FR2716931B1 - Système d'équilibrage et d'amortissement d'un dique de turbomachine. - Google Patents
Système d'équilibrage et d'amortissement d'un dique de turbomachine.Info
- Publication number
- FR2716931B1 FR2716931B1 FR9402441A FR9402441A FR2716931B1 FR 2716931 B1 FR2716931 B1 FR 2716931B1 FR 9402441 A FR9402441 A FR 9402441A FR 9402441 A FR9402441 A FR 9402441A FR 2716931 B1 FR2716931 B1 FR 2716931B1
- Authority
- FR
- France
- Prior art keywords
- balancing
- damping system
- turbomachine
- turbomachine disc
- disc
- 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 - Lifetime
Links
- 238000013016 damping Methods 0.000 title 1
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
- F01D5/02—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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/027—Arrangements for balancing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
- F16B2200/69—Redundant disconnection blocking means
-
- 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
- Y10T403/00—Joints and connections
- Y10T403/70—Interfitted members
- Y10T403/7005—Lugged member, rotary engagement
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9402441A FR2716931B1 (fr) | 1994-03-03 | 1994-03-03 | Système d'équilibrage et d'amortissement d'un dique de turbomachine. |
US08/393,358 US5582077A (en) | 1994-03-03 | 1995-02-23 | System for balancing and damping a turbojet engine disk |
GB9504347A GB2287510B (en) | 1994-03-03 | 1995-03-03 | Balancing and damping system for a turbomachine rotor disc |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9402441A FR2716931B1 (fr) | 1994-03-03 | 1994-03-03 | Système d'équilibrage et d'amortissement d'un dique de turbomachine. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2716931A1 FR2716931A1 (fr) | 1995-09-08 |
FR2716931B1 true FR2716931B1 (fr) | 1996-04-05 |
Family
ID=9460629
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9402441A Expired - Lifetime FR2716931B1 (fr) | 1994-03-03 | 1994-03-03 | Système d'équilibrage et d'amortissement d'un dique de turbomachine. |
Country Status (3)
Country | Link |
---|---|
US (1) | US5582077A (fr) |
FR (1) | FR2716931B1 (fr) |
GB (1) | GB2287510B (fr) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU5006900A (en) | 1999-05-13 | 2000-12-05 | Rolls-Royce Corporation | Method for designing a cyclic symmetric structure |
US6302650B1 (en) * | 1999-12-23 | 2001-10-16 | Borgwarner Inc. | Molded cooling fan |
US6375428B1 (en) * | 2000-08-10 | 2002-04-23 | The Boeing Company | Turbine blisk rim friction finger damper |
US6354780B1 (en) * | 2000-09-15 | 2002-03-12 | General Electric Company | Eccentric balanced blisk |
US6588298B2 (en) * | 2001-03-23 | 2003-07-08 | United Technologies Corporation | Rotor balancing system for turbomachinery |
US6769877B2 (en) * | 2002-10-18 | 2004-08-03 | General Electric Company | Undercut leading edge for compressor blades and related method |
US6902376B2 (en) * | 2002-12-26 | 2005-06-07 | General Electric Company | Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge |
US20040213672A1 (en) * | 2003-04-25 | 2004-10-28 | Gautreau James Charles | Undercut leading edge for compressor blades and related method |
US7121803B2 (en) * | 2002-12-26 | 2006-10-17 | General Electric Company | Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge |
FR2868807B1 (fr) * | 2004-04-09 | 2008-12-05 | Snecma Moteurs Sa | Dispositif d'equilibrage d'une piece en rotation en particulier d'un rotor de turboreacteur |
US7334960B2 (en) * | 2005-06-23 | 2008-02-26 | Siemens Power Generation, Inc. | Attachment device for removable components in hot gas paths in a turbine engine |
US20070022738A1 (en) * | 2005-07-27 | 2007-02-01 | United Technologies Corporation | Reinforcement rings for a tip turbine engine fan-turbine rotor assembly |
KR101612090B1 (ko) * | 2008-02-22 | 2016-04-12 | 호르톤 인코포레이티드 | 하이브리드 흐름 팬 장치 |
FR2930603B1 (fr) * | 2008-04-24 | 2010-04-30 | Snecma | Dispositif de retention axiale d'aubes mobiles sur un disque de rotor |
US8348616B2 (en) * | 2009-06-16 | 2013-01-08 | General Electric Company | Trapped spring balance weight and rotor assembly |
US9297258B2 (en) * | 2009-06-16 | 2016-03-29 | General Electric Company | Trapped spring balance weight and rotor assembly |
GB2481582A (en) * | 2010-06-28 | 2012-01-04 | Rolls Royce Plc | A method for predicting initial unbalance in a component such as a blisk |
US9410436B2 (en) | 2010-12-08 | 2016-08-09 | Pratt & Whitney Canada Corp. | Blade disk arrangement for blade frequency tuning |
EP2839114A1 (fr) * | 2012-04-20 | 2015-02-25 | General Electric Company | Masselotte d'équilibrage à ressort arrêté et ensemble rotor |
US9249676B2 (en) * | 2012-06-05 | 2016-02-02 | United Technologies Corporation | Turbine rotor cover plate lock |
KR101371474B1 (ko) * | 2012-08-22 | 2014-03-10 | 현대자동차주식회사 | 회전체의 밸런스 조절 장치 및 이를 이용한 동력전달 시스템 |
US9567857B2 (en) | 2013-03-08 | 2017-02-14 | Rolls-Royce North American Technologies, Inc. | Turbine split ring retention and anti-rotation method |
US10024183B2 (en) * | 2013-03-14 | 2018-07-17 | United Technologies Corporation | Gas turbine engine rotor disk-seal arrangement |
EP3049624B1 (fr) | 2013-09-26 | 2018-10-31 | United Technologies Corporation | Bague d'équilibrage pour composant rotatif |
EP2960432B1 (fr) * | 2014-05-08 | 2021-10-20 | Raytheon Technologies Corporation | Rotor et moteur à turbine à gaz comprenant un rotor |
US10415391B2 (en) | 2014-05-15 | 2019-09-17 | United Technologies Corporation | Rotor and gas turbine engine including a rotor |
US9513011B2 (en) * | 2014-06-03 | 2016-12-06 | Siemens Energy, Inc. | Gas turbine engine combustor top hat cover attachment system with lugged interlocking backing plate |
US9638037B2 (en) * | 2014-11-03 | 2017-05-02 | Pratt & Whitney Canada Corp. | Method of balancing a gas turbine engine rotor |
US10450882B2 (en) * | 2016-03-22 | 2019-10-22 | United Technologies Corporation | Anti-rotation shim seal |
US10436032B2 (en) * | 2016-05-03 | 2019-10-08 | Pratt & Whitney Canada Corp. | Damper ring |
US10450865B2 (en) | 2016-05-27 | 2019-10-22 | Pratt & Whitney Canada Corp. | Friction damper |
US10502061B2 (en) | 2016-09-28 | 2019-12-10 | Pratt & Whitney Canada Corp. | Damper groove with strain derivative amplifying pockets |
FR3057908B1 (fr) * | 2016-10-21 | 2019-11-22 | Safran Aircraft Engines | Ensemble rotatif d'une turbomachine muni d'un systeme de maintien axial d'une aube |
US10865646B2 (en) | 2017-05-04 | 2020-12-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
US10968744B2 (en) * | 2017-05-04 | 2021-04-06 | Rolls-Royce Corporation | Turbine rotor assembly having a retaining collar for a bayonet mount |
US20180320522A1 (en) * | 2017-05-04 | 2018-11-08 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
US10774678B2 (en) | 2017-05-04 | 2020-09-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
GB2571176B (en) * | 2017-12-14 | 2022-07-20 | Safran Aircraft Engines | Damping device |
US11578599B2 (en) * | 2021-02-02 | 2023-02-14 | Pratt & Whitney Canada Corp. | Rotor balance assembly |
US11525464B2 (en) | 2021-03-23 | 2022-12-13 | Pratt & Whitney Canada Corp. | Rotor with centrifugally wedged damper |
US11391157B1 (en) | 2021-03-23 | 2022-07-19 | Pratt & Whitney Canada Corp. | Damped rotor assembly |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2893694A (en) * | 1958-01-27 | 1959-07-07 | Ross A Mcclintoch | Torque, releasing, safety joint for well tool strings |
US3181835A (en) * | 1964-01-07 | 1965-05-04 | Carroll C Davis | Blade vibration damping device |
US3888601A (en) * | 1974-05-23 | 1975-06-10 | Gen Electric | Turbomachine with balancing means |
US3881844A (en) * | 1974-05-28 | 1975-05-06 | Gen Electric | Blade platform vibration dampers |
US4177692A (en) * | 1977-11-25 | 1979-12-11 | General Motors Corporation | Shaft balancing |
US4477226A (en) * | 1983-05-09 | 1984-10-16 | General Electric Company | Balance for rotating member |
GB8709421D0 (en) * | 1987-04-21 | 1987-05-28 | Lucas Ind Plc | Pressure cylinder |
US4835827A (en) * | 1987-09-08 | 1989-06-06 | United Technologies Corporation | Method of balancing a rotor |
US4848182A (en) * | 1987-09-08 | 1989-07-18 | United Technologies Corporation | Rotor balance system |
US4926710A (en) * | 1987-09-08 | 1990-05-22 | United Technologies Corporation | Method of balancing bladed gas turbine engine rotor |
US4803893A (en) * | 1987-09-24 | 1989-02-14 | United Technologies Corporation | High speed rotor balance system |
US4817455A (en) * | 1987-10-15 | 1989-04-04 | United Technologies Corporation | Gas turbine engine balancing |
FR2674569A1 (fr) * | 1991-03-27 | 1992-10-02 | Snecma | Disque ailete monobloc avec amortissement des vibrations pour turbomachine. |
US5373922A (en) * | 1993-10-12 | 1994-12-20 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Tuned mass damper for integrally bladed turbine rotor |
-
1994
- 1994-03-03 FR FR9402441A patent/FR2716931B1/fr not_active Expired - Lifetime
-
1995
- 1995-02-23 US US08/393,358 patent/US5582077A/en not_active Expired - Lifetime
- 1995-03-03 GB GB9504347A patent/GB2287510B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2716931A1 (fr) | 1995-09-08 |
GB9504347D0 (en) | 1995-04-19 |
GB2287510A (en) | 1995-09-20 |
GB2287510B (en) | 1997-07-16 |
US5582077A (en) | 1996-12-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
CD | Change of name or company name |