ES2570969T3 - Grado de turbina de gas - Google Patents
Grado de turbina de gasInfo
- Publication number
- ES2570969T3 ES2570969T3 ES13176420T ES13176420T ES2570969T3 ES 2570969 T3 ES2570969 T3 ES 2570969T3 ES 13176420 T ES13176420 T ES 13176420T ES 13176420 T ES13176420 T ES 13176420T ES 2570969 T3 ES2570969 T3 ES 2570969T3
- Authority
- ES
- Spain
- Prior art keywords
- blade
- arrangement
- impeller blades
- director
- front surface
- 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.)
- Active
Links
Classifications
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- 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
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
- F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Grado de turbina de gas con una disposición de álabes de rodete con varios álabes de rodete (1) y una disposición de álabes directores contigua con varios álabes directores (2) con bordes delanteros de la hoja del álabe director (2.1), que están opuestos a la disposición de álabes de rodete, que se caracteriza por que una ranura axial (A) mínima está conformada entre la disposición de álabes de rodete y la disposición de álabes directores, en una primera posición radial de una superficie frontal (1.2) de la disposición de álabes de rodete, entre esta superficie frontal y una primera zona de contacto (Ka) opuesta a la misma, de al menos, uno de los bordes delanteros de hoja de álabe director, y en una segunda posición radial distinta a ésta de la superficie frontal, la ranura axial (A) mínima está conformada entre la superficie frontal y una segunda zona de contacto (K¡), opuesta a la misma, de este borde delantero de la hoja de álabe director, presentando este borde delantero de la hoja de álabe director, entre la primera y la segunda zona de contacto, un desplazamiento axial de máximo 0,6% de una altura radial del borde delantero de la hoja de álabe director.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP13176420.1A EP2824277B1 (de) | 2013-07-12 | 2013-07-12 | Gasturbinenstufe |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2570969T3 true ES2570969T3 (es) | 2016-05-23 |
Family
ID=48795429
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES13176420T Active ES2570969T3 (es) | 2013-07-12 | 2013-07-12 | Grado de turbina de gas |
Country Status (3)
Country | Link |
---|---|
US (1) | US9617863B2 (es) |
EP (1) | EP2824277B1 (es) |
ES (1) | ES2570969T3 (es) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2932601C (en) | 2015-06-17 | 2023-10-03 | Rolls-Royce Corporation | Labyrinth seal with tunable flow splitter |
US10815824B2 (en) | 2017-04-04 | 2020-10-27 | General Electric | Method and system for rotor overspeed protection |
US11408300B2 (en) | 2018-12-03 | 2022-08-09 | Raytheon Technologies Corporation | Rotor overspeed protection assembly |
CN114837752A (zh) * | 2021-02-02 | 2022-08-02 | 中国航发商用航空发动机有限责任公司 | 航空发动机 |
CN114961880B (zh) * | 2021-02-22 | 2024-07-23 | 中国航发商用航空发动机有限责任公司 | 航空发动机 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1008526A (en) * | 1964-04-09 | 1965-10-27 | Rolls Royce | Axial flow bladed rotor, e.g. for a turbine |
US4238170A (en) * | 1978-06-26 | 1980-12-09 | United Technologies Corporation | Blade tip seal for an axial flow rotary machine |
US4645417A (en) * | 1984-02-06 | 1987-02-24 | General Electric Company | Compressor casing recess |
DE4344189C1 (de) * | 1993-12-23 | 1995-08-03 | Mtu Muenchen Gmbh | Axial-Schaufelgitter mit gepfeilten Schaufelvorderkanten |
US5645399A (en) * | 1995-03-15 | 1997-07-08 | United Technologies Corporation | Gas turbine engine case coated with thermal barrier coating to control axial airfoil clearance |
US6120242A (en) * | 1998-11-13 | 2000-09-19 | General Electric Company | Blade containing turbine shroud |
US6312219B1 (en) | 1999-11-05 | 2001-11-06 | General Electric Company | Narrow waist vane |
FR2875842B1 (fr) | 2004-09-28 | 2010-09-24 | Snecma Moteurs | Dispositif de limitation de survitesse de turbine dans une turbomachine |
CA2695474A1 (en) * | 2007-04-24 | 2008-10-30 | Alstom Technology Ltd. | Fluid flow engine |
US8439626B2 (en) * | 2008-12-29 | 2013-05-14 | General Electric Company | Turbine airfoil clocking |
US8562289B2 (en) * | 2010-02-26 | 2013-10-22 | Ge Aviation Systems, Llc | Method and system for a leakage controlled fan housing |
US8734113B2 (en) * | 2010-07-26 | 2014-05-27 | Snecma | Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbine |
US9037434B2 (en) * | 2012-01-03 | 2015-05-19 | General Electric Company | Method and apparatus for obtaining discrete axial clearance data using radial clearance sensors |
-
2013
- 2013-07-12 ES ES13176420T patent/ES2570969T3/es active Active
- 2013-07-12 EP EP13176420.1A patent/EP2824277B1/de active Active
-
2014
- 2014-07-08 US US14/325,785 patent/US9617863B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US9617863B2 (en) | 2017-04-11 |
EP2824277A1 (de) | 2015-01-14 |
US20150016985A1 (en) | 2015-01-15 |
EP2824277B1 (de) | 2016-03-23 |
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