FR2970999B1 - Aubes de turbomachine en cmc, roue mobile de turbomachine et turbomachine les comportant et procede pour leur fabrication - Google Patents
Aubes de turbomachine en cmc, roue mobile de turbomachine et turbomachine les comportant et procede pour leur fabricationInfo
- Publication number
- FR2970999B1 FR2970999B1 FR1150821A FR1150821A FR2970999B1 FR 2970999 B1 FR2970999 B1 FR 2970999B1 FR 1150821 A FR1150821 A FR 1150821A FR 1150821 A FR1150821 A FR 1150821A FR 2970999 B1 FR2970999 B1 FR 2970999B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- aubes
- manufacture
- mobile
- same
- 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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- 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
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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 (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1150821A FR2970999B1 (fr) | 2011-02-02 | 2011-02-02 | Aubes de turbomachine en cmc, roue mobile de turbomachine et turbomachine les comportant et procede pour leur fabrication |
US13/362,489 US20120195766A1 (en) | 2011-02-02 | 2012-01-31 | Cmc turbine engine blades and a rotor wheel for a turbine engine and a turbine engine integrating them |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1150821A FR2970999B1 (fr) | 2011-02-02 | 2011-02-02 | Aubes de turbomachine en cmc, roue mobile de turbomachine et turbomachine les comportant et procede pour leur fabrication |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2970999A1 FR2970999A1 (fr) | 2012-08-03 |
FR2970999B1 true FR2970999B1 (fr) | 2015-03-06 |
Family
ID=44534897
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1150821A Active FR2970999B1 (fr) | 2011-02-02 | 2011-02-02 | Aubes de turbomachine en cmc, roue mobile de turbomachine et turbomachine les comportant et procede pour leur fabrication |
Country Status (2)
Country | Link |
---|---|
US (1) | US20120195766A1 (fr) |
FR (1) | FR2970999B1 (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3107723A1 (fr) | 2020-03-02 | 2021-09-03 | Safran Aircraft Engines | Aube de rotor de turbomachine |
FR3129685A1 (fr) | 2021-11-29 | 2023-06-02 | Safran Aircraft Engines | Aube de moteur d’aéronef comprenant un talon avec un assemblage en puzzle |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6174839B2 (ja) * | 2011-10-14 | 2017-08-02 | 株式会社Ihi | セラミックス基複合部材およびその製造方法 |
EP2669477B1 (fr) * | 2012-05-31 | 2017-04-05 | General Electric Technology GmbH | Carénage pour aubes |
FR3001758B1 (fr) | 2013-02-01 | 2016-07-15 | Snecma | Aube de rotor de turbomachine |
US9683446B2 (en) | 2013-03-07 | 2017-06-20 | Rolls-Royce Energy Systems, Inc. | Gas turbine engine shrouded blade |
DE102013224199A1 (de) | 2013-11-27 | 2015-05-28 | MTU Aero Engines AG | Gasturbinen-Laufschaufel |
EP3105447A4 (fr) * | 2014-02-05 | 2017-12-13 | United Technologies Corporation | Carénage plateforme de ventilateur jetable |
JP6066948B2 (ja) * | 2014-03-13 | 2017-01-25 | 三菱重工業株式会社 | シュラウド、動翼体、及び回転機械 |
FR3021349B1 (fr) * | 2014-05-22 | 2021-07-02 | Herakles | Procede de fabrication d'une aube de turbomachine en materiau composite, aube ainsi obtenue et turbomachine l'incorporant |
US20150354374A1 (en) * | 2014-06-09 | 2015-12-10 | General Electric Company | Turbine blisk and method of manufacturing thereof |
US10253639B2 (en) * | 2015-02-05 | 2019-04-09 | Rolls-Royce North American Technologies, Inc. | Ceramic matrix composite gas turbine engine blade |
US10053993B2 (en) * | 2015-03-17 | 2018-08-21 | Siemens Energy, Inc. | Shrouded turbine airfoil with leakage flow conditioner |
JP2017160808A (ja) * | 2016-03-08 | 2017-09-14 | 三菱重工コンプレッサ株式会社 | タービン動翼組立体 |
EP3228819B1 (fr) | 2016-04-08 | 2021-06-09 | Ansaldo Energia Switzerland AG | Aube comprenant des couches à cmc |
EP3269932A1 (fr) * | 2016-07-13 | 2018-01-17 | MTU Aero Engines GmbH | Aube carénée pour turbine à gaz |
US10400610B2 (en) * | 2017-02-14 | 2019-09-03 | General Electric Company | Turbine blade having a tip shroud notch |
US10526899B2 (en) | 2017-02-14 | 2020-01-07 | General Electric Company | Turbine blade having a tip shroud |
FR3066780B1 (fr) | 2017-05-24 | 2019-07-19 | Safran Aircraft Engines | Piece amovible anti-usure pour talon d'aube |
FR3077601B1 (fr) * | 2018-02-08 | 2020-01-17 | Safran Aircraft Engines | Aube de turbomachine d'aeronef |
FR3077600B1 (fr) * | 2018-02-08 | 2020-03-06 | Safran Aircraft Engines | Aube de turbomachine d'aeronef |
US11346232B2 (en) | 2018-04-23 | 2022-05-31 | Rolls-Royce Corporation | Turbine blade with abradable tip |
US10995623B2 (en) | 2018-04-23 | 2021-05-04 | Rolls-Royce Corporation | Ceramic matrix composite turbine blade with abrasive tip |
JP6986155B2 (ja) * | 2018-06-19 | 2021-12-22 | 三菱パワー株式会社 | タービン動翼、ターボ機械及びコンタクト面製造方法 |
FR3084398B1 (fr) | 2018-07-24 | 2021-04-16 | Safran Aircraft Engines | Aube de turbine |
FR3085993B1 (fr) | 2018-09-17 | 2020-12-25 | Safran Aircraft Engines | Aube mobile pour une roue d'une turbomachine |
FR3086692B1 (fr) * | 2018-09-28 | 2022-07-29 | Safran Aircraft Engines | Aube de turbomachine equipee d'une piece rapportee anti-usure |
JP7398198B2 (ja) * | 2019-03-12 | 2023-12-14 | 三菱重工業株式会社 | タービン動翼及びコンタクト面製造方法 |
US11549373B2 (en) * | 2020-12-16 | 2023-01-10 | Raytheon Technologies Corporation | Reduced deflection turbine rotor |
JP7434199B2 (ja) * | 2021-03-08 | 2024-02-20 | 株式会社東芝 | タービン動翼 |
FR3127984B1 (fr) * | 2021-10-07 | 2023-10-06 | Safran Aircraft Engines | Aube de turbine de turbomachine avec un effort de contact de prétorsion en fonctionnement auto-généré |
US20250067189A1 (en) * | 2023-08-24 | 2025-02-27 | Rtx Corporation | Cmc vane arc segments with friction damper |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3752599A (en) * | 1971-03-29 | 1973-08-14 | Gen Electric | Bucket vibration damping device |
US5201850A (en) * | 1991-02-15 | 1993-04-13 | General Electric Company | Rotor tip shroud damper including damper wires |
EP1559499A1 (fr) * | 2004-01-27 | 2005-08-03 | Siemens Aktiengesellschaft | Procédé de réparation d'un élément d'une turbomachine |
FR2915510B1 (fr) * | 2007-04-27 | 2009-11-06 | Snecma Sa | Amortisseur pour aubes de turbomachines |
GB2449493B (en) * | 2007-05-25 | 2009-08-12 | Rolls Royce Plc | Vibration damper assembly |
FR2939130B1 (fr) * | 2008-11-28 | 2011-09-16 | Snecma Propulsion Solide | Procede de fabrication de piece de forme de forme complexe en materiau composite. |
US8251651B2 (en) * | 2009-01-28 | 2012-08-28 | United Technologies Corporation | Segmented ceramic matrix composite turbine airfoil component |
-
2011
- 2011-02-02 FR FR1150821A patent/FR2970999B1/fr active Active
-
2012
- 2012-01-31 US US13/362,489 patent/US20120195766A1/en not_active Abandoned
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3107723A1 (fr) | 2020-03-02 | 2021-09-03 | Safran Aircraft Engines | Aube de rotor de turbomachine |
FR3129685A1 (fr) | 2021-11-29 | 2023-06-02 | Safran Aircraft Engines | Aube de moteur d’aéronef comprenant un talon avec un assemblage en puzzle |
Also Published As
Publication number | Publication date |
---|---|
FR2970999A1 (fr) | 2012-08-03 |
US20120195766A1 (en) | 2012-08-02 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 6 |
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Year of fee payment: 10 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20200319 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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Year of fee payment: 12 |
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