FR2404101A1 - Structure d'aubage pour machine a fluide axiale - Google Patents
Structure d'aubage pour machine a fluide axialeInfo
- Publication number
- FR2404101A1 FR2404101A1 FR7827406A FR7827406A FR2404101A1 FR 2404101 A1 FR2404101 A1 FR 2404101A1 FR 7827406 A FR7827406 A FR 7827406A FR 7827406 A FR7827406 A FR 7827406A FR 2404101 A1 FR2404101 A1 FR 2404101A1
- Authority
- FR
- France
- Prior art keywords
- side wall
- fixed
- fluid machine
- blade structure
- axial fluid
- 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.)
- Granted
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/145—Means for influencing boundary layers or secondary circulations
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/127—Vortex generators, turbulators, or the like, for mixing
-
- 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/17—Purpose of the control system to control boundary layer
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
La structure comprend des aubes fixes 27a, 27b disposées circonférentiellement à la machine, une paroi latérale supérieure 5 et une paroi latérale inférieure 6 auxquelles lesdites aubes fixes sont fixées respectivement par leurs bouts et par leurs bases, un trajet d'écoulement annulaire étant défini entre les surfaces extérieures des aubes fixes et des parois latérales. Chaque aube fixe a une forme de section droite telle que son épaisseur t, T augmente dans la direction d'une surface 24 de la paroi latérale supérieure, à partir d'un point de hauteur arbitrairement choisi h par rapport à une surface 23 de la paroi latérale inférieure, grâce à quoi la section d'une gorge, pour chaque partie de l'aube fixe, peut varier suivant sa hauteur. Turbine à vapeur, turbines à gaz, compresseurs axiaux, etc.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP11463177A JPS5447907A (en) | 1977-09-26 | 1977-09-26 | Blading structure for axial-flow fluid machine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2404101A1 true FR2404101A1 (fr) | 1979-04-20 |
FR2404101B1 FR2404101B1 (fr) | 1981-05-29 |
Family
ID=14642664
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7827406A Granted FR2404101A1 (fr) | 1977-09-26 | 1978-09-25 | Structure d'aubage pour machine a fluide axiale |
Country Status (5)
Country | Link |
---|---|
US (1) | US4208167A (fr) |
JP (1) | JPS5447907A (fr) |
DE (1) | DE2841616C3 (fr) |
FR (1) | FR2404101A1 (fr) |
GB (1) | GB2004599B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0118769A2 (fr) * | 1983-03-08 | 1984-09-19 | Mtu Motoren- Und Turbinen-Union MàNchen Gmbh | Turbine à plusieurs étages avec bandages extérieurs |
Families Citing this family (52)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3202855C1 (de) * | 1982-01-29 | 1983-03-31 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur Verminderung von Sekundaerstroemungsverlusten in einem beschaufelten Stroemungskanal |
GB2128687B (en) * | 1982-10-13 | 1986-10-29 | Rolls Royce | Rotor or stator blade for an axial flow compressor |
FR2556409B1 (fr) * | 1983-12-12 | 1991-07-12 | Gen Electric | Aube perfectionnee pour moteur a turbine a gaz et procede de fabrication |
US4681509A (en) * | 1984-07-23 | 1987-07-21 | American Davidson, Inc. | Variable inlet fan assembly |
JPS6182208U (fr) * | 1984-11-05 | 1986-05-31 | ||
GB2177163B (en) * | 1985-06-28 | 1988-12-07 | Rolls Royce | Improvements in or relating to aerofoil section members for gas turbine engines |
US5221181A (en) * | 1990-10-24 | 1993-06-22 | Westinghouse Electric Corp. | Stationary turbine blade having diaphragm construction |
DE4228879A1 (de) * | 1992-08-29 | 1994-03-03 | Asea Brown Boveri | Axialdurchströmte Turbine |
US5326221A (en) * | 1993-08-27 | 1994-07-05 | General Electric Company | Over-cambered stage design for steam turbines |
DE4344189C1 (de) * | 1993-12-23 | 1995-08-03 | Mtu Muenchen Gmbh | Axial-Schaufelgitter mit gepfeilten Schaufelvorderkanten |
US6375419B1 (en) * | 1995-06-02 | 2002-04-23 | United Technologies Corporation | Flow directing element for a turbine engine |
ES2163678T3 (es) * | 1996-03-28 | 2002-02-01 | Mtu Aero Engines Gmbh | Hoja de paleta para turbinas. |
DE19612394C2 (de) * | 1996-03-28 | 1999-03-11 | Mtu Muenchen Gmbh | Schaufelblatt für Strömungsmaschinen |
DE19612396C2 (de) * | 1996-03-28 | 1998-02-05 | Univ Dresden Tech | Schaufelblatt mit unterschiedlich ausgebildeten Profilquerschnitten |
US6139265A (en) * | 1996-05-01 | 2000-10-31 | Valeo Thermique Moteur | Stator fan |
CN1100195C (zh) | 1997-09-08 | 2003-01-29 | 西门子公司 | 用于叶片机械的叶片和汽轮机 |
US5951245A (en) * | 1997-10-06 | 1999-09-14 | Ford Motor Company | Centrifugal fan assembly for an automotive vehicle |
US6092988A (en) * | 1998-07-06 | 2000-07-25 | Ford Motor Company | Centrifugal blower assembly with a pre-swirler for an automotive vehicle |
US6142733A (en) * | 1998-12-30 | 2000-11-07 | Valeo Thermique Moteur | Stator for fan |
WO2000061918A2 (fr) * | 1999-03-22 | 2000-10-19 | Siemens Westinghouse Power Corporation | Dispositif d'elimination de tourbillon du bord d'attaque de la surface portante |
US6419446B1 (en) * | 1999-08-05 | 2002-07-16 | United Technologies Corporation | Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engine |
JP2002213206A (ja) * | 2001-01-12 | 2002-07-31 | Mitsubishi Heavy Ind Ltd | ガスタービンにおける翼構造 |
US6884029B2 (en) | 2002-09-26 | 2005-04-26 | Siemens Westinghouse Power Corporation | Heat-tolerated vortex-disrupting fluid guide component |
US6969232B2 (en) * | 2002-10-23 | 2005-11-29 | United Technologies Corporation | Flow directing device |
JP4346412B2 (ja) * | 2003-10-31 | 2009-10-21 | 株式会社東芝 | タービン翼列装置 |
GB2417053B (en) * | 2004-08-11 | 2006-07-12 | Rolls Royce Plc | Turbine |
GB2436597A (en) * | 2006-03-27 | 2007-10-03 | Alstom Technology Ltd | Turbine blade and diaphragm |
DE102006048933A1 (de) * | 2006-10-17 | 2008-04-24 | Mtu Aero Engines Gmbh | Anordnung zur Strömungsbeeinflussung |
US7628585B2 (en) * | 2006-12-15 | 2009-12-08 | General Electric Company | Airfoil leading edge end wall vortex reducing plasma |
GB0704426D0 (en) * | 2007-03-08 | 2007-04-18 | Rolls Royce Plc | Aerofoil members for a turbomachine |
DE102007027427A1 (de) * | 2007-06-14 | 2008-12-18 | Rolls-Royce Deutschland Ltd & Co Kg | Schaufeldeckband mit Überstand |
JP4929193B2 (ja) * | 2008-01-21 | 2012-05-09 | 三菱重工業株式会社 | タービン翼列エンドウォール |
US8105037B2 (en) * | 2009-04-06 | 2012-01-31 | United Technologies Corporation | Endwall with leading-edge hump |
DE102009036406A1 (de) | 2009-08-06 | 2011-02-10 | Mtu Aero Engines Gmbh | Schaufelblatt |
DE102009052142B3 (de) * | 2009-11-06 | 2011-07-14 | MTU Aero Engines GmbH, 80995 | Axialverdichter |
US8517686B2 (en) * | 2009-11-20 | 2013-08-27 | United Technologies Corporation | Flow passage for gas turbine engine |
US10287987B2 (en) * | 2010-07-19 | 2019-05-14 | United Technologies Corporation | Noise reducing vane |
FR2989415B1 (fr) * | 2012-04-12 | 2016-02-12 | Snecma | Aube de turbine axiale |
US9644483B2 (en) * | 2013-03-01 | 2017-05-09 | General Electric Company | Turbomachine bucket having flow interrupter and related turbomachine |
FR3009589B1 (fr) * | 2013-08-12 | 2015-09-04 | Snecma | Aube de redresseur de turbomachine |
US9797258B2 (en) | 2013-10-23 | 2017-10-24 | General Electric Company | Turbine bucket including cooling passage with turn |
US9347320B2 (en) | 2013-10-23 | 2016-05-24 | General Electric Company | Turbine bucket profile yielding improved throat |
US9638041B2 (en) | 2013-10-23 | 2017-05-02 | General Electric Company | Turbine bucket having non-axisymmetric base contour |
US9376927B2 (en) * | 2013-10-23 | 2016-06-28 | General Electric Company | Turbine nozzle having non-axisymmetric endwall contour (EWC) |
US9551226B2 (en) | 2013-10-23 | 2017-01-24 | General Electric Company | Turbine bucket with endwall contour and airfoil profile |
US9670784B2 (en) | 2013-10-23 | 2017-06-06 | General Electric Company | Turbine bucket base having serpentine cooling passage with leading edge cooling |
US9528379B2 (en) | 2013-10-23 | 2016-12-27 | General Electric Company | Turbine bucket having serpentine core |
US10107108B2 (en) | 2015-04-29 | 2018-10-23 | General Electric Company | Rotor blade having a flared tip |
US20170030213A1 (en) * | 2015-07-31 | 2017-02-02 | Pratt & Whitney Canada Corp. | Turbine section with tip flow vanes |
US20170130587A1 (en) * | 2015-11-09 | 2017-05-11 | General Electric Company | Last stage airfoil design for optimal diffuser performance |
DE102017215874A1 (de) * | 2017-09-08 | 2019-03-14 | Man Diesel & Turbo Se | Leitschaufel, Leitvorrichtung und Strömungsmaschine |
CN112594111B (zh) * | 2020-12-17 | 2022-10-11 | 东方电气集团东方电机有限公司 | 一种降低固定导叶根部应力的方法 |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1456085A (en) * | 1921-12-29 | 1923-05-22 | Gen Electric | Elastic-fluid turbine |
US2355413A (en) * | 1942-01-21 | 1944-08-08 | Gen Electric | Elastic fluid turbine blading |
CH586841A5 (en) * | 1972-06-09 | 1977-04-15 | Hitachi Ltd | Axial-flow turbine with twisted nozzle blades - efflux angle is reduced continuously from middle point |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2735612A (en) * | 1956-02-21 | hausmann | ||
GB100055A (en) * | 1915-02-03 | 1916-11-02 | Oerlikon Maschf | Method of Constructing Turbine Stators. |
US2650752A (en) * | 1949-08-27 | 1953-09-01 | United Aircraft Corp | Boundary layer control in blowers |
US2801790A (en) * | 1950-06-21 | 1957-08-06 | United Aircraft Corp | Compressor blading |
US2938662A (en) * | 1953-03-24 | 1960-05-31 | Daimler Benz Ag | Turbo compressor |
FR1110068A (fr) * | 1953-10-22 | 1956-02-06 | Maschf Augsburg Nuernberg Ag | Aube directrice pour machines à circulation axiale |
FR1442526A (fr) * | 1965-05-07 | 1966-06-17 | Rateau Soc | Perfectionnements aux canaux courbes parcourus par un gaz ou une vapeur |
US4023350A (en) * | 1975-11-10 | 1977-05-17 | United Technologies Corporation | Exhaust case for a turbine machine |
-
1977
- 1977-09-26 JP JP11463177A patent/JPS5447907A/ja active Granted
-
1978
- 1978-09-22 US US05/945,054 patent/US4208167A/en not_active Expired - Lifetime
- 1978-09-25 DE DE2841616A patent/DE2841616C3/de not_active Expired
- 1978-09-25 FR FR7827406A patent/FR2404101A1/fr active Granted
- 1978-09-25 GB GB7838021A patent/GB2004599B/en not_active Expired
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1456085A (en) * | 1921-12-29 | 1923-05-22 | Gen Electric | Elastic-fluid turbine |
US2355413A (en) * | 1942-01-21 | 1944-08-08 | Gen Electric | Elastic fluid turbine blading |
CH586841A5 (en) * | 1972-06-09 | 1977-04-15 | Hitachi Ltd | Axial-flow turbine with twisted nozzle blades - efflux angle is reduced continuously from middle point |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0118769A2 (fr) * | 1983-03-08 | 1984-09-19 | Mtu Motoren- Und Turbinen-Union MàNchen Gmbh | Turbine à plusieurs étages avec bandages extérieurs |
EP0118769A3 (en) * | 1983-03-08 | 1985-04-24 | Mtu Muenchen Gmbh | Shrouded multistage turbine |
US4571937A (en) * | 1983-03-08 | 1986-02-25 | Mtu - Motoren-Und Turbinen-Munchen Gmbh | Apparatus for controlling the flow of leakage and cooling air of a rotor of a multi-stage turbine |
Also Published As
Publication number | Publication date |
---|---|
US4208167A (en) | 1980-06-17 |
DE2841616C3 (de) | 1981-06-11 |
DE2841616A1 (de) | 1979-03-29 |
GB2004599B (en) | 1982-01-27 |
JPS5633563B2 (fr) | 1981-08-04 |
JPS5447907A (en) | 1979-04-16 |
DE2841616B2 (de) | 1980-10-16 |
FR2404101B1 (fr) | 1981-05-29 |
GB2004599A (en) | 1979-04-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |