FR3078100B1 - Couronne aubagee pour stator de turbomachine dont les aubes sont reliees a la virole externe par appui conique et pion frangible - Google Patents
Couronne aubagee pour stator de turbomachine dont les aubes sont reliees a la virole externe par appui conique et pion frangible Download PDFInfo
- Publication number
- FR3078100B1 FR3078100B1 FR1851347A FR1851347A FR3078100B1 FR 3078100 B1 FR3078100 B1 FR 3078100B1 FR 1851347 A FR1851347 A FR 1851347A FR 1851347 A FR1851347 A FR 1851347A FR 3078100 B1 FR3078100 B1 FR 3078100B1
- Authority
- FR
- France
- Prior art keywords
- blade
- head
- frangible
- pione
- blades
- 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
- 241000135194 Pione Species 0.000 title 1
Classifications
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- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/246—Fastening of diaphragms or stator-rings
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- 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
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
- F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
- F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- 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
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
-
- 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
- F05D2260/30—Retaining components in desired mutual position
-
- 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
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/31—Retaining bolts or nuts
- F05D2260/311—Retaining bolts or nuts of the frangible or shear type
-
- 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
- F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
- F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Une couronne aubagée pour stator de turbomachine comprend une virole externe (42), une aube (46) ayant une tête d'aube (52), et deux plateformes (60) agencées circonférentiellement de part et d'autre de la tête d'aube, et fixées sur une face radialement interne (61) de la virole externe au moyen d'organes de fixation démontables. La tête d'aube présente des premières portées coniques (70) en appui sur des deuxièmes portées coniques (72) respectives des deux plateformes de manière à empêcher un déplacement de l'aube radialement vers l'intérieur et selon la direction circonférentielle. La couronne aubagée comporte un pion frangible (73) comprenant une embase (73A) montée sur la virole externe et une tête (73B) faisant saillie radialement vers l'intérieur par rapport à la virole externe et présentant une surface de tête (73C) formant, vis-à-vis d'une surface de sommet (74) de la tête d'aube, une butée s'opposant à un déplacement de l'aube radialement vers l'extérieur.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1851347A FR3078100B1 (fr) | 2018-02-16 | 2018-02-16 | Couronne aubagee pour stator de turbomachine dont les aubes sont reliees a la virole externe par appui conique et pion frangible |
US16/271,991 US10907489B2 (en) | 2018-02-16 | 2019-02-11 | Vaned ring for turbomachine stator having vanes connected to an outer shell by conical seating and frangible pin |
GB1902152.6A GB2573037B (en) | 2018-02-16 | 2019-02-15 | Vaned ring for turbomachine stator having vanes connected to an outer shell by conical seating and frangible pin |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1851347 | 2018-02-16 | ||
FR1851347A FR3078100B1 (fr) | 2018-02-16 | 2018-02-16 | Couronne aubagee pour stator de turbomachine dont les aubes sont reliees a la virole externe par appui conique et pion frangible |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3078100A1 FR3078100A1 (fr) | 2019-08-23 |
FR3078100B1 true FR3078100B1 (fr) | 2020-03-20 |
Family
ID=61913432
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1851347A Active FR3078100B1 (fr) | 2018-02-16 | 2018-02-16 | Couronne aubagee pour stator de turbomachine dont les aubes sont reliees a la virole externe par appui conique et pion frangible |
Country Status (3)
Country | Link |
---|---|
US (1) | US10907489B2 (fr) |
FR (1) | FR3078100B1 (fr) |
GB (1) | GB2573037B (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11828197B2 (en) | 2021-12-03 | 2023-11-28 | Rolls-Royce North American Technologies Inc. | Outlet guide vane mounting assembly for turbine engines |
US11952917B2 (en) * | 2022-08-05 | 2024-04-09 | Rtx Corporation | Vane multiplet with conjoined singlet vanes |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2834537A (en) * | 1954-01-18 | 1958-05-13 | Ryan Aeronautical Co | Compressor stator structure |
US4498291A (en) * | 1982-10-06 | 1985-02-12 | Rolls-Royce Limited | Turbine overspeed limiter for turbomachines |
DE3341871A1 (de) * | 1983-11-19 | 1985-05-30 | Brown, Boveri & Cie Ag, 6800 Mannheim | Axialverdichter |
JPS60209604A (ja) * | 1984-04-04 | 1985-10-22 | Mitsubishi Heavy Ind Ltd | ガスタ−ビン静翼 |
FR2568953B1 (fr) * | 1984-08-08 | 1989-02-10 | Ratier Figeac Soc | Aube fixe pour reacteurs |
US5074752A (en) * | 1990-08-06 | 1991-12-24 | General Electric Company | Gas turbine outlet guide vane mounting assembly |
US7614848B2 (en) * | 2006-10-10 | 2009-11-10 | United Technologies Corporation | Fan exit guide vane repair method and apparatus |
FR2923529B1 (fr) * | 2007-11-09 | 2014-05-16 | Snecma | Raccordement de bras radiaux a une virole circulaire par imbrication de pieces rapportees |
FR2956876B1 (fr) | 2010-02-26 | 2012-10-19 | Snecma | Module structural et aerodynamique d'un carter de turbomachine et structure de carter comportant une pluralite d'un tel module |
CH703997A1 (de) * | 2010-10-27 | 2012-04-30 | Alstom Technology Ltd | Schaufelanordnung, insbesondere Leitschaufelanordnung. |
US8684697B2 (en) * | 2010-12-13 | 2014-04-01 | General Electric Company | Steam turbine singlet nozzle design for breech loaded assembly |
FR2977635B1 (fr) | 2011-07-04 | 2017-03-24 | Snecma | Dispositif d'arbre d'entrainement d'une turbomachine |
FR2978196B1 (fr) | 2011-07-20 | 2016-12-09 | Snecma | Aubes de turbomachine comprenant une plaque rapportee sur une partie principale |
FR3005693B1 (fr) | 2013-05-16 | 2017-12-22 | Snecma | Turbomachine d'aeronef a double flux comprenant une virole inter-veine a maintien aval simplifie |
GB201414587D0 (en) * | 2014-08-18 | 2014-10-01 | Rolls Royce Plc | Mounting Arrangement For Aerofoil Body |
FR3038344B1 (fr) * | 2015-06-30 | 2017-08-04 | Snecma | Assemblage aubage utilisant un emboitement |
DE202016103137U1 (de) * | 2016-06-14 | 2016-08-03 | Man Diesel & Turbo Se | Lauf- oder Leitvorrichtung für eine Strömungsmaschine |
-
2018
- 2018-02-16 FR FR1851347A patent/FR3078100B1/fr active Active
-
2019
- 2019-02-11 US US16/271,991 patent/US10907489B2/en active Active
- 2019-02-15 GB GB1902152.6A patent/GB2573037B/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20200024997A1 (en) | 2020-01-23 |
GB201902152D0 (en) | 2019-04-03 |
GB2573037B (en) | 2022-04-06 |
US10907489B2 (en) | 2021-02-02 |
FR3078100A1 (fr) | 2019-08-23 |
GB2573037A (en) | 2019-10-23 |
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Year of fee payment: 2 |
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