EP1154125A3 - Aubage avec des éléments amortisseurs - Google Patents
Aubage avec des éléments amortisseurs Download PDFInfo
- Publication number
- EP1154125A3 EP1154125A3 EP01109099A EP01109099A EP1154125A3 EP 1154125 A3 EP1154125 A3 EP 1154125A3 EP 01109099 A EP01109099 A EP 01109099A EP 01109099 A EP01109099 A EP 01109099A EP 1154125 A3 EP1154125 A3 EP 1154125A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- blades
- damping elements
- damping
- blade arrangement
- 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.)
- Granted
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
- F01D5/22—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
- 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
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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10022244 | 2000-05-08 | ||
DE10022244A DE10022244A1 (de) | 2000-05-08 | 2000-05-08 | Schaufelanordnung mit Dämpfungselementen |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1154125A2 EP1154125A2 (fr) | 2001-11-14 |
EP1154125A3 true EP1154125A3 (fr) | 2003-10-29 |
EP1154125B1 EP1154125B1 (fr) | 2006-03-15 |
Family
ID=7641102
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP01109099A Expired - Lifetime EP1154125B1 (fr) | 2000-05-08 | 2001-04-12 | Aubage avec des éléments amortisseurs |
Country Status (3)
Country | Link |
---|---|
US (1) | US6478544B2 (fr) |
EP (1) | EP1154125B1 (fr) |
DE (2) | DE10022244A1 (fr) |
Families Citing this family (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6851932B2 (en) * | 2003-05-13 | 2005-02-08 | General Electric Company | Vibration damper assembly for the buckets of a turbine |
DE10340773A1 (de) * | 2003-09-02 | 2005-03-24 | Man Turbomaschinen Ag | Rotor einer Dampf- oder Gasturbine |
US7270517B2 (en) * | 2005-10-06 | 2007-09-18 | Siemens Power Generation, Inc. | Turbine blade with vibration damper |
EP1818506A1 (fr) | 2006-02-08 | 2007-08-15 | Siemens Aktiengesellschaft | Réduction de la fatigue répétitive dans un pied de sapin |
US7534090B2 (en) * | 2006-06-13 | 2009-05-19 | General Electric Company | Enhanced bucket vibration system |
DE102006041322A1 (de) * | 2006-09-01 | 2008-04-24 | Rolls-Royce Deutschland Ltd & Co Kg | Dämpfungs- und Dichtungssystem für Turbinenschaufeln |
US7762773B2 (en) * | 2006-09-22 | 2010-07-27 | Siemens Energy, Inc. | Turbine airfoil cooling system with platform edge cooling channels |
EP1925781A1 (fr) | 2006-11-23 | 2008-05-28 | Siemens Aktiengesellschaft | Agencement d'aubes |
GB0814018D0 (en) * | 2008-08-01 | 2008-09-10 | Rolls Royce Plc | Vibration damper |
US8137072B2 (en) * | 2008-10-31 | 2012-03-20 | Solar Turbines Inc. | Turbine blade including a seal pocket |
US8393869B2 (en) | 2008-12-19 | 2013-03-12 | Solar Turbines Inc. | Turbine blade assembly including a damper |
CA2754795C (fr) * | 2009-03-09 | 2016-06-07 | Avio S.P.A. | Rotor pour turbomachines |
EP2434098A1 (fr) | 2010-09-24 | 2012-03-28 | Siemens Aktiengesellschaft | Agencement d'aubes et turbine à gaz associée |
JP5675282B2 (ja) * | 2010-11-09 | 2015-02-25 | 三菱重工業株式会社 | 動翼体及び回転機械 |
US8577504B1 (en) * | 2010-11-24 | 2013-11-05 | United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration | System for suppressing vibration in turbomachine components |
US9366142B2 (en) * | 2011-10-28 | 2016-06-14 | General Electric Company | Thermal plug for turbine bucket shank cavity and related method |
US9140132B2 (en) | 2012-05-31 | 2015-09-22 | Solar Turbines Incorporated | Turbine blade support |
US9309782B2 (en) | 2012-09-14 | 2016-04-12 | General Electric Company | Flat bottom damper pin for turbine blades |
US9353629B2 (en) | 2012-11-30 | 2016-05-31 | Solar Turbines Incorporated | Turbine blade apparatus |
EP3077625B1 (fr) * | 2013-12-05 | 2019-09-25 | United Technologies Corporation | Aube creuse avec amortisseur interne |
DE102013226015A1 (de) * | 2013-12-16 | 2015-07-16 | MTU Aero Engines AG | Schaufelgitter |
US9624780B2 (en) * | 2013-12-17 | 2017-04-18 | General Electric Company | System and method for securing axially inserted buckets to a rotor assembly |
US9797270B2 (en) * | 2013-12-23 | 2017-10-24 | Rolls-Royce North American Technologies Inc. | Recessable damper for turbine |
JP6366310B2 (ja) * | 2014-03-18 | 2018-08-01 | 三菱日立パワーシステムズ株式会社 | シール構造、動翼、及び回転機械 |
EP2942481B1 (fr) | 2014-05-07 | 2019-03-27 | Rolls-Royce Corporation | Rotor pour un moteur à turbine à gaz |
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 |
EP3023584B1 (fr) * | 2014-11-24 | 2019-07-17 | MTU Aero Engines GmbH | Aube de turbomachine et turbomachine axiale |
EP3043085A1 (fr) | 2015-01-08 | 2016-07-13 | Siemens Aktiengesellschaft | Agencement d'aubes pour une turbo-machine thermique à flux axial et procédé de montage d'un élément amortisseur entre deux aubes d'une couronne d'aube d'une turbo-machine thermique |
EP3078808A1 (fr) | 2015-04-07 | 2016-10-12 | Siemens Aktiengesellschaft | Rangée d'aubes pour une turbomachine |
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 |
US10385701B2 (en) | 2015-09-03 | 2019-08-20 | General Electric Company | Damper pin for a turbine blade |
US10443408B2 (en) | 2015-09-03 | 2019-10-15 | General Electric Company | Damper pin for a turbine blade |
US10662784B2 (en) * | 2016-11-28 | 2020-05-26 | Raytheon Technologies Corporation | Damper with varying thickness for a blade |
US10731479B2 (en) | 2017-01-03 | 2020-08-04 | Raytheon Technologies Corporation | Blade platform with damper restraint |
US10677073B2 (en) | 2017-01-03 | 2020-06-09 | Raytheon Technologies Corporation | Blade platform with damper restraint |
JP7039355B2 (ja) * | 2018-03-28 | 2022-03-22 | 三菱重工業株式会社 | 回転機械 |
EP3880936B1 (fr) * | 2018-12-20 | 2023-10-18 | Siemens Energy Global GmbH & Co. KG | Système de rotor aubagé et procédé d'entretien d'un système de rotor aubagé |
CN110925030B (zh) * | 2019-12-05 | 2022-03-08 | 中国航发四川燃气涡轮研究院 | 一种带嵌入式叶冠阻尼的低压涡轮模拟叶片 |
CN113803115B (zh) * | 2020-06-16 | 2024-04-05 | 中国航发商用航空发动机有限责任公司 | 涡轮叶片缘板阻尼器、涡轮叶片和航空发动机 |
CN114382549B (zh) * | 2020-10-21 | 2024-04-23 | 中国航发商用航空发动机有限责任公司 | 涡轮和航空发动机 |
US11391157B1 (en) | 2021-03-23 | 2022-07-19 | Pratt & Whitney Canada Corp. | Damped rotor assembly |
US11525464B2 (en) | 2021-03-23 | 2022-12-13 | Pratt & Whitney Canada Corp. | Rotor with centrifugally wedged damper |
JP2023093088A (ja) * | 2021-12-22 | 2023-07-04 | 三菱重工業株式会社 | 回転機械 |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2942843A (en) * | 1956-06-15 | 1960-06-28 | Westinghouse Electric Corp | Blade vibration damping structure |
FR1263677A (fr) * | 1960-07-29 | 1961-06-09 | Havilland Engine Co Ltd | Dispositif antivibratoire applicable à des organes rotatifs |
GB2112466A (en) * | 1981-12-30 | 1983-07-20 | Rolls Royce | Rotor blade vibration damping |
SU1127979A1 (ru) * | 1983-02-23 | 1984-12-07 | Предприятие П/Я Р-6837 | Рабочее колесо турбомашины |
US5143517A (en) * | 1990-08-08 | 1992-09-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation"S.N.E.M.C.A." | Turbofan with dynamic vibration damping |
US5700133A (en) * | 1995-09-21 | 1997-12-23 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation Snecma | Damper disposition mounted between rotor vanes |
EP0918139A2 (fr) * | 1997-11-25 | 1999-05-26 | ROLLS-ROYCE plc | Amortisseur à friction |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE6910098U (de) | 1969-03-12 | 1969-07-03 | Hasso Bodenstein | Zerlegbare anbaukueche mit montagerahmen |
US4767247A (en) * | 1987-02-24 | 1988-08-30 | Westinghouse Electric Corp. | Apparatus and method for preventing relative blade motion in steam turbine |
GB2223277B (en) | 1988-09-30 | 1992-08-12 | Rolls Royce Plc | Aerofoil blade damping |
US5156528A (en) | 1991-04-19 | 1992-10-20 | General Electric Company | Vibration damping of gas turbine engine buckets |
US5205713A (en) * | 1991-04-29 | 1993-04-27 | General Electric Company | Fan blade damper |
US5261790A (en) * | 1992-02-03 | 1993-11-16 | General Electric Company | Retention device for turbine blade damper |
-
2000
- 2000-05-08 DE DE10022244A patent/DE10022244A1/de not_active Withdrawn
-
2001
- 2001-04-12 EP EP01109099A patent/EP1154125B1/fr not_active Expired - Lifetime
- 2001-04-12 DE DE50109189T patent/DE50109189D1/de not_active Expired - Lifetime
- 2001-04-12 US US09/832,846 patent/US6478544B2/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2942843A (en) * | 1956-06-15 | 1960-06-28 | Westinghouse Electric Corp | Blade vibration damping structure |
FR1263677A (fr) * | 1960-07-29 | 1961-06-09 | Havilland Engine Co Ltd | Dispositif antivibratoire applicable à des organes rotatifs |
GB2112466A (en) * | 1981-12-30 | 1983-07-20 | Rolls Royce | Rotor blade vibration damping |
SU1127979A1 (ru) * | 1983-02-23 | 1984-12-07 | Предприятие П/Я Р-6837 | Рабочее колесо турбомашины |
US5143517A (en) * | 1990-08-08 | 1992-09-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation"S.N.E.M.C.A." | Turbofan with dynamic vibration damping |
US5700133A (en) * | 1995-09-21 | 1997-12-23 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation Snecma | Damper disposition mounted between rotor vanes |
EP0918139A2 (fr) * | 1997-11-25 | 1999-05-26 | ROLLS-ROYCE plc | Amortisseur à friction |
Also Published As
Publication number | Publication date |
---|---|
US20010038793A1 (en) | 2001-11-08 |
DE50109189D1 (de) | 2006-05-11 |
US6478544B2 (en) | 2002-11-12 |
EP1154125A2 (fr) | 2001-11-14 |
EP1154125B1 (fr) | 2006-03-15 |
DE10022244A1 (de) | 2001-11-15 |
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