IN2014DN06185A - - Google Patents

Info

Publication number
IN2014DN06185A
IN2014DN06185A IN6185DEN2014A IN2014DN06185A IN 2014DN06185 A IN2014DN06185 A IN 2014DN06185A IN 6185DEN2014 A IN6185DEN2014 A IN 6185DEN2014A IN 2014DN06185 A IN2014DN06185 A IN 2014DN06185A
Authority
IN
India
Prior art keywords
vane
ring
bearing ring
intake duct
unison
Prior art date
Application number
Other languages
English (en)
Inventor
Urban Radke
Nermin Osmanovic
Original Assignee
Borgwarner Inc
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 Borgwarner Inc filed Critical Borgwarner Inc
Publication of IN2014DN06185A publication Critical patent/IN2014DN06185A/en

Links

Classifications

    • 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
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • 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
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • 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
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • 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
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/22—Control 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
    • 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
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/24—Control of the pumps by using pumps or turbines with adjustable guide vanes
    • 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
    • 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
    • F05D2250/90—Variable geometry
    • 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
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
IN6185DEN2014 2012-04-27 2013-04-19 IN2014DN06185A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012008466 2012-04-27
PCT/US2013/037325 WO2013163023A1 (en) 2012-04-27 2013-04-19 Exhaust-gas turbocharger

Publications (1)

Publication Number Publication Date
IN2014DN06185A true IN2014DN06185A (ko) 2015-10-23

Family

ID=49483781

Family Applications (1)

Application Number Title Priority Date Filing Date
IN6185DEN2014 IN2014DN06185A (ko) 2012-04-27 2013-04-19

Country Status (7)

Country Link
US (1) US9664061B2 (ko)
JP (1) JP6085670B2 (ko)
KR (1) KR102034097B1 (ko)
CN (1) CN104220720B (ko)
DE (1) DE112013001527B4 (ko)
IN (1) IN2014DN06185A (ko)
WO (1) WO2013163023A1 (ko)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10968768B2 (en) * 2014-06-20 2021-04-06 Borgwarner Inc. Turbocharger with adjustable vanes
DE102015209813A1 (de) * 2015-05-28 2016-12-01 Bosch Mahle Turbo Systems Gmbh & Co. Kg Variable Turbinen- oder Verdichtergeometrie für einen Abgasturbolader
US9874106B2 (en) * 2015-10-21 2018-01-23 Borgwarner Inc. VTG lever positive displacement press joint
WO2018037807A1 (ja) * 2016-08-24 2018-03-01 株式会社Ihi 可変容量型過給機
WO2018037970A1 (ja) * 2016-08-24 2018-03-01 株式会社Ihi 可変容量型過給機
JP7040473B2 (ja) * 2019-01-31 2022-03-23 株式会社豊田自動織機 可変ノズルユニット

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4679984A (en) * 1985-12-11 1987-07-14 The Garrett Corporation Actuation system for variable nozzle turbine
US4804316A (en) 1985-12-11 1989-02-14 Allied-Signal Inc. Suspension for the pivoting vane actuation mechanism of a variable nozzle turbocharger
CA1270120A (en) * 1985-12-11 1990-06-12 Alliedsignal Inc. Suspension for the pivoting vane actuation mechanism of a variable nozzle turbocharger
JP3473562B2 (ja) * 2000-07-31 2003-12-08 トヨタ自動車株式会社 可変ノズルベーン付きターボチャージャ
DE10209484B4 (de) * 2002-03-05 2004-06-24 Borgwarner Turbo Systems Gmbh Turbolader für Fahrzeuge mit verbesserter Aufhängung für den Betätigungsmechanismus der variablen Düsen
US6709232B1 (en) * 2002-09-05 2004-03-23 Honeywell International Inc. Cambered vane for use in turbochargers
JP4008404B2 (ja) * 2002-10-18 2007-11-14 三菱重工業株式会社 可変容量型排気ターボ過給機
EP1418311B1 (de) * 2002-11-11 2007-01-17 BorgWarner Inc. Leitgitter variabler Geometrie
JP2005207373A (ja) * 2004-01-26 2005-08-04 Toyota Motor Corp 可変ノズルベーン付きターボチャージャおよびそれに含まれるユニゾンリングの組付方法
DE102004023210B4 (de) 2004-05-11 2018-07-26 Volkswagen Ag Abgasturbolader für eine Brennkraftmaschine mit variabler Turbinengeometrie
DE102004057864A1 (de) * 2004-11-30 2006-06-01 Borgwarner Inc.(N.D.Ges.D.Staates Delaware), Auburn Hills Abgasturbolader, Leitapparat für einen Abgasturbolader sowie Schaufelhebel für einen Leitapparat
US7559199B2 (en) * 2006-09-22 2009-07-14 Honeywell International Inc. Variable-nozzle cartridge for a turbocharger
US7670107B2 (en) * 2007-03-26 2010-03-02 Honeywell International Inc. Variable-vane assembly having fixed axial-radial guides and fixed radial-only guides for unison ring
JP4875602B2 (ja) 2007-12-14 2012-02-15 三菱重工業株式会社 可変ノズル機構
US8267647B2 (en) * 2008-07-09 2012-09-18 Borgwarner Inc. Variable geometry turbocharger lower vane ring retaining system
JP5029546B2 (ja) * 2008-09-10 2012-09-19 株式会社Ｉｈｉ ターボチャージャ
US20110138805A1 (en) 2009-12-15 2011-06-16 Honeywell International Inc. Conjugate curve profiles for vane arms, main-arms, and unison rings
JP2012062808A (ja) * 2010-09-15 2012-03-29 Toyota Motor Corp 可変容量型ターボチャージャ
US9308576B2 (en) * 2010-09-27 2016-04-12 Borgwarner Inc. Method for manufacturing a turbocharger with variable turbine geometry
DE102010042181A1 (de) 2010-10-08 2012-04-12 Bosch Mahle Turbo Systems Gmbh & Co. Kg Variable Turbinen- und/oder Verdichtergeometrie

Also Published As

Publication number Publication date
JP2015518543A (ja) 2015-07-02
DE112013001527T5 (de) 2014-12-04
WO2013163023A1 (en) 2013-10-31
KR20150003833A (ko) 2015-01-09
JP6085670B2 (ja) 2017-02-22
CN104220720B (zh) 2020-03-03
US9664061B2 (en) 2017-05-30
CN104220720A (zh) 2014-12-17
KR102034097B1 (ko) 2019-10-18
DE112013001527B4 (de) 2023-12-14
US20150118029A1 (en) 2015-04-30

Similar Documents

Publication Publication Date Title
IN2014DN06185A (ko)
IN2014DN06186A (ko)
WO2013165521A3 (en) Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections
EP2551488A3 (en) Three spool engine bearing configuration
WO2012027184A3 (en) Exhaust-gas turbocharger
IN2012DE00184A (ko)
EP2597274A3 (en) Gas turbine engine lockout-time reduction
WO2012064575A3 (en) Exhaust-gas turbocharger
WO2010068557A3 (en) Simplified variable geometry turbocharger with vane rings
IN2014DN05889A (ko)
WO2013165515A3 (en) Gas turbine engine with fan-tied inducer section
WO2011143079A3 (en) Exhaust-gas turbocharger
WO2014143413A3 (en) Seal assembly in a gas turbine engine including grooves in a radially outwardly facing side of a platform and in a inwardly facing side of an inner shroud
WO2014007880A3 (en) Reverse core gear turbofan
WO2011066130A3 (en) Turbocharger
EP2597292B8 (en) Gas turbine engine architecture with low pressure compressor hub between high and low rotor thrust bearings
WO2011146555A3 (en) Turbocharger
GB201120675D0 (en) Turbocharger arrangement
FR2961554B1 (fr) Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
WO2013180897A3 (en) Gas turbine engine compressor stator seal
WO2012154432A3 (en) Turbocharger with variable turbine geometry
WO2012021362A3 (en) Exhaust-gas turbocharger
IN2014DN10368A (ko)
IN2014DN06183A (ko)
IN2014DN08863A (ko)