AU2003264764A1 - Slide vane turbocharger - Google Patents

Slide vane turbocharger

Info

Publication number
AU2003264764A1
AU2003264764A1 AU2003264764A AU2003264764A AU2003264764A1 AU 2003264764 A1 AU2003264764 A1 AU 2003264764A1 AU 2003264764 A AU2003264764 A AU 2003264764A AU 2003264764 A AU2003264764 A AU 2003264764A AU 2003264764 A1 AU2003264764 A1 AU 2003264764A1
Authority
AU
Australia
Prior art keywords
slide vane
vane turbocharger
turbocharger
slide
vane
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.)
Abandoned
Application number
AU2003264764A
Inventor
Edwin Richard Deacon
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 UK Ltd
Original Assignee
Honeywell UK Ltd
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 Honeywell UK Ltd filed Critical Honeywell UK Ltd
Publication of AU2003264764A1 publication Critical patent/AU2003264764A1/en
Abandoned 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
    • F01D17/165—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
    • 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)
AU2003264764A 2002-09-12 2003-09-12 Slide vane turbocharger Abandoned AU2003264764A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0221199.3 2002-09-12
GB0221199A GB2392956A (en) 2002-09-12 2002-09-12 Controlling inlet to turbocharger turbine
PCT/GB2003/003980 WO2004025088A1 (en) 2002-09-12 2003-09-12 Slide vane turbocharger

Publications (1)

Publication Number Publication Date
AU2003264764A1 true AU2003264764A1 (en) 2004-04-30

Family

ID=9943962

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003264764A Abandoned AU2003264764A1 (en) 2002-09-12 2003-09-12 Slide vane turbocharger

Country Status (3)

Country Link
AU (1) AU2003264764A1 (en)
GB (1) GB2392956A (en)
WO (1) WO2004025088A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8191367B2 (en) 2005-11-16 2012-06-05 Honeywell International Inc. Sliding piston cartridge and turbocharger incorporating same
US7338254B2 (en) * 2005-11-29 2008-03-04 Honeywell International, Inc. Turbocharger with sliding piston assembly
GB0710670D0 (en) 2007-06-05 2007-07-11 Cummins Turbo Tech Ltd Turbocharger
US7762067B2 (en) * 2007-08-21 2010-07-27 Honeywell International, Inc. Turbocharger with sliding piston assembly
GB0807721D0 (en) 2008-04-29 2008-06-04 Cummins Turbo Tech Ltd A variable geometry turbine
DE102009059127A1 (en) * 2009-12-19 2011-06-22 Daimler AG, 70327 Adjusting device for a charging device, in particular for an exhaust gas turbocharger

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH553921A (en) * 1972-07-13 1974-09-13 Bbc Sulzer Turbomaschinen ADJUSTING DEVICE FOR THE VANES OF AN AXIAL COMPRESSOR.
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
GB2218745B (en) * 1988-05-17 1992-07-01 Holset Engineering Co Variable geometry turbine actuator assembly
GB2236806B (en) * 1988-05-27 1992-12-09 Malcolm George Leavesley Turbocharger apparatus
US5214920A (en) * 1990-11-27 1993-06-01 Leavesley Malcolm G Turbocharger apparatus
DE4232400C1 (en) * 1992-03-14 1993-08-19 Mercedes-Benz Aktiengesellschaft, 7000 Stuttgart, De
US5267829A (en) * 1992-03-14 1993-12-07 Mercedes Benz A.G. Flow control apparatus for a turbocharger turbine
US5231831A (en) * 1992-07-28 1993-08-03 Leavesley Malcolm G Turbocharger apparatus
GB9222133D0 (en) * 1992-10-21 1992-12-02 Leavesley Malcolm G Turbocharger apparatus
DE19816645B4 (en) * 1998-04-15 2005-12-01 Daimlerchrysler Ag Turbocharger turbine

Also Published As

Publication number Publication date
GB0221199D0 (en) 2002-10-23
GB2392956A (en) 2004-03-17
WO2004025088A1 (en) 2004-03-25

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Legal Events

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