EP3025029A1 - Anordnung zur befestigung von turbinenschaufeln - Google Patents
Anordnung zur befestigung von turbinenschaufelnInfo
- Publication number
- EP3025029A1 EP3025029A1 EP14759132.5A EP14759132A EP3025029A1 EP 3025029 A1 EP3025029 A1 EP 3025029A1 EP 14759132 A EP14759132 A EP 14759132A EP 3025029 A1 EP3025029 A1 EP 3025029A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- turbine
- arrangement
- turbine blade
- stemmstück
- turbine blades
- 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.)
- Withdrawn
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
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
-
- 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
- F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/31—Application in turbines in steam turbines
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
-
- 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
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/502—Thermal properties
- F05D2300/5021—Expansivity
- F05D2300/50212—Expansivity dissimilar
Definitions
- the invention relates to an arrangement for mounting turbine blades, wherein the turbine blades have a turbine blade root which is fitted in a groove in a component, wherein between the turbine blade root and the component a Stemm forum is arranged.
- the invention seeks to remedy this situation.
- the object of the invention is to provide an arrangement for which less effort has to be expended. This object is achieved by an arrangement for fastening ⁇ tion of turbine blades, wherein the turbine blades have a turbine blade root, which is fitted into a groove in a Kom ⁇ component, between the turbine blade foot and the component a Stemm Gi is arranged, wherein the Stemm Gi is a bi-metal and the turbine blade is designed as a turbine vane.
- the Stemm caravane for fixing the turbine blade from a bi-metalmainsti ⁇ ren proposed.
- the Stemm conductede should be performed straight at installation temperature and have a small excess between 0.1mm and 0.2mm. In this case, the turbine blades can be pushed over the retaining pieces with little effort. From vorzu to the blade ⁇ tension or to jam and thus fixed in their final position, the small excess is sufficient.
- Tempe ⁇ temperature is forcibly increased in operation, which leads to a bending of the bimetal in the direction of the turbine blade root. This means that a force is exerted by the bi-metal on the turbine blade root and the groove, resulting in a fixation.
- FIG. 1 shows a schematic representation of a turbine blade root in a component
- FIG. 2 shows a bi-metal clamping piece at installation temperature
- FIG. 3 shows a bi-metal clamping piece at the operating temperature
- FIG. 4 shows a schematic illustration of a turbine guide blade foot
- FIG. 5 shows a schematic representation of a turbine guide blade foot with a hammer foot shape.
- FIG. 1 shows an arrangement for fastening turbine blades 2 in a groove 3 of a component 4.
- the turbine blade 2 has a turbine blade root 5, which is fitted into the corresponding groove 3.
- a Stemm merging 6 is arranged, wherein the Stemm facilitator 6 is a bi-metal.
- the turbine blade 2 is designed as a turbine guide vane for a steam turbine. Likewise, the turbine blade 2 could be formed as a compressor blade for a gas turbine or a Ver ⁇ poet .
- the component 4 is formed as a housing, in particular inner casing of a steam turbine.
- the caulking piece 6 comprises a first material 7 and a second one Material 8, which is connected by rigid end connections 9 firmly together.
- the first material 7 has a different thermal expansion behavior compared to the second material 8.
- the geometric shape of the Stemm couples 6 is changed with an increase in the temperature, which is shown in Figure 3.
- the Stemm generate 6 shows a deflection in one direction. Since the Stemm poll 6 is arranged at installation temperature in a gap 10 between the turbine blade root 5 and the groove 3, carried by a temperature increase during operation, a power increase between the turbine blade root 5 and the groove 3, which leads to a better fixation of the turbine blade 2 ,
- Tur ⁇ binenleitschaufel has a designed as a hook leg Tur ⁇ binenschaufelfuß. 5 This has a surface 12 pointing to a guide slide carrier 11. In the guide vane ⁇ carrier 11, a gap 13 is formed, in which the Stemm forum 6 is arranged.
- FIG. 5 shows a turbine blade root 5 designed as a hammer base.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP14759132.5A EP3025029A1 (de) | 2013-09-24 | 2014-08-29 | Anordnung zur befestigung von turbinenschaufeln |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP13185739.3A EP2851515A1 (de) | 2013-09-24 | 2013-09-24 | Anordnung zur Befestigung von Turbinenschaufeln |
PCT/EP2014/068354 WO2015043874A1 (de) | 2013-09-24 | 2014-08-29 | Anordnung zur befestigung von turbinenschaufeln |
EP14759132.5A EP3025029A1 (de) | 2013-09-24 | 2014-08-29 | Anordnung zur befestigung von turbinenschaufeln |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3025029A1 true EP3025029A1 (de) | 2016-06-01 |
Family
ID=49303725
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13185739.3A Withdrawn EP2851515A1 (de) | 2013-09-24 | 2013-09-24 | Anordnung zur Befestigung von Turbinenschaufeln |
EP14759132.5A Withdrawn EP3025029A1 (de) | 2013-09-24 | 2014-08-29 | Anordnung zur befestigung von turbinenschaufeln |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13185739.3A Withdrawn EP2851515A1 (de) | 2013-09-24 | 2013-09-24 | Anordnung zur Befestigung von Turbinenschaufeln |
Country Status (3)
Country | Link |
---|---|
US (1) | US20160194970A1 (de) |
EP (2) | EP2851515A1 (de) |
WO (1) | WO2015043874A1 (de) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP7011952B2 (ja) * | 2018-03-01 | 2022-01-27 | 三菱パワー株式会社 | 静翼セグメント、及びこれを備えている蒸気タービン |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2013512A (en) * | 1933-03-11 | 1935-09-03 | Laval Steam Turbine Co | Guide vane and diaphragm construction for turbines |
US2807435A (en) * | 1951-06-12 | 1957-09-24 | Fairchild Engine & Airplane | Turbine stator blade |
CH655547B (de) * | 1981-11-10 | 1986-04-30 | ||
JPS61129405A (ja) * | 1984-11-28 | 1986-06-17 | Hitachi Ltd | タ−ビン動翼固定方法 |
CH676735A5 (de) * | 1988-08-03 | 1991-02-28 | Asea Brown Boveri | |
US6290466B1 (en) * | 1999-09-17 | 2001-09-18 | General Electric Company | Composite blade root attachment |
US7488153B2 (en) * | 2002-07-01 | 2009-02-10 | Alstom Technology Ltd. | Steam turbine |
EP1548232A1 (de) * | 2003-12-23 | 2005-06-29 | Siemens Aktiengesellschaft | Strömungsmaschine mit einem Leitschaufelträger und Verfahren zum Montieren von Leitschaufeln an einen Leitschaufelträger |
EP2239423A1 (de) * | 2009-03-31 | 2010-10-13 | Siemens Aktiengesellschaft | Axialturbomaschine mit passiver Kontrolle des Schaufelspitzenspiels |
EP2372095A1 (de) * | 2010-03-26 | 2011-10-05 | Siemens Aktiengesellschaft | Verfahren und Vorrichtung zur Befestigung einer Schaufel am Rotor mittels Formgedächtniswerkstoff |
FR2975428B1 (fr) * | 2011-05-17 | 2015-11-20 | Snecma | Roue a aubes de turbomachine |
FR2978796B1 (fr) * | 2011-08-03 | 2013-08-09 | Snecma | Roue a aubes de turbomachine |
DE102013213834A1 (de) * | 2013-07-15 | 2015-02-19 | MTU Aero Engines AG | Verfahren zum Herstellen eines Isolationselements und Isolationselement für ein Gehäuse eines Flugtriebwerks |
-
2013
- 2013-09-24 EP EP13185739.3A patent/EP2851515A1/de not_active Withdrawn
-
2014
- 2014-08-29 US US14/915,686 patent/US20160194970A1/en not_active Abandoned
- 2014-08-29 WO PCT/EP2014/068354 patent/WO2015043874A1/de active Application Filing
- 2014-08-29 EP EP14759132.5A patent/EP3025029A1/de not_active Withdrawn
Non-Patent Citations (2)
Title |
---|
None * |
See also references of WO2015043874A1 * |
Also Published As
Publication number | Publication date |
---|---|
WO2015043874A1 (de) | 2015-04-02 |
EP2851515A1 (de) | 2015-03-25 |
US20160194970A1 (en) | 2016-07-07 |
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Legal Events
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PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
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Effective date: 20160224 |
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AX | Request for extension of the european patent |
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DAX | Request for extension of the european patent (deleted) | ||
GRAP | Despatch of communication of intention to grant a patent |
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INTG | Intention to grant announced |
Effective date: 20170531 |
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RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: SIEMENS AKTIENGESELLSCHAFT |
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STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
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18D | Application deemed to be withdrawn |
Effective date: 20171011 |