CA1285778C - Turbocompresseur a aubes orientables - Google Patents

Turbocompresseur a aubes orientables

Info

Publication number
CA1285778C
CA1285778C CA000521245A CA521245A CA1285778C CA 1285778 C CA1285778 C CA 1285778C CA 000521245 A CA000521245 A CA 000521245A CA 521245 A CA521245 A CA 521245A CA 1285778 C CA1285778 C CA 1285778C
Authority
CA
Canada
Prior art keywords
turbine
turbocharger
vane
accordance
shaft
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.)
Expired - Lifetime
Application number
CA000521245A
Other languages
English (en)
Inventor
Steven D. Arnold
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.)
Household Manufacturing Inc
Original Assignee
Household Manufacturing Inc
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 Household Manufacturing Inc filed Critical Household Manufacturing Inc
Application granted granted Critical
Publication of CA1285778C publication Critical patent/CA1285778C/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165Final 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
CA000521245A 1985-10-24 1986-10-23 Turbocompresseur a aubes orientables Expired - Lifetime CA1285778C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US79107185A 1985-10-24 1985-10-24
US791,071 1985-10-24

Publications (1)

Publication Number Publication Date
CA1285778C true CA1285778C (fr) 1991-07-09

Family

ID=25152597

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000521245A Expired - Lifetime CA1285778C (fr) 1985-10-24 1986-10-23 Turbocompresseur a aubes orientables

Country Status (4)

Country Link
JP (1) JPS62162729A (fr)
BR (1) BR8605218A (fr)
CA (1) CA1285778C (fr)
GB (2) GB2183302B (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3659869B2 (ja) * 2000-05-22 2005-06-15 三菱重工業株式会社 可変容量タービン
KR100459750B1 (ko) * 2001-02-27 2004-12-03 미츠비시 쥬고교 가부시키가이샤 가변 용량 터빈용 베인 조정 기구 및 그 조립 방법
US6527508B2 (en) * 2001-08-03 2003-03-04 Mark Groskreutz Actuator crank arm design for variable nozzle turbocharger
DE10311227B4 (de) 2003-03-14 2005-03-31 Man B & W Diesel Ag Leitapparat
GB2416568A (en) * 2004-07-24 2006-02-01 Rolls Royce Plc Aerofoil with support member
JP4545068B2 (ja) * 2005-08-25 2010-09-15 三菱重工業株式会社 可変容量型排気ターボ過給機及び可変ノズル機構構成部材の製造方法
EP1811134A1 (fr) * 2006-01-23 2007-07-25 ABB Turbo Systems AG Dispositif de guidage réglable
GB201717091D0 (en) 2017-10-18 2017-11-29 Rolls Royce Plc A variable vane actuation arrangement

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB701561A (en) * 1949-03-25 1953-12-30 Centrax Power Units Ltd Improvements relating to gas turbine plant
DE1071420B (de) * 1956-05-31 1959-12-17 The Garrett Corporation, Los Aneles, Calif. (V. St. A.) Verstellbarer Leitapparat für Turbinen, insbesondere Gasturbinen
DE2333525C3 (de) * 1973-07-02 1975-11-27 Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen Hydraulische Leitschaufel-Verstelleinrichtung
WO1980002585A1 (fr) * 1979-05-14 1980-11-27 Norbert L Osborn Turbochargeur et ses adaptations
US4302149A (en) * 1980-02-19 1981-11-24 General Motors Corporation Ceramic vane drive joint
DE3023705A1 (de) * 1980-06-25 1982-05-19 Atlas Copco AB, Nacka Leitschaufelverstellvorrichtung an radialturbokompressoren
DE3531296A1 (de) * 1984-06-29 1986-03-13 Ishikawajima-Harima Jukogyo K.K., Tokio/Tokyo Steuervorrichtung fuer einen turbolader mit veraenderlicher leistung

Also Published As

Publication number Publication date
BR8605218A (pt) 1987-07-28
GB2216604B (en) 1990-07-04
GB2183302B (en) 1990-07-04
GB8625450D0 (en) 1986-11-26
GB8910350D0 (en) 1989-06-21
JPS62162729A (ja) 1987-07-18
GB2183302A (en) 1987-06-03
GB2216604A (en) 1989-10-11

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Legal Events

Date Code Title Description
MKLA Lapsed
MKLA Lapsed

Effective date: 19960109