TURBOCHARGER WITH TWO-STAGE COMPRESSOR, INCLUDING A TWIN-WHEEL PARALLEL-FLOW FIRST STAGE

A single-shaft exhaust gas-driven turbocharger includes two parallel-flow first-stage centrifugal compressors in series with a single second-stage centrifugal compressor, and a one-stage turbine arranged to drive both the first- and second-stage centrifugal compressors via a single shaft on which th...

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Hauptverfasser: ARNOLD, STEVEN D, REYENGA, JAMES, LEI, VAI-MAN, SINGHAL, ASIT, LOTTERMAN, JEFF, BUNSIRISERT, KEVIN, SMITH, WILL J, GUIDRY, MIKE
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creator ARNOLD, STEVEN D
REYENGA, JAMES
LEI, VAI-MAN
SINGHAL, ASIT
LOTTERMAN, JEFF
BUNSIRISERT, KEVIN
SMITH, WILL J
GUIDRY, MIKE
description A single-shaft exhaust gas-driven turbocharger includes two parallel-flow first-stage centrifugal compressors in series with a single second-stage centrifugal compressor, and a one-stage turbine arranged to drive both the first- and second-stage centrifugal compressors via a single shaft on which the compressors and turbine are fixedly mounted. The compressor housing defines from one to a plurality of circumferentially spaced inlet ducts for the second wheel of the first stage, and from one to a plurality of circumferentially spaced interstage ducts leading from a vaneless diffuser of the first stage into the inlet of the second stage. L'invention porte sur un turbocompresseur entraîné par un gaz d'échappement à arbre unique, lequel turbocompresseur comprend deux compresseurs centrifuges de premier étage à écoulement parallèle en série avec un unique compresseur centrifuge de second étage, et une turbine à un étage agencée pour entraîner à la fois les compresseurs centrifuges de premier et de second étages par l'intermédiaire d'un unique arbre sur lequel les compresseurs et la turbine sont montés de manière fixe. Le boîtier de compresseur est défini à partir d'une à une pluralité de conduites d'entrée espacées circonférentiellement pour la seconde roue du premier étage, et à partir d'une à une pluralité de conduites entre étages espacées circonférentiellement menant à partir d'un diffuseur sans aubes du premier étage dans l'entrée du second étage.
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The compressor housing defines from one to a plurality of circumferentially spaced inlet ducts for the second wheel of the first stage, and from one to a plurality of circumferentially spaced interstage ducts leading from a vaneless diffuser of the first stage into the inlet of the second stage. L'invention porte sur un turbocompresseur entraîné par un gaz d'échappement à arbre unique, lequel turbocompresseur comprend deux compresseurs centrifuges de premier étage à écoulement parallèle en série avec un unique compresseur centrifuge de second étage, et une turbine à un étage agencée pour entraîner à la fois les compresseurs centrifuges de premier et de second étages par l'intermédiaire d'un unique arbre sur lequel les compresseurs et la turbine sont montés de manière fixe. 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REYENGA, JAMES ; LEI, VAI-MAN ; SINGHAL, ASIT ; LOTTERMAN, JEFF ; BUNSIRISERT, KEVIN ; SMITH, WILL J ; GUIDRY, MIKE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_WO2011005455A33</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2011</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION</topic><topic>COMBUSTION ENGINES</topic><topic>COMBUSTION ENGINES IN GENERAL</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>GAS-TURBINE PLANTS</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS</topic><topic>INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04</topic><topic>INTERNAL-COMBUSTION PISTON ENGINES</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>NON-POSITIVE DISPLACEMENT PUMPS</topic><topic>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</topic><topic>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</topic><topic>STEAM ENGINES</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ARNOLD, STEVEN D</creatorcontrib><creatorcontrib>REYENGA, JAMES</creatorcontrib><creatorcontrib>LEI, VAI-MAN</creatorcontrib><creatorcontrib>SINGHAL, ASIT</creatorcontrib><creatorcontrib>LOTTERMAN, JEFF</creatorcontrib><creatorcontrib>BUNSIRISERT, KEVIN</creatorcontrib><creatorcontrib>SMITH, WILL J</creatorcontrib><creatorcontrib>GUIDRY, MIKE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ARNOLD, STEVEN D</au><au>REYENGA, JAMES</au><au>LEI, VAI-MAN</au><au>SINGHAL, ASIT</au><au>LOTTERMAN, JEFF</au><au>BUNSIRISERT, KEVIN</au><au>SMITH, WILL J</au><au>GUIDRY, MIKE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TURBOCHARGER WITH TWO-STAGE COMPRESSOR, INCLUDING A TWIN-WHEEL PARALLEL-FLOW FIRST STAGE</title><date>2011-04-21</date><risdate>2011</risdate><abstract>A single-shaft exhaust gas-driven turbocharger includes two parallel-flow first-stage centrifugal compressors in series with a single second-stage centrifugal compressor, and a one-stage turbine arranged to drive both the first- and second-stage centrifugal compressors via a single shaft on which the compressors and turbine are fixedly mounted. The compressor housing defines from one to a plurality of circumferentially spaced inlet ducts for the second wheel of the first stage, and from one to a plurality of circumferentially spaced interstage ducts leading from a vaneless diffuser of the first stage into the inlet of the second stage. L'invention porte sur un turbocompresseur entraîné par un gaz d'échappement à arbre unique, lequel turbocompresseur comprend deux compresseurs centrifuges de premier étage à écoulement parallèle en série avec un unique compresseur centrifuge de second étage, et une turbine à un étage agencée pour entraîner à la fois les compresseurs centrifuges de premier et de second étages par l'intermédiaire d'un unique arbre sur lequel les compresseurs et la turbine sont montés de manière fixe. Le boîtier de compresseur est défini à partir d'une à une pluralité de conduites d'entrée espacées circonférentiellement pour la seconde roue du premier étage, et à partir d'une à une pluralité de conduites entre étages espacées circonférentiellement menant à partir d'un diffuseur sans aubes du premier étage dans l'entrée du second étage.</abstract><oa>free_for_read</oa></addata></record>
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBUSTION ENGINES
COMBUSTION ENGINES IN GENERAL
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
INTERNAL-COMBUSTION PISTON ENGINES
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
NON-POSITIVE DISPLACEMENT PUMPS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
STEAM ENGINES
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
WEAPONS
title TURBOCHARGER WITH TWO-STAGE COMPRESSOR, INCLUDING A TWIN-WHEEL PARALLEL-FLOW FIRST STAGE
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