DE50013633D1 - Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine - Google Patents
Rückhaltevorrichtung für Rotorschaufeln einer AxialturbomaschineInfo
- Publication number
- DE50013633D1 DE50013633D1 DE50013633T DE50013633T DE50013633D1 DE 50013633 D1 DE50013633 D1 DE 50013633D1 DE 50013633 T DE50013633 T DE 50013633T DE 50013633 T DE50013633 T DE 50013633T DE 50013633 D1 DE50013633 D1 DE 50013633D1
- Authority
- DE
- Germany
- Prior art keywords
- rotor blades
- retaining device
- axial turbomachine
- turbomachine
- axial
- 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
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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/32—Locking, e.g. by final locking blades or keys
- F01D5/326—Locking of axial insertion type blades by other 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE50013633T DE50013633D1 (de) | 1999-12-17 | 2000-08-31 | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19960896A DE19960896A1 (de) | 1999-12-17 | 1999-12-17 | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
DE50013633T DE50013633D1 (de) | 1999-12-17 | 2000-08-31 | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
Publications (1)
Publication Number | Publication Date |
---|---|
DE50013633D1 true DE50013633D1 (de) | 2006-11-30 |
Family
ID=7933025
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19960896A Withdrawn DE19960896A1 (de) | 1999-12-17 | 1999-12-17 | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
DE50013633T Expired - Lifetime DE50013633D1 (de) | 1999-12-17 | 2000-08-31 | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19960896A Withdrawn DE19960896A1 (de) | 1999-12-17 | 1999-12-17 | Rückhaltevorrichtung für Rotorschaufeln einer Axialturbomaschine |
Country Status (3)
Country | Link |
---|---|
US (1) | US6488473B1 (de) |
EP (1) | EP1120545B1 (de) |
DE (2) | DE19960896A1 (de) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB9925261D0 (en) * | 1999-10-27 | 1999-12-29 | Rolls Royce Plc | Locking devices |
US6951448B2 (en) * | 2002-04-16 | 2005-10-04 | United Technologies Corporation | Axial retention system and components thereof for a bladed rotor |
GB0302116D0 (en) * | 2003-01-30 | 2003-03-05 | Rolls Royce Plc | A rotor |
GB0413652D0 (en) | 2004-06-18 | 2004-07-21 | Rolls Royce Plc | Gas turbine engine structure |
US7530791B2 (en) * | 2005-12-22 | 2009-05-12 | Pratt & Whitney Canada Corp. | Turbine blade retaining apparatus |
JP2007247406A (ja) * | 2006-03-13 | 2007-09-27 | Ihi Corp | ファンブレードの保持構造 |
FR2900437B1 (fr) * | 2006-04-27 | 2008-07-25 | Snecma Sa | Systeme de retention des aubes dans un rotor |
FR2928406A1 (fr) * | 2008-03-07 | 2009-09-11 | Snecma Sa | Dispositif de retenue axiale d'aubes montees sur un disque de rotor de turbomachine, disque de rotor et flasque de maintien d'un tel dispositif |
US8814524B2 (en) * | 2008-12-11 | 2014-08-26 | Rolls-Royce Corporation | Wheel formed from a bladed ring and disk |
FR2939832B1 (fr) * | 2008-12-11 | 2011-01-07 | Turbomeca | Roue de turbine equipee d'un dispositif de retenue axiale verrouillant des pales par rapport a un disque. |
FR2939834B1 (fr) * | 2008-12-17 | 2016-02-19 | Turbomeca | Roue de turbine avec systeme de retention axiale des aubes |
US8905717B2 (en) | 2010-10-06 | 2014-12-09 | General Electric Company | Turbine bucket lockwire rotation prevention |
US8864471B2 (en) | 2011-08-12 | 2014-10-21 | Hamilton Sundstrand Corporation | Gas turbine rotor with purge blades |
US9112383B2 (en) | 2011-10-31 | 2015-08-18 | General Electric Company | System and method for Var injection at a distributed power generation source |
EP2696035A1 (de) | 2012-08-09 | 2014-02-12 | MTU Aero Engines GmbH | Rückhaltevorrichtung für Laufschaufeln einer Strömungsmaschine und zugehöriges Montageverfahren |
US9664056B2 (en) * | 2013-08-23 | 2017-05-30 | General Electric Company | Turbine system and adapter |
GB201317161D0 (en) * | 2013-09-27 | 2013-11-06 | Rolls Royce Plc | Retainer plate |
EP2860349A1 (de) * | 2013-10-10 | 2015-04-15 | Siemens Aktiengesellschaft | Turbinenschaufel sowie Gasturbine |
EP2860350A1 (de) * | 2013-10-10 | 2015-04-15 | Siemens Aktiengesellschaft | Turbinenschaufel sowie Gasturbine |
FR3024491B1 (fr) * | 2014-08-01 | 2018-12-07 | Safran Aircraft Engines | Ensemble rotatif pour turbomachine a dispositif de mise en place d'aubes |
KR102182102B1 (ko) | 2014-11-27 | 2020-11-23 | 한화에어로스페이스 주식회사 | 터빈 장치 |
FR3029962B1 (fr) * | 2014-12-11 | 2019-08-23 | Safran Aircraft Engines | Blocage axial des aubes dans une roue de turbomachine |
EP3564489A1 (de) * | 2018-05-03 | 2019-11-06 | Siemens Aktiengesellschaft | Rotor mit fliehkraft-optimierten kontaktflächen |
EP3581765A1 (de) * | 2018-06-11 | 2019-12-18 | Siemens Aktiengesellschaft | Rotor mit an der rotorscheibe axial verriegelten laufschaufeln |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1479332A (en) * | 1974-11-06 | 1977-07-13 | Rolls Royce | Means for retaining blades to a disc or like structure |
GB2042652B (en) * | 1979-02-21 | 1983-07-20 | Rolls Royce | Joint making packing |
US4566857A (en) * | 1980-12-19 | 1986-01-28 | United Technologies Corporation | Locking of rotor blades on a rotor disk |
FR2524932A1 (fr) * | 1982-04-08 | 1983-10-14 | Snecma | Dispositif de retenue axiale de pieds d'aube dans un disque de turbomachine |
FR2603333B1 (fr) * | 1986-09-03 | 1990-07-20 | Snecma | Rotor de turbomachine comportant un moyen de verrouillage axial et d'etancheite d'aubes montees dans des brochages axiaux du disque et procede de montage |
GB8705216D0 (en) * | 1987-03-06 | 1987-04-08 | Rolls Royce Plc | Rotor assembly |
FR2637321B1 (fr) * | 1988-10-05 | 1990-11-30 | Snecma | Rotor de turbomachine muni d'un dispositif de fixation des aubes |
US4921405A (en) * | 1988-11-10 | 1990-05-01 | Allied-Signal Inc. | Dual structure turbine blade |
US4846628A (en) | 1988-12-23 | 1989-07-11 | United Technologies Corporation | Rotor assembly for a turbomachine |
FR2663997B1 (fr) | 1990-06-27 | 1993-12-24 | Snecma | Dispositif de fixation d'une couronne de revolution sur un disque de turbomachine. |
US5112193A (en) * | 1990-09-11 | 1992-05-12 | Pratt & Whitney Canada | Fan blade axial retention device |
GB2258273B (en) * | 1991-08-02 | 1994-08-10 | Ruston Gas Turbines Ltd | Rotor blade locking arrangement |
US5256035A (en) * | 1992-06-01 | 1993-10-26 | United Technologies Corporation | Rotor blade retention and sealing construction |
FR2695433B1 (fr) * | 1992-09-09 | 1994-10-21 | Snecma | Joint annulaire d'étanchéité disposé à une extrémité axiale d'un rotor et recouvrant des brochages d'aubes. |
FR2710103B1 (fr) * | 1993-09-16 | 1995-10-20 | Snecma | Flasque de rotor de turbomachine et assemblage de ce flasque avec un rotor. |
GB9517369D0 (en) | 1995-08-24 | 1995-10-25 | Rolls Royce Plc | Bladed rotor |
GB2317652B (en) * | 1996-09-26 | 2000-05-17 | Rolls Royce Plc | Seal arrangement |
-
1999
- 1999-12-17 DE DE19960896A patent/DE19960896A1/de not_active Withdrawn
-
2000
- 2000-08-31 DE DE50013633T patent/DE50013633D1/de not_active Expired - Lifetime
- 2000-08-31 EP EP00118862A patent/EP1120545B1/de not_active Expired - Lifetime
- 2000-09-20 US US09/666,145 patent/US6488473B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1120545A3 (de) | 2004-01-14 |
DE19960896A1 (de) | 2001-06-28 |
EP1120545B1 (de) | 2006-10-18 |
US6488473B1 (en) | 2002-12-03 |
EP1120545A2 (de) | 2001-08-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |