BR112013023299A2 - turbocharger; and turbocharger operation method - Google Patents

turbocharger; and turbocharger operation method

Info

Publication number
BR112013023299A2
BR112013023299A2 BR112013023299A BR112013023299A BR112013023299A2 BR 112013023299 A2 BR112013023299 A2 BR 112013023299A2 BR 112013023299 A BR112013023299 A BR 112013023299A BR 112013023299 A BR112013023299 A BR 112013023299A BR 112013023299 A2 BR112013023299 A2 BR 112013023299A2
Authority
BR
Brazil
Prior art keywords
turbocharger
operation method
gas
pressure
propensity
Prior art date
Application number
BR112013023299A
Other languages
Portuguese (pt)
Inventor
House Timothy
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 BR112013023299A2 publication Critical patent/BR112013023299A2/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/025Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20Actively adjusting tip-clearance
    • F01D11/22Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/16Other safety measures for, or other control of, pumps
    • 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
    • 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

Abstract

resumo do pedido de patente de invenção para: "turbocarregador; e método de operação de turbocarregador". a propensão para vazamento de gás ao redor de uma haste que se estende através de um furo que conecta volumes de pressões diferentes, por exemplo, um alojamento de turbina de turbocarregador e o ar ambiente, é minimizada com a adição de um par de anéis de vedação inclinado por uma pressão do gás para fornecer uma vedação de fuligem e gás contínua. 1/1Summary of Patent Application for: "Turbocharger; and Turbocharger Operation Method". The propensity for gas leakage around a rod extending through a bore that connects different pressure volumes, for example, a turbocharger turbine housing and ambient air, is minimized by the addition of a pair of pressure rings. gasket inclined by a gas pressure to provide a continuous gas and soot seal. 1/1

BR112013023299A 2011-03-17 2012-03-08 turbocharger; and turbocharger operation method BR112013023299A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201161453637P 2011-03-17 2011-03-17
PCT/US2012/028170 WO2012125387A2 (en) 2011-03-17 2012-03-08 Gas pressure biased sealing method for an actuating shaft

Publications (1)

Publication Number Publication Date
BR112013023299A2 true BR112013023299A2 (en) 2017-04-25

Family

ID=46831257

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013023299A BR112013023299A2 (en) 2011-03-17 2012-03-08 turbocharger; and turbocharger operation method

Country Status (7)

Country Link
US (1) US20140003908A1 (en)
KR (1) KR20140012715A (en)
CN (1) CN103403321A (en)
BR (1) BR112013023299A2 (en)
DE (1) DE112012000911T5 (en)
RU (1) RU2013144940A (en)
WO (1) WO2012125387A2 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9032727B2 (en) * 2012-11-28 2015-05-19 Honeywell International Inc. Suction sealing for turbocharger
US9103271B2 (en) * 2013-04-04 2015-08-11 Ford Global Technologies, Llc Exhaust leakage management
JP6260698B2 (en) * 2014-06-20 2018-01-17 株式会社Ihi Turbocharger
US10012138B2 (en) * 2015-12-10 2018-07-03 Honeywell International Inc. Exhaust bypass valve of multi-stage turbocharger
US20170175619A1 (en) * 2015-12-21 2017-06-22 Borgwarner Inc. Exhaust soot utilized for extending the life of a wastegate
US10215088B2 (en) * 2016-07-24 2019-02-26 Garrett Transporation I Inc. Method of assembling a turbine wastegate assembly
CN106150572B (en) * 2016-08-29 2017-11-14 无锡康明斯涡轮增压技术有限公司 The volute modular construction of turbocharger
GB201816680D0 (en) * 2018-10-12 2018-11-28 Cummins Ltd Turbine
EP3772569A1 (en) * 2019-08-09 2021-02-10 Borgwarner Inc. Actuator assembly with sealing arrangement

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2860827A (en) * 1953-06-08 1958-11-18 Garrett Corp Turbosupercharger
US3033519A (en) * 1958-09-12 1962-05-08 United Aircraft Corp Turbine nozzle vane construction
US4245953A (en) * 1979-01-18 1981-01-20 General Motors Corporation Engine turbocharger with cartridge wastegate valve
US4659295A (en) * 1984-04-20 1987-04-21 The Garrett Corporation Gas seal vanes of 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
US5207559A (en) * 1991-07-25 1993-05-04 Allied-Signal Inc. Variable geometry diffuser assembly
DE10209484B4 (en) * 2002-03-05 2004-06-24 Borgwarner Turbo Systems Gmbh Turbocharger for vehicles with improved suspension for the actuation mechanism of the variable nozzles
DE20218878U1 (en) * 2002-12-06 2003-02-13 Burgmann Dichtungswerke Gmbh The mechanical seal assembly
ATE546627T1 (en) * 2003-07-11 2012-03-15 Malcolm George Leavesley TURBOCHARGER DEVICE HAVING AN EXHAUST GAS SEALING SYSTEM FOR PREVENTING GAS LEAKAGE FROM THE TURBOCHARGER DEVICE
JP2005113797A (en) * 2003-10-08 2005-04-28 Aisin Seiki Co Ltd Exhaust-gas sealing structure for turbocharger
JP4440819B2 (en) * 2005-04-07 2010-03-24 アイシン精機株式会社 Exhaust gas seal structure of turbocharger
DE202005008606U1 (en) * 2005-06-02 2005-08-04 Borgwarner Inc., Auburn Hills Setting shaft fitting for supercharger has base body of setting shaft with stepped external outline and bush with complementary internal outline
CN201057273Y (en) * 2007-07-04 2008-05-07 何全波 Gas sealing structure of slide bearing

Also Published As

Publication number Publication date
WO2012125387A2 (en) 2012-09-20
KR20140012715A (en) 2014-02-03
CN103403321A (en) 2013-11-20
WO2012125387A3 (en) 2013-02-28
US20140003908A1 (en) 2014-01-02
RU2013144940A (en) 2015-04-27
DE112012000911T5 (en) 2013-11-14

Similar Documents

Publication Publication Date Title
BR112013023299A2 (en) turbocharger; and turbocharger operation method
IN2014DN09988A (en)
WO2012094153A3 (en) Spring biased sealing method for an actuating shaft
ATE552407T1 (en) SEALING DEVICE OF AN EXHAUST TURBOCHARGER
BR112013030715A2 (en) supercharged turbocharged engine
EP2587000A3 (en) Seal plate with cooling passage
BRPI1013414A2 (en) gas cylinder actuator
BR112015017960A2 (en) method for drilling a well in an underground formation, and inverted emulsion drilling fluid
BR112014016321A2 (en) ring seal on a rotary control device
BR112013020137A2 (en) high pressure hydrogen gas compressor
BR112015010811A2 (en) turbine section of a gas turbine engine, and, gas turbine engine
GB201116666D0 (en) Sealing arrangement
BR112014030742A2 (en) control of a compression release brake
BR112014007438A2 (en) gas turbine engine, and arrangement for a gas turbine engine
EP2543827A3 (en) A sealing arrangement
BR112013001930A2 (en) method and system for reducing gas seal consumption and regulating pressure reductions in high pressure compression systems
EP2615259A3 (en) Gas turbine engine bearing chamber seals
SA515360327B1 (en) Gas turbine including belly band seal anti-rotation device
BR112012032163A2 (en) trigger actuator
CO6362068A2 (en) DIAPHRAGM PUMPS AND TRANSPORTATION OF DRAG REDUCERS
BR112015018957A2 (en) backlash control apparatus for a gas turbine engine and method for controlling backlash control in a gas turbine engine
BR102016013663A8 (en) gas turbine engine mechanism
FR3002283B1 (en) METHOD FOR DETERMINING THE EXHAUST GAS PRESSURE BEYOND THE TURBOCHARGER AND THE FLOW THROUGH ITS TURBINE
BR112013027147A2 (en) sliding joint, and method for operating a sliding joint
EP3617456A3 (en) Oil supply assembly for gas turbine engine

Legal Events

Date Code Title Description
B08F Application fees: application dismissed [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]
B350 Update of information on the portal [chapter 15.35 patent gazette]