FR1548701A - - Google Patents
Info
- Publication number
- FR1548701A FR1548701A FR1548701DA FR1548701A FR 1548701 A FR1548701 A FR 1548701A FR 1548701D A FR1548701D A FR 1548701DA FR 1548701 A FR1548701 A FR 1548701A
- 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
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
-
- 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
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US590809A US3367628A (en) | 1966-10-31 | 1966-10-31 | Movable vane unit |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1548701A true FR1548701A (fr) | 1968-12-06 |
Family
ID=24363805
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1548701D Expired FR1548701A (fr) | 1966-10-31 | 1967-10-31 |
Country Status (5)
Country | Link |
---|---|
US (1) | US3367628A (fr) |
DE (1) | DE1576987C3 (fr) |
FR (1) | FR1548701A (fr) |
GB (1) | GB1201949A (fr) |
SE (1) | SE326071B (fr) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2419390A1 (fr) * | 1978-03-09 | 1979-10-05 | Mtu Muenchen Gmbh | Distributeur a aubes orientables pour turbine axiale de moteur a turbine a gaz |
FR2423640A1 (fr) * | 1978-04-20 | 1979-11-16 | Gen Electric | Ensemble mecanique de turbine et son procede de montage |
FR2423638A1 (fr) * | 1978-04-20 | 1979-11-16 | Gen Electric | Collecteur d'air de refroidissement pour moteurs a turbine a gaz |
FR2433118A1 (fr) * | 1978-08-11 | 1980-03-07 | Mtu Muenchen Gmbh | Compresseur, notamment de moteur a turbine a gaz |
FR2583817A1 (fr) * | 1985-06-20 | 1986-12-26 | Snecma | Biellette de commande d'aube a calage variable de stator de compresseur de turbomachine |
US7214030B2 (en) | 2003-07-17 | 2007-05-08 | Snecma Moteurs | Guide system for the outer pivot of a variable stator vane, for a turbojet stator |
EP2738356A1 (fr) * | 2012-11-29 | 2014-06-04 | Techspace Aero S.A. | Aube de redresseur de turbomachine, redresseur de turbomachine et procédé de montage associé |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH494895A (de) * | 1968-07-26 | 1970-08-15 | Sulzer Ag | Leitschaufelkranz für Turbomaschinen |
CH494340A (de) * | 1968-07-26 | 1970-07-31 | Sulzer Ag | Leitschaufelkranz für Turbomaschinen III |
FR2030895A5 (fr) * | 1969-05-23 | 1970-11-13 | Motoren Turbinen Union | |
US3614056A (en) * | 1970-02-12 | 1971-10-19 | Jonathan Mfg Co | Flush bottom tank ball valve |
US3663118A (en) * | 1970-06-01 | 1972-05-16 | Gen Motors Corp | Turbine cooling control |
US3687569A (en) * | 1971-03-19 | 1972-08-29 | Gen Electric | Rotor with variable angle blades |
US3730640A (en) * | 1971-06-28 | 1973-05-01 | United Aircraft Corp | Seal ring for gas turbine |
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 |
US4307994A (en) * | 1979-10-15 | 1981-12-29 | General Motors Corporation | Variable vane position adjuster |
DE3278510D1 (en) * | 1981-03-23 | 1988-06-23 | Toshiba Kk | Multi-stage hydraulic rotating machine |
FR2524934B1 (fr) * | 1982-04-08 | 1986-12-26 | Snecma | Dispositif de butee de securite pour pivot d'aubes de stator a calage variable |
US4755104A (en) * | 1986-04-29 | 1988-07-05 | United Technologies Corporation | Stator vane linkage |
GB2210935B (en) * | 1987-10-10 | 1992-05-27 | Rolls Royce Plc | Variable stator vane assembly |
US4990056A (en) * | 1989-11-16 | 1991-02-05 | General Motors Corporation | Stator vane stage in axial flow compressor |
DE4309636C2 (de) * | 1993-03-25 | 2001-11-08 | Abb Turbo Systems Ag Baden | Radialdurchströmte Abgasturboladerturbine |
US6682299B2 (en) | 2001-11-15 | 2004-01-27 | General Electric Company | Variable stator vane support arrangement |
US6767183B2 (en) * | 2002-09-18 | 2004-07-27 | General Electric Company | Methods and apparatus for sealing gas turbine engine variable vane assemblies |
US7220098B2 (en) * | 2003-05-27 | 2007-05-22 | General Electric Company | Wear resistant variable stator vane assemblies |
US20060280597A1 (en) * | 2003-06-11 | 2006-12-14 | Ishikawajima-Harima Heavy Industries Co., Ltd. | Rotating member, housing, bearing, gearbox, rotating machine, shaft structure, and surface treatment method |
DE102006052003A1 (de) * | 2006-11-03 | 2008-05-08 | Rolls-Royce Deutschland Ltd & Co Kg | Strömungsarbeitsmaschine mit verstellbaren Statorschaufeln |
FR2913050B1 (fr) * | 2007-02-28 | 2011-06-17 | Snecma | Turbine haute-pression d'une turbomachine |
AU2011205659B2 (en) | 2010-01-15 | 2014-09-25 | Skyventure International (Uk) Ltd | Wind tunnel turning vane heat exchanger |
US20130106061A1 (en) * | 2011-10-28 | 2013-05-02 | General Electric Company | High temperature seal system |
US9394915B2 (en) * | 2012-06-04 | 2016-07-19 | United Technologies Corporation | Seal land for static structure of a gas turbine engine |
DE102013222980A1 (de) * | 2013-11-12 | 2015-06-11 | MTU Aero Engines AG | Leitschaufel für eine Strömungsmaschine mit einer Dichtungsvorrichtung, Leitrad sowie Strömungsmaschine |
EP2960438B1 (fr) * | 2014-06-26 | 2020-09-02 | MTU Aero Engines GmbH | Système d'aubes de guidage variables pour une turbine à gaz et turbine à gaz dotée d'un tel système |
EP3449100A2 (fr) * | 2016-04-25 | 2019-03-06 | Florida Turbine Technologies, Inc. | Moteur à turbine à gaz industriel à deux bobines pourvu d'aubes de guidage d'entrée variables |
US10544699B2 (en) * | 2017-12-19 | 2020-01-28 | Rolls-Royce Corporation | System and method for minimizing the turbine blade to vane platform overlap gap |
DE102018213983A1 (de) * | 2018-08-20 | 2020-02-20 | MTU Aero Engines AG | Verstellbare Leitschaufelanordnung, Leitschaufel, Dichtungsträger und Turbomaschine |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE529252A (fr) * | 1953-06-01 | |||
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 |
US2930579A (en) * | 1955-09-19 | 1960-03-29 | Dominion Eng Works Ltd | Turbine guide vane locking and vibration preventing arrangement |
FR1325261A (fr) * | 1961-05-23 | 1963-04-26 | Rolls Royce | Machine à écoulement d'un fluide |
GB946185A (en) * | 1961-06-26 | 1964-01-08 | Karlstad Mekaniska Ab | Improvements in and relating to turbines |
US3224194A (en) * | 1963-06-26 | 1965-12-21 | Curtiss Wright Corp | Gas turbine engine |
-
1966
- 1966-10-31 US US590809A patent/US3367628A/en not_active Expired - Lifetime
-
1967
- 1967-10-27 GB GB49028/67A patent/GB1201949A/en not_active Expired
- 1967-10-28 DE DE19671576987 patent/DE1576987C3/de not_active Expired
- 1967-10-30 SE SE14830/67A patent/SE326071B/xx unknown
- 1967-10-31 FR FR1548701D patent/FR1548701A/fr not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2419390A1 (fr) * | 1978-03-09 | 1979-10-05 | Mtu Muenchen Gmbh | Distributeur a aubes orientables pour turbine axiale de moteur a turbine a gaz |
FR2423640A1 (fr) * | 1978-04-20 | 1979-11-16 | Gen Electric | Ensemble mecanique de turbine et son procede de montage |
FR2423638A1 (fr) * | 1978-04-20 | 1979-11-16 | Gen Electric | Collecteur d'air de refroidissement pour moteurs a turbine a gaz |
FR2433118A1 (fr) * | 1978-08-11 | 1980-03-07 | Mtu Muenchen Gmbh | Compresseur, notamment de moteur a turbine a gaz |
FR2583817A1 (fr) * | 1985-06-20 | 1986-12-26 | Snecma | Biellette de commande d'aube a calage variable de stator de compresseur de turbomachine |
EP0209428A1 (fr) * | 1985-06-20 | 1987-01-21 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Biellette de commande pour aube à calage variable |
US4732536A (en) * | 1985-06-20 | 1988-03-22 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Turbo-machine compressor with variable incidence stator vanes |
US7214030B2 (en) | 2003-07-17 | 2007-05-08 | Snecma Moteurs | Guide system for the outer pivot of a variable stator vane, for a turbojet stator |
EP2738356A1 (fr) * | 2012-11-29 | 2014-06-04 | Techspace Aero S.A. | Aube de redresseur de turbomachine, redresseur de turbomachine et procédé de montage associé |
US10202859B2 (en) | 2012-11-29 | 2019-02-12 | Safran Aero Boosters Sa | Axial turbomachine blade with platforms having an angular profile |
Also Published As
Publication number | Publication date |
---|---|
DE1576987A1 (de) | 1970-05-21 |
US3367628A (en) | 1968-02-06 |
SE326071B (fr) | 1970-07-13 |
DE1576987B2 (de) | 1971-08-12 |
GB1201949A (en) | 1970-08-12 |
DE1576987C3 (de) | 1972-03-30 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |