FR2874232B1 - Rotor metallique renforce de fibres. - Google Patents
Rotor metallique renforce de fibres.Info
- Publication number
- FR2874232B1 FR2874232B1 FR9809633A FR9809633A FR2874232B1 FR 2874232 B1 FR2874232 B1 FR 2874232B1 FR 9809633 A FR9809633 A FR 9809633A FR 9809633 A FR9809633 A FR 9809633A FR 2874232 B1 FR2874232 B1 FR 2874232B1
- Authority
- FR
- France
- Prior art keywords
- strengthened
- fibers
- metallic rotor
- rotor
- metallic
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/006—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels
-
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
-
- 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
- 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
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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9809633A FR2874232B1 (fr) | 1998-07-28 | 1998-07-28 | Rotor metallique renforce de fibres. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9809633A FR2874232B1 (fr) | 1998-07-28 | 1998-07-28 | Rotor metallique renforce de fibres. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2874232A1 FR2874232A1 (fr) | 2006-02-17 |
FR2874232B1 true FR2874232B1 (fr) | 2007-06-15 |
Family
ID=35768611
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9809633A Expired - Lifetime FR2874232B1 (fr) | 1998-07-28 | 1998-07-28 | Rotor metallique renforce de fibres. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2874232B1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2887919B1 (fr) * | 2005-06-29 | 2010-12-31 | Snecma Moteurs | Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite |
US7547194B2 (en) * | 2006-07-31 | 2009-06-16 | General Electric Company | Rotor blade and method of fabricating the same |
US7784182B2 (en) * | 2006-11-08 | 2010-08-31 | General Electric Company | System for manufacturing a rotor having an MMC ring component and a unitary airfoil component |
US7766623B2 (en) | 2006-11-08 | 2010-08-03 | General Electric Company | System for manufacturing a rotor having an MMC ring component and an airfoil component having monolithic airfoils |
FR2956599B1 (fr) * | 2010-02-22 | 2012-04-27 | Snecma | Procede pour la realisation d'un anneau aubage monobloc |
DE102016120346A1 (de) | 2016-10-25 | 2018-04-26 | Rolls-Royce Deutschland Ltd & Co Kg | Verdichterrotor einer Strömungsmaschine |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1040697A (fr) * | 1951-04-14 | 1953-10-16 | Perfectionnements aux rotors et notamment à ceux de compresseurs, turbines et moteurs à réaction | |
US4011295A (en) * | 1974-10-07 | 1977-03-08 | The Garrett Corporation | Ceramic rotor for gas turbine engine |
GB2161109B (en) * | 1984-07-07 | 1988-12-21 | Rolls Royce | Integral bladed member |
US4867644A (en) * | 1987-05-15 | 1989-09-19 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US5030277A (en) * | 1990-12-17 | 1991-07-09 | The United States Of America As Represented By The Secretary Of The Air Force | Method and titanium aluminide matrix composite |
DE4319727C2 (de) * | 1993-06-15 | 1996-08-29 | Mtu Muenchen Gmbh | Verfahren zur Herstellung eines Schaufelringes für einen trommelartig aufgebauten Rotor, insbesondere Verdichterrotor einer Turbomaschine |
US5660526A (en) * | 1995-06-05 | 1997-08-26 | Allison Engine Company, Inc. | Gas turbine rotor with remote support rings |
GB9619890D0 (en) * | 1996-09-24 | 1996-11-06 | Rolls Royce Plc | A method of making a fibre reinforced metal component |
-
1998
- 1998-07-28 FR FR9809633A patent/FR2874232B1/fr not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2874232A1 (fr) | 2006-02-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 18 |
|
PLFP | Fee payment |
Year of fee payment: 19 |
|
PLFP | Fee payment |
Year of fee payment: 20 |