialmente uma turbina de gás, compreendendo uma carcaça (2, 22), um rotor da turbina (4), um espiral de entrada de fluido (1) que circundo o referido rotor da turbina, um bocal em formato de aleta interposto entre o referido espiral de entrada e o referido rotor da turbina concebido para acelerar o fluxo de fluido, o referido bocal compreendendo um anel axialmente ajustável (5, 25) concebido para variar a abertura de bocal (3, 23) e tendo uma parede (19) delimitando a referida abertura de bocal, a referida parede tendo furos de contrapeso (6, 26, 26<39>) conectando a abertura de bocal com uma câmara (12) limitada pela referida carcaça e pelo referido anel, caracterizada pelo fato de que as bordas (16), formadas pelos referidos furos com a superfície (18) da referida parede faceiam a referida abertura de bocal, são arredondadas generosamente na porção (17, 17<39> localizada a montante do furo com relação ao fluxo de fluido. Turbocharger e motor sobrealimentado que compreendem a referida turbina.
BRPI0704032-6A 2006-09-12 2007-09-12 turbina de geometria variável BRPI0704032A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT001738A ITMI20061738A1 (it) 2006-09-12 2006-09-12 Turbina a geometria variabile

Publications (1)

Publication Number Publication Date
BRPI0704032A true BRPI0704032A (pt) 2008-04-29

Family

ID=37116136

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0704032-6A BRPI0704032A (pt) 2006-09-12 2007-09-12 turbina de geometria variável

Country Status (7)

Country Link
US (1) US7955047B2 (pt)
EP (1) EP1900908B8 (pt)
JP (1) JP4944717B2 (pt)
CN (1) CN101144394B (pt)
BR (1) BRPI0704032A (pt)
ES (1) ES2401455T3 (pt)
IT (1) ITMI20061738A1 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0521354D0 (en) * 2005-10-20 2005-11-30 Holset Engineering Co Variable geometry turbine
GB0615495D0 (en) 2006-08-04 2006-09-13 Cummins Turbo Tech Ltd Variable geometry turbine
GB0805519D0 (en) * 2008-03-27 2008-04-30 Cummins Turbo Tech Ltd Variable geometry turbine
GB0921350D0 (en) 2009-12-05 2010-01-20 Cummins Turbo Tech Ltd Vaariable geometry turbomachine
GB201015679D0 (en) * 2010-09-20 2010-10-27 Cummins Ltd Variable geometry turbine
GB2497786B (en) 2011-12-21 2016-09-07 Cummins Ltd Variable geometry turbine having vane slots with portions of increased clearance
EP2984299B1 (en) 2013-04-10 2018-10-03 Cummins Ltd Variable geometry turbine
US9650911B1 (en) * 2014-10-10 2017-05-16 Cummins Ltd Variable geometry turbine
DE102015219374B4 (de) * 2015-10-07 2022-05-25 Vitesco Technologies GmbH Verfahren zum Einbringen einer Wuchtmarke in das Verdichterrad eines Abgasturboladers und Abgasturbolader mit einem eine Wuchtmarke aufweisenden Verdichterrad
DE102017123819A1 (de) * 2017-10-12 2019-04-18 Ihi Charging Systems International Germany Gmbh Laufrad für einen Abgasturbolader, Abgasturbolader und Verfahren zum Auswuchten eines Laufzeugs für einen Abgasturbolader
CN109505663B (zh) * 2018-11-29 2021-08-17 江西省萍乡市三善机电有限公司 一种涡轮增压器上用的喷嘴环
GB202108695D0 (en) * 2021-06-17 2021-08-04 Cummins Ltd Nozzle ring for a variable geometry turbine
CN113513373B (zh) * 2021-07-08 2023-05-30 哈尔滨工程大学 一种变几何涡轮一维气动设计方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044683A (en) * 1960-01-18 1962-07-17 Schwitzer Corp Pressure control for turbochargers
US4499731A (en) * 1981-12-09 1985-02-19 Bbc Brown, Boveri & Company, Limited Controllable exhaust gas turbocharger
JPH0610403B2 (ja) * 1984-02-22 1994-02-09 日産自動車株式会社 ラジアルタ−ビンの可変ノズル
EP0654587B1 (en) * 1993-11-19 1999-01-20 Holset Engineering Company Limited Turbine with variable inlet geometry
JP3432674B2 (ja) * 1996-04-05 2003-08-04 株式会社日立製作所 多段遠心圧縮機
GB2319811A (en) 1996-10-03 1998-06-03 Holset Engineering Co A variable geometry turbocharger for an internal combustion engine
DE19905637C1 (de) * 1999-02-11 2000-08-31 Daimler Chrysler Ag Abgasturbolader für eine Brennkraftmaschine
ITTO20010505A1 (it) * 2001-05-25 2002-11-25 Iveco Motorenforschung Ag Turbina a geometria variabile.
GB0213910D0 (en) * 2002-06-17 2002-07-31 Holset Engineering Co Turbine
US6931849B2 (en) 2002-11-19 2005-08-23 Holset Engineering Company, Limited Variable geometry turbine
GB0226943D0 (en) * 2002-11-19 2002-12-24 Holset Engineering Co Variable geometry turbine
US7207176B2 (en) * 2002-11-19 2007-04-24 Cummins Inc. Method of controlling the exhaust gas temperature for after-treatment systems on a diesel engine using a variable geometry turbine
JP2006029228A (ja) * 2004-07-16 2006-02-02 Toshiba Corp フランシス型水力機械

Also Published As

Publication number Publication date
JP2008069779A (ja) 2008-03-27
EP1900908B8 (en) 2013-01-23
CN101144394A (zh) 2008-03-19
US20090097969A1 (en) 2009-04-16
ITMI20061738A1 (it) 2008-03-13
EP1900908A2 (en) 2008-03-19
US7955047B2 (en) 2011-06-07
JP4944717B2 (ja) 2012-06-06
ES2401455T3 (es) 2013-04-19
CN101144394B (zh) 2012-06-27
EP1900908A3 (en) 2011-09-28
EP1900908B1 (en) 2012-12-19

Similar Documents

Publication Publication Date Title
BRPI0704032A (pt) turbina de geometria variável
EP1980754A3 (en) Compressor and compressor housing
BRPI0512178A (pt) intensificador do fluxo do gás para motores de combustão
EP1911937A3 (en) A flow cavity arrangement for gas turbine engine
EP2075437A3 (en) Multi-source gas turbine cooling
EP1939404A3 (en) Stator assembly
EP1691034A3 (en) Variable geometry exhaust turbocharger and method of manufacturing
WO2010019177A3 (en) Transition with a linear flow path with exhaust mouths for use in a gas turbine engine
EP2060741A3 (en) Turbine arrangement
WO2006059980A3 (en) Diffuser aspiration for a tip turbine engine
BRPI0703627A (pt) dispositivo para silenciar um motor de turbina a gás para helicóptero, e, motor de turbina a gás para helicóptero
EP2025871A3 (en) Centripetal turbine and internal combustion engine with such a turbine
GB2467888A (en) Compressor
EP1916399A3 (en) Heat exchanger assembly for a gas turbine engine
RU2009139764A (ru) Эксцентрическая фаска у входа ответвлений в проточном канале
EP1847458A3 (en) Diffusing air inlet door assembly
EP2239428A3 (en) Exhaust plenum for a turbine engine
EP1985865A3 (en) Compressor and compressor housing
EP2060745A3 (en) Gas turbine sealing segment
WO2007019336A3 (en) Gas turbine exhaust diffuser
EP1849974A3 (en) Turbine engine tailcone resonator
GB2476223A (en) Shroud hanger with diffused cooling passage
FI20055492A0 (fi) Järjestely ja menetelmä turbokompressorilla varustetun mäntämoottorin yhteydessä
EP1775425A3 (en) Turbine shroud section and method for cooling such a section
EP1688603A3 (en) Gas turbine engine assembly

Legal Events

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

Owner name: FPT MOTORENFORSCHUNG AG (CH)

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2479 DE 10-07-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.