EP1329593B1 - Turbinenschaufel mit einer Heissgasplattform und einer Lastplattform - Google Patents
Turbinenschaufel mit einer Heissgasplattform und einer Lastplattform Download PDFInfo
- Publication number
- EP1329593B1 EP1329593B1 EP02001267A EP02001267A EP1329593B1 EP 1329593 B1 EP1329593 B1 EP 1329593B1 EP 02001267 A EP02001267 A EP 02001267A EP 02001267 A EP02001267 A EP 02001267A EP 1329593 B1 EP1329593 B1 EP 1329593B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- platform
- blade
- vane
- turbine
- turbine blade
- 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
Images
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
- 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
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
-
- 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
- F05D2240/80—Platforms for stationary or moving blades
Description
Claims (5)
- Turbinenschaufel (1) mit einem profilierten, entlang einer Schaufelachse (4) erstreckten Schaufelblatt (2), an das in einem Endbereich (8) eine sich quer zur Schaufelachse (4) erstreckende Heißgasplattform (12) und darüberliegend eine Lastplattform (14) angeformt sind,
dadurch gekennzeichnet, dass
eine mechanische Verbindung der Lastplattform (14) mit der Heißgasplattform (12) ausschließlich über das Schaufelblatt (2) erfolgt. - Turbinenschaufel (1) nach Anspruch 1,
dadurch gekennzeichnet, dass
die Lastplattform (14) für eine Aufnahme von Kräften ausgelegt ist, die durch ein das Schaufelblatt (2) umströmendes Arbeitsmedium hervorgerufen sind. - Turbinenschaufel (1) nach Anspruch 1 oder 2,
dadurch gekennzeichnet, dass
die Lastplattform (14) in einem Aufhängungsbereich an einer, bezogen auf ein das Schaufelblatt (2) umströmende Arbeitsmedium, abströmseitigen Kante (18) des Schaufelblatts (2) angeformt ist. - Turbinenschaufel (1) nach einem der Ansprüche 1 bis 3,
dadurch gekennzeichnet, dass
die Lastplattform (14) eine angeformte Rippe (22) zu einer Radialverhakung mit Bezug auf die Rotationsachse einer Turbinewelle und eine auf dieser aufgesetzte Rippe (24) zur Axialverhakung aufweist. - Turbinenschaufel (1) nach einem der Ansprüche 1 bis 4,
dadurch gekennzeichnet, dass
die als Leitschaufel für eine Gasturbine, insbesondere für eine stationäre Gasturbine, ausgebildet ist.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE50202538T DE50202538D1 (de) | 2002-01-17 | 2002-01-17 | Turbinenschaufel mit einer Heissgasplattform und einer Lastplattform |
AT02001267T ATE291677T1 (de) | 2002-01-17 | 2002-01-17 | Turbinenschaufel mit einer heissgasplattform und einer lastplattform |
EP02001267A EP1329593B1 (de) | 2002-01-17 | 2002-01-17 | Turbinenschaufel mit einer Heissgasplattform und einer Lastplattform |
JP2003007396A JP4249990B2 (ja) | 2002-01-17 | 2003-01-15 | タービン翼 |
US10/345,967 US6887040B2 (en) | 2001-09-12 | 2003-01-17 | Turbine blade/vane |
CNB031207006A CN1313707C (zh) | 2002-01-17 | 2003-01-17 | 透平机叶片 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02001267A EP1329593B1 (de) | 2002-01-17 | 2002-01-17 | Turbinenschaufel mit einer Heissgasplattform und einer Lastplattform |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1329593A1 EP1329593A1 (de) | 2003-07-23 |
EP1329593B1 true EP1329593B1 (de) | 2005-03-23 |
Family
ID=8185296
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP02001267A Expired - Lifetime EP1329593B1 (de) | 2001-09-12 | 2002-01-17 | Turbinenschaufel mit einer Heissgasplattform und einer Lastplattform |
Country Status (6)
Country | Link |
---|---|
US (1) | US6887040B2 (de) |
EP (1) | EP1329593B1 (de) |
JP (1) | JP4249990B2 (de) |
CN (1) | CN1313707C (de) |
AT (1) | ATE291677T1 (de) |
DE (1) | DE50202538D1 (de) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7604456B2 (en) * | 2006-04-11 | 2009-10-20 | Siemens Energy, Inc. | Vane shroud through-flow platform cover |
FR2953252B1 (fr) * | 2009-11-30 | 2012-11-02 | Snecma | Secteur de distributeur pour une turbomachine |
US20110200430A1 (en) * | 2010-02-16 | 2011-08-18 | General Electric Company | Steam turbine nozzle segment having arcuate interface |
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 |
US8920117B2 (en) | 2011-10-07 | 2014-12-30 | Pratt & Whitney Canada Corp. | Fabricated gas turbine duct |
US9546557B2 (en) * | 2012-06-29 | 2017-01-17 | General Electric Company | Nozzle, a nozzle hanger, and a ceramic to metal attachment system |
US20140023517A1 (en) * | 2012-07-23 | 2014-01-23 | General Electric Company | Nozzle for turbine system |
US9289826B2 (en) * | 2012-09-17 | 2016-03-22 | Honeywell International Inc. | Turbine stator airfoil assemblies and methods for their manufacture |
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 |
US11346234B2 (en) | 2020-01-02 | 2022-05-31 | Rolls-Royce Plc | Turbine vane assembly incorporating ceramic matrix composite materials |
US11732596B2 (en) | 2021-12-22 | 2023-08-22 | Rolls-Royce Plc | Ceramic matrix composite turbine vane assembly having minimalistic support spars |
Family Cites Families (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2500745A (en) | 1944-09-21 | 1950-03-14 | Gen Electric | Bucket structure for high-temperature turbomachines |
US3610769A (en) * | 1970-06-08 | 1971-10-05 | Gen Motors Corp | Porous facing attachment |
BE794195A (fr) | 1972-01-18 | 1973-07-18 | Bbc Sulzer Turbomaschinen | Aube directrice refroidie pour des turbines a gaz |
GB1605309A (en) | 1975-03-14 | 1989-02-01 | Rolls Royce | Stator blade for a gas turbine engine |
IT1079131B (it) | 1975-06-30 | 1985-05-08 | Gen Electric | Perfezionato raffreddamento applicabile particolarmente a elementi di turbomotori a gas |
GB1605219A (en) * | 1975-10-02 | 1984-08-30 | Rolls Royce | Stator vane for a gas turbine engine |
DE2643049A1 (de) | 1975-10-14 | 1977-04-21 | United Technologies Corp | Schaufel mit gekuehlter plattform fuer eine stroemungsmaschine |
US4283822A (en) | 1979-12-26 | 1981-08-18 | General Electric Company | Method of fabricating composite nozzles for water cooled gas turbines |
DE3244255A1 (de) * | 1982-11-30 | 1984-06-14 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Bahnvermessungs- und ueberwachungssystem |
US4987736A (en) | 1988-12-14 | 1991-01-29 | General Electric Company | Lightweight gas turbine engine frame with free-floating heat shield |
US5076049A (en) | 1990-04-02 | 1991-12-31 | General Electric Company | Pretensioned frame |
US5249418A (en) * | 1991-09-16 | 1993-10-05 | General Electric Company | Gas turbine engine polygonal structural frame with axially curved panels |
EP0550126A1 (de) | 1992-01-02 | 1993-07-07 | General Electric Company | Hitzeschild für Nachbrenner |
FR2707698B1 (fr) | 1993-07-15 | 1995-08-25 | Snecma | Turbomachine munie d'un moyen de soufflage d'air sur un élément de rotor. |
US5396763A (en) | 1994-04-25 | 1995-03-14 | General Electric Company | Cooled spraybar and flameholder assembly including a perforated hollow inner air baffle for impingement cooling an outer heat shield |
JPH08135402A (ja) | 1994-11-11 | 1996-05-28 | Mitsubishi Heavy Ind Ltd | ガスタービン静翼構造 |
US5797725A (en) * | 1997-05-23 | 1998-08-25 | Allison Advanced Development Company | Gas turbine engine vane and method of manufacture |
US6533544B1 (en) * | 1998-04-21 | 2003-03-18 | Siemens Aktiengesellschaft | Turbine blade |
EP1112440B1 (de) * | 1998-08-31 | 2003-06-18 | Siemens Aktiengesellschaft | Turbinenleitschaufel |
US6375415B1 (en) * | 2000-04-25 | 2002-04-23 | General Electric Company | Hook support for a closed circuit fluid cooled gas turbine nozzle stage segment |
-
2002
- 2002-01-17 DE DE50202538T patent/DE50202538D1/de not_active Expired - Lifetime
- 2002-01-17 AT AT02001267T patent/ATE291677T1/de not_active IP Right Cessation
- 2002-01-17 EP EP02001267A patent/EP1329593B1/de not_active Expired - Lifetime
-
2003
- 2003-01-15 JP JP2003007396A patent/JP4249990B2/ja not_active Expired - Fee Related
- 2003-01-17 CN CNB031207006A patent/CN1313707C/zh not_active Expired - Fee Related
- 2003-01-17 US US10/345,967 patent/US6887040B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE50202538D1 (de) | 2005-04-28 |
EP1329593A1 (de) | 2003-07-23 |
US6887040B2 (en) | 2005-05-03 |
ATE291677T1 (de) | 2005-04-15 |
US20030133802A1 (en) | 2003-07-17 |
CN1313707C (zh) | 2007-05-02 |
CN1436920A (zh) | 2003-08-20 |
JP2003214109A (ja) | 2003-07-30 |
JP4249990B2 (ja) | 2009-04-08 |
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