GB201213456D0 - A variable geometry turbine - Google Patents

A variable geometry turbine

Info

Publication number
GB201213456D0
GB201213456D0 GBGB1213456.5A GB201213456A GB201213456D0 GB 201213456 D0 GB201213456 D0 GB 201213456D0 GB 201213456 A GB201213456 A GB 201213456A GB 201213456 D0 GB201213456 D0 GB 201213456D0
Authority
GB
United Kingdom
Prior art keywords
yoke
variable geometry
guide rods
actuator
arms
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Withdrawn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
GBGB1213456.5A
Other versions
GB2504482A (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.)
Cummins Ltd
Original Assignee
Cummins 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 Cummins Ltd filed Critical Cummins Ltd
Priority to GB1213456.5A priority Critical patent/GB2504482A/en
Publication of GB201213456D0 publication Critical patent/GB201213456D0/en
Publication of GB2504482A publication Critical patent/GB2504482A/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Withdrawn legal-status Critical Current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
    • F01D17/167—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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/22—Control 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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)

Abstract

A variable geometry turbine of the kind used in a turbocharger has a variable geometry element, such as a nozzle ring mounted on guide rods 126, which is operated by an actuator. The actuator comprises a yoke defining a pair of arms 132 which extend into engagement with the guide rods. The actuator further comprises a motor to drive a toothed gear wheel 137 which is operatively connected to a sector gear 136 fixedly mounted on the yoke. The sector gear is defined by a rim that extends radially from the yoke pivot axis to one side of a plane which extends substantially parallel to the turbine axis and which contains the yoke pivot axis, and the arms of the yoke extend to the other side of said plane. Operation of the motor drives rotation of the yoke via the gears, which in turn drives the guide rods in translation.
GB1213456.5A 2012-07-27 2012-07-27 Variable geometry turbine for a turbocharger Withdrawn GB2504482A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1213456.5A GB2504482A (en) 2012-07-27 2012-07-27 Variable geometry turbine for a turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1213456.5A GB2504482A (en) 2012-07-27 2012-07-27 Variable geometry turbine for a turbocharger

Publications (2)

Publication Number Publication Date
GB201213456D0 true GB201213456D0 (en) 2012-09-12
GB2504482A GB2504482A (en) 2014-02-05

Family

ID=46881314

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1213456.5A Withdrawn GB2504482A (en) 2012-07-27 2012-07-27 Variable geometry turbine for a turbocharger

Country Status (1)

Country Link
GB (1) GB2504482A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105179024A (en) * 2015-10-19 2015-12-23 福州大学 Turbocharger nozzle opening degree executing mechanism with bevel gears being used for positioning

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0710670D0 (en) * 2007-06-05 2007-07-11 Cummins Turbo Tech Ltd Turbocharger

Also Published As

Publication number Publication date
GB2504482A (en) 2014-02-05

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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)