BE794573A - Dispositif de fixation d'aubes - Google Patents
Dispositif de fixation d'aubesInfo
- Publication number
- BE794573A BE794573A BE794573DA BE794573A BE 794573 A BE794573 A BE 794573A BE 794573D A BE794573D A BE 794573DA BE 794573 A BE794573 A BE 794573A
- Authority
- BE
- Belgium
- Prior art keywords
- aubes
- fixing device
- fixing
- aubes fixing
- Prior art date
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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US22284772A | 1972-02-02 | 1972-02-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
BE794573A true BE794573A (fr) | 1973-05-16 |
Family
ID=22833952
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE794573D BE794573A (fr) | 1972-02-02 | Dispositif de fixation d'aubes |
Country Status (4)
Country | Link |
---|---|
US (1) | US3734646A (xx) |
BE (1) | BE794573A (xx) |
DE (1) | DE2304291A1 (xx) |
FR (1) | FR2170692A5 (xx) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3957393A (en) * | 1974-10-29 | 1976-05-18 | United Technologies Corporation | Turbine disk and sideplate construction |
GB1479332A (en) * | 1974-11-06 | 1977-07-13 | Rolls Royce | Means for retaining blades to a disc or like structure |
US4257741A (en) * | 1978-11-02 | 1981-03-24 | General Electric Company | Turbine engine blade with airfoil projection |
US4344740A (en) * | 1979-09-28 | 1982-08-17 | United Technologies Corporation | Rotor assembly |
US4326836A (en) * | 1979-12-13 | 1982-04-27 | United Technologies Corporation | Shroud for a rotor blade |
US4453890A (en) * | 1981-06-18 | 1984-06-12 | General Electric Company | Blading system for a gas turbine engine |
FR2535793B1 (fr) * | 1982-11-08 | 1987-04-10 | Snecma | Dispositif de verrouillage axial d'aubes de soufflante |
US4480958A (en) * | 1983-02-09 | 1984-11-06 | The United States Of America As Represented By The Secretary Of The Air Force | High pressure turbine rotor two-piece blade retainer |
US4483661A (en) * | 1983-05-02 | 1984-11-20 | General Electric Company | Blade assembly for a turbomachine |
FR2586061B1 (fr) * | 1985-08-08 | 1989-06-09 | Snecma | Disque porte labyrinthe multifonction pour rotor de turbomachine |
US5030063A (en) * | 1990-02-08 | 1991-07-09 | General Motors Corporation | Turbomachine rotor |
US5205714A (en) * | 1990-07-30 | 1993-04-27 | General Electric Company | Aircraft fan blade damping apparatus |
US5137426A (en) * | 1990-08-06 | 1992-08-11 | General Electric Company | Blade shroud deformable protective coating |
US5067877A (en) * | 1990-09-11 | 1991-11-26 | United Technologies Corporation | Fan blade axial retention device |
US5302086A (en) * | 1992-08-18 | 1994-04-12 | General Electric Company | Apparatus for retaining rotor blades |
JP2726895B2 (ja) * | 1994-09-14 | 1998-03-11 | 川崎重工業株式会社 | セラミックブレードの取付構造 |
US6951448B2 (en) | 2002-04-16 | 2005-10-04 | United Technologies Corporation | Axial retention system and components thereof for a bladed rotor |
GB2396389B (en) * | 2002-12-20 | 2006-01-18 | Rolls Royce Plc | Blade arrangement for gas turbine engine |
MX2010001538A (es) * | 2007-08-08 | 2010-03-15 | Alstom Technology Ltd | Dispositivo de rotor de una turbina. |
US8182228B2 (en) * | 2007-08-16 | 2012-05-22 | General Electric Company | Turbine blade having midspan shroud with recessed wear pad and methods for manufacture |
US8206119B2 (en) * | 2009-02-05 | 2012-06-26 | General Electric Company | Turbine coverplate systems |
GB0910752D0 (en) * | 2009-06-23 | 2009-08-05 | Rolls Royce Plc | An annulus filler for a gas turbine engine |
GB0914060D0 (en) * | 2009-08-12 | 2009-09-16 | Rolls Royce Plc | A rotor assembly for a gas turbine |
GB2478918B8 (en) * | 2010-03-23 | 2013-06-19 | Rolls Royce Plc | Interstage seal |
FR2961847B1 (fr) * | 2010-06-25 | 2012-08-17 | Snecma | Roue mobile a aubes en materiau composite pour moteur a turbine a gaz a liaison pied d'aube/disque par serrage |
FR3011032B1 (fr) * | 2013-09-25 | 2017-12-29 | Snecma | Ensemble rotatif pour turbomachine |
GB2571176B (en) * | 2017-12-14 | 2022-07-20 | Safran Aircraft Engines | Damping device |
US10746098B2 (en) * | 2018-03-09 | 2020-08-18 | General Electric Company | Compressor rotor cooling apparatus |
FR3109604B1 (fr) * | 2020-04-27 | 2022-08-26 | Safran Aircraft Engines | Roue aubagee a performances d’etancheite et de retention des aubes ameliorees |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE540433A (xx) * | 1954-08-12 | |||
US3047268A (en) * | 1960-03-14 | 1962-07-31 | Stanley L Leavitt | Blade retention device |
US3216699A (en) * | 1963-10-24 | 1965-11-09 | Gen Electric | Airfoil member assembly |
US3395891A (en) * | 1967-09-21 | 1968-08-06 | Gen Electric | Lock for turbomachinery blades |
US3572970A (en) * | 1969-01-23 | 1971-03-30 | Gen Electric | Turbomachinery blade spacer |
US3644058A (en) * | 1970-05-18 | 1972-02-22 | Westinghouse Electric Corp | Axial positioner and seal for turbine blades |
-
0
- BE BE794573D patent/BE794573A/xx unknown
-
1972
- 1972-02-02 US US00222847A patent/US3734646A/en not_active Expired - Lifetime
-
1973
- 1973-01-30 FR FR7303125A patent/FR2170692A5/fr not_active Expired
- 1973-01-30 DE DE2304291A patent/DE2304291A1/de active Pending
Also Published As
Publication number | Publication date |
---|---|
DE2304291A1 (de) | 1973-08-09 |
US3734646A (en) | 1973-05-22 |
FR2170692A5 (xx) | 1973-09-14 |
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