FR2523209B1 - Amortisseur d'aube et assemblage d'amortissement d'aubes dans un rotor - Google Patents
Amortisseur d'aube et assemblage d'amortissement d'aubes dans un rotorInfo
- Publication number
- FR2523209B1 FR2523209B1 FR8303676A FR8303676A FR2523209B1 FR 2523209 B1 FR2523209 B1 FR 2523209B1 FR 8303676 A FR8303676 A FR 8303676A FR 8303676 A FR8303676 A FR 8303676A FR 2523209 B1 FR2523209 B1 FR 2523209B1
- Authority
- FR
- France
- Prior art keywords
- blade
- rotor
- damping assembly
- damper
- blade damper
- 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
- 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
- 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
-
- 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)
- Fluid-Damping Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/358,136 US4473337A (en) | 1982-03-12 | 1982-03-12 | Blade damper seal |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2523209A1 FR2523209A1 (fr) | 1983-09-16 |
FR2523209B1 true FR2523209B1 (fr) | 1988-04-29 |
Family
ID=23408447
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8303676A Expired FR2523209B1 (fr) | 1982-03-12 | 1983-03-07 | Amortisseur d'aube et assemblage d'amortissement d'aubes dans un rotor |
Country Status (5)
Country | Link |
---|---|
US (1) | US4473337A (fr) |
JP (1) | JPS58167804A (fr) |
DE (1) | DE3307571A1 (fr) |
FR (1) | FR2523209B1 (fr) |
GB (1) | GB2116641B (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4568247A (en) * | 1984-03-29 | 1986-02-04 | United Technologies Corporation | Balanced blade vibration damper |
US4743164A (en) * | 1986-12-29 | 1988-05-10 | United Technologies Corporation | Interblade seal for turbomachine rotor |
US4872810A (en) * | 1988-12-14 | 1989-10-10 | United Technologies Corporation | Turbine rotor retention system |
FR2726323B1 (fr) * | 1994-10-26 | 1996-12-13 | Snecma | Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine |
FR2732416B1 (fr) * | 1995-03-29 | 1997-04-30 | Snecma | Agencement de raccordement de deux secteurs angulaires de turbomachine et joint concu pour servir dans cet agencement |
US5785499A (en) * | 1996-12-24 | 1998-07-28 | United Technologies Corporation | Turbine blade damper and seal |
GB0814018D0 (en) * | 2008-08-01 | 2008-09-10 | Rolls Royce Plc | Vibration damper |
US9366142B2 (en) * | 2011-10-28 | 2016-06-14 | General Electric Company | Thermal plug for turbine bucket shank cavity and related method |
US9650901B2 (en) * | 2012-05-31 | 2017-05-16 | Solar Turbines Incorporated | Turbine damper |
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 |
US9297263B2 (en) | 2012-10-31 | 2016-03-29 | Solar Turbines Incorporated | Turbine blade for a gas turbine engine |
US9228443B2 (en) | 2012-10-31 | 2016-01-05 | Solar Turbines Incorporated | Turbine rotor assembly |
US9303519B2 (en) | 2012-10-31 | 2016-04-05 | Solar Turbines Incorporated | Damper for a turbine rotor assembly |
EP2984303A4 (fr) | 2013-04-12 | 2016-12-21 | United Technologies Corp | Couvercle pour un ensemble rotor d'une turbine à gaz |
US10184345B2 (en) | 2013-08-09 | 2019-01-22 | United Technologies Corporation | Cover plate assembly for a gas turbine engine |
FR3027949B1 (fr) * | 2014-11-04 | 2019-07-26 | Safran Aircraft Engines | Roue de turbine pour une turbomachine |
EP4316979A4 (fr) | 2021-03-30 | 2024-07-31 | Sony Group Corp | Procédé de traitement d'informations, dispositif de traitement d'informations, support lisible par ordinateur et système d'imagerie |
CN114542522A (zh) * | 2022-02-21 | 2022-05-27 | 杭州汽轮机股份有限公司 | 一种压气机叶片阻尼器及装配方法 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3112915A (en) * | 1961-12-22 | 1963-12-03 | Gen Electric | Rotor assembly air baffle |
GB996729A (en) * | 1963-12-16 | 1965-06-30 | Rolls Royce | Improvements relating to turbines and compressors |
US3318573A (en) * | 1964-08-19 | 1967-05-09 | Director Of Nat Aerospace Lab | Apparatus for maintaining rotor disc of gas turbine engine at a low temperature |
US3295825A (en) * | 1965-03-10 | 1967-01-03 | Gen Motors Corp | Multi-stage turbine rotor |
CH494896A (de) * | 1968-08-09 | 1970-08-15 | Sulzer Ag | Halterung von Laufschaufeln im Rotor einer Turbomaschine |
GB1259750A (en) * | 1970-07-23 | 1972-01-12 | Rolls Royce | Rotor for a fluid flow machine |
US3666376A (en) * | 1971-01-05 | 1972-05-30 | United Aircraft Corp | Turbine blade damper |
US3709631A (en) * | 1971-03-18 | 1973-01-09 | Caterpillar Tractor Co | Turbine blade seal arrangement |
US3841792A (en) * | 1973-03-09 | 1974-10-15 | Westinghouse Electric Corp | Turbomachine blade lock and seal device |
US3936222A (en) * | 1974-03-28 | 1976-02-03 | United Technologies Corporation | Gas turbine construction |
US3887298A (en) * | 1974-05-30 | 1975-06-03 | United Aircraft Corp | Apparatus for sealing turbine blade damper cavities |
US4101245A (en) * | 1976-12-27 | 1978-07-18 | United Technologies Corporation | Interblade damper and seal for turbomachinery rotor |
US4182598A (en) * | 1977-08-29 | 1980-01-08 | United Technologies Corporation | Turbine blade damper |
JPS5517204A (en) * | 1978-07-19 | 1980-02-06 | Itsuki Ban | Brushless dc motor |
-
1982
- 1982-03-12 US US06/358,136 patent/US4473337A/en not_active Expired - Fee Related
-
1983
- 1983-03-03 DE DE19833307571 patent/DE3307571A1/de active Granted
- 1983-03-07 GB GB08306222A patent/GB2116641B/en not_active Expired
- 1983-03-07 FR FR8303676A patent/FR2523209B1/fr not_active Expired
- 1983-03-11 JP JP58041382A patent/JPS58167804A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
US4473337A (en) | 1984-09-25 |
JPS58167804A (ja) | 1983-10-04 |
DE3307571C2 (fr) | 1992-02-27 |
FR2523209A1 (fr) | 1983-09-16 |
DE3307571A1 (de) | 1983-09-22 |
GB2116641A (en) | 1983-09-28 |
JPH0477121B2 (fr) | 1992-12-07 |
GB8306222D0 (en) | 1983-04-13 |
GB2116641B (en) | 1985-03-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |