FR2518164B1 - Dispositif pour amortir l'energie vibratoire des pales d'un rotor et assemblage de rotor avec un tel dispositif d'amortissement - Google Patents
Dispositif pour amortir l'energie vibratoire des pales d'un rotor et assemblage de rotor avec un tel dispositif d'amortissementInfo
- Publication number
- FR2518164B1 FR2518164B1 FR8220821A FR8220821A FR2518164B1 FR 2518164 B1 FR2518164 B1 FR 2518164B1 FR 8220821 A FR8220821 A FR 8220821A FR 8220821 A FR8220821 A FR 8220821A FR 2518164 B1 FR2518164 B1 FR 2518164B1
- Authority
- FR
- France
- Prior art keywords
- rotor
- damping
- blades
- assembly
- vibratory energy
- 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.)
- Expired
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
- 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
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/330,423 US4455122A (en) | 1981-12-14 | 1981-12-14 | Blade to blade vibration damper |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2518164A1 FR2518164A1 (fr) | 1983-06-17 |
FR2518164B1 true FR2518164B1 (fr) | 1986-01-17 |
Family
ID=23289718
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8220821A Expired FR2518164B1 (fr) | 1981-12-14 | 1982-12-13 | Dispositif pour amortir l'energie vibratoire des pales d'un rotor et assemblage de rotor avec un tel dispositif d'amortissement |
Country Status (5)
Country | Link |
---|---|
US (1) | US4455122A (fr) |
JP (1) | JPS58107802A (fr) |
DE (1) | DE3245069A1 (fr) |
FR (1) | FR2518164B1 (fr) |
GB (1) | GB2111130B (fr) |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4505642A (en) * | 1983-10-24 | 1985-03-19 | United Technologies Corporation | Rotor blade interplatform seal |
US4505640A (en) * | 1983-12-13 | 1985-03-19 | United Technologies Corporation | Seal means for a blade attachment slot of a rotor assembly |
US4659285A (en) * | 1984-07-23 | 1987-04-21 | United Technologies Corporation | Turbine cover-seal assembly |
US4743164A (en) * | 1986-12-29 | 1988-05-10 | United Technologies Corporation | Interblade seal for turbomachine rotor |
US4872812A (en) * | 1987-08-05 | 1989-10-10 | General Electric Company | Turbine blade plateform sealing and vibration damping apparatus |
CA1340877C (fr) * | 1987-12-28 | 2000-01-18 | Takashi Sugiyama | Polypeptide inhibant l'elastage et procede de production par la technologie de l'adn recombinant |
GB2223277B (en) * | 1988-09-30 | 1992-08-12 | Rolls Royce Plc | Aerofoil blade damping |
US4872810A (en) * | 1988-12-14 | 1989-10-10 | United Technologies Corporation | Turbine rotor retention system |
US4936749A (en) * | 1988-12-21 | 1990-06-26 | General Electric Company | Blade-to-blade vibration damper |
GB2228541B (en) * | 1989-02-23 | 1993-04-14 | Rolls Royce Plc | Device for damping vibrations in turbomachinery blades |
EP0437977A1 (fr) * | 1990-01-18 | 1991-07-24 | United Technologies Corporation | Configuration de jante de disque de turbine |
US5313786A (en) * | 1992-11-24 | 1994-05-24 | United Technologies Corporation | Gas turbine blade damper |
US5284421A (en) * | 1992-11-24 | 1994-02-08 | United Technologies Corporation | Rotor blade with platform support and damper positioning means |
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 |
US5478207A (en) * | 1994-09-19 | 1995-12-26 | General Electric Company | Stable blade vibration damper for gas turbine engine |
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 |
US5993160A (en) * | 1997-12-11 | 1999-11-30 | Pratt & Whitney Canada Inc. | Cover plate for gas turbine rotor |
US6171058B1 (en) * | 1999-04-01 | 2001-01-09 | General Electric Company | Self retaining blade damper |
US6575704B1 (en) * | 1999-06-07 | 2003-06-10 | Siemens Aktiengesellschaft | Turbomachine and sealing element for a rotor thereof |
US6607359B2 (en) | 2001-03-02 | 2003-08-19 | Hood Technology Corporation | Apparatus for passive damping of flexural blade vibration in turbo-machinery |
US6932575B2 (en) * | 2003-10-08 | 2005-08-23 | United Technologies Corporation | Blade damper |
US7467924B2 (en) * | 2005-08-16 | 2008-12-23 | United Technologies Corporation | Turbine blade including revised platform |
US9022727B2 (en) * | 2010-11-15 | 2015-05-05 | Mtu Aero Engines Gmbh | Rotor for a turbo machine |
US10113434B2 (en) | 2012-01-31 | 2018-10-30 | United Technologies Corporation | Turbine blade damper seal |
US10641109B2 (en) * | 2013-03-13 | 2020-05-05 | United Technologies Corporation | Mass offset for damping performance |
EP2806106A1 (fr) | 2013-05-23 | 2014-11-26 | MTU Aero Engines GmbH | Aube de turbomachine avec corps d'impulsion |
US9765625B2 (en) * | 2013-05-23 | 2017-09-19 | MTU Aero Engines AG | Turbomachine blade |
CN103790709B (zh) * | 2014-02-19 | 2017-07-28 | 中国航空动力机械研究所 | 涡轮轮盘 |
DE102014214270A1 (de) * | 2014-07-22 | 2016-02-18 | MTU Aero Engines AG | Schaufelgitter für eine Turbomaschine |
DE102014223231B4 (de) | 2014-11-13 | 2017-09-07 | MTU Aero Engines AG | Turbomaschinenschaufelanordnung |
US9920637B2 (en) | 2015-04-07 | 2018-03-20 | United Technologies Corporation | Gas turbine engine damping device |
EP3477048B1 (fr) * | 2017-10-27 | 2021-08-18 | MTU Aero Engines AG | Agencement d'étanchéité d'une interstice entre aubes de turbomachine et de réduction des vibrations des aubes de turbomachine |
JP7039355B2 (ja) * | 2018-03-28 | 2022-03-22 | 三菱重工業株式会社 | 回転機械 |
US11162368B2 (en) * | 2019-06-13 | 2021-11-02 | Raytheon Technologies Corporation | Airfoil assembly with ceramic airfoil pieces and seal |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB670665A (en) * | 1949-07-28 | 1952-04-23 | Rolls Royce | Improvements in or relating to compressors and turbines |
US2935297A (en) * | 1954-06-09 | 1960-05-03 | Stalker Corp | Vibration dampers for rotor blades |
US2912223A (en) * | 1955-03-17 | 1959-11-10 | Gen Electric | Turbine bucket vibration dampener and sealing assembly |
US2948505A (en) * | 1956-12-26 | 1960-08-09 | Gen Electric | Gas turbine rotor |
US3037741A (en) * | 1958-12-29 | 1962-06-05 | Gen Electric | Damping turbine buckets |
GB1259750A (en) * | 1970-07-23 | 1972-01-12 | Rolls Royce | Rotor for a fluid flow machine |
US3752599A (en) * | 1971-03-29 | 1973-08-14 | Gen Electric | Bucket vibration damping device |
US3752598A (en) * | 1971-11-17 | 1973-08-14 | United Aircraft Corp | Segmented duct seal |
-
1981
- 1981-12-14 US US06/330,423 patent/US4455122A/en not_active Expired - Lifetime
-
1982
- 1982-12-03 GB GB08234470A patent/GB2111130B/en not_active Expired
- 1982-12-06 DE DE19823245069 patent/DE3245069A1/de active Granted
- 1982-12-13 FR FR8220821A patent/FR2518164B1/fr not_active Expired
- 1982-12-14 JP JP57220018A patent/JPS58107802A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
DE3245069C2 (fr) | 1991-12-19 |
GB2111130B (en) | 1984-10-03 |
JPS58107802A (ja) | 1983-06-27 |
FR2518164A1 (fr) | 1983-06-17 |
GB2111130A (en) | 1983-06-29 |
JPH0319881B2 (fr) | 1991-03-18 |
DE3245069A1 (de) | 1983-06-16 |
US4455122A (en) | 1984-06-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |