IT1237095B - Dispositivo per l'alimentazione di aria di raffreddamento per palette di rotore di turbine a gas. - Google Patents

Dispositivo per l'alimentazione di aria di raffreddamento per palette di rotore di turbine a gas.

Info

Publication number
IT1237095B
IT1237095B IT02205389A IT2205389A IT1237095B IT 1237095 B IT1237095 B IT 1237095B IT 02205389 A IT02205389 A IT 02205389A IT 2205389 A IT2205389 A IT 2205389A IT 1237095 B IT1237095 B IT 1237095B
Authority
IT
Italy
Prior art keywords
supply
gas turbine
cooling air
rotor blades
turbine rotor
Prior art date
Application number
IT02205389A
Other languages
English (en)
Other versions
IT8922053A1 (it
IT8922053A0 (it
Inventor
Ulrich Radons
Original Assignee
Mtu Muenchen Gmbh
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mtu Muenchen Gmbh filed Critical Mtu Muenchen Gmbh
Publication of IT8922053A0 publication Critical patent/IT8922053A0/it
Publication of IT8922053A1 publication Critical patent/IT8922053A1/it
Application granted granted Critical
Publication of IT1237095B publication Critical patent/IT1237095B/it

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/081Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT02205389A 1988-10-21 1989-10-18 Dispositivo per l'alimentazione di aria di raffreddamento per palette di rotore di turbine a gas. IT1237095B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3835932A DE3835932A1 (de) 1988-10-21 1988-10-21 Vorrichtung zur kuehlluftzufuehrung fuer gasturbinen-rotorschaufeln

Publications (3)

Publication Number Publication Date
IT8922053A0 IT8922053A0 (it) 1989-10-18
IT8922053A1 IT8922053A1 (it) 1991-04-18
IT1237095B true IT1237095B (it) 1993-05-18

Family

ID=6365646

Family Applications (1)

Application Number Title Priority Date Filing Date
IT02205389A IT1237095B (it) 1988-10-21 1989-10-18 Dispositivo per l'alimentazione di aria di raffreddamento per palette di rotore di turbine a gas.

Country Status (4)

Country Link
DE (1) DE3835932A1 (it)
FR (1) FR2638206B1 (it)
GB (1) GB2225063B (it)
IT (1) IT1237095B (it)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2661946B1 (fr) * 1990-05-14 1994-06-10 Alsthom Gec Etage de turbine a action avec pertes secondaires reduites.
FR2707698B1 (fr) * 1993-07-15 1995-08-25 Snecma Turbomachine munie d'un moyen de soufflage d'air sur un élément de rotor.
US5403156A (en) * 1993-10-26 1995-04-04 United Technologies Corporation Integral meter plate for turbine blade and method
DE4422965A1 (de) * 1994-06-30 1996-01-04 Mtu Muenchen Gmbh Einrichtung zur Abscheidung von Fremdpartikeln aus der den Laufschaufeln einer Turbine zuzuführenden Kühlluft
US5511945A (en) * 1994-10-31 1996-04-30 Solar Turbines Incorporated Turbine motor and blade interface cooling system
DE19854908A1 (de) 1998-11-27 2000-05-31 Rolls Royce Deutschland Schaufel und Laufscheibe einer Strömungsmaschine
US6272844B1 (en) 1999-03-11 2001-08-14 Alm Development, Inc. Gas turbine engine having a bladed disk
EP1041246A1 (de) * 1999-03-29 2000-10-04 Siemens Aktiengesellschaft Kühlmitteldurchströmte, gegossene Gasturbinenschaufel sowie Vorrichtung und Verfahren zur Herstellung eines Verteilerraums der Gasturbinenschaufel
US6460324B1 (en) 1999-10-12 2002-10-08 Alm Development, Inc. Gas turbine engine
US6397576B1 (en) 1999-10-12 2002-06-04 Alm Development, Inc. Gas turbine engine with exhaust compressor having outlet tap control
US6363708B1 (en) 1999-10-12 2002-04-02 Alm Development, Inc. Gas turbine engine
US6442945B1 (en) 2000-08-04 2002-09-03 Alm Development, Inc. Gas turbine engine
FR2823794B1 (fr) * 2001-04-19 2003-07-11 Snecma Moteurs Aube rapportee et refroidie pour turbine
GB0227745D0 (en) 2002-11-28 2003-01-08 Rolls Royce Plc Blade cooling
US6933459B2 (en) * 2003-02-03 2005-08-23 General Electric Company Methods and apparatus for fabricating a turbine engine blade
US6964557B2 (en) * 2003-02-03 2005-11-15 General Electric Company Methods and apparatus for coupling a component to a turbine engine blade
US6974306B2 (en) * 2003-07-28 2005-12-13 Pratt & Whitney Canada Corp. Blade inlet cooling flow deflector apparatus and method
GB2413598A (en) * 2004-05-01 2005-11-02 Rolls Royce Plc Providing cooling gas to turbine blade and disc in gas turbine engine
GB2435909A (en) * 2006-03-07 2007-09-12 Rolls Royce Plc Turbine blade arrangement
US8708652B2 (en) * 2007-06-27 2014-04-29 United Technologies Corporation Cover plate for turbine rotor having enclosed pump for cooling air
KR20120092111A (ko) 2009-09-13 2012-08-20 린 플레임 인코포레이티드 연소 기구를 위한 와류 선혼합기
RU2543100C2 (ru) * 2010-11-29 2015-02-27 Альстом Текнолоджи Лтд Рабочая лопатка для газовой турбины, способ изготовления указанной лопатки и газовая турбина с такой лопаткой
EP2535515A1 (en) 2011-06-16 2012-12-19 Siemens Aktiengesellschaft Rotor blade root section with cooling passage and method for supplying cooling fluid to a rotor blade
EP2725191B1 (en) 2012-10-23 2016-03-16 Alstom Technology Ltd Gas turbine and turbine blade for such a gas turbine
CN103922103A (zh) * 2014-04-17 2014-07-16 中发电气(铜陵)海德精密工业有限公司 高承载负荷防水托辊密封装置

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3286461A (en) * 1965-07-22 1966-11-22 Gen Motors Corp Turbine starter and cooling
US3490852A (en) * 1967-12-21 1970-01-20 Gen Electric Gas turbine rotor bucket cooling and sealing arrangement
DE1942346A1 (de) * 1969-08-20 1971-03-04 Motoren Turbinen Union Vorrichtung zur Abdichtung des Rotors gegenueber dem Stator bei einer zu einem Gasturbinentriebwerk gehoerigen Turbine
GB1350471A (en) * 1971-05-06 1974-04-18 Secr Defence Gas turbine engine
GB1479332A (en) * 1974-11-06 1977-07-13 Rolls Royce Means for retaining blades to a disc or like structure
GB2010404B (en) * 1977-12-17 1982-02-10 Rolls Royce Gas turbine engines
DE2941866C2 (de) * 1978-10-26 1982-08-19 Rolls-Royce Ltd., London Turbine für ein Gasturbinentriebwerk mit lufgekühlten Turbinenschaufeln
GB2042643B (en) * 1979-01-02 1982-12-08 Rolls Royce Cooled gas turbine engine
JPS6056883B2 (ja) * 1979-02-28 1985-12-12 株式会社東芝 ガスタ−ビンの動翼
GB2054046A (en) * 1979-07-12 1981-02-11 Rolls Royce Cooling turbine rotors
FR2485632B1 (fr) * 1980-06-30 1985-07-05 Snecma Perfectionnement aux systemes de ventilation des aubes et disques de turbines
GB2189845B (en) * 1986-04-30 1991-01-23 Gen Electric Turbine cooling air transferring apparatus
US4666368A (en) * 1986-05-01 1987-05-19 General Electric Company Swirl nozzle for a cooling system in gas turbine engines

Also Published As

Publication number Publication date
DE3835932A1 (de) 1990-04-26
FR2638206A1 (fr) 1990-04-27
GB8923696D0 (en) 1989-12-06
DE3835932C2 (it) 1992-04-02
IT8922053A1 (it) 1991-04-18
GB2225063A (en) 1990-05-23
FR2638206B1 (fr) 1994-07-08
GB2225063B (en) 1992-12-02
IT8922053A0 (it) 1989-10-18

Similar Documents

Publication Publication Date Title
IT1237095B (it) Dispositivo per l'alimentazione di aria di raffreddamento per palette di rotore di turbine a gas.
IT8020835A0 (it) Apparati di modulazione dell'aria di rappreddamento in turbine a gas.
NO934894D0 (no) Damp- og luftkjoeling for en turbins statortrinn
IT1163508B (it) Guarnizione di tenuta all'aria esterna rivestita in ceramica per motori a turbina a gas
DE3780563D1 (de) Kuehlluftverteiler fuer den rotor einer gasturbine.
DE3760627D1 (en) Control device for the flux of cooling air for the rotor of a turbine engine
NL194342B (nl) Gekoelde bladen voor een gasturbinemotor.
IT1151593B (it) Iniettore di aria di raffreddamento per palette di turbina
DE3261740D1 (en) Stage of a gas turbine jet engine with air cooling means for the turbine rotor disc
DE69206556D1 (de) Schaufeleinsatz für die Luftkühlung von Gasturbinenschaufeln.
NO924449D0 (no) Integrert damp/luft-kjoelesystem for gassturbiner
IT7926822A0 (it) Tenuta per l'aria di raffreddamento di turbomotori a gas.
EP0473991A3 (en) Gas turbine with cooled rotor blades
DE3880995D1 (de) Rotor fuer eine gasturbine.
DE69503616D1 (de) Doppelte kühlluftversorgung des deckbandes einer turbinenleitschaufel
DE69107988D1 (de) Gasturbine mit modulierter Kühlluft.
IL89040A (en) Cooled gas turbine blade
DE69205656D1 (de) Gasturbinendeckband.
IT1202579B (it) Meccanismo di ritenuta per un motore montato girevolmente su un compressore d'aria
DE59300290D1 (de) Kühlluftversorgung eines turbinengehäuses einer fluggasturbine.
IT1168124B (it) Dispositivo antivortice per l'aria di raffreddamento di una turbina a gas
DE3681526D1 (de) Lufteinlassfilter fuer eine gasturbine.
IT8619648A1 (it) Estrattore di aria particolarmente impiegato in turbomotori a gas
IT7922830A0 (it) Sistema di alimentazione di aria di raffreddamento per motore a turbina a gas.
GB9321721D0 (en) Hollow blade for the fan or compressor of a turbomachine

Legal Events

Date Code Title Description
0001 Granted