FR2959271B1 - Element d'interface entre un pied d'une aube et un logement du pied d'aube d'un disque de turbine, rotor de turbine comprenant un element d'interface - Google Patents
Element d'interface entre un pied d'une aube et un logement du pied d'aube d'un disque de turbine, rotor de turbine comprenant un element d'interfaceInfo
- Publication number
- FR2959271B1 FR2959271B1 FR1053184A FR1053184A FR2959271B1 FR 2959271 B1 FR2959271 B1 FR 2959271B1 FR 1053184 A FR1053184 A FR 1053184A FR 1053184 A FR1053184 A FR 1053184A FR 2959271 B1 FR2959271 B1 FR 2959271B1
- Authority
- FR
- France
- Prior art keywords
- interface element
- foot
- dawn
- turbine
- dust
- 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
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 2
- 239000000428 dust Substances 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
- 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
- F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
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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
- 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
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
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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
- 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
- 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
- F05D2240/81—Cooled platforms
-
- 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
- F05D2250/70—Shape
-
- 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
- F05D2250/70—Shape
- F05D2250/71—Shape curved
-
- 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
- F05D2260/20—Heat transfer, e.g. cooling
-
- 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
- F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
-
- 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
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1053184A FR2959271B1 (fr) | 2010-04-26 | 2010-04-26 | Element d'interface entre un pied d'une aube et un logement du pied d'aube d'un disque de turbine, rotor de turbine comprenant un element d'interface |
US13/643,569 US9103220B2 (en) | 2010-04-26 | 2011-04-20 | Interface element between a blade root and a blade root housing of a turbine disc, and turbine rotor comprising an interface element |
PCT/FR2011/050913 WO2011135234A2 (fr) | 2010-04-26 | 2011-04-20 | Elément d'interface entre un pied d'une aube et un logement du pied d'aube d'un disque de turbine, rotor de turbine comprenant un élément d'interface |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1053184A FR2959271B1 (fr) | 2010-04-26 | 2010-04-26 | Element d'interface entre un pied d'une aube et un logement du pied d'aube d'un disque de turbine, rotor de turbine comprenant un element d'interface |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2959271A1 FR2959271A1 (fr) | 2011-10-28 |
FR2959271B1 true FR2959271B1 (fr) | 2012-09-28 |
Family
ID=43087095
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1053184A Active FR2959271B1 (fr) | 2010-04-26 | 2010-04-26 | Element d'interface entre un pied d'une aube et un logement du pied d'aube d'un disque de turbine, rotor de turbine comprenant un element d'interface |
Country Status (3)
Country | Link |
---|---|
US (1) | US9103220B2 (fr) |
FR (1) | FR2959271B1 (fr) |
WO (1) | WO2011135234A2 (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2953555B1 (fr) * | 2009-12-07 | 2012-04-06 | Snecma | Ensemble d'un jonc de retenue et d'un flasque de maintien dudit jonc |
FR2981132B1 (fr) * | 2011-10-10 | 2013-12-06 | Snecma | Ensemble pour turbomachine a refroidissement de disque |
US9410439B2 (en) | 2012-09-14 | 2016-08-09 | United Technologies Corporation | CMC blade attachment shim relief |
FR3005684B1 (fr) * | 2013-05-17 | 2015-06-05 | Snecma | Pivot de pale d'helice |
CA2936196A1 (fr) | 2014-01-16 | 2015-07-23 | General Electric Company | Cale de reduction de contrainte de pied de pale composite |
FR3055654B1 (fr) * | 2016-09-08 | 2019-11-08 | Safran Aircraft Engines | Rotor de turbine a viroles de separation d'air pour le refroidissement de parties de couplage d'aubes et de disques, pour une turbomachine |
GB201700535D0 (en) * | 2017-01-12 | 2017-03-01 | Rolls Royce Plc | Thermal shielding in a gas turbine |
US10968744B2 (en) | 2017-05-04 | 2021-04-06 | Rolls-Royce Corporation | Turbine rotor assembly having a retaining collar for a bayonet mount |
US10774678B2 (en) | 2017-05-04 | 2020-09-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
US10865646B2 (en) | 2017-05-04 | 2020-12-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
CN109798153B (zh) * | 2019-03-28 | 2023-08-22 | 中国船舶重工集团公司第七0三研究所 | 一种应用于船用燃气轮机涡轮轮盘的冷却结构 |
US11286796B2 (en) | 2019-05-08 | 2022-03-29 | Raytheon Technologies Corporation | Cooled attachment sleeve for a ceramic matrix composite rotor blade |
DE102019215220A1 (de) * | 2019-10-02 | 2021-04-08 | MTU Aero Engines AG | System mit einer Laufschaufel für eine Gasturbine mit einem einen Dichtungsabschnitt aufweisenden Schaufelfußschutzblech |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2779565A (en) * | 1948-01-05 | 1957-01-29 | Bruno W Bruckmann | Air cooling of turbine blades |
IL36770A (en) * | 1970-09-25 | 1973-07-30 | Gen Electric | Turbomachinery blade wear insert |
US5003766A (en) * | 1984-10-10 | 1991-04-02 | Paul Marius A | Gas turbine engine |
JP2743066B2 (ja) * | 1985-08-15 | 1998-04-22 | 株式会社日立製作所 | ガスタービン用動翼構造 |
JPS63173801A (ja) * | 1987-01-12 | 1988-07-18 | Toshiba Corp | ガスタ−ビン |
JPH07189606A (ja) * | 1993-12-28 | 1995-07-28 | Toshiba Corp | ガスタービン動翼およびその動翼製造用繊維強化セラミックス基複合材料ならびにガスタービン動翼の製造方法 |
JPH09250303A (ja) * | 1996-03-12 | 1997-09-22 | Ishikawajima Harima Heavy Ind Co Ltd | タービン動翼植込部の緩衝材 |
GB0307043D0 (en) | 2003-03-26 | 2003-04-30 | Rolls Royce Plc | A method of and structure for enabling cooling of the engaging firtree features of a turbine disk and associated blades |
-
2010
- 2010-04-26 FR FR1053184A patent/FR2959271B1/fr active Active
-
2011
- 2011-04-20 US US13/643,569 patent/US9103220B2/en active Active
- 2011-04-20 WO PCT/FR2011/050913 patent/WO2011135234A2/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
US20130078101A1 (en) | 2013-03-28 |
FR2959271A1 (fr) | 2011-10-28 |
US9103220B2 (en) | 2015-08-11 |
WO2011135234A2 (fr) | 2011-11-03 |
WO2011135234A3 (fr) | 2011-12-29 |
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