FR2887919B1 - Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite - Google Patents
Rotor de turbomachine comprenant au moins un disque renforce par un anneau compositeInfo
- Publication number
- FR2887919B1 FR2887919B1 FR0506629A FR0506629A FR2887919B1 FR 2887919 B1 FR2887919 B1 FR 2887919B1 FR 0506629 A FR0506629 A FR 0506629A FR 0506629 A FR0506629 A FR 0506629A FR 2887919 B1 FR2887919 B1 FR 2887919B1
- Authority
- FR
- France
- Prior art keywords
- composite ring
- turbomachine rotor
- reinforced disk
- reinforced
- disk
- 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
- 239000002131 composite material Substances 0.000 title 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C49/00—Alloys containing metallic or non-metallic fibres or 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
- F01D5/12—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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
-
- 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
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
- F05D2230/232—Manufacture essentially without removing material by permanently joining parts together by welding
- F05D2230/237—Brazing
-
- 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
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
- F05D2300/133—Titanium
-
- 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
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
- F05D2300/2112—Aluminium oxides
-
- 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
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/22—Non-oxide ceramics
- F05D2300/226—Carbides
- F05D2300/2261—Carbides of silicon
-
- 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
- F05D2300/6032—Metal matrix composites [MMC]
-
- 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
- F05D2300/614—Fibres or filaments
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0506629A FR2887919B1 (fr) | 2005-06-29 | 2005-06-29 | Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite |
EP06116258.2A EP1739282B1 (fr) | 2005-06-29 | 2006-06-28 | Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite |
CA2551342A CA2551342C (fr) | 2005-06-29 | 2006-06-28 | Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite |
US11/427,106 US7334999B2 (en) | 2005-06-29 | 2006-06-28 | Turbomachine rotor including at least one disk reinforced by a composite ring |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0506629A FR2887919B1 (fr) | 2005-06-29 | 2005-06-29 | Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2887919A1 FR2887919A1 (fr) | 2007-01-05 |
FR2887919B1 true FR2887919B1 (fr) | 2010-12-31 |
Family
ID=35809820
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0506629A Active FR2887919B1 (fr) | 2005-06-29 | 2005-06-29 | Rotor de turbomachine comprenant au moins un disque renforce par un anneau composite |
Country Status (4)
Country | Link |
---|---|
US (1) | US7334999B2 (fr) |
EP (1) | EP1739282B1 (fr) |
CA (1) | CA2551342C (fr) |
FR (1) | FR2887919B1 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006015838A1 (de) * | 2006-04-03 | 2007-10-04 | Rolls-Royce Deutschland Ltd & Co Kg | Axialkompressor für ein Gasturbinentriebwerk |
US7748959B1 (en) * | 2006-04-20 | 2010-07-06 | Florida Turbine Technologies, Inc. | Insulated turbine disc of a turbo-pump |
US8011877B2 (en) * | 2008-11-24 | 2011-09-06 | General Electric Company | Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades |
CN102032213B (zh) * | 2010-12-30 | 2012-09-26 | 北京理工大学 | 一种端区叶片前缘仿生处理方法 |
CN102031466B (zh) * | 2011-01-10 | 2012-10-10 | 哈尔滨工业大学 | 一种TiN涂层碳化硅纤维增强钛基复合材料及其制备方法 |
FR2970266B1 (fr) * | 2011-01-10 | 2013-12-06 | Snecma | Procede de fabrication d'une piece metallique annulaire monobloc a insert de renfort en materiau composite, et piece obtenue |
FR2970715B1 (fr) * | 2011-01-21 | 2014-10-17 | Snecma | Structure fibreuse tissee multicouches ayant une partie tubulaire creuse, procede de fabrication et piece composite la comportant |
US10648481B2 (en) * | 2014-11-17 | 2020-05-12 | United Technologies Corporation | Fiber reinforced spacer for a gas turbine engine |
GB201707836D0 (en) * | 2017-05-16 | 2017-06-28 | Oscar Propulsion Ltd | Outlet guide vanes |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE7033020U (de) * | 1970-09-04 | 1972-04-06 | Motoren Turbinen Union | Turbinenradscheibe. |
US3966523A (en) * | 1975-08-11 | 1976-06-29 | United Technologies Corporation | Method of making filament reinforced composite rings from plural flat filamentary spiral layers |
DE3037388C1 (de) * | 1980-10-03 | 1982-06-16 | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5300 Bonn | Bandage zur radialen Spannung der Segmente eines aus Einzelsegmenten aufgebauten Verdichterlaufrades fuer Gasturbinen |
US4782992A (en) * | 1986-11-21 | 1988-11-08 | Textron Inc. | Method of forming articles |
FR2609500B1 (fr) * | 1987-01-14 | 1991-04-12 | Snecma | Disque de compresseur de turbomachine avec accelerateur centripete pour l'aspiration d'air de refroidissement de la turbine |
US4919594A (en) * | 1987-05-15 | 1990-04-24 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US4867644A (en) * | 1987-05-15 | 1989-09-19 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US5305520A (en) * | 1990-09-01 | 1994-04-26 | Rolls-Royce Plc | Method of making fibre reinforced metal component |
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 |
FR2874232B1 (fr) * | 1998-07-28 | 2007-06-15 | Rolls Royce Plc Plc | Rotor metallique renforce de fibres. |
DE10218459B3 (de) * | 2002-04-25 | 2004-01-15 | Mtu Aero Engines Gmbh | Verdichter in mehrstufiger Axialbauart |
DE102004001260A1 (de) * | 2004-01-08 | 2005-08-04 | Mtu Aero Engines Gmbh | Rotor für eine Turbomaschine und Verfahren zur Herstellung eines solchen Rotors |
-
2005
- 2005-06-29 FR FR0506629A patent/FR2887919B1/fr active Active
-
2006
- 2006-06-28 CA CA2551342A patent/CA2551342C/fr active Active
- 2006-06-28 US US11/427,106 patent/US7334999B2/en active Active
- 2006-06-28 EP EP06116258.2A patent/EP1739282B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
EP1739282B1 (fr) | 2018-01-03 |
CA2551342C (fr) | 2013-09-10 |
FR2887919A1 (fr) | 2007-01-05 |
US7334999B2 (en) | 2008-02-26 |
CA2551342A1 (fr) | 2006-12-29 |
EP1739282A1 (fr) | 2007-01-03 |
US20070086896A1 (en) | 2007-04-19 |
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Legal Events
Date | Code | Title | Description |
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CD | Change of name or company name | ||
PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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PLFP | Fee payment |
Year of fee payment: 14 |
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PLFP | Fee payment |
Year of fee payment: 16 |
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PLFP | Fee payment |
Year of fee payment: 17 |
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PLFP | Fee payment |
Year of fee payment: 18 |
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PLFP | Fee payment |
Year of fee payment: 19 |
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PLFP | Fee payment |
Year of fee payment: 20 |