DE50111350D1 - Leitschaufelkranzsegmente mit Flanschverbindung - Google Patents
Leitschaufelkranzsegmente mit FlanschverbindungInfo
- Publication number
- DE50111350D1 DE50111350D1 DE50111350T DE50111350T DE50111350D1 DE 50111350 D1 DE50111350 D1 DE 50111350D1 DE 50111350 T DE50111350 T DE 50111350T DE 50111350 T DE50111350 T DE 50111350T DE 50111350 D1 DE50111350 D1 DE 50111350D1
- Authority
- DE
- Germany
- Prior art keywords
- guide vane
- flange connection
- vane segments
- segments
- flange
- 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 - Lifetime
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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE50111350T DE50111350D1 (de) | 2000-10-16 | 2001-09-21 | Leitschaufelkranzsegmente mit Flanschverbindung |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10051223A DE10051223A1 (de) | 2000-10-16 | 2000-10-16 | Verbindbare Statorelemente |
DE50111350T DE50111350D1 (de) | 2000-10-16 | 2001-09-21 | Leitschaufelkranzsegmente mit Flanschverbindung |
Publications (1)
Publication Number | Publication Date |
---|---|
DE50111350D1 true DE50111350D1 (de) | 2006-12-14 |
Family
ID=7659952
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE10051223A Withdrawn DE10051223A1 (de) | 2000-10-16 | 2000-10-16 | Verbindbare Statorelemente |
DE50111350T Expired - Lifetime DE50111350D1 (de) | 2000-10-16 | 2001-09-21 | Leitschaufelkranzsegmente mit Flanschverbindung |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE10051223A Withdrawn DE10051223A1 (de) | 2000-10-16 | 2000-10-16 | Verbindbare Statorelemente |
Country Status (3)
Country | Link |
---|---|
US (2) | US6592326B2 (de) |
EP (1) | EP1199440B1 (de) |
DE (2) | DE10051223A1 (de) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2388161A (en) * | 2002-05-02 | 2003-11-05 | Rolls Royce Plc | Gas turbine engine compressor casing |
US7101150B2 (en) * | 2004-05-11 | 2006-09-05 | Power Systems Mfg, Llc | Fastened vane assembly |
JP4918263B2 (ja) * | 2006-01-27 | 2012-04-18 | 三菱重工業株式会社 | 軸流圧縮機の静翼環 |
US8950069B2 (en) * | 2006-12-29 | 2015-02-10 | Rolls-Royce North American Technologies, Inc. | Integrated compressor vane casing |
SE0700823L (sv) | 2007-03-30 | 2008-10-01 | Volvo Aero Corp | Komponent för en gasturbinmotor, jetmotor försedd med en sådan komponent, samt en flygmaskin försedd med en sådan jetmotor |
US7837435B2 (en) * | 2007-05-04 | 2010-11-23 | Power System Mfg., Llc | Stator damper shim |
US8202043B2 (en) * | 2007-10-15 | 2012-06-19 | United Technologies Corp. | Gas turbine engines and related systems involving variable vanes |
FR2933130B1 (fr) | 2008-06-25 | 2012-02-24 | Snecma | Carter structural pour turbomachine |
US8511982B2 (en) * | 2008-11-24 | 2013-08-20 | Alstom Technology Ltd. | Compressor vane diaphragm |
DE102009007999A1 (de) * | 2009-02-07 | 2010-08-12 | Hobis Ag | Leitringelement für Turbinen und Verfahren zu dessen Herstellung |
GB2468848B (en) * | 2009-03-23 | 2011-10-26 | Rolls Royce Plc | An assembly for a turbomachine |
US8371810B2 (en) | 2009-03-26 | 2013-02-12 | General Electric Company | Duct member based nozzle for turbine |
US8360716B2 (en) * | 2010-03-23 | 2013-01-29 | United Technologies Corporation | Nozzle segment with reduced weight flange |
US8356975B2 (en) * | 2010-03-23 | 2013-01-22 | United Technologies Corporation | Gas turbine engine with non-axisymmetric surface contoured vane platform |
US9976433B2 (en) | 2010-04-02 | 2018-05-22 | United Technologies Corporation | Gas turbine engine with non-axisymmetric surface contoured rotor blade platform |
US9303531B2 (en) | 2011-12-09 | 2016-04-05 | General Electric Company | Quick engine change assembly for outlet guide vanes |
US9303520B2 (en) * | 2011-12-09 | 2016-04-05 | General Electric Company | Double fan outlet guide vane with structural platforms |
US9127568B2 (en) * | 2012-01-04 | 2015-09-08 | General Electric Company | Turbine casing |
CA2872038C (en) * | 2012-06-15 | 2018-10-16 | United Technologies Corporation | High durability turbine exhaust case |
US20140314547A1 (en) * | 2012-08-31 | 2014-10-23 | United Technologies Corporation | Attachment apparatus for ceramic matrix composite materials |
US20140248146A1 (en) * | 2012-08-31 | 2014-09-04 | United Technologies Corporation | Attachment apparatus for ceramic matrix composite materials |
WO2014130214A1 (en) * | 2013-02-22 | 2014-08-28 | United Technologies Corporation | Stator vane assembly and method therefore |
WO2015023324A2 (en) * | 2013-04-12 | 2015-02-19 | United Technologies Corporation | Stator vane platform with flanges |
US9506362B2 (en) | 2013-11-20 | 2016-11-29 | General Electric Company | Steam turbine nozzle segment having transitional interface, and nozzle assembly and steam turbine including such nozzle segment |
FR3051832B1 (fr) * | 2016-05-26 | 2019-09-06 | Safran Aircraft Engines | Procede de fabrication d'un carter d'echappement de turbomachine |
US10724390B2 (en) | 2018-03-16 | 2020-07-28 | General Electric Company | Collar support assembly for airfoils |
US11655758B1 (en) * | 2022-03-31 | 2023-05-23 | Raytheon Technologies Corporation | CMC vane mate face flanges with through-ply seal slots |
Family Cites Families (65)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4063849A (en) | 1975-02-12 | 1977-12-20 | Modianos Doan D | Non-clogging, centrifugal, coaxial discharge pump |
GB1501916A (en) | 1975-06-20 | 1978-02-22 | Rolls Royce | Matching thermal expansions of components of turbo-machines |
US4000955A (en) | 1975-09-22 | 1977-01-04 | Kiyoshi Tokutomi | Fan with wide curved blades |
US3975114A (en) | 1975-09-23 | 1976-08-17 | Westinghouse Electric Corporation | Seal arrangement for turbine diaphragms and the like |
US4021135A (en) | 1975-10-09 | 1977-05-03 | Pedersen Nicholas F | Wind turbine |
US4015910A (en) * | 1976-03-09 | 1977-04-05 | The United States Of America As Represented By The Secretary Of The Air Force | Bolted paired vanes for turbine |
US4204810A (en) | 1976-11-03 | 1980-05-27 | Tokheim Corporation | Bi-directional pump |
US4309145A (en) | 1978-10-30 | 1982-01-05 | General Electric Company | Cooling air seal |
US4240990A (en) | 1979-04-10 | 1980-12-23 | Aeration Industries, Inc. | Aeration propeller and apparatus |
US4576549A (en) | 1980-07-03 | 1986-03-18 | Garden City Fan & Blower Co. | Vortex generator for centrifugal fans |
US4365929A (en) | 1981-01-16 | 1982-12-28 | Philip Retz | Vertical wind turbine power generating tower |
US4492517A (en) * | 1983-01-06 | 1985-01-08 | General Electric Company | Segmented inlet nozzle for gas turbine, and methods of installation |
DE3315350C2 (de) | 1983-04-28 | 1985-10-03 | Klein, Schanzlin & Becker Ag, 6710 Frankenthal | Leitrad für Kreiselpumpen |
EP0131736B1 (de) | 1983-06-29 | 1987-01-21 | BBC Brown Boveri AG | Axialturbine für Abgasturbolader |
US4576548A (en) | 1984-01-17 | 1986-03-18 | Westinghouse Electric Corp. | Self-aligning static seal for gas turbine stator vanes |
US4606699A (en) | 1984-02-06 | 1986-08-19 | General Electric Company | Compressor casing recess |
US4594761A (en) | 1984-02-13 | 1986-06-17 | General Electric Company | Method of fabricating hollow composite airfoils |
US4679990A (en) | 1984-12-28 | 1987-07-14 | Matsushita Electric Industrial Co., Ltd. | Electric blower |
US4686376A (en) | 1986-07-22 | 1987-08-11 | Philip Retz | Tide turbine |
CH672004A5 (de) | 1986-09-26 | 1989-10-13 | Bbc Brown Boveri & Cie | |
FR2616889B1 (fr) | 1987-06-18 | 1992-07-31 | Snecma | Carter de chambre de combustion de turboreacteur comportant des orifices de prelevement d'air |
US4907946A (en) | 1988-08-10 | 1990-03-13 | General Electric Company | Resiliently mounted outlet guide vane |
US4957412A (en) | 1988-09-06 | 1990-09-18 | Westinghouse Electric Corp. | Apparatus and method for supporting the torque load on a gas turbine vane |
JPH07101141B2 (ja) | 1989-03-14 | 1995-11-01 | シャープ株式会社 | 冷蔵庫用送風装置 |
US5253472A (en) | 1990-02-28 | 1993-10-19 | Dev Sudarshan P | Small gas turbine having enhanced fuel economy |
US5115642A (en) | 1991-01-07 | 1992-05-26 | United Technologies Corporation | Gas turbine engine case with intergral shroud support ribs |
US5149248A (en) | 1991-01-10 | 1992-09-22 | Westinghouse Electric Corp. | Apparatus and method for adapting an enlarged flow guide to an existing steam turbine |
US5066194A (en) | 1991-02-11 | 1991-11-19 | Carrier Corporation | Fan orifice structure and cover for outside enclosure of an air conditioning system |
US5209634A (en) | 1991-02-20 | 1993-05-11 | Owczarek Jerzy A | Adjustable guide vane assembly for the exhaust flow passage of a steam turbine |
US5161947A (en) | 1991-05-08 | 1992-11-10 | United Technologies Corporation | Fan case strut for turbomachine |
ES2128357T3 (es) | 1991-08-30 | 1999-05-16 | Airflow Res & Mfg | Aparato ventilador sesgado hacia adelante con inclinacion. |
US5141395A (en) * | 1991-09-05 | 1992-08-25 | General Electric Company | Flow activated flowpath liner seal |
US5244347A (en) | 1991-10-11 | 1993-09-14 | Siemens Automotive Limited | High efficiency, low noise, axial flow fan |
US5249921A (en) | 1991-12-23 | 1993-10-05 | General Electric Company | Compressor outlet guide vane support |
JP3437597B2 (ja) | 1992-03-04 | 2003-08-18 | ラツィオナル アクチエンゲゼルシャフト | ガス成分除去装置 |
EP0566089B1 (de) | 1992-04-14 | 1996-09-18 | Ebara Corporation | Pumpengehäuse in Blechbauweise |
KR950008058B1 (ko) | 1992-07-24 | 1995-07-24 | 한라공조주식회사 | 팬과 쉬라우드 조립체 |
DE4232385A1 (de) | 1992-09-26 | 1994-03-31 | Asea Brown Boveri | Gasturbine mit angeflanschtem Abgasgehäuse |
JP3232844B2 (ja) | 1993-03-29 | 2001-11-26 | 株式会社デンソー | 送風装置 |
JP3110205B2 (ja) | 1993-04-28 | 2000-11-20 | 株式会社日立製作所 | 遠心圧縮機及び羽根付ディフューザ |
JP2906939B2 (ja) | 1993-09-20 | 1999-06-21 | 株式会社日立製作所 | 軸流圧縮機 |
US5441385A (en) * | 1993-12-13 | 1995-08-15 | Solar Turbines Incorporated | Turbine nozzle/nozzle support structure |
US5454690A (en) | 1994-01-13 | 1995-10-03 | Shop Vac Corporation | Air flow housing |
DE59507918D1 (de) | 1994-03-19 | 2000-04-06 | Ksb Ag | Einrichtung zur geräuschreduzierung bei kreiselpumpen |
GB2291130B (en) | 1994-07-12 | 1998-09-30 | Rolls Royce Plc | A gas turbine engine |
FR2728015B1 (fr) * | 1994-12-07 | 1997-01-17 | Snecma | Distributeur monobloc sectorise d'un stator de turbine de turbomachine |
JP3188128B2 (ja) | 1995-02-21 | 2001-07-16 | 株式会社豊田中央研究所 | 車輌用トルクコンバータのステータ |
US5772401A (en) | 1995-10-13 | 1998-06-30 | Dresser-Rand Company | Diaphragm construction for turbomachinery |
DE19547653C2 (de) | 1995-12-20 | 1999-08-19 | Abb Patent Gmbh | Leitvorrichtung für eine Turbine mit einem Leitschaufelträger und Verfahren zur Herstellung dieser Leitvorrichtung |
US5749702A (en) | 1996-10-15 | 1998-05-12 | Air Handling Engineering Ltd. | Fan for air handling system |
JPH10205497A (ja) | 1996-11-21 | 1998-08-04 | Zexel Corp | 冷却空気導入排出装置 |
DE19753373A1 (de) | 1996-12-10 | 1998-06-25 | Papst Motoren Gmbh & Co Kg | Axiallüfter-Gehäuse |
EP0949404A1 (de) * | 1997-01-10 | 1999-10-13 | Mitsubishi Heavy Industries, Ltd. | Leitgitter, das aus einzelnen Leitschaufeln zusammengeschraubt ist |
CA2231986A1 (en) * | 1997-01-10 | 1999-09-12 | Masahito Kataoka | Stationary blade of integrated segment construction and manufacturing method therefor |
JP3794098B2 (ja) | 1997-01-31 | 2006-07-05 | 株式会社デンソー | 遠心送風機 |
DE19703033A1 (de) | 1997-01-29 | 1998-07-30 | Asea Brown Boveri | Abgasturbine eines Turboladers |
JP3604110B2 (ja) | 1997-04-25 | 2004-12-22 | 株式会社エクセディ | トルクコンバータのステータ |
DE69824925T2 (de) * | 1997-09-17 | 2005-08-25 | Mitsubishi Heavy Industries, Ltd. | Leitschaufelpaar |
DE59709447D1 (de) | 1997-11-17 | 2003-04-10 | Alstom Switzerland Ltd | Endstufe für axialdurchströmte Turbine |
JP3500292B2 (ja) | 1998-01-30 | 2004-02-23 | 日本電産コパル株式会社 | 軸流ファン |
GB9805030D0 (en) | 1998-03-11 | 1998-05-06 | Rolls Royce Plc | A stator vane assembly for a turbomachine |
US6092988A (en) | 1998-07-06 | 2000-07-25 | Ford Motor Company | Centrifugal blower assembly with a pre-swirler for an automotive vehicle |
US6077032A (en) | 1998-07-16 | 2000-06-20 | Felchar Manufacturing Corporation | Housing assembly for a vacuum cleaner |
US6077036A (en) | 1998-08-20 | 2000-06-20 | General Electric Company | Bowed nozzle vane with selective TBC |
US6109868A (en) | 1998-12-07 | 2000-08-29 | General Electric Company | Reduced-length high flow interstage air extraction |
-
2000
- 2000-10-16 DE DE10051223A patent/DE10051223A1/de not_active Withdrawn
-
2001
- 2001-09-21 DE DE50111350T patent/DE50111350D1/de not_active Expired - Lifetime
- 2001-09-21 EP EP01122716A patent/EP1199440B1/de not_active Expired - Lifetime
- 2001-10-16 US US09/977,195 patent/US6592326B2/en not_active Ceased
-
2005
- 2005-07-14 US US11/181,003 patent/USRE43611E1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1199440A3 (de) | 2004-01-21 |
EP1199440A2 (de) | 2002-04-24 |
US6592326B2 (en) | 2003-07-15 |
US20020044868A1 (en) | 2002-04-18 |
DE10051223A1 (de) | 2002-04-25 |
USRE43611E1 (en) | 2012-08-28 |
EP1199440B1 (de) | 2006-11-02 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |