BR112015015854A2 - dispositivo de expansão em série, turbocompressor com tal dispositivo, motor com tal turbocompressor, veículo com tal motor e método para controle de um motor - Google Patents

dispositivo de expansão em série, turbocompressor com tal dispositivo, motor com tal turbocompressor, veículo com tal motor e método para controle de um motor

Info

Publication number
BR112015015854A2
BR112015015854A2 BR112015015854A BR112015015854A BR112015015854A2 BR 112015015854 A2 BR112015015854 A2 BR 112015015854A2 BR 112015015854 A BR112015015854 A BR 112015015854A BR 112015015854 A BR112015015854 A BR 112015015854A BR 112015015854 A2 BR112015015854 A2 BR 112015015854A2
Authority
BR
Brazil
Prior art keywords
engine
turbocharger
exhaust gas
turbine
vehicle
Prior art date
Application number
BR112015015854A
Other languages
English (en)
Other versions
BR112015015854B1 (pt
Inventor
Spontón Ove
Original Assignee
Scania Cv Ab
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 Scania Cv Ab filed Critical Scania Cv Ab
Publication of BR112015015854A2 publication Critical patent/BR112015015854A2/pt
Publication of BR112015015854B1 publication Critical patent/BR112015015854B1/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D9/00Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
    • F02D9/04Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits concerning exhaust conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
    • F01N13/08Other arrangements or adaptations of exhaust conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/18Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/18Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • F02B37/183Arrangements of bypass valves or actuators therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/22Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
    • 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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/34Gas-turbine plants characterised by the use of combustion products as the working fluid with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
    • 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
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M26/00Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
    • F02M26/02EGR systems specially adapted for supercharged engines
    • F02M26/04EGR systems specially adapted for supercharged engines with a single turbocharger
    • F02M26/05High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M26/00Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
    • F02M26/02EGR systems specially adapted for supercharged engines
    • F02M26/09Constructional details, e.g. structural combinations of EGR systems and supercharger systems; Arrangement of the EGR and supercharger systems with respect to the engine
    • F02M26/10Constructional details, e.g. structural combinations of EGR systems and supercharger systems; Arrangement of the EGR and supercharger systems with respect to the engine having means to increase the pressure difference between the exhaust and intake system, e.g. venturis, variable geometry turbines, check valves using pressure pulsations or throttles in the air intake or exhaust system
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2240/00Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being
    • F01N2240/20Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being a flow director or deflector
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2260/00Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/14Exhaust treating devices having provisions not otherwise provided for for modifying or adapting flow area or back-pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2260/00Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/16Exhaust treating devices having provisions not otherwise provided for for reducing exhaust flow pulsations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M26/00Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
    • F02M26/13Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
    • F02M26/22Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories with coolers in the recirculation passage
    • F02M26/23Layout, e.g. schematics
    • 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
    • F05D2260/00Function
    • F05D2260/60Fluid transfer
    • F05D2260/606Bypassing the fluid
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Supercharger (AREA)
  • Exhaust-Gas Circulating Devices (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)

Abstract

1/1 resumo “dispositivo de expansão em série, turbocompressor com tal dispositivo, motor com tal turbocompressor, veículo com tal motor e método para controle de um motor” a invenção é relativa a um dispositivo de expansão (4) para uma turbina (3) em uma unidade turbo (29), que inclui uma entrada de turbina (48) e saída de turbina (50) para o fluxo de gases de descarga para e a partir da turbina (30), um primeiro tubo de gás de descarga (52) que é conectado à entrada da turbina (48), um segundo tubo de gás de descarga (54) que é conectado à saída da turbina (50), um duto de porta de resíduos (56), que é conectado aos primeiro e segundo tubos de gás de descarga (52, 54) e uma unidade de limitação de fluxo (60) colocada no segundo tubo de gás de descarga (54). o duto de porta de resíduos (56) tem uma superfície de seção transversal (aw) que é menor do que a segunda superfície de seção transversal (ae) do segundo tubo de gás de descarga (54). a invenção também é relativa a uma unidade turbo (29) com um tal dispositivo de expansão em série (4), um motor de combustão (2) com tal unidade turbo (29), um veículo (1) com tal motor de combustão (2), e um método para regular um motor de combustão (2).
BR112015015854-4A 2013-01-31 2014-01-27 Motor de combustão e veículo com tal motor BR112015015854B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE1350110A SE538907C2 (sv) 2013-01-31 2013-01-31 Serieexpansionsanordning för en turbin i ett turboaggregat anslutet till ett EGR-system
SE1350110-1 2013-01-31
PCT/SE2014/050103 WO2014120067A1 (en) 2013-01-31 2014-01-27 Serial expansion device, turbocharger with such device, engine with such turbocharger, vehicle with such engine and method for control of an engine

Publications (2)

Publication Number Publication Date
BR112015015854A2 true BR112015015854A2 (pt) 2017-07-11
BR112015015854B1 BR112015015854B1 (pt) 2024-04-02

Family

ID=

Also Published As

Publication number Publication date
SE1350110A1 (sv) 2014-08-01
EP2951415A1 (en) 2015-12-09
KR101731007B1 (ko) 2017-04-27
EP2951415B1 (en) 2021-10-27
EP2951415A4 (en) 2016-11-02
KR20150105477A (ko) 2015-09-16
SE538907C2 (sv) 2017-02-07
WO2014120067A1 (en) 2014-08-07

Similar Documents

Publication Publication Date Title
BR112017010008A2 (pt) seção de escape para um motor de turbina a gás da aeronave
BR112015026459A2 (pt) motor de turboventilador de aeronave
MX2016009562A (es) Un difusor variable de recirculacion de gases de escape.
JP2015045330A5 (pt)
BR102014011863B8 (pt) Método e sistema de operação de um motor de combustão interna e controlador
BR112013000862A2 (pt) sistema de recuperação de calor desperdiçado com recuperação parcial
BR112013027662A2 (pt) compressor de um turbocompressor de gás de escape
JP2013249836A5 (pt)
WO2011002697A3 (en) Turbocharger system for air-throttled engines
RU2013110498A (ru) Способ управления потоком на впуске компрессора компрессионной системы (варианты) и система турбонагнетателя двигателя внутреннего сгорания
BR112015008638A2 (pt) motor de combustão interna
EP2527742A3 (en) System and method for flow control in gas turbine engine
FR2990468B1 (fr) Systeme de recuperation d'energie dans un circuit de gaz d'echappement
GB2533351A8 (en) Internal combustion engine having a two stage turbocharger
UA107163C2 (xx) Повітронагрівник з верхнім обігрівом
MX2017006053A (es) Un metodo de hacer funcionar un montaje de motor.
WO2012167052A8 (en) Systems and methods for an engine
MY192725A (en) Exhaust gas recirculation control method and exhaust gas recirculation control device
WO2013122643A3 (en) Device to lower nox in a gas turbine engine combustion system
BR112016028811A2 (pt) um sistema de turbina
BR112019006203A2 (pt) sistema de escape de múltiplos bancos compreendendo sistema de suprimento de agente redutor disposto à montante de uma turbina
BRPI0803661B8 (pt) turbomáquina de fluxo duplo
WO2010095983A8 (en) Method and apparatus for controlling turbine efficiency
BR112017025775A8 (pt) Turbocompressor de gases de escape com geometria de turbina ajustável
FI20085298A0 (fi) Aluksen koneistojärjestely

Legal Events

Date Code Title Description
B15K Others concerning applications: alteration of classification

Ipc: F02B 37/18 (2006.01), F02D 9/04 (2006.01), F02M 25

B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 27/01/2014, OBSERVADAS AS CONDICOES LEGAIS. PATENTE CONCEDIDA CONFORME ADI 5.529/DF, QUE DETERMINA A ALTERACAO DO PRAZO DE CONCESSAO.