GB9206950D0 - Turbocharger apparatus - Google Patents

Turbocharger apparatus

Info

Publication number
GB9206950D0
GB9206950D0 GB929206950A GB9206950A GB9206950D0 GB 9206950 D0 GB9206950 D0 GB 9206950D0 GB 929206950 A GB929206950 A GB 929206950A GB 9206950 A GB9206950 A GB 9206950A GB 9206950 D0 GB9206950 D0 GB 9206950D0
Authority
GB
United Kingdom
Prior art keywords
turbine
compressor
housing
exhaust gases
conducted
Prior art date
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.)
Pending
Application number
GB929206950A
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.)
Individual
Original Assignee
Individual
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
Priority claimed from GB888812664A external-priority patent/GB8812664D0/en
Priority claimed from GB888817230A external-priority patent/GB8817230D0/en
Priority claimed from GB888827153A external-priority patent/GB8827153D0/en
Priority claimed from GB888827761A external-priority patent/GB8827761D0/en
Priority claimed from GB898901803A external-priority patent/GB8901803D0/en
Application filed by Individual filed Critical Individual
Publication of GB9206950D0 publication Critical patent/GB9206950D0/en
Pending legal-status Critical Current

Links

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
    • 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

Abstract

Variable turbocharger apparatus (2) comprising a compressor housing (64), a compressor (6) mounted for rotation in the housing (64), a turbine housing (4), a turbine (12) mounted for rotation in the housing (4), a first inlet (16) for enabling air to be conducted to the compressor (6), an outlet (18) for air from the compressor (6), a second inlet (20) for enabling exhaust gases from an engine to be conducted to the turbine (12), a chamber (22) which surrounds the turbine (12) and which receives the exhaust gases from the second inlet (20) before the exhaust gases are conducted to the turbine (12), a piston (24) which is positioned between the turbine (12) and the housing (4) and which is slidable backwards and forwards to form a movable wall separating the turbine (12) from the chamber (22) which surrounds the turbine (12), a bearing assembly (68) for allowing the rotation of the compressor (6) and the turbine, and a heat shield (201) for shielding the bearing assembly (68) from the exhaust gases, and the piston (24) having a plurality of vanes (102) which enter into slots (260) in the heat shield (201). <IMAGE>
GB929206950A 1988-05-27 1992-03-31 Turbocharger apparatus Pending GB9206950D0 (en)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
GB888812664A GB8812664D0 (en) 1988-05-27 1988-05-27 Turbocharger apparatus
GB888817230A GB8817230D0 (en) 1988-07-20 1988-07-20 Turbocharger apparatus
GB888827153A GB8827153D0 (en) 1988-11-21 1988-11-21 Turbocharger apparatus
GB888827761A GB8827761D0 (en) 1988-11-28 1988-11-28 Turbocharger apparatus
GB898901803A GB8901803D0 (en) 1989-01-27 1989-01-27 Turbocharger apparatus
PCT/GB1989/000584 WO1989011583A1 (en) 1988-05-27 1989-05-26 Turbocharger apparatus

Publications (1)

Publication Number Publication Date
GB9206950D0 true GB9206950D0 (en) 1992-05-13

Family

ID=27516817

Family Applications (1)

Application Number Title Priority Date Filing Date
GB929206950A Pending GB9206950D0 (en) 1988-05-27 1992-03-31 Turbocharger apparatus

Country Status (6)

Country Link
EP (2) EP0442884B1 (en)
AT (2) ATE135440T1 (en)
AU (1) AU3693089A (en)
DE (2) DE68925977T2 (en)
GB (1) GB9206950D0 (en)
WO (1) WO1989011583A1 (en)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4232400C1 (en) * 1992-03-14 1993-08-19 Mercedes-Benz Aktiengesellschaft, 7000 Stuttgart, De
DE4215301A1 (en) * 1992-05-09 1993-11-11 Mak Maschinenbau Krupp Exhaust gas turbocharger with a radial turbine
EP0571205B1 (en) * 1992-05-21 1997-03-05 Alliedsignal Limited Variable exhaust driven turbochargers
GB9222133D0 (en) * 1992-10-21 1992-12-02 Leavesley Malcolm G Turbocharger apparatus
US5443362A (en) * 1994-03-16 1995-08-22 The Hoover Company Air turbine
DE19615237C2 (en) * 1996-04-18 1999-10-28 Daimler Chrysler Ag Exhaust gas turbocharger for an internal combustion engine
DE19805476C1 (en) * 1998-02-11 1999-10-07 Daimler Chrysler Ag Exhaust gas turbocharger for an internal combustion engine
DE19816645B4 (en) 1998-04-15 2005-12-01 Daimlerchrysler Ag Turbocharger turbine
EP1247012B1 (en) 2000-01-14 2004-05-12 Honeywell Garrett SA Turbocharger with sliding blades having combined dynamic surfaces and heat screen and uncoupled axial actuating device
DE60032523T2 (en) 2000-11-30 2007-11-22 Honeywell Garrett S.A. Exhaust gas turbocharger with variable geometry and a ring cutter
ITTO20010506A1 (en) 2001-05-25 2002-11-25 Iveco Motorenforschung Ag VARIABLE GEOMETRY TURBINE.
ITTO20010505A1 (en) 2001-05-25 2002-11-25 Iveco Motorenforschung Ag VARIABLE GEOMETRY TURBINE.
GB0227473D0 (en) 2002-11-25 2002-12-31 Leavesley Malcolm G Variable turbocharger apparatus with bypass apertures
US7581394B2 (en) * 2003-12-10 2009-09-01 Honeywell International Inc. Variable nozzle device for a turbocharger
GB2427446B (en) * 2005-06-20 2010-06-30 Malcolm George Leavesley Variable turbocharger apparatus
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
GB0811228D0 (en) * 2008-06-19 2008-07-30 Cummins Turbo Tech Ltd Variable geometric turbine
GB201015679D0 (en) 2010-09-20 2010-10-27 Cummins Ltd Variable geometry turbine
GB201119386D0 (en) 2011-11-10 2011-12-21 Cummins Ltd A variable geometry turbine
GB2585634A (en) * 2019-05-14 2021-01-20 Cummins Ltd Turbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1074206B (en) * 1958-01-20 1960-01-28 Gebrüder Sulzer Aktiengesellschaft, Winterthur (Schweiz) Idler wheel for turbo machines
NL121768C (en) * 1964-05-11
EP0034915A1 (en) * 1980-02-22 1981-09-02 Holset Engineering Company Limited Radially inward flow turbine
US4403914A (en) * 1981-07-13 1983-09-13 Teledyne Industries, Inc. Variable geometry device for turbomachinery
DE3244190A1 (en) * 1981-12-24 1983-10-20 Daimler-Benz Ag, 7000 Stuttgart Radial turbine
DE3375419D1 (en) * 1982-04-29 1988-02-25 Bbc Brown Boveri & Cie Turbo charger with a sliding ring valve

Also Published As

Publication number Publication date
DE68925977T2 (en) 1996-10-24
ATE135440T1 (en) 1996-03-15
EP0678657A3 (en) 1995-11-22
EP0678657B1 (en) 1998-11-25
WO1989011583A1 (en) 1989-11-30
DE68925977D1 (en) 1996-04-18
EP0678657A2 (en) 1995-10-25
DE68928865T2 (en) 1999-07-01
EP0442884B1 (en) 1996-03-13
EP0442884A1 (en) 1991-08-28
DE68928865D1 (en) 1999-01-07
ATE173794T1 (en) 1998-12-15
AU3693089A (en) 1989-12-12

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