FR2940352B1 - Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques. - Google Patents
Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques.Info
- Publication number
- FR2940352B1 FR2940352B1 FR0859000A FR0859000A FR2940352B1 FR 2940352 B1 FR2940352 B1 FR 2940352B1 FR 0859000 A FR0859000 A FR 0859000A FR 0859000 A FR0859000 A FR 0859000A FR 2940352 B1 FR2940352 B1 FR 2940352B1
- Authority
- FR
- France
- Prior art keywords
- heel
- blades
- composite material
- metal
- lechettes
- 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 abstract 3
- 239000000463 material Substances 0.000 title abstract 2
- 239000002184 metal Substances 0.000 title abstract 2
- VJYFKVYYMZPMAB-UHFFFAOYSA-N ethoprophos Chemical compound CCCSP(=O)(OCC)SCCC VJYFKVYYMZPMAB-UHFFFAOYSA-N 0.000 title 1
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
- F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
-
- 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
- F01D5/30—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
- 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
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/161—Sealings between pressure and suction sides especially adapted for elastic fluid pumps
- F04D29/164—Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
-
- 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
- F04D29/324—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
- 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
-
- 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
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. 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
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
L'invention concerne une roue mobile (2) de turbomachine à aubes en matériau composite, comprenant un disque de montage (4), une pluralité d'aubes (8) en matériau composite montées sur le disque de montage par leur pied (10) et munies chacune à leur extrémité libre d'un talon (14), et une virole métallique (18) positionnée sur le talon des aubes de façon concentrique au disque de montage et comprenant des léchettes (20) faisant saillie radialement vers l'extérieur et destinées à venir abraser un matériau abradable (16) porté par un carter entourant la roue, la virole étant fixe axialement et circonférentiellement par rapport au talon des aubes et apte à se déplacer radialement vers l'extérieur par rapport au talon des aubes.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0859000A FR2940352B1 (fr) | 2008-12-23 | 2008-12-23 | Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques. |
US12/636,041 US8870531B2 (en) | 2008-12-23 | 2009-12-11 | Turbomachine rotor having blades of composite material provided with metal labyrinth teeth |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0859000A FR2940352B1 (fr) | 2008-12-23 | 2008-12-23 | Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2940352A1 FR2940352A1 (fr) | 2010-06-25 |
FR2940352B1 true FR2940352B1 (fr) | 2014-11-28 |
Family
ID=40933787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0859000A Active FR2940352B1 (fr) | 2008-12-23 | 2008-12-23 | Roue mobile de turbomachine a aubes en materiau composite munies de lechettes metalliques. |
Country Status (2)
Country | Link |
---|---|
US (1) | US8870531B2 (fr) |
FR (1) | FR2940352B1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2940350B1 (fr) | 2008-12-23 | 2011-03-18 | Snecma | Roue mobile de turbomachine a aubes en materiau composite munie d'un anneau ressort. |
US9598969B2 (en) * | 2012-07-20 | 2017-03-21 | Kabushiki Kaisha Toshiba | Turbine, manufacturing method thereof, and power generating system |
GB201222973D0 (en) * | 2012-12-19 | 2013-01-30 | Composite Technology & Applic Ltd | An aerofoil structure |
CA2932601C (fr) | 2015-06-17 | 2023-10-03 | Rolls-Royce Corporation | Joint labyrinthe dote d'un diviseur de flux modulable |
BE1025283B1 (fr) * | 2017-06-02 | 2019-01-11 | Safran Aero Boosters S.A. | Systeme d'etancheite pour compresseur de turbomachine |
CN116291762B (zh) * | 2023-04-07 | 2023-10-13 | 南京航空航天大学 | 叶尖间隙可控的航空发动机高压涡轮部件及航空发动机 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2610823A (en) * | 1947-02-11 | 1952-09-16 | Gen Electric | Turbine bucket damping arrangement |
US3095138A (en) * | 1957-05-28 | 1963-06-25 | Studebaker Corp | Rotating shroud |
US3048365A (en) * | 1959-12-22 | 1962-08-07 | Curtiss Wright Corp | Rotor blade shroud and vibration damping structure |
US3556675A (en) * | 1969-01-29 | 1971-01-19 | Gen Electric | Turbomachinery rotor with integral shroud |
FR2051912A5 (fr) * | 1969-07-01 | 1971-04-09 | Rabouyt Denis | |
GB1299929A (en) * | 1970-04-10 | 1972-12-13 | Secr Defence | A bladed rotor for a gas turbine engine |
US3728044A (en) * | 1970-06-29 | 1973-04-17 | Hitachi Ltd | Turbine rotor |
IT975329B (it) * | 1972-10-23 | 1974-07-20 | Fiat Spa | Struttura di parti metalliche e nom metalliche statiche o rotanti per ambienti ad alta temperatura particolarmente per rotori e stato ri di turbine a gas |
GB1432994A (en) * | 1973-05-02 | 1976-04-22 | Rolls Royce | Compressor for gas turbine engines |
JPS5330844B2 (fr) * | 1975-01-24 | 1978-08-30 | ||
US4832568A (en) * | 1982-02-26 | 1989-05-23 | General Electric Company | Turbomachine airfoil mounting assembly |
DE3842710C1 (fr) * | 1988-12-19 | 1989-08-03 | Mtu Muenchen Gmbh | |
GB9109016D0 (en) * | 1991-04-26 | 1991-06-12 | Turbine Blading Ltd | Turbine blade repair |
DE19531561A1 (de) * | 1995-08-28 | 1997-03-06 | Abb Research Ltd | Versteifungen für Turbinenschaufeln |
US6371725B1 (en) * | 2000-06-30 | 2002-04-16 | General Electric Company | Conforming platform guide vane |
FR2853931A1 (fr) * | 2003-04-16 | 2004-10-22 | Snecma Moteurs | Reduction de jeux dans une turbine a gaz |
EP1825105B1 (fr) * | 2004-12-08 | 2009-03-18 | Volvo Aero Corporation | Roue pour machine a flux rotatif |
US7393182B2 (en) * | 2005-05-05 | 2008-07-01 | Florida Turbine Technologies, Inc. | Composite tip shroud ring |
EP1801357B1 (fr) * | 2005-12-22 | 2010-10-27 | Techspace Aero | Aubage statorique de turbomachine, turbomachine comportant l'aubage et aube de turbomachine |
-
2008
- 2008-12-23 FR FR0859000A patent/FR2940352B1/fr active Active
-
2009
- 2009-12-11 US US12/636,041 patent/US8870531B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US8870531B2 (en) | 2014-10-28 |
US20100158675A1 (en) | 2010-06-24 |
FR2940352A1 (fr) | 2010-06-25 |
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Legal Events
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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