EP2011966A3 - Luftzuführvorrichtung für die Belüftung von Laufradschaufeln einer Niederdruckturbine eines Gasturbinenmotors - Google Patents
Luftzuführvorrichtung für die Belüftung von Laufradschaufeln einer Niederdruckturbine eines Gasturbinenmotors Download PDFInfo
- Publication number
- EP2011966A3 EP2011966A3 EP08159726A EP08159726A EP2011966A3 EP 2011966 A3 EP2011966 A3 EP 2011966A3 EP 08159726 A EP08159726 A EP 08159726A EP 08159726 A EP08159726 A EP 08159726A EP 2011966 A3 EP2011966 A3 EP 2011966A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- vanes
- ventilation air
- low
- turbine
- gas turbine
- 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.)
- Granted
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
- F01D5/02—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
- F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
-
- 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
- F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
-
- 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
- F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0704918A FR2918414B1 (fr) | 2007-07-06 | 2007-07-06 | Dispositif d'alimentation en air de ventilation des aubes de turbine basse pression d'un moteur a turbine a gaz ; segment pour l'arret axial et la ventilation des aubes de turbine basse pression |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP2011966A2 EP2011966A2 (de) | 2009-01-07 |
| EP2011966A3 true EP2011966A3 (de) | 2010-03-03 |
| EP2011966B1 EP2011966B1 (de) | 2012-03-28 |
Family
ID=39052417
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP08159726A Active EP2011966B1 (de) | 2007-07-06 | 2008-07-04 | Luftzuführvorrichtung für die Belüftung von Laufradschaufeln einer Niederdruckturbine eines Gasturbinenmotors |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US8157506B2 (de) |
| EP (1) | EP2011966B1 (de) |
| JP (1) | JP5035146B2 (de) |
| CA (1) | CA2636665C (de) |
| FR (1) | FR2918414B1 (de) |
| RU (1) | RU2481481C2 (de) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2958322B1 (fr) * | 2010-04-01 | 2013-03-15 | Snecma | Rotor de moteur a turbine a gaz comprenant un tambour de rotor et une couronne de rotor |
| FR2963806B1 (fr) * | 2010-08-10 | 2013-05-03 | Snecma | Dispositif de blocage d'un pied d'une aube de rotor |
| FR2965291B1 (fr) * | 2010-09-27 | 2015-01-23 | Snecma | Ensemble unitaire de disques de rotor pour une turbomachine |
| FR2973433A1 (fr) * | 2011-04-04 | 2012-10-05 | Snecma | Rotor de turbine pour une turbomachine |
| FR2995021B1 (fr) * | 2012-09-04 | 2017-08-25 | Snecma | Dispositif d'alimentation en air pour turbines de moteurs d'aeronefs |
| US10001061B2 (en) * | 2014-06-06 | 2018-06-19 | United Technologies Corporation | Cooling system for gas turbine engines |
| US10408087B2 (en) * | 2014-11-07 | 2019-09-10 | United Technologies Corporation | Turbine rotor segmented sideplates with anti-rotation |
| US9732619B2 (en) * | 2015-03-31 | 2017-08-15 | United Technologies Corporation | Retaining rings for turbomachine disk and coverplate assemblies |
| EP3124742B1 (de) * | 2015-07-28 | 2018-11-07 | MTU Aero Engines GmbH | Gasturbine |
| EP3141698A1 (de) * | 2015-09-10 | 2017-03-15 | Siemens Aktiengesellschaft | Anordnung für eine gasturbine |
| JP6773404B2 (ja) | 2015-10-23 | 2020-10-21 | 三菱パワー株式会社 | 圧縮機ロータ、これを備えるガスタービンロータ、及びガスタービン |
| JP6554736B2 (ja) | 2015-10-23 | 2019-08-07 | 三菱日立パワーシステムズ株式会社 | ガスタービンロータ、ガスタービン、及びガスタービン設備 |
| FR3062415B1 (fr) * | 2017-02-02 | 2019-06-07 | Safran Aircraft Engines | Rotor de turbine de turbomachine a ventilation par lamage |
| FR3062677B1 (fr) * | 2017-02-07 | 2019-12-13 | Safran Aircraft Engines | Turboreacteur a double flux comprenant un distributeur precedant deux etages de turbines basse pression qui sont ventiles par de l'air de refroidissement du distributeur |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3356339A (en) * | 1966-12-12 | 1967-12-05 | Gen Motors Corp | Turbine rotor |
| DE19950109A1 (de) * | 1999-10-18 | 2001-04-19 | Asea Brown Boveri | Rotor für eine Gasturbine |
| EP1264964A1 (de) * | 2001-06-07 | 2002-12-11 | Snecma Moteurs | Anordung für einen Turbomachinenrotor mit zwei durch einen Abstandshalter getrennten Scheiben |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB612097A (en) * | 1946-10-09 | 1948-11-08 | English Electric Co Ltd | Improvements in and relating to the cooling of gas turbine rotors |
| JPH07324632A (ja) * | 1994-05-30 | 1995-12-12 | Mitsubishi Heavy Ind Ltd | ガスタービン動翼の冷却空気シール装置 |
| US5932940A (en) * | 1996-07-16 | 1999-08-03 | Massachusetts Institute Of Technology | Microturbomachinery |
| RU2230195C2 (ru) * | 2002-05-30 | 2004-06-10 | Открытое акционерное общество "Авиадвигатель" | Ротор многоступенчатой турбины |
| US7192244B2 (en) * | 2004-02-23 | 2007-03-20 | Grande Iii Salvatore F | Bladeless conical radial turbine and method |
| GB2420155B (en) * | 2004-11-12 | 2008-08-27 | Rolls Royce Plc | Turbine blade cooling system |
| FR2892454B1 (fr) * | 2005-10-21 | 2008-01-25 | Snecma Sa | Dispositif de ventilation de disques de turbine dans un moteur a turbine a gaz |
| GB0603030D0 (en) * | 2006-02-15 | 2006-03-29 | Rolls Royce Plc | Gas turbine engine rotor ventilation arrangement |
-
2007
- 2007-07-06 FR FR0704918A patent/FR2918414B1/fr not_active Expired - Fee Related
-
2008
- 2008-07-03 JP JP2008174224A patent/JP5035146B2/ja active Active
- 2008-07-03 US US12/167,541 patent/US8157506B2/en active Active
- 2008-07-03 RU RU2008127152/06A patent/RU2481481C2/ru active
- 2008-07-04 EP EP08159726A patent/EP2011966B1/de active Active
- 2008-07-04 CA CA2636665A patent/CA2636665C/fr active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3356339A (en) * | 1966-12-12 | 1967-12-05 | Gen Motors Corp | Turbine rotor |
| DE19950109A1 (de) * | 1999-10-18 | 2001-04-19 | Asea Brown Boveri | Rotor für eine Gasturbine |
| EP1264964A1 (de) * | 2001-06-07 | 2002-12-11 | Snecma Moteurs | Anordung für einen Turbomachinenrotor mit zwei durch einen Abstandshalter getrennten Scheiben |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2011966A2 (de) | 2009-01-07 |
| JP5035146B2 (ja) | 2012-09-26 |
| FR2918414B1 (fr) | 2013-04-12 |
| RU2481481C2 (ru) | 2013-05-10 |
| US8157506B2 (en) | 2012-04-17 |
| FR2918414A1 (fr) | 2009-01-09 |
| EP2011966B1 (de) | 2012-03-28 |
| RU2008127152A (ru) | 2010-01-10 |
| US20090304495A1 (en) | 2009-12-10 |
| JP2009013981A (ja) | 2009-01-22 |
| CA2636665A1 (fr) | 2009-01-06 |
| CA2636665C (fr) | 2015-02-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2011966A3 (de) | Luftzuführvorrichtung für die Belüftung von Laufradschaufeln einer Niederdruckturbine eines Gasturbinenmotors | |
| EP1865184B1 (de) | Turbomachine mit einem Abblassystem eines Niederdruckverdichters. | |
| EP1965030A3 (de) | Rotordichtungssegment | |
| EP1586744A3 (de) | Verstellbare Leitschaufelanordnung einer Gasturbine | |
| WO2004035991A3 (en) | Variable nozzle turbocharger and manufacturing method | |
| FR3027053B1 (fr) | Stator de turbomachine d'aeronef | |
| EP1939404A3 (de) | Statoranordnung | |
| EP1816317A3 (de) | Turbolader mit variabler Geometrie | |
| CA2838919C (fr) | Dispositif d'arbre d'entrainement d'une turbomachine | |
| EP1749995A3 (de) | Gasturbinensystem mit mehreren Wellen | |
| EP2096264A3 (de) | Turbine mit variabler Geometrie und Turbolader | |
| EP1998006A3 (de) | Haltesystem für eine Einlassleitschaufel | |
| FR2872870A1 (fr) | Commande de jeu de pale | |
| JP4991765B2 (ja) | 調整可能なガイド装置 | |
| EP1512841A3 (de) | Gasturbinendichtungen mit verringerter Reibung | |
| WO2009000436A3 (de) | Abgasturbolader für eine brennkraftmaschine | |
| EP1811131A3 (de) | Anordnung von Statorsektoren für einen Verdichter eines Turbotriebwerks | |
| EP1911936B1 (de) | Übergangskanal zwischen zwei Turbinenstufen | |
| CA2442952A1 (fr) | Tambour formant en particulier un rotor de turbo machine, compresseur et turbo moteur comprenant un tel tambour | |
| EP1930552A3 (de) | Turbinenanordnung zur Vereinfachung der Veminderung von Verlusten in Turbinentriebwerken | |
| EP1876324A3 (de) | Laufschaufel einer Gasturbine | |
| EP1561998B1 (de) | Diffusor für Turbinentriebwerk | |
| IL157989A (en) | Integral swirl knife edge injection assembly | |
| KR101055231B1 (ko) | 터빈 하우징 | |
| EP1746347A3 (de) | Verfahren und System zum Betrieb einer mehrstufigen Brennkammer |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| 17P | Request for examination filed |
Effective date: 20080704 |
|
| AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR |
|
| AX | Request for extension of the european patent |
Extension state: AL BA MK RS |
|
| PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
| AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR |
|
| AX | Request for extension of the european patent |
Extension state: AL BA MK RS |
|
| AKX | Designation fees paid |
Designated state(s): DE FR GB |
|
| GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
| RIC1 | Information provided on ipc code assigned before grant |
Ipc: F01D 5/08 20060101ALI20110316BHEP Ipc: F01D 5/30 20060101ALI20110316BHEP Ipc: F01D 5/06 20060101AFI20110316BHEP |
|
| GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
| GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
| AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE FR GB |
|
| REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 602008014391 Country of ref document: DE Effective date: 20120524 |
|
| PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
| 26N | No opposition filed |
Effective date: 20130103 |
|
| REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 602008014391 Country of ref document: DE Effective date: 20130103 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 8 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 9 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 10 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 11 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: CD Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20250722 Year of fee payment: 18 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20250724 Year of fee payment: 18 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20250722 Year of fee payment: 18 |