FR2990462B1 - Dispositif d'attache d'aubes sur un disque de rotor de turbomachine - Google Patents
Dispositif d'attache d'aubes sur un disque de rotor de turbomachineInfo
- Publication number
- FR2990462B1 FR2990462B1 FR1254371A FR1254371A FR2990462B1 FR 2990462 B1 FR2990462 B1 FR 2990462B1 FR 1254371 A FR1254371 A FR 1254371A FR 1254371 A FR1254371 A FR 1254371A FR 2990462 B1 FR2990462 B1 FR 2990462B1
- Authority
- FR
- France
- Prior art keywords
- aubes
- attaching
- rotor disc
- turbomachine rotor
- turbomachine
- 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.)
- Active
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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
-
- 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
-
- 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
- F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/90—Coating; Surface treatment
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
- F05D2300/6033—Ceramic matrix composites [CMC]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1254371A FR2990462B1 (fr) | 2012-05-14 | 2012-05-14 | Dispositif d'attache d'aubes sur un disque de rotor de turbomachine |
GB1308312.6A GB2503976B (en) | 2012-05-14 | 2013-05-09 | A device for attaching blades to a turbine engine rotor disk |
US13/892,601 US9518470B2 (en) | 2012-05-14 | 2013-05-13 | Device for attaching blades to a turbine engine rotor disk |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1254371A FR2990462B1 (fr) | 2012-05-14 | 2012-05-14 | Dispositif d'attache d'aubes sur un disque de rotor de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2990462A1 FR2990462A1 (fr) | 2013-11-15 |
FR2990462B1 true FR2990462B1 (fr) | 2014-05-30 |
Family
ID=48672014
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1254371A Active FR2990462B1 (fr) | 2012-05-14 | 2012-05-14 | Dispositif d'attache d'aubes sur un disque de rotor de turbomachine |
Country Status (3)
Country | Link |
---|---|
US (1) | US9518470B2 (fr) |
FR (1) | FR2990462B1 (fr) |
GB (1) | GB2503976B (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3006616B1 (fr) * | 2013-06-05 | 2016-03-04 | Snecma | Preforme d'aube de turbomachine |
US10215035B2 (en) * | 2014-12-29 | 2019-02-26 | Rolls-Royce North American Technologies Inc. | Turbine wheels with preloaded blade attachment |
US20160305260A1 (en) * | 2015-03-04 | 2016-10-20 | Rolls-Royce North American Technologies, Inc. | Bladed wheel with separable platform |
US11454118B2 (en) * | 2020-09-04 | 2022-09-27 | General Electric Company | Gas turbine engine rotor blade having a root section with composite and metallic portions |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2651494A (en) * | 1949-11-24 | 1953-09-08 | Svenska Flygmotor Aktiebolaget | Turbine disk |
DE941292C (de) * | 1952-01-19 | 1956-04-05 | Escher Wyss Gmbh | Beschaufelung an axial durchstroemten Turbomaschinen |
BE517285A (fr) * | 1952-02-13 | |||
US2790620A (en) * | 1952-07-09 | 1957-04-30 | Gen Electric | Multiple finger dovetail attachment for turbine bucket |
GB731456A (en) * | 1952-11-20 | 1955-06-08 | Rolls Royce | Improvements in or relating to bladed rotors of axial-flow machines and blade elements therefor |
DE1023052B (de) * | 1955-03-31 | 1958-01-23 | Escher Wyss Gmbh | Laufrad fuer axial durchstroemte Turbomaschine |
US2957675A (en) * | 1956-05-07 | 1960-10-25 | Gen Electric | Damping means |
US2974924A (en) * | 1956-12-05 | 1961-03-14 | Gen Electric | Turbine bucket retaining means and sealing assembly |
US2999668A (en) * | 1958-08-28 | 1961-09-12 | Curtiss Wright Corp | Self-balanced rotor blade |
US2970809A (en) * | 1958-08-29 | 1961-02-07 | Westinghouse Electric Corp | Blade vibration damping arrangement for elastic fluid machines |
FR1234275A (fr) * | 1959-05-14 | 1960-10-17 | Westinghouse Electric Corp | Appareil utilisant un fluide élastique |
US3746468A (en) * | 1971-10-05 | 1973-07-17 | Westinghouse Electric Corp | Device for attaching turbine blades to a rotor |
US4084922A (en) * | 1976-12-27 | 1978-04-18 | Electric Power Research Institute, Inc. | Turbine rotor with pin mounted ceramic turbine blades |
US4767275A (en) * | 1986-07-11 | 1988-08-30 | Westinghouse Electric Corp. | Locking pin system for turbine curved root side entry closing blades |
FR2608674B1 (fr) | 1986-12-17 | 1991-04-19 | Snecma | Roue de turbine a aubes ceramique |
US5062769A (en) * | 1989-11-22 | 1991-11-05 | Ortolano Ralph J | Connector for turbine element |
FR2700362B1 (fr) * | 1993-01-14 | 1995-02-10 | Snecma | Rotor de turbomachine à attaches d'aubes par broches. |
US6364613B1 (en) * | 2000-08-15 | 2002-04-02 | General Electric Company | Hollow finger dovetail pin and method of bucket attachment using the same |
US20110206522A1 (en) * | 2010-02-24 | 2011-08-25 | Ioannis Alvanos | Rotating airfoil fabrication utilizing cmc |
EP2386721A1 (fr) * | 2010-05-14 | 2011-11-16 | Siemens Aktiengesellschaft | Dispositif de fixation pour pales de turbomachines pouvant s'écouler axialement et son procédé de fabrication |
US9175571B2 (en) * | 2012-03-19 | 2015-11-03 | General Electric Company | Connecting system for metal components and CMC components, a turbine blade retaining system and a rotating component retaining system |
-
2012
- 2012-05-14 FR FR1254371A patent/FR2990462B1/fr active Active
-
2013
- 2013-05-09 GB GB1308312.6A patent/GB2503976B/en active Active
- 2013-05-13 US US13/892,601 patent/US9518470B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20130302171A1 (en) | 2013-11-14 |
US9518470B2 (en) | 2016-12-13 |
GB201308312D0 (en) | 2013-06-19 |
FR2990462A1 (fr) | 2013-11-15 |
GB2503976A (en) | 2014-01-15 |
GB2503976B (en) | 2018-11-14 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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CD | Change of name or company name |
Owner name: SAFRAN CERAMICS, FR Effective date: 20200409 Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20200409 |
|
CD | Change of name or company name |
Owner name: SAFRAN CERAMICS, FR Effective date: 20200424 Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20200424 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |