FR2030895A5 - - Google Patents

Info

Publication number
FR2030895A5
FR2030895A5 FR6943948A FR6943948A FR2030895A5 FR 2030895 A5 FR2030895 A5 FR 2030895A5 FR 6943948 A FR6943948 A FR 6943948A FR 6943948 A FR6943948 A FR 6943948A FR 2030895 A5 FR2030895 A5 FR 2030895A5
Authority
FR
France
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
FR6943948A
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.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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
Priority claimed from DE19691926327 external-priority patent/DE1926327C/en
Application filed by MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Application granted granted Critical
Publication of FR2030895A5 publication Critical patent/FR2030895A5/fr
Expired 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
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
FR6943948A 1969-05-23 1969-12-18 Expired FR2030895A5 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691926327 DE1926327C (en) 1969-05-23 Bearing of pivotable guide vanes

Publications (1)

Publication Number Publication Date
FR2030895A5 true FR2030895A5 (en) 1970-11-13

Family

ID=5734972

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6943948A Expired FR2030895A5 (en) 1969-05-23 1969-12-18

Country Status (4)

Country Link
US (1) US3652177A (en)
FR (1) FR2030895A5 (en)
GB (1) GB1249279A (en)
SE (1) SE358441B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2423640A1 (en) * 1978-04-20 1979-11-16 Gen Electric TURBINE MECHANICAL ASSEMBLY AND ITS MOUNTING PROCESS
DE2931766A1 (en) * 1979-08-04 1981-02-05 Motoren Turbinen Union GASKET DEVICE FOR THE FREE BLADES OF AN ADJUSTMENT APPARATUS OF GAS TURBINES
FR2570133A1 (en) * 1984-09-12 1986-03-14 Szydlowski Joseph Device for directing a flow of air at any point over an entire blade height at the inlet of a wheel of an axial compressor
EP0253234A1 (en) * 1986-07-09 1988-01-20 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Variable guide vane actuating device for a turbine engine

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3788763A (en) * 1972-11-01 1974-01-29 Gen Motors Corp Variable vanes
US4025227A (en) * 1975-06-30 1977-05-24 United Technologies Corporation Variable area turbine
US3966352A (en) * 1975-06-30 1976-06-29 United Technologies Corporation Variable area turbine
US4007998A (en) * 1975-08-22 1977-02-15 Carrier Corporation Blade assembly
FR2519374B1 (en) * 1982-01-07 1986-01-24 Snecma DEVICE FOR COOLING THE HEELS OF MOBILE BLADES OF A TURBINE
US4767264A (en) * 1986-10-31 1988-08-30 United Technologies Corporation Vane lever arm construction
GB2210935B (en) * 1987-10-10 1992-05-27 Rolls Royce Plc Variable stator vane assembly
DE4309636C2 (en) * 1993-03-25 2001-11-08 Abb Turbo Systems Ag Baden Radially flow-through turbocharger turbine
DE4309637A1 (en) * 1993-03-25 1994-09-29 Abb Management Ag Radially flow-through turbocharger turbine
US5622473A (en) * 1995-11-17 1997-04-22 General Electric Company Variable stator vane assembly
SE512085C2 (en) * 1998-05-28 2000-01-24 Abb Ab A rotor machine arrangement
GB2339244B (en) 1998-06-19 2002-12-18 Rolls Royce Plc A variable camber vane
DE10016745B4 (en) * 2000-04-04 2005-05-19 Man B & W Diesel Ag Axial flow machine with a nozzle comprising a number of adjustable guide vanes
US6435821B1 (en) * 2000-12-20 2002-08-20 United Technologies Corporation Variable vane for use in turbo machines
ITTO20010446A1 (en) * 2001-05-11 2002-11-11 Fiatavio Spa VANE FOR A STATOR OF A VARIABLE GEOMETRY TURBINE, IN PARTICULAR FOR AIRCRAFT ENGINES.
ITTO20020624A1 (en) * 2002-07-16 2004-01-16 Fiatavio Spa HINGE DEVICE OF A ROTATING BODY IN AN AIRCRAFT ENGINE
DE102005040574A1 (en) * 2005-08-26 2007-03-15 Rolls-Royce Deutschland Ltd & Co Kg Gap control device for a gas turbine
ITMI20061086A1 (en) * 2006-06-01 2007-12-02 Nuovo Pignone Spa DEVICE TO OPTIMIZE COOLING IN GAS TURBINES
US9243648B2 (en) * 2009-07-20 2016-01-26 Ingersoll-Rand Company Removable throat mounted inlet guide vane
CN102713304B (en) 2009-11-03 2015-01-28 英格索尔-兰德公司 Inlet guide vane for a compressor
US8668445B2 (en) * 2010-10-15 2014-03-11 General Electric Company Variable turbine nozzle system
US10830096B2 (en) * 2013-10-03 2020-11-10 Raytheon Technologies Corporation Rotating turbine vane bearing cooling
DE102015110249A1 (en) * 2015-06-25 2017-01-12 Rolls-Royce Deutschland Ltd & Co Kg Stator device for a turbomachine with a housing device and a plurality of guide vanes
DE102015110250A1 (en) * 2015-06-25 2016-12-29 Rolls-Royce Deutschland Ltd & Co Kg Stator device for a turbomachine with a housing device and a plurality of guide vanes
CN107509353A (en) * 2016-06-14 2017-12-22 伊姆西公司 Bar and the fixing device that is used cooperatively with frame for frame

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR518916A (en) * 1916-08-25 1921-06-02 Weise Sohne Sealing device of a machine shaft by means of a stop liquid
GB755527A (en) * 1953-10-15 1956-08-22 Power Jets Res & Dev Ltd Mounting of swivelling guide vane elements in axial flow elastic fluid turbines
US3367628A (en) * 1966-10-31 1968-02-06 United Aircraft Corp Movable vane unit
CH494340A (en) * 1968-07-26 1970-07-31 Sulzer Ag Guide vane ring for turbo machines III

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2423640A1 (en) * 1978-04-20 1979-11-16 Gen Electric TURBINE MECHANICAL ASSEMBLY AND ITS MOUNTING PROCESS
DE2931766A1 (en) * 1979-08-04 1981-02-05 Motoren Turbinen Union GASKET DEVICE FOR THE FREE BLADES OF AN ADJUSTMENT APPARATUS OF GAS TURBINES
FR2570133A1 (en) * 1984-09-12 1986-03-14 Szydlowski Joseph Device for directing a flow of air at any point over an entire blade height at the inlet of a wheel of an axial compressor
EP0253234A1 (en) * 1986-07-09 1988-01-20 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Variable guide vane actuating device for a turbine engine

Also Published As

Publication number Publication date
GB1249279A (en) 1971-10-13
US3652177A (en) 1972-03-28
SE358441B (en) 1973-07-30
DE1926327A1 (en) 1970-12-03
DE1926327B2 (en) 1972-09-14

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Legal Events

Date Code Title Description
ST Notification of lapse