GB0221199D0 - Slide vane turbocharger - Google Patents

Slide vane turbocharger

Info

Publication number
GB0221199D0
GB0221199D0 GB0221199A GB0221199A GB0221199D0 GB 0221199 D0 GB0221199 D0 GB 0221199D0 GB 0221199 A GB0221199 A GB 0221199A GB 0221199 A GB0221199 A GB 0221199A GB 0221199 D0 GB0221199 D0 GB 0221199D0
Authority
GB
United Kingdom
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.)
Withdrawn
Application number
GB0221199A
Other versions
GB2392956A (en
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
Priority to GB0221199A priority Critical patent/GB2392956A/en
Publication of GB0221199D0 publication Critical patent/GB0221199D0/en
Priority to AU2003264764A priority patent/AU2003264764A1/en
Priority to PCT/GB2003/003980 priority patent/WO2004025088A1/en
Publication of GB2392956A publication Critical patent/GB2392956A/en
Withdrawn legal-status Critical Current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)
GB0221199A 2002-09-12 2002-09-12 Controlling inlet to turbocharger turbine Withdrawn GB2392956A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB0221199A GB2392956A (en) 2002-09-12 2002-09-12 Controlling inlet to turbocharger turbine
AU2003264764A AU2003264764A1 (en) 2002-09-12 2003-09-12 Slide vane turbocharger
PCT/GB2003/003980 WO2004025088A1 (en) 2002-09-12 2003-09-12 Slide vane turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0221199A GB2392956A (en) 2002-09-12 2002-09-12 Controlling inlet to turbocharger turbine

Publications (2)

Publication Number Publication Date
GB0221199D0 true GB0221199D0 (en) 2002-10-23
GB2392956A GB2392956A (en) 2004-03-17

Family

ID=9943962

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0221199A Withdrawn GB2392956A (en) 2002-09-12 2002-09-12 Controlling inlet to turbocharger turbine

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
EP1957757B1 (en) 2005-11-16 2013-02-13 Honeywell International Inc. Turbocharger having an axially sliding piston cartridge
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
AU2003264764A1 (en) 2004-04-30
GB2392956A (en) 2004-03-17
WO2004025088A1 (en) 2004-03-25

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)