BR0101675A - Amortecedor de lâmina e método para fazer o mesmo - Google Patents
Amortecedor de lâmina e método para fazer o mesmoInfo
- Publication number
- BR0101675A BR0101675A BR0101675-0A BR0101675A BR0101675A BR 0101675 A BR0101675 A BR 0101675A BR 0101675 A BR0101675 A BR 0101675A BR 0101675 A BR0101675 A BR 0101675A
- Authority
- BR
- Brazil
- Prior art keywords
- blades
- retainer
- doing
- damper
- blade
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
-
- 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
- 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
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/50—Vibration damping features
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49337—Composite blade
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)
Abstract
Patente de Invenção: "AMORTECEDOR DE LâMINA E MéTODO PARA FAZER O MESMO". Amortecedor de lâmina (50) de motor de turbina (10) para vibrações de amortecimento de lâminas(12) em um motor de turbina (10). O amortecedor de lâmina (50) inclui um corpo alongado (52) que se estende entre uma extremidade dianteira (54) e uma extremidade traseira (56) oposta à extremidade dianteira (54). O corpo é dimensionado e moldado para receber dentro um vão (46) formado entre plataformas adjacentes (22) das lâminas (12), de modo que o corpo (52) engate, em forma de atrito, tais plataformas adjacentes (22) para amortecer as vibrações de tais lâminas (12) e para impedir que o ar passe através de tal vão (46) durante a operação do motor (10). O amortecedor (50) também inclui um retentor (70) montado pelo menos em uma de tais extremidades dianteira e traseira (56) do corpo (52). O retentor (70) é dimensionado e moldado em pelo menos uma das lâminas adjacentes (12) para manter o corpo (52) entre as lâminas (12). O retentor (70) é dimensionado e moldado para impedir que o ar passe entre as lâminas (12) e o retentor (70) durante a operação do motor (10).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/607,750 US6354803B1 (en) | 2000-06-30 | 2000-06-30 | Blade damper and method for making same |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0101675A true BR0101675A (pt) | 2002-02-13 |
Family
ID=24433565
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR0101675-0A BR0101675A (pt) | 2000-06-30 | 2001-04-27 | Amortecedor de lâmina e método para fazer o mesmo |
Country Status (7)
Country | Link |
---|---|
US (1) | US6354803B1 (pt) |
EP (1) | EP1167691B1 (pt) |
JP (1) | JP2002030902A (pt) |
BR (1) | BR0101675A (pt) |
CA (1) | CA2344628C (pt) |
DE (1) | DE60112516T2 (pt) |
ES (1) | ES2245671T3 (pt) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6901821B2 (en) * | 2001-11-20 | 2005-06-07 | United Technologies Corporation | Stator damper anti-rotation assembly |
JP3782367B2 (ja) * | 2002-03-29 | 2006-06-07 | ミネベア株式会社 | ブレード保持金具の製造方法及びその製造装置 |
US6776583B1 (en) * | 2003-02-27 | 2004-08-17 | General Electric Company | Turbine bucket damper pin |
US6851932B2 (en) * | 2003-05-13 | 2005-02-08 | General Electric Company | Vibration damper assembly for the buckets of a turbine |
JP4254352B2 (ja) * | 2003-06-04 | 2009-04-15 | 株式会社Ihi | タービンブレード |
US6932575B2 (en) | 2003-10-08 | 2005-08-23 | United Technologies Corporation | Blade damper |
US7367123B2 (en) * | 2005-05-12 | 2008-05-06 | General Electric Company | Coated bucket damper pin and related method |
US7270517B2 (en) * | 2005-10-06 | 2007-09-18 | Siemens Power Generation, Inc. | Turbine blade with vibration damper |
WO2007101757A1 (de) * | 2006-03-06 | 2007-09-13 | Alstom Technology Ltd | Gasturbine mit ringförmigem hitzeschild und abgewinkelten dichtungsstreifen |
US7534090B2 (en) * | 2006-06-13 | 2009-05-19 | General Electric Company | Enhanced bucket vibration system |
US7731482B2 (en) * | 2006-06-13 | 2010-06-08 | General Electric Company | Bucket vibration damper system |
US7762780B2 (en) * | 2007-01-25 | 2010-07-27 | Siemens Energy, Inc. | Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies |
GB2463036B (en) * | 2008-08-29 | 2011-04-20 | Rolls Royce Plc | A blade arrangement |
GB0816467D0 (en) * | 2008-09-10 | 2008-10-15 | Rolls Royce Plc | Turbine blade damper arrangement |
US8137072B2 (en) * | 2008-10-31 | 2012-03-20 | Solar Turbines Inc. | Turbine blade including a seal pocket |
US9840931B2 (en) * | 2008-11-25 | 2017-12-12 | Ansaldo Energia Ip Uk Limited | Axial retention of a platform seal |
US8393869B2 (en) | 2008-12-19 | 2013-03-12 | Solar Turbines Inc. | Turbine blade assembly including a damper |
EP2280151A1 (en) * | 2009-06-23 | 2011-02-02 | Alstom Technology Ltd | Method for operating a gas turbine and rotor of a gas turbine |
US20110255958A1 (en) * | 2010-04-16 | 2011-10-20 | General Electric Company | Seal member for hot gas path component |
FR2963383B1 (fr) * | 2010-07-27 | 2016-09-09 | Snecma | Aube de turbomachine, rotor, turbine basse pression et turbomachine equipes d'une telle aube |
EP2418356A1 (de) * | 2010-08-10 | 2012-02-15 | Siemens Aktiengesellschaft | Dämpfungselement für ein Turbinenschaufelrad und entsprechend ausgebildete Turbinenschaufel |
US8790086B2 (en) * | 2010-11-11 | 2014-07-29 | General Electric Company | Turbine blade assembly for retaining sealing and dampening elements |
EP2455587B1 (de) * | 2010-11-17 | 2019-01-23 | MTU Aero Engines GmbH | Rotor für eine Strömungsmaschine, zugehörige Strömungsmaschine und Verfahren zum Herstellen, Reparieren oder Überholen |
US9133855B2 (en) | 2010-11-15 | 2015-09-15 | 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 |
GB2486488A (en) | 2010-12-17 | 2012-06-20 | Ge Aviat Systems Ltd | Testing a transient voltage protection device |
US8905715B2 (en) * | 2011-03-17 | 2014-12-09 | General Electric Company | Damper and seal pin arrangement for a turbine blade |
RU2553049C2 (ru) * | 2011-07-01 | 2015-06-10 | Альстом Текнолоджи Лтд | Лопатка ротора турбины, ротор турбины и турбина |
US10287897B2 (en) | 2011-09-08 | 2019-05-14 | General Electric Company | Turbine rotor blade assembly and method of assembling same |
US9039382B2 (en) | 2011-11-29 | 2015-05-26 | General Electric Company | Blade skirt |
US10113434B2 (en) * | 2012-01-31 | 2018-10-30 | United Technologies Corporation | Turbine blade damper seal |
CN109386310A (zh) | 2012-06-30 | 2019-02-26 | 通用电气公司 | 涡轮机叶片密封结构 |
US9309782B2 (en) | 2012-09-14 | 2016-04-12 | General Electric Company | Flat bottom damper pin for turbine blades |
US9194238B2 (en) | 2012-11-28 | 2015-11-24 | General Electric Company | System for damping vibrations in a turbine |
US10202853B2 (en) | 2013-09-11 | 2019-02-12 | General Electric Company | Ply architecture for integral platform and damper retaining features in CMC turbine blades |
US9797270B2 (en) * | 2013-12-23 | 2017-10-24 | Rolls-Royce North American Technologies Inc. | Recessable damper for turbine |
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 |
JP5863894B2 (ja) * | 2014-07-09 | 2016-02-17 | 三菱日立パワーシステムズ株式会社 | 動翼体及び回転機械 |
EP2985419B1 (en) * | 2014-08-13 | 2020-01-08 | United Technologies Corporation | Turbomachine blade assembly with blade root seals |
US10443408B2 (en) | 2015-09-03 | 2019-10-15 | General Electric Company | Damper pin for a turbine blade |
US10385701B2 (en) | 2015-09-03 | 2019-08-20 | General Electric Company | Damper pin for a turbine blade |
US10472975B2 (en) | 2015-09-03 | 2019-11-12 | General Electric Company | Damper pin having elongated bodies for damping adjacent turbine blades |
US10584597B2 (en) | 2015-09-03 | 2020-03-10 | General Electric Company | Variable cross-section damper pin for a turbine blade |
EP3438410B1 (en) | 2017-08-01 | 2021-09-29 | General Electric Company | Sealing system for a rotary machine |
DE102018218944A1 (de) * | 2018-11-07 | 2020-05-07 | Siemens Aktiengesellschaft | Rotor mit Abdichtung zwischen Laufschaufeln |
FR3124214A1 (fr) * | 2021-06-18 | 2022-12-23 | Safran Aircraft Engines | Module de soufflante a joint ameliore |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1460714A (en) * | 1973-06-26 | 1977-01-06 | Rolls Royce | Bladed rotor for a gas turbine engine |
JPS6075660U (ja) * | 1983-10-31 | 1985-05-27 | 株式会社小松製作所 | 内燃機関のシ−ル装置 |
US4936749A (en) | 1988-12-21 | 1990-06-26 | General Electric Company | Blade-to-blade vibration damper |
US5215442A (en) * | 1991-10-04 | 1993-06-01 | General Electric Company | Turbine blade platform damper |
US5302085A (en) | 1992-02-03 | 1994-04-12 | General Electric Company | Turbine blade damper |
US5749705A (en) | 1996-10-11 | 1998-05-12 | General Electric Company | Retention system for bar-type damper of rotor blade |
US5746578A (en) | 1996-10-11 | 1998-05-05 | General Electric Company | Retention system for bar-type damper of rotor |
-
2000
- 2000-06-30 US US09/607,750 patent/US6354803B1/en not_active Expired - Fee Related
-
2001
- 2001-04-19 CA CA002344628A patent/CA2344628C/en not_active Expired - Fee Related
- 2001-04-20 ES ES01303645T patent/ES2245671T3/es not_active Expired - Lifetime
- 2001-04-20 DE DE60112516T patent/DE60112516T2/de not_active Expired - Lifetime
- 2001-04-20 EP EP01303645A patent/EP1167691B1/en not_active Expired - Lifetime
- 2001-04-27 JP JP2001130944A patent/JP2002030902A/ja active Pending
- 2001-04-27 BR BR0101675-0A patent/BR0101675A/pt active Search and Examination
Also Published As
Publication number | Publication date |
---|---|
DE60112516D1 (de) | 2005-09-15 |
CA2344628C (en) | 2007-07-03 |
EP1167691A2 (en) | 2002-01-02 |
EP1167691B1 (en) | 2005-08-10 |
JP2002030902A (ja) | 2002-01-31 |
CA2344628A1 (en) | 2001-12-30 |
EP1167691A3 (en) | 2003-10-15 |
DE60112516T2 (de) | 2006-06-08 |
US6354803B1 (en) | 2002-03-12 |
ES2245671T3 (es) | 2006-01-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B11D | Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time |