EP2527600A1 - Turbomaschine - Google Patents
Turbomaschine Download PDFInfo
- Publication number
- EP2527600A1 EP2527600A1 EP12167451A EP12167451A EP2527600A1 EP 2527600 A1 EP2527600 A1 EP 2527600A1 EP 12167451 A EP12167451 A EP 12167451A EP 12167451 A EP12167451 A EP 12167451A EP 2527600 A1 EP2527600 A1 EP 2527600A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- selbstjustiervorrichtung
- game
- turbomachine according
- rotor
- stationary
- 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- Withdrawn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
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
- F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
-
- 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
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
-
- 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
- F05D2300/505—Shape memory behaviour
Definitions
- the shape of the Disjustiervoriques 20 can be largely arbitrary and generally depends on the available space. Decisive in the form is the height, as in Fig. 4 is shown. In the example shown there, the height of the self-aligning device 20 under the condition of machine standstill corresponds to the minimum difference g t, min (the transient gap contribution) that would be present without the use of the self-aligning device 20.
- the centrifugal forces acting on the blade are transmitted via the finger 18 through the self-aligning device 20 to the groove 17 in the rotor 12. These forces increase with increasing rotational speed.
- the elastic properties of the self-aligning device 20 at the height g t prevent the device from being pushed flat. As a result, the game at the blade tip remains the same Bucket length greater than without the Disjustiervorides 20. However, a certain flattening of the Disjustiervorides 20 due to the mechanical stress can be accepted.
- NiTi-based shape memory alloys could be considered in the area of the hot blade root whose allowable working temperature reaches up to 200 ° C when cooling with secondary air is available in a gas turbine.
- Ternary high-temperature NiTiX alloys and others containing Hafnium Hf, Palladium Pd and / or Platinum Pt as element X extend the working temperature range up to 800 ° C and more.
- other materials / alloys may be used, provided they have the desired and required properties.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH00882/11A CH704995A1 (de) | 2011-05-24 | 2011-05-24 | Turbomaschine. |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2527600A1 true EP2527600A1 (de) | 2012-11-28 |
Family
ID=46025573
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12167451A Withdrawn EP2527600A1 (de) | 2011-05-24 | 2012-05-10 | Turbomaschine |
Country Status (6)
Country | Link |
---|---|
US (1) | US9169741B2 (ru) |
EP (1) | EP2527600A1 (ru) |
JP (1) | JP6025398B2 (ru) |
CN (1) | CN102797513B (ru) |
CH (1) | CH704995A1 (ru) |
RU (1) | RU2549922C2 (ru) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3324003A1 (en) * | 2016-11-18 | 2018-05-23 | Ansaldo Energia Switzerland AG | Blade to stator heat shield interface in a gas turbine |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20120148382A1 (en) * | 2010-12-09 | 2012-06-14 | Basf Se | Method and apparatus for the model-based monitoring of a 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 |
US9988928B2 (en) * | 2016-05-17 | 2018-06-05 | Siemens Energy, Inc. | Systems and methods for determining turbomachine engine safe start clearances following a shutdown of the turbomachine engine |
US11674399B2 (en) | 2021-07-07 | 2023-06-13 | General Electric Company | Airfoil arrangement for a gas turbine engine utilizing a shape memory alloy |
US11668317B2 (en) | 2021-07-09 | 2023-06-06 | General Electric Company | Airfoil arrangement for a gas turbine engine utilizing a shape memory alloy |
JP2023042786A (ja) * | 2021-09-15 | 2023-03-28 | 東芝エネルギーシステムズ株式会社 | タービン段落シール機構およびタービン段落シール機構の製造方法 |
US12049828B2 (en) | 2022-07-12 | 2024-07-30 | General Electric Company | Active clearance control of fan blade tip closure using a variable sleeve system |
US12006829B1 (en) | 2023-02-16 | 2024-06-11 | General Electric Company | Seal member support system for a gas turbine engine |
CN118070455B (zh) * | 2024-04-17 | 2024-07-05 | 中国航发四川燃气涡轮研究院 | 一种涡轮转静子径向装配间隙的设计方法及系统 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58206807A (ja) * | 1982-05-28 | 1983-12-02 | Hitachi Ltd | 軸流タ−ビンの動翼先端すき間制御装置 |
JPS60111004A (ja) * | 1983-11-21 | 1985-06-17 | Hitachi Ltd | 軸流形流体機械のケ−シング |
GB2354290A (en) | 1999-09-18 | 2001-03-21 | Rolls Royce Plc | Gas turbine cooling air flow control using shaped memory metal valve |
EP1467066A2 (en) | 2003-04-09 | 2004-10-13 | Rolls-Royce Plc | Corrugated seal |
EP1686243A2 (en) * | 2005-01-26 | 2006-08-02 | General Electric Company | Turbine engine stator including shape memory alloy and blade clearance control |
US20090226327A1 (en) | 2008-03-07 | 2009-09-10 | Siemens Power Generation, Inc. | Gas Turbine Engine Including Temperature Control Device and Method Using Memory Metal |
US7686569B2 (en) | 2006-12-04 | 2010-03-30 | Siemens Energy, Inc. | Blade clearance system for a turbine engine |
Family Cites Families (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1506209A (en) * | 1922-11-20 | 1924-08-26 | Ernest C Wehnert | Capping machine |
US4247247A (en) * | 1979-05-29 | 1981-01-27 | General Motors Corporation | Blade tip clearance control |
JPS57195803A (en) | 1981-05-27 | 1982-12-01 | Hitachi Ltd | Adjusting device of tip clearance in turbo fluidic machine |
JPS61103504U (ru) | 1984-12-12 | 1986-07-01 | ||
SU1506209A1 (ru) | 1986-12-15 | 1989-09-07 | Всесоюзный научно-исследовательский институт гелиевой техники | Лабиринтное уплотнение |
US5403158A (en) | 1993-12-23 | 1995-04-04 | United Technologies Corporation | Aerodynamic tip sealing for rotor blades |
DE19756734A1 (de) * | 1997-12-19 | 1999-06-24 | Bmw Rolls Royce Gmbh | Passives Spalthaltungssystem einer Gasturbine |
JPH11257014A (ja) | 1998-03-06 | 1999-09-21 | Toshiba Corp | 軸流タービンの作動流体漏洩防止装置 |
US6427712B1 (en) * | 1999-06-09 | 2002-08-06 | Robertshaw Controls Company | Ambient temperature shape memory alloy actuator |
US6367253B2 (en) * | 1999-12-20 | 2002-04-09 | Las, L.L.C. | Shape memory alloy actuators for aircraft landing gear |
US6318070B1 (en) * | 2000-03-03 | 2001-11-20 | United Technologies Corporation | Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
US8172458B2 (en) * | 2001-03-23 | 2012-05-08 | Petrakis Dennis N | Temperature responsive systems |
JP2002285802A (ja) * | 2001-03-26 | 2002-10-03 | Toshiba Corp | 回転機械のラビリンスシール装置 |
GB0326544D0 (en) * | 2003-11-14 | 2003-12-17 | Rolls Royce Plc | Variable stator vane arrangement for a compressor |
JP2005273646A (ja) | 2004-02-25 | 2005-10-06 | Mitsubishi Heavy Ind Ltd | 動翼体及びこの動翼体を有する回転機械 |
FR2881174B1 (fr) * | 2005-01-27 | 2010-08-20 | Snecma Moteurs | Dispositif de positionnement d'une aube et disque aubage comportant un tel dispositif |
GB2437298B (en) * | 2006-04-18 | 2008-10-01 | Rolls Royce Plc | A Seal Between Rotor Blade Platforms And Stator Vane Platforms, A Rotor Blade And A Stator Vane |
US7572099B2 (en) | 2006-07-06 | 2009-08-11 | United Technologies Corporation | Seal for turbine engine |
US20080079222A1 (en) * | 2006-09-28 | 2008-04-03 | Gm Global Technology Operations, Inc. | Temperature adaptive radial shaft seal assemblies using shape memory alloy elements |
JP2009203948A (ja) | 2008-02-29 | 2009-09-10 | Hitachi Ltd | シール装置,シール方法及びシール装置を有するガスタービン |
JP2009243444A (ja) | 2008-03-31 | 2009-10-22 | Ihi Corp | ジェットエンジン |
US8052380B2 (en) * | 2008-10-29 | 2011-11-08 | General Electric Company | Thermally-activated clearance reduction for a steam turbine |
FR2940350B1 (fr) * | 2008-12-23 | 2011-03-18 | Snecma | Roue mobile de turbomachine a aubes en materiau composite munie d'un anneau ressort. |
US8113771B2 (en) * | 2009-03-20 | 2012-02-14 | General Electric Company | Spring system designs for active and passive retractable seals |
US8142141B2 (en) * | 2009-03-23 | 2012-03-27 | General Electric Company | Apparatus for turbine engine cooling air management |
EP2239423A1 (de) | 2009-03-31 | 2010-10-13 | Siemens Aktiengesellschaft | Axialturbomaschine mit passiver Kontrolle des Schaufelspitzenspiels |
RU87213U1 (ru) | 2009-05-05 | 2009-09-27 | Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации | Система регулирования радиального зазора в проточной части турбомашины |
US9181817B2 (en) * | 2010-06-30 | 2015-11-10 | General Electric Company | Method and apparatus for labyrinth seal packing rings |
-
2011
- 2011-05-24 CH CH00882/11A patent/CH704995A1/de not_active Application Discontinuation
-
2012
- 2012-05-10 EP EP12167451A patent/EP2527600A1/de not_active Withdrawn
- 2012-05-23 RU RU2012121355/06A patent/RU2549922C2/ru active
- 2012-05-24 US US13/479,315 patent/US9169741B2/en active Active
- 2012-05-24 CN CN201210163558.2A patent/CN102797513B/zh active Active
- 2012-05-24 JP JP2012118739A patent/JP6025398B2/ja not_active Expired - Fee Related
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS58206807A (ja) * | 1982-05-28 | 1983-12-02 | Hitachi Ltd | 軸流タ−ビンの動翼先端すき間制御装置 |
JPS60111004A (ja) * | 1983-11-21 | 1985-06-17 | Hitachi Ltd | 軸流形流体機械のケ−シング |
GB2354290A (en) | 1999-09-18 | 2001-03-21 | Rolls Royce Plc | Gas turbine cooling air flow control using shaped memory metal valve |
EP1467066A2 (en) | 2003-04-09 | 2004-10-13 | Rolls-Royce Plc | Corrugated seal |
EP1686243A2 (en) * | 2005-01-26 | 2006-08-02 | General Electric Company | Turbine engine stator including shape memory alloy and blade clearance control |
US7686569B2 (en) | 2006-12-04 | 2010-03-30 | Siemens Energy, Inc. | Blade clearance system for a turbine engine |
US20090226327A1 (en) | 2008-03-07 | 2009-09-10 | Siemens Power Generation, Inc. | Gas Turbine Engine Including Temperature Control Device and Method Using Memory Metal |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3324003A1 (en) * | 2016-11-18 | 2018-05-23 | Ansaldo Energia Switzerland AG | Blade to stator heat shield interface in a gas turbine |
US11255212B2 (en) | 2016-11-18 | 2022-02-22 | Ansaldo Energia Switzerland AG | Blade to stator heat shield interface in a gas turbine |
Also Published As
Publication number | Publication date |
---|---|
US9169741B2 (en) | 2015-10-27 |
CN102797513B (zh) | 2016-06-15 |
JP2012246923A (ja) | 2012-12-13 |
CH704995A1 (de) | 2012-11-30 |
JP6025398B2 (ja) | 2016-11-16 |
RU2012121355A (ru) | 2013-11-27 |
RU2549922C2 (ru) | 2015-05-10 |
CN102797513A (zh) | 2012-11-28 |
US20120301280A1 (en) | 2012-11-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
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AX | Request for extension of the european patent |
Extension state: BA ME |
|
17P | Request for examination filed |
Effective date: 20130517 |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ANSALDO ENERGIA SWITZERLAND AG |
|
17Q | First examination report despatched |
Effective date: 20170906 |
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GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
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INTG | Intention to grant announced |
Effective date: 20180222 |
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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: 20180705 |