NO20052830L - Tetnings- og dempningsanordning for turbinblad - Google Patents
Tetnings- og dempningsanordning for turbinbladInfo
- Publication number
- NO20052830L NO20052830L NO20052830A NO20052830A NO20052830L NO 20052830 L NO20052830 L NO 20052830L NO 20052830 A NO20052830 A NO 20052830A NO 20052830 A NO20052830 A NO 20052830A NO 20052830 L NO20052830 L NO 20052830L
- Authority
- NO
- Norway
- Prior art keywords
- damper
- turbine blade
- damping device
- seal
- blade sealing
- Prior art date
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
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
- F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
-
- 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
-
- 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
- F01D11/006—Sealing the gap between rotor blades or blades and rotor
-
- 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
- F01D25/04—Antivibration arrangements
- F01D25/06—Antivibration arrangements for preventing blade vibration
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/10—Anti- vibration means
-
- 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
-
- 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
- F01D5/16—Form or construction for counteracting blade vibration
-
- 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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Gasket Seals (AREA)
Abstract
Demper- og tetningsanordning for turbinblad omfattende en tetning og en demper som begge grenser mot ei radialt ytterste flate hvor det ikke er noen gassvei. Tetningen er laget av et plastisk deformerbart materiale og er irmfelt i en utsparing i demperen. Demperen er laget av et stivt materiale som absorberer vibrasjonsenergi som bhr darmet under drift. Utsparingen i demperen muliggjør at både demperen og tetningen kan være posisjonert ved den radialt ytterste flata hvor det ikke er noen gassvei.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/939,766 US7121800B2 (en) | 2004-09-13 | 2004-09-13 | Turbine blade nested seal damper assembly |
Publications (2)
Publication Number | Publication Date |
---|---|
NO20052830D0 NO20052830D0 (no) | 2005-06-10 |
NO20052830L true NO20052830L (no) | 2006-03-14 |
Family
ID=35241055
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO20052830A NO20052830L (no) | 2004-09-13 | 2005-06-10 | Tetnings- og dempningsanordning for turbinblad |
Country Status (9)
Country | Link |
---|---|
US (1) | US7121800B2 (no) |
EP (1) | EP1635037A3 (no) |
JP (1) | JP2006077759A (no) |
KR (1) | KR20060048029A (no) |
CN (1) | CN1749531A (no) |
AU (1) | AU2005202260B2 (no) |
CA (1) | CA2507086A1 (no) |
NO (1) | NO20052830L (no) |
SG (1) | SG121034A1 (no) |
Families Citing this family (71)
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GB0611031D0 (en) | 2006-06-06 | 2006-07-12 | Rolls Royce Plc | An aerofoil stage and a seal for use therein |
GB2446812A (en) | 2007-02-21 | 2008-08-27 | Rolls Royce Plc | Damping member positioned between blades of an aerofoil assembly |
US8011892B2 (en) * | 2007-06-28 | 2011-09-06 | United Technologies Corporation | Turbine blade nested seal and damper assembly |
EP2053286A1 (en) * | 2007-10-25 | 2009-04-29 | Siemens Aktiengesellschaft | Seal strip and turbine blade assembly |
WO2009053169A1 (en) * | 2007-10-25 | 2009-04-30 | Siemens Aktiengesellschaft | Turbine blade assembly and seal strip |
US7918265B2 (en) * | 2008-02-14 | 2011-04-05 | United Technologies Corporation | Method and apparatus for as-cast seal on turbine blades |
US8070448B2 (en) * | 2008-10-30 | 2011-12-06 | Honeywell International Inc. | Spacers and turbines |
US8393869B2 (en) * | 2008-12-19 | 2013-03-12 | Solar Turbines Inc. | Turbine blade assembly including a damper |
US8167566B2 (en) * | 2008-12-31 | 2012-05-01 | General Electric Company | Rotor dovetail hook-to-hook fit |
ES2542160T3 (es) | 2009-03-09 | 2015-07-31 | Ge Avio S.R.L. | Rotor para turbomáquinas con álabes con corona |
WO2010103551A1 (en) * | 2009-03-09 | 2010-09-16 | Avio S.P.A. | Rotor for turbomachines |
US8696320B2 (en) * | 2009-03-12 | 2014-04-15 | General Electric Company | Gas turbine having seal assembly with coverplate and seal |
US20100232939A1 (en) * | 2009-03-12 | 2010-09-16 | General Electric Company | Machine Seal Assembly |
US8529201B2 (en) * | 2009-12-17 | 2013-09-10 | United Technologies Corporation | Blade outer air seal formed of stacked panels |
US8672626B2 (en) * | 2010-04-21 | 2014-03-18 | United Technologies Corporation | Engine assembled seal |
FR2963383B1 (fr) * | 2010-07-27 | 2016-09-09 | Snecma | Aube de turbomachine, rotor, turbine basse pression et turbomachine equipes d'une telle aube |
US8790086B2 (en) | 2010-11-11 | 2014-07-29 | General Electric Company | Turbine blade assembly for retaining sealing and dampening elements |
US9022727B2 (en) * | 2010-11-15 | 2015-05-05 | Mtu Aero Engines Gmbh | Rotor for a turbo machine |
US8876478B2 (en) | 2010-11-17 | 2014-11-04 | General Electric Company | Turbine blade combined damper and sealing pin and related method |
FR2970033B1 (fr) | 2011-01-04 | 2015-10-16 | Turbomeca | Procede d'amortissement de pale de turbine a gaz et amortisseur de vibration de mise en oeuvre |
EP2520768A1 (de) * | 2011-05-02 | 2012-11-07 | MTU Aero Engines AG | Dichteinrichtung für einen integral beschaufelten Rotorgrundkörper einer Strömungsmaschine |
US10287897B2 (en) * | 2011-09-08 | 2019-05-14 | General Electric Company | Turbine rotor blade assembly and method of assembling same |
US9366142B2 (en) * | 2011-10-28 | 2016-06-14 | General Electric Company | Thermal plug for turbine bucket shank cavity and related method |
US10113434B2 (en) | 2012-01-31 | 2018-10-30 | United Technologies Corporation | Turbine blade damper seal |
US9121286B2 (en) | 2012-04-24 | 2015-09-01 | United Technologies Corporation | Airfoil having tapered buttress |
US9296039B2 (en) | 2012-04-24 | 2016-03-29 | United Technologies Corporation | Gas turbine engine airfoil impingement cooling |
US8915718B2 (en) | 2012-04-24 | 2014-12-23 | United Technologies Corporation | Airfoil including damper member |
US9267380B2 (en) | 2012-04-24 | 2016-02-23 | United Technologies Corporation | Airfoil including loose damper |
US9243502B2 (en) | 2012-04-24 | 2016-01-26 | United Technologies Corporation | Airfoil cooling enhancement and method of making the same |
US9181806B2 (en) | 2012-04-24 | 2015-11-10 | United Technologies Corporation | Airfoil with powder damper |
US9470095B2 (en) | 2012-04-24 | 2016-10-18 | United Technologies Corporation | Airfoil having internal lattice network |
US9175570B2 (en) | 2012-04-24 | 2015-11-03 | United Technologies Corporation | Airfoil including member connected by articulated joint |
US9133712B2 (en) | 2012-04-24 | 2015-09-15 | United Technologies Corporation | Blade having porous, abradable element |
US9249668B2 (en) | 2012-04-24 | 2016-02-02 | United Technologies Corporation | Airfoil with break-way, free-floating damper member |
US9074482B2 (en) | 2012-04-24 | 2015-07-07 | United Technologies Corporation | Airfoil support method and apparatus |
US9404369B2 (en) | 2012-04-24 | 2016-08-02 | United Technologies Corporation | Airfoil having minimum distance ribs |
EP2679770A1 (en) * | 2012-06-26 | 2014-01-01 | Siemens Aktiengesellschaft | Platform seal strip for a gas turbine |
US9587495B2 (en) * | 2012-06-29 | 2017-03-07 | United Technologies Corporation | Mistake proof damper pocket seals |
EP2882941B1 (en) | 2012-06-30 | 2021-09-29 | General Electric Company | A turbine blade sealing structure with a specific arrangement of plies |
US10247023B2 (en) | 2012-09-28 | 2019-04-02 | United Technologies Corporation | Seal damper with improved retention |
US9151165B2 (en) | 2012-10-22 | 2015-10-06 | United Technologies Corporation | Reversible blade damper |
US9347325B2 (en) * | 2012-10-31 | 2016-05-24 | Solar Turbines Incorporated | Damper for a turbine rotor assembly |
US20140271205A1 (en) * | 2013-03-12 | 2014-09-18 | Solar Turbines Incorporated | Turbine blade pin seal |
US10641109B2 (en) | 2013-03-13 | 2020-05-05 | United Technologies Corporation | Mass offset for damping performance |
WO2014159152A1 (en) * | 2013-03-13 | 2014-10-02 | United Technologies Corporation | Turbine blade and damper retention |
US10036260B2 (en) * | 2013-03-13 | 2018-07-31 | United Technologies Corporation | Damper mass distribution to prevent damper rotation |
US9903434B2 (en) | 2013-08-21 | 2018-02-27 | General Electric Company | Components having vibration dampers enclosed therein and methods of forming such components |
JP6240786B2 (ja) | 2013-09-11 | 2017-11-29 | ゼネラル・エレクトリック・カンパニイ | Cmcタービンブレードの一体のプラットフォーム及びダンパ保持特徴のためのプライ構造 |
WO2015069362A2 (en) * | 2013-09-17 | 2015-05-14 | United Technologies Corporation | Gas turbine engine with seal having protrusions |
US9732620B2 (en) | 2013-09-26 | 2017-08-15 | United Technologies Corporation | Snap in platform damper and seal assembly for a gas turbine engine |
EP2881544A1 (en) * | 2013-12-09 | 2015-06-10 | Siemens Aktiengesellschaft | Airfoil device for a gas turbine and corresponding arrangement |
JP6272044B2 (ja) * | 2014-01-17 | 2018-01-31 | 三菱重工業株式会社 | 動翼体のシール構造、動翼体及び回転機械 |
US9856737B2 (en) * | 2014-03-27 | 2018-01-02 | United Technologies Corporation | Blades and blade dampers for gas turbine engines |
CN103982250B (zh) * | 2014-05-12 | 2015-07-22 | 天津大学 | 具有冷却功能的金属橡胶减振器 |
US10030530B2 (en) | 2014-07-31 | 2018-07-24 | United Technologies Corporation | Reversible blade rotor seal |
US9995162B2 (en) * | 2014-10-20 | 2018-06-12 | United Technologies Corporation | Seal and clip-on damper system and device |
US9863257B2 (en) * | 2015-02-04 | 2018-01-09 | United Technologies Corporation | Additive manufactured inseparable platform damper and seal assembly for a gas turbine engine |
US9822644B2 (en) | 2015-02-27 | 2017-11-21 | Pratt & Whitney Canada Corp. | Rotor blade vibration damper |
US9810075B2 (en) * | 2015-03-20 | 2017-11-07 | United Technologies Corporation | Faceted turbine blade damper-seal |
US9790809B2 (en) * | 2015-03-24 | 2017-10-17 | United Technologies Corporation | Damper for stator assembly |
JP6554882B2 (ja) * | 2015-04-07 | 2019-08-07 | 株式会社Ihi | シールド部材及びそれを用いたジェットエンジン |
US9920637B2 (en) | 2015-04-07 | 2018-03-20 | United Technologies Corporation | Gas turbine engine damping device |
US10472975B2 (en) * | 2015-09-03 | 2019-11-12 | General Electric Company | Damper pin having elongated bodies for damping adjacent turbine blades |
US10100648B2 (en) | 2015-12-07 | 2018-10-16 | United Technologies Corporation | Damper seal installation features |
US10316673B2 (en) | 2016-03-24 | 2019-06-11 | General Electric Company | CMC turbine blade platform damper |
JP6689117B2 (ja) * | 2016-03-31 | 2020-04-28 | 三菱日立パワーシステムズ株式会社 | 軸流回転機械に装備される静翼環及び軸流回転機械 |
EP3438410B1 (en) | 2017-08-01 | 2021-09-29 | General Electric Company | Sealing system for a rotary machine |
US10746047B2 (en) * | 2017-10-27 | 2020-08-18 | General Electric Company | Structure for mitigating vibratory modes of counter-rotating engine rotors |
US10927692B2 (en) | 2018-08-06 | 2021-02-23 | General Electric Company | Turbomachinery sealing apparatus and method |
US10774653B2 (en) | 2018-12-11 | 2020-09-15 | Raytheon Technologies Corporation | Composite gas turbine engine component with lattice structure |
US11401815B2 (en) * | 2018-12-20 | 2022-08-02 | Siemens Energy Global GmbH & Co. KG | Bladed rotor system and corresponding method of servicing |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4101245A (en) * | 1976-12-27 | 1978-07-18 | United Technologies Corporation | Interblade damper and seal for turbomachinery rotor |
GB1549152A (en) * | 1977-01-11 | 1979-08-01 | Rolls Royce | Rotor stage for a gas trubine engine |
FR2527260A1 (fr) * | 1982-05-18 | 1983-11-25 | Snecma | Dispositif d'amortissement escamotable pour aubes d'une turbomachine |
JP3230091B2 (ja) * | 1990-06-25 | 2001-11-19 | ウェルファイド株式会社 | ヒト血清アルブミンの着色抑制方法 |
US5228835A (en) * | 1992-11-24 | 1993-07-20 | United Technologies Corporation | Gas turbine blade seal |
US5415526A (en) * | 1993-11-19 | 1995-05-16 | Mercadante; Anthony J. | Coolable rotor assembly |
US5460489A (en) | 1994-04-12 | 1995-10-24 | United Technologies Corporation | Turbine blade damper and seal |
US5573375A (en) | 1994-12-14 | 1996-11-12 | United Technologies Corporation | Turbine engine rotor blade platform sealing and vibration damping device |
US5513955A (en) * | 1994-12-14 | 1996-05-07 | United Technologies Corporation | Turbine engine rotor blade platform seal |
US5827047A (en) * | 1996-06-27 | 1998-10-27 | United Technologies Corporation | Turbine blade damper and seal |
US5924699A (en) * | 1996-12-24 | 1999-07-20 | United Technologies Corporation | Turbine blade platform seal |
US5785499A (en) * | 1996-12-24 | 1998-07-28 | United Technologies Corporation | Turbine blade damper and seal |
JPH1181906A (ja) | 1997-09-04 | 1999-03-26 | Ishikawajima Harima Heavy Ind Co Ltd | タービン動翼のハイブリット緩衝体 |
US6273683B1 (en) * | 1999-02-05 | 2001-08-14 | Siemens Westinghouse Power Corporation | Turbine blade platform seal |
US6171058B1 (en) * | 1999-04-01 | 2001-01-09 | General Electric Company | Self retaining blade damper |
JP2001021245A (ja) * | 1999-07-09 | 2001-01-26 | Irie Koken Kk | 蓄冷材及び蓄冷器 |
US6315298B1 (en) * | 1999-11-22 | 2001-11-13 | United Technologies Corporation | Turbine disk and blade assembly seal |
US6471484B1 (en) * | 2001-04-27 | 2002-10-29 | General Electric Company | Methods and apparatus for damping rotor assembly vibrations |
-
2004
- 2004-09-13 US US10/939,766 patent/US7121800B2/en active Active
-
2005
- 2005-05-10 SG SG200502935A patent/SG121034A1/en unknown
- 2005-05-11 CA CA002507086A patent/CA2507086A1/en not_active Abandoned
- 2005-05-20 KR KR1020050042237A patent/KR20060048029A/ko not_active Application Discontinuation
- 2005-05-24 AU AU2005202260A patent/AU2005202260B2/en not_active Expired - Fee Related
- 2005-06-10 NO NO20052830A patent/NO20052830L/no not_active Application Discontinuation
- 2005-07-12 JP JP2005202609A patent/JP2006077759A/ja active Pending
- 2005-07-13 EP EP05254378A patent/EP1635037A3/en not_active Withdrawn
- 2005-07-13 CN CNA2005100832831A patent/CN1749531A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
SG121034A1 (en) | 2006-04-26 |
KR20060048029A (ko) | 2006-05-18 |
US7121800B2 (en) | 2006-10-17 |
US20060056974A1 (en) | 2006-03-16 |
CA2507086A1 (en) | 2006-03-13 |
EP1635037A3 (en) | 2009-06-24 |
EP1635037A2 (en) | 2006-03-15 |
AU2005202260B2 (en) | 2007-05-10 |
JP2006077759A (ja) | 2006-03-23 |
NO20052830D0 (no) | 2005-06-10 |
AU2005202260A1 (en) | 2006-03-30 |
CN1749531A (zh) | 2006-03-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FC2A | Withdrawal, rejection or dismissal of laid open patent application |