ATE20119T1 - Leitschaufeln fuer divergente kanaele in dampfturbinen. - Google Patents
Leitschaufeln fuer divergente kanaele in dampfturbinen.Info
- Publication number
- ATE20119T1 ATE20119T1 AT82103671T AT82103671T ATE20119T1 AT E20119 T1 ATE20119 T1 AT E20119T1 AT 82103671 T AT82103671 T AT 82103671T AT 82103671 T AT82103671 T AT 82103671T AT E20119 T1 ATE20119 T1 AT E20119T1
- Authority
- AT
- Austria
- Prior art keywords
- guide vanes
- steam turbines
- jet stream
- divergent duct
- ceiling plate
- Prior art date
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
-
- 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
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S415/00—Rotary kinetic fluid motors or pumps
- Y10S415/914—Device 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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8108884A FR2505399A1 (fr) | 1981-05-05 | 1981-05-05 | Aubage directeur pour veines divergentes de turbine a vapeur |
EP82103671A EP0064679B1 (de) | 1981-05-05 | 1982-04-29 | Leitschaufeln für divergente Kanäle in Dampfturbinen |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE20119T1 true ATE20119T1 (de) | 1986-06-15 |
Family
ID=9258069
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT82103671T ATE20119T1 (de) | 1981-05-05 | 1982-04-29 | Leitschaufeln fuer divergente kanaele in dampfturbinen. |
Country Status (7)
Country | Link |
---|---|
US (1) | US4470755A (de) |
EP (1) | EP0064679B1 (de) |
JP (1) | JPS57193703A (de) |
AT (1) | ATE20119T1 (de) |
DE (1) | DE3271339D1 (de) |
FR (1) | FR2505399A1 (de) |
ZA (1) | ZA823055B (de) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2523642A1 (fr) * | 1982-03-19 | 1983-09-23 | Alsthom Atlantique | Aubage directeur pour veines divergentes de turbine a vapeur |
GB2128687B (en) * | 1982-10-13 | 1986-10-29 | Rolls Royce | Rotor or stator blade for an axial flow compressor |
US4682935A (en) * | 1983-12-12 | 1987-07-28 | General Electric Company | Bowed turbine blade |
GB2164098B (en) * | 1984-09-07 | 1988-12-07 | Rolls Royce | Improvements in or relating to aerofoil section members for turbine engines |
JPS6244719A (ja) * | 1985-08-23 | 1987-02-26 | Alps Electric Co Ltd | エレクトロクロミツク表示素子 |
US4826400A (en) * | 1986-12-29 | 1989-05-02 | General Electric Company | Curvilinear turbine airfoil |
FR2643940B1 (fr) * | 1989-03-01 | 1991-05-17 | Snecma | Aube mobile de turbomachine a moment de pied compense |
JP2753382B2 (ja) * | 1990-09-17 | 1998-05-20 | 株式会社日立製作所 | 軸流タービン静翼装置及び軸流タービン |
US5167489A (en) * | 1991-04-15 | 1992-12-01 | General Electric Company | Forward swept rotor blade |
GB9210421D0 (en) * | 1992-05-15 | 1992-07-01 | Gec Alsthom Ltd | Turbine blade assembly |
DE4228879A1 (de) * | 1992-08-29 | 1994-03-03 | Asea Brown Boveri | Axialdurchströmte Turbine |
EP0916812B1 (de) * | 1997-11-17 | 2003-03-05 | ALSTOM (Switzerland) Ltd | Endstufe für axialdurchströmte Turbine |
US6299412B1 (en) * | 1999-12-06 | 2001-10-09 | General Electric Company | Bowed compressor airfoil |
US6682301B2 (en) | 2001-10-05 | 2004-01-27 | General Electric Company | Reduced shock transonic airfoil |
WO2003033880A1 (fr) * | 2001-10-10 | 2003-04-24 | Hitachi, Ltd. | Aube de turbine |
US6554564B1 (en) * | 2001-11-14 | 2003-04-29 | United Technologies Corporation | Reduced noise fan exit guide vane configuration for turbofan engines |
US7740347B2 (en) | 2002-12-02 | 2010-06-22 | Silverbrook Research Pty Ltd | Ink usage tracking in a cartridge for a mobile device |
JP4045993B2 (ja) * | 2003-03-28 | 2008-02-13 | 株式会社Ihi | ファン静翼、航空エンジン用ファン、及び航空エンジン |
US7547187B2 (en) * | 2005-03-31 | 2009-06-16 | Hitachi, Ltd. | Axial turbine |
CN101460706B (zh) * | 2006-03-31 | 2012-02-08 | 阿尔斯通技术有限公司 | 用于流体机械、尤其是用于蒸汽涡轮机的导向叶片 |
US7806653B2 (en) * | 2006-12-22 | 2010-10-05 | General Electric Company | Gas turbine engines including multi-curve stator vanes and methods of assembling the same |
GB2471152B (en) * | 2009-06-17 | 2016-08-10 | Dresser-Rand Company | Use of bowed nozzle vanes to reduce acoustic signature |
US9011084B2 (en) * | 2010-09-28 | 2015-04-21 | Mitsubishi Hitachi Power Systems, Ltd. | Steam turbine stator vane and steam turbine using the same |
US11566530B2 (en) * | 2019-11-26 | 2023-01-31 | General Electric Company | Turbomachine nozzle with an airfoil having a circular trailing edge |
US11629599B2 (en) | 2019-11-26 | 2023-04-18 | General Electric Company | Turbomachine nozzle with an airfoil having a curvilinear trailing edge |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA503596A (en) * | 1954-06-08 | A. V. Roe Canada Limited | Blading for compressors, turbines and the like | |
US850200A (en) * | 1905-11-28 | 1907-04-16 | Gen Electric | Turbine bucket and nozzle. |
US1062258A (en) * | 1911-07-07 | 1913-05-20 | Georg Arthur Schlotter | Propeller. |
US1966787A (en) * | 1931-03-27 | 1934-07-17 | Sulzer Ag | Cooling fan for vehicles driven by internal combustion engines |
US2029813A (en) * | 1932-10-25 | 1936-02-04 | Mey Rene De | Guiding vane for fans or the like |
FR759166A (fr) * | 1932-10-25 | 1934-01-30 | Perfectionnements aux aubes directrices des ventilateurs et semblables | |
US2154313A (en) * | 1938-04-01 | 1939-04-11 | Gen Electric | Directing vane |
FR1037610A (fr) * | 1950-03-03 | 1953-09-22 | Rolls Royce | Perfectionnements aux ensembles d'aubes de guidage pour conduits annulaires de fluide |
US2795373A (en) * | 1950-03-03 | 1957-06-11 | Rolls Royce | Guide vane assemblies in annular fluid ducts |
US3316714A (en) * | 1963-06-20 | 1967-05-02 | Rolls Royce | Gas turbine engine combustion equipment |
GB1116580A (en) * | 1965-11-17 | 1968-06-06 | Bristol Siddeley Engines Ltd | Stator blade assemblies for axial-flow turbine engines |
GB1284341A (en) * | 1970-01-28 | 1972-08-09 | Rolls Royce | Fluid flow machine |
US3989406A (en) * | 1974-11-26 | 1976-11-02 | Bolt Beranek And Newman, Inc. | Method of and apparatus for preventing leading edge shocks and shock-related noise in transonic and supersonic rotor blades and the like |
US4075500A (en) * | 1975-08-13 | 1978-02-21 | Grumman Aerospace Corporation | Variable stator, diffuser augmented wind turbine electrical generation system |
US4131387A (en) * | 1976-02-27 | 1978-12-26 | General Electric Company | Curved blade turbomachinery noise reduction |
SE410331B (sv) * | 1976-09-24 | 1979-10-08 | Kronogard Sven Olof | Statorkonstruktion avsedd att placeras nedstroms en separat arbetsturbinrotor |
JPS5445405A (en) * | 1977-09-16 | 1979-04-10 | Hitachi Ltd | Turbine cascade |
-
1981
- 1981-05-05 FR FR8108884A patent/FR2505399A1/fr active Granted
-
1982
- 1982-04-22 US US06/370,715 patent/US4470755A/en not_active Expired - Lifetime
- 1982-04-29 DE DE8282103671T patent/DE3271339D1/de not_active Expired
- 1982-04-29 AT AT82103671T patent/ATE20119T1/de not_active IP Right Cessation
- 1982-04-29 EP EP82103671A patent/EP0064679B1/de not_active Expired
- 1982-05-04 JP JP57075050A patent/JPS57193703A/ja active Pending
- 1982-05-04 ZA ZA823055A patent/ZA823055B/xx unknown
Also Published As
Publication number | Publication date |
---|---|
FR2505399A1 (fr) | 1982-11-12 |
ZA823055B (en) | 1983-03-30 |
FR2505399B1 (de) | 1985-05-03 |
EP0064679A1 (de) | 1982-11-17 |
EP0064679B1 (de) | 1986-05-28 |
US4470755A (en) | 1984-09-11 |
JPS57193703A (en) | 1982-11-29 |
DE3271339D1 (en) | 1986-07-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
UEP | Publication of translation of european patent specification | ||
REN | Ceased due to non-payment of the annual fee |