FR667306A - Device for adjusting the operating conditions of centrifugal machines - Google Patents

Device for adjusting the operating conditions of centrifugal machines

Info

Publication number
FR667306A
FR667306A FR667306DA FR667306A FR 667306 A FR667306 A FR 667306A FR 667306D A FR667306D A FR 667306DA FR 667306 A FR667306 A FR 667306A
Authority
FR
France
Prior art keywords
adjusting
operating conditions
centrifugal machines
centrifugal
machines
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
Application number
Other languages
French (fr)
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.)
Rateau SA
Original Assignee
Rateau SA
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 Rateau SA filed Critical Rateau SA
Application granted granted Critical
Publication of FR667306A publication Critical patent/FR667306A/en
Expired 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
    • F01D17/167Final 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
    • 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
    • F01D17/141Final 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
    • F01D17/143Final 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR667306D 1928-02-02 1929-01-12 Device for adjusting the operating conditions of centrifugal machines Expired FR667306A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE667306X 1928-02-02

Publications (1)

Publication Number Publication Date
FR667306A true FR667306A (en) 1929-10-15

Family

ID=3877329

Family Applications (1)

Application Number Title Priority Date Filing Date
FR667306D Expired FR667306A (en) 1928-02-02 1929-01-12 Device for adjusting the operating conditions of centrifugal machines

Country Status (1)

Country Link
FR (1) FR667306A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0080810A1 (en) * 1981-11-14 1983-06-08 Holset Engineering Company Limited A variable inlet area turbine
EP0083199A2 (en) * 1981-12-22 1983-07-06 The Garrett Corporation Surge control of a fluid compressor
EP0095853A1 (en) * 1982-05-28 1983-12-07 Holset Engineering Company Limited A variable inlet area turbine
FR2552501A1 (en) * 1983-09-22 1985-03-29 Dresser Ind Multistage centrifugal compressor
EP0569702A1 (en) * 1992-05-09 1993-11-18 Krupp MaK Maschinenbau GmbH Turbocharger with radial turbine
EP0814235A1 (en) * 1996-06-13 1997-12-29 MaK Motoren GmbH Radial turbine for a turbocharger
EP1571298A1 (en) * 2004-03-02 2005-09-07 Siemens Aktiengesellschaft Blade for a turbomachine and turbomachine
WO2011015908A1 (en) * 2009-08-04 2011-02-10 Renault Trucks Variable geometry turbine
WO2015130782A1 (en) * 2014-02-25 2015-09-03 Fluid Equipment Development Company, Llc Method and system for varying the width of a turbine nozzle

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0080810A1 (en) * 1981-11-14 1983-06-08 Holset Engineering Company Limited A variable inlet area turbine
EP0083199A2 (en) * 1981-12-22 1983-07-06 The Garrett Corporation Surge control of a fluid compressor
EP0083199A3 (en) * 1981-12-22 1983-08-03 The Garrett Corporation Surge control of a fluid compressor
EP0095853A1 (en) * 1982-05-28 1983-12-07 Holset Engineering Company Limited A variable inlet area turbine
FR2552501A1 (en) * 1983-09-22 1985-03-29 Dresser Ind Multistage centrifugal compressor
EP0569702A1 (en) * 1992-05-09 1993-11-18 Krupp MaK Maschinenbau GmbH Turbocharger with radial turbine
EP0814235A1 (en) * 1996-06-13 1997-12-29 MaK Motoren GmbH Radial turbine for a turbocharger
EP1571298A1 (en) * 2004-03-02 2005-09-07 Siemens Aktiengesellschaft Blade for a turbomachine and turbomachine
WO2005085601A1 (en) * 2004-03-02 2005-09-15 Siemens Aktiengesellschaft Stationary axial flow gas turbine
WO2011015908A1 (en) * 2009-08-04 2011-02-10 Renault Trucks Variable geometry turbine
WO2015130782A1 (en) * 2014-02-25 2015-09-03 Fluid Equipment Development Company, Llc Method and system for varying the width of a turbine nozzle
US9845701B2 (en) 2014-02-25 2017-12-19 Fluid Equipment Development Company, Llc Method and system for varying the width of a turbine nozzle

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