MX171869B - Ensamble de montaje de pared de entrada de una turbina de geometria variable - Google Patents

Ensamble de montaje de pared de entrada de una turbina de geometria variable

Info

Publication number
MX171869B
MX171869B MX016079A MX1607989A MX171869B MX 171869 B MX171869 B MX 171869B MX 016079 A MX016079 A MX 016079A MX 1607989 A MX1607989 A MX 1607989A MX 171869 B MX171869 B MX 171869B
Authority
MX
Mexico
Prior art keywords
wall
mounting assembly
variable geometry
geometry turbine
wall member
Prior art date
Application number
MX016079A
Other languages
English (en)
Inventor
Peter Mckean
Original Assignee
Holset Engineering Co
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 Holset Engineering Co filed Critical Holset Engineering Co
Publication of MX171869B publication Critical patent/MX171869B/es

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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00—Manufacture
    • F05B2230/60—Assembly methods
    • F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
    • F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

La presente invención se refiere a un ensamble de montaje para un miembro anular de pared movible de un pasaje de entrada de una turbina de geometría variable, en donde el pasaje de entrada está definido entre la pared movible y una pared confrontante, el miembro de pared está formado de un material laminado, y el miembro de pared está soportado sobre una pluralidad de pasadores que se extienden paralelamente a su dirección de movimiento, caracterizado porque el miembro de pared comprende una porción tubular que se extiende en alejamiento con respecto a dicha pared confrontante, cada pasador soporta un eslabón que se extiende radialmente, y cada eslabón está acoplado en una ranura respectiva en la porción tubular del miembro de pared, los eslabones teniendo un ajuste relativamente estrecho en dicha dirección de movimiento y un ajuste relativamente flojo en la dirección circunferencial.
MX016079A 1988-05-17 1989-05-17 Ensamble de montaje de pared de entrada de una turbina de geometria variable MX171869B (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8811621A GB2218743A (en) 1988-05-17 1988-05-17 Variable geometry turbine

Publications (1)

Publication Number Publication Date
MX171869B true MX171869B (es) 1993-11-22

Family

ID=10637016

Family Applications (1)

Application Number Title Priority Date Filing Date
MX016079A MX171869B (es) 1988-05-17 1989-05-17 Ensamble de montaje de pared de entrada de una turbina de geometria variable

Country Status (8)

Country Link
US (1) US4984965A (es)
EP (1) EP0342888B1 (es)
JP (1) JPH0264202A (es)
BR (1) BR8902301A (es)
DE (1) DE68901359D1 (es)
ES (1) ES2030972T3 (es)
GB (1) GB2218743A (es)
MX (1) MX171869B (es)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5183381A (en) * 1988-05-17 1993-02-02 Holset Engineering Company Limited Variable geometry turbine inlet wall mounting assembly
US5683225A (en) * 1991-10-28 1997-11-04 General Electric Company Jet engine variable area turbine nozzle
GB9305331D0 (en) * 1993-03-16 1993-05-05 Wilde Geoffrey L Variable geometry turbo charger
GB9707453D0 (en) * 1997-04-12 1997-05-28 Holset Engineering Co Linkage mechanism
GB9711893D0 (en) 1997-06-10 1997-08-06 Holset Engineering Co Variable geometry turbine
DE19816645B4 (de) * 1998-04-15 2005-12-01 Daimlerchrysler Ag Abgasturboladerturbine
US6158956A (en) * 1998-10-05 2000-12-12 Allied Signal Inc. Actuating mechanism for sliding vane variable geometry turbine
AU2002338857A1 (en) * 2002-09-06 2004-03-29 Honeywell Garrett Sa Self regulating slide vane turbocharger
US7393179B1 (en) * 2004-04-13 2008-07-01 Brayton Energy, Llc Variable position turbine nozzle
US20100172745A1 (en) * 2007-04-10 2010-07-08 Elliott Company Centrifugal compressor having adjustable inlet guide vanes
GB0805519D0 (en) * 2008-03-27 2008-04-30 Cummins Turbo Tech Ltd Variable geometry turbine
GB2461720B (en) * 2008-07-10 2012-09-05 Cummins Turbo Tech Ltd A variable geometry turbine
US20110173973A1 (en) * 2010-01-20 2011-07-21 International Engine Intellectrual Property Company, LLC Turbine inlet flow modulator
KR101829289B1 (ko) * 2010-11-24 2018-02-19 보르그워너 인코퍼레이티드 배기가스 터보차저
US9222673B2 (en) 2012-10-09 2015-12-29 General Electric Company Fuel nozzle and method of assembling the same
US11732601B2 (en) 2021-12-06 2023-08-22 Borgwarner Inc. Variable turbine geometry assembly

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3079127A (en) * 1956-11-23 1963-02-26 Garrett Corp Temperature responsive variable means for controlling flow in turbomachines
US3478955A (en) * 1968-03-11 1969-11-18 Dresser Ind Variable area diffuser for compressor
JPS58594B2 (ja) * 1978-03-31 1983-01-07 日立造船株式会社 遠心圧縮機
US4403914A (en) * 1981-07-13 1983-09-13 Teledyne Industries, Inc. Variable geometry device for turbomachinery
DE3377587D1 (en) * 1982-05-28 1988-09-08 Holset Engineering Co A variable inlet area turbine
US4643639A (en) * 1984-12-24 1987-02-17 Sundstrand Corporation Adjustable centrifugal pump

Also Published As

Publication number Publication date
JPH0264202A (ja) 1990-03-05
GB2218743A (en) 1989-11-22
ES2030972T3 (es) 1992-11-16
EP0342888A1 (en) 1989-11-23
US4984965A (en) 1991-01-15
GB8811621D0 (en) 1988-06-22
BR8902301A (pt) 1990-01-09
DE68901359D1 (de) 1992-06-04
EP0342888B1 (en) 1992-04-29

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