AU2003278524A1 - Sector-divided turbine assembly with axial piston variable-geometry mechanism - Google Patents

Sector-divided turbine assembly with axial piston variable-geometry mechanism

Info

Publication number: AU2003278524A1
Authority: AU; Australia
Prior art keywords: sector; axial piston; turbine assembly; geometry mechanism; piston variable
Prior art date: 2003-10-24
Legal status (The legal status 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 status listed.): Abandoned

Application number

AU2003278524A

Inventor

Luciano Bernardini

Alain Lombard

Jeff Lotterman

Dominique Petitjean

Quentin Roberts

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

Honeywell International Inc

Original Assignee

Honeywell International 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.)

2003-10-24

Filing date

2003-10-24

Publication date

2005-05-11

2003-10-24 Application filed by Honeywell International Inc filed Critical Honeywell International Inc

2005-05-11 Publication of AU2003278524A1 publication Critical patent/AU2003278524A1/en

Status Abandoned legal-status Critical Current

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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/026—Scrolls for radial machines or engines
- 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
- 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
- F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
- 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

Landscapes

Engineering & Computer Science (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Supercharger (AREA)

AU2003278524A 2003-10-24 2003-10-24 Sector-divided turbine assembly with axial piston variable-geometry mechanism Abandoned AU2003278524A1 (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
PCT/IB2003/005142 WO2005040560A1 (en)	2003-10-24	2003-10-24	Sector-divided turbine assembly with axial piston variable-geometry mechanism

Publications (1)

Publication Number	Publication Date
AU2003278524A1 true AU2003278524A1 (en)	2005-05-11

Family

ID=34509324

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
AU2003278524A Abandoned AU2003278524A1 (en)	2003-10-24	2003-10-24	Sector-divided turbine assembly with axial piston variable-geometry mechanism

Country Status (4)

Country	Link
US (1)	US20080038110A1 (en)
EP (1)	EP1725742A1 (en)
AU (1)	AU2003278524A1 (en)
WO (1)	WO2005040560A1 (en)

Families Citing this family (28)

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GB0227473D0 (en) *	2002-11-25	2002-12-31	Leavesley Malcolm G	Variable turbocharger apparatus with bypass apertures
AT501234B1 (en) *	2006-03-30	2008-02-15	Avl List Gmbh	GAS TURBINE FOR AN INTERNAL COMBUSTION ENGINE
EP1957757B1 (en)	2005-11-16	2013-02-13	Honeywell International Inc.	Turbocharger having an axially sliding piston cartridge
EP2035673B1 (en)	2006-06-19	2014-06-11	Turbo Energy Limited	Variable stator blade mechanism for turbochargers
FR2911386B1 (en) *	2007-01-16	2009-03-06	Genius Soc Responsabilite Limi	AIR CONDITIONING APPARATUS WITH COMPRESSOR AND VORTEX
US8123470B2 (en) *	2007-08-10	2012-02-28	Honeywell International Inc.	Turbine assembly with semi-divided nozzle and half-collar piston
AT505407B1 (en) *	2007-08-16	2009-01-15	Ghm Engineering	EXHAUST BOLDER FOR AN INTERNAL COMBUSTION ENGINE
FR2925572B1 (en) *	2007-12-24	2010-02-12	Snecma Services	METHOD FOR CHOOSING A SECTOR ARRANGEMENT FOR A TURBOMACHINE DISPENSER
US8070425B2 (en) *	2008-03-28	2011-12-06	Honeywell International Inc.	Turbocharger with sliding piston, and having vanes and leakage dams
DE102008039085A1 (en) *	2008-08-21	2010-02-25	Daimler Ag	Internal combustion engine with an exhaust gas turbocharger
DE102009004890A1 (en) *	2009-01-16	2010-07-22	Bosch Mahle Turbo Systems Gmbh & Co. Kg	Charging device, particularly exhaust gas turbocharger for motor vehicle, has adjusting element, which is adjusted parallel to turbine wheel axis that is operatively connected with rotatably supported guide vane
US8113770B2 (en) *	2009-02-03	2012-02-14	Honeywell International Inc.	Turbine assembly for an exhaust gas-driven turbocharger having a variable nozzle
DE102009018583A1 (en) *	2009-04-23	2010-10-28	Daimler Ag	Internal combustion engine and method for operating an internal combustion engine
WO2011042691A2 (en) *	2009-10-06	2011-04-14	Cummins Ltd	Turbomachine
GB2474342A (en) *	2009-10-06	2011-04-13	Cummins Ltd	Turbine nozzle component connection
FR2968717B1 (en) *	2010-12-14	2014-06-13	Faurecia Sys Echappement	TURBINE HOUSING FOR TURBOCOMPRESSOR, TURBINE AND CORRESPONDING TURBOCOMPRESSOR.
CN102297016B (en) *	2011-08-15	2012-12-12	无锡凯迪增压器配件有限公司	Turbocharger for double-vane nozzle systems
DE102011121330A1 (en) *	2011-12-16	2013-06-20	Ihi Charging Systems International Gmbh	Turbine for an exhaust gas turbocharger
WO2014175765A1 (en) *	2013-04-25	2014-10-30	Siemens Aktiengesellschaft	Set of channel nozzles for a centripetal turboexpander
US9593690B2 (en)	2013-06-26	2017-03-14	Honeywell International Inc.	Turbocharger with an annular rotary bypass valve
WO2015051891A1 (en) *	2013-10-10	2015-04-16	Ihi Charging Systems International Gmbh	Heat shield for a turbocharger, turbocharger and a method for producing a heat shield
SE539442C2 (en) *	2014-09-12	2017-09-26	Scania Cv Ab	Turbine arrangement comprising two inlet pipes, each with bypass pipes, whose flow areas are variable by means of a common valve body
EP3350418B1 (en) *	2015-09-16	2019-08-21	BorgWarner Inc.	A cartridge for pulse-separated variable turbine geometry turbochargers
US9932886B2 (en) *	2016-02-17	2018-04-03	Honeywell International Inc.	Turbocharger with rotary bypass valve operable to selectively configure the turbine volute as single-scroll or twin-scroll
EP3546720B1 (en) *	2017-02-28	2021-07-21	Mitsubishi Heavy Industries Engine & Turbocharger, Ltd.	Exhaust turbine supercharger
GB201909819D0 (en) *	2019-07-09	2019-08-21	Cummins Ltd	Turbine assembly
JP7298525B2 (en) *	2020-03-24	2023-06-27	株式会社豊田自動織機	turbocharger
IL287648B2 (en) *	2021-10-28	2023-06-01	Gregory KATS	Rotary engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2861774A (en) *	1950-02-16	1958-11-25	Alfred J Buchi	Inlet control for radial flow turbines
CH668455A5 (en) *	1984-06-29	1988-12-30	Bbc Brown Boveri & Cie	Exhaust turbocharger with adjustable inlet - has blade ring on sleeve sliding on cylindrical surface
US5441383A (en) *	1992-05-21	1995-08-15	Alliedsignal Inc.	Variable exhaust driven turbochargers
US5231831A (en) *	1992-07-28	1993-08-03	Leavesley Malcolm G	Turbocharger apparatus
DE4242494C1 (en) *	1992-12-16	1993-09-09	Mercedes-Benz Aktiengesellschaft, 70327 Stuttgart, De	Adjustable flow-guide for engine exhaust turbocharger - has axially-adjustable annular insert in sectors forming different kinds of guide grilles supplied simultaneously by spiral passages
US6521408B1 (en) *	1997-09-25	2003-02-18	National Institute Of Agrobiological Sciences	Method for assessing a function of a gene
US6165780A (en) *	1996-09-26	2000-12-26	National Institute Of Agrobiological Resources, Ministry Of Agriculture, Forestry And Fisheries	Shuttle vector comprising a T-DNA Region and RI and RK2 origins of replication
DE10212675B4 (en) *	2002-03-22	2006-05-18	Daimlerchrysler Ag	Exhaust gas turbocharger in an internal combustion engine

2003
- 2003-10-24 AU AU2003278524A patent/AU2003278524A1/en not_active Abandoned
- 2003-10-24 US US10/576,663 patent/US20080038110A1/en not_active Abandoned
- 2003-10-24 WO PCT/IB2003/005142 patent/WO2005040560A1/en not_active Ceased
- 2003-10-24 EP EP03769824A patent/EP1725742A1/en not_active Withdrawn

Also Published As

Publication number	Publication date
EP1725742A1 (en)	2006-11-29
WO2005040560A1 (en)	2005-05-06
US20080038110A1 (en)	2008-02-14

Publication	Publication Date	Title
AU2003278524A1 (en)	2005-05-11	Sector-divided turbine assembly with axial piston variable-geometry mechanism
AU2003276753A1 (en)	2005-04-11	Wind turbine
AU2003294548A1 (en)	2004-08-10	External combustion rotary piston engine
AU2003262186A1 (en)	2003-10-27	Bearing assembly with an oil damper
AU2003252290A1 (en)	2005-02-14	Turbocharger
AU2003295525A1 (en)	2004-06-15	Rodless slide assembly
AU2003293712A1 (en)	2005-06-17	Wind turbine
AU2002303047A1 (en)	2003-11-11	Axially aligned opposed piston engine
AU2003239282A1 (en)	2004-01-19	Piston engine
AU2003900549A0 (en)	2003-02-20	An assembly
AU2003222775A1 (en)	2003-10-08	Tubekite with an improved aerodynamic profile
AU2003273004A1 (en)	2005-05-05	Lightweight engine
AU2003207994A1 (en)	2004-08-13	Engine
AU2005903587A0 (en)	2005-07-21	Piston rotor engine
AU2003296047A1 (en)	2004-06-30	Hydraulic engine
AU2003297530A1 (en)	2004-04-30	Unitary rod/piston assembly
AUPS249302A0 (en)	2002-06-13	Turbine engine
HK1093362A (en)	2007-03-02	Firing pin assembly
WO2006090191A8 (en)	2009-08-20	Engines with amplifiers
AU2003906200A0 (en)	2003-11-27	Engine mechanism
AU2003906039A0 (en)	2003-11-13	Engine mechanism
AU2003904582A0 (en)	2003-09-11	Engine mechanism
AU2003901898A0 (en)	2003-05-08	Turbine
AU2003903067A0 (en)	2003-07-03	Turbocharger with egr turbine
HK1094979A (en)	2007-04-20	An engine

Legal Events

Date	Code	Title	Description
2006-07-13	MK6	Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase