ITMI991208A0 - Dispositivo per il posizionamento di ugelli di uno stadio statorico e per il raffreddamento di dischi rotorici in turbine a gas - Google Patents

Dispositivo per il posizionamento di ugelli di uno stadio statorico e per il raffreddamento di dischi rotorici in turbine a gas

Info

Publication number
ITMI991208A0
ITMI991208A0 IT99MI001208A ITMI991208A ITMI991208A0 IT MI991208 A0 ITMI991208 A0 IT MI991208A0 IT 99MI001208 A IT99MI001208 A IT 99MI001208A IT MI991208 A ITMI991208 A IT MI991208A IT MI991208 A0 ITMI991208 A0 IT MI991208A0
Authority
IT
Italy
Prior art keywords
statorist
stage
gas turbine
rotor discs
cooling rotor
Prior art date
Application number
IT99MI001208A
Other languages
English (en)
Inventor
Franco Frosini
Piero Iacopetti
Original Assignee
Nuovo Pignone Spa
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
Publication of ITMI991208A0 publication Critical patent/ITMI991208A0/it
Priority to IT1999MI001208A priority Critical patent/ITMI991208A1/it
Application filed by Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Priority to US09/579,520 priority patent/US6398485B1/en
Priority to DZ000099A priority patent/DZ3089A1/xx
Priority to NO20002769A priority patent/NO330493B1/no
Priority to RU2000113794/06A priority patent/RU2224895C2/ru
Priority to EP00304595A priority patent/EP1057974B1/en
Priority to EG20000717A priority patent/EG22666A/xx
Priority to DE60038653T priority patent/DE60038653T2/de
Priority to ES00304595T priority patent/ES2304233T3/es
Priority to BR0002535-6A priority patent/BR0002535A/pt
Priority to ARP000102689A priority patent/AR024170A1/es
Priority to MXPA00005368A priority patent/MXPA00005368A/es
Publication of ITMI991208A1 publication Critical patent/ITMI991208A1/it

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
    • 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
    • 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
    • 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
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
IT1999MI001208A 1999-05-31 1999-05-31 Dispositivo per il posizionamento di ugelli di uno stadio statorico eper il raffreddamento di dischi rotorici in turbine a gas ITMI991208A1 (it)

Priority Applications (12)

Application Number Priority Date Filing Date Title
IT1999MI001208A ITMI991208A1 (it) 1999-05-31 1999-05-31 Dispositivo per il posizionamento di ugelli di uno stadio statorico eper il raffreddamento di dischi rotorici in turbine a gas
US09/579,520 US6398485B1 (en) 1999-05-31 2000-05-26 Device for positioning of nozzles of a stator stage and for cooling of rotor discs in gas turbines
DZ000099A DZ3089A1 (fr) 1999-05-31 2000-05-29 Dispositif pour le positionnement des becs de létage du stator et pour le refroidissement des disques du rotor dans les turbines à gaz.
NO20002769A NO330493B1 (no) 1999-05-31 2000-05-30 Innretning for posisjonering av dyser i et statortrinn og for kjoling av rotorskiver i en gassturbin
RU2000113794/06A RU2224895C2 (ru) 1999-05-31 2000-05-30 Средство для установки сопел ступени статора и для охлаждения дисков ротора в газовой турбине
EP00304595A EP1057974B1 (en) 1999-05-31 2000-05-31 Stator nozzle for gas turbines
MXPA00005368A MXPA00005368A (es) 1999-05-31 2000-05-31 Dispositivo para la colocacion de boquillas de una etapa de estator y para el enfriamiento de discos de rotor en turbinas de gas.
EG20000717A EG22666A (en) 1999-05-31 2000-05-31 Device for positioning of nozzles of a stator stage and for cooling or rotor discs in gas turbines
DE60038653T DE60038653T2 (de) 1999-05-31 2000-05-31 Gasturbinenleitapparat
ES00304595T ES2304233T3 (es) 1999-05-31 2000-05-31 Tobera de estator para turbina de gas.
BR0002535-6A BR0002535A (pt) 1999-05-31 2000-05-31 Dispositivo para posionamento de bocais de um estágio de estator e para refrigeração de discos de rotor em turbinas a gás
ARP000102689A AR024170A1 (es) 1999-05-31 2000-05-31 Dispositivo para posicionamiento de toberas de una etapa estatorica y para enfriamiento de discos rotoricos en turbinas de gas

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT1999MI001208A ITMI991208A1 (it) 1999-05-31 1999-05-31 Dispositivo per il posizionamento di ugelli di uno stadio statorico eper il raffreddamento di dischi rotorici in turbine a gas

Publications (2)

Publication Number Publication Date
ITMI991208A0 true ITMI991208A0 (it) 1999-05-31
ITMI991208A1 ITMI991208A1 (it) 2000-12-01

Family

ID=11383083

Family Applications (1)

Application Number Title Priority Date Filing Date
IT1999MI001208A ITMI991208A1 (it) 1999-05-31 1999-05-31 Dispositivo per il posizionamento di ugelli di uno stadio statorico eper il raffreddamento di dischi rotorici in turbine a gas

Country Status (12)

Country Link
US (1) US6398485B1 (it)
EP (1) EP1057974B1 (it)
AR (1) AR024170A1 (it)
BR (1) BR0002535A (it)
DE (1) DE60038653T2 (it)
DZ (1) DZ3089A1 (it)
EG (1) EG22666A (it)
ES (1) ES2304233T3 (it)
IT (1) ITMI991208A1 (it)
MX (1) MXPA00005368A (it)
NO (1) NO330493B1 (it)
RU (1) RU2224895C2 (it)

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US6832891B2 (en) * 2001-10-29 2004-12-21 Man Turbomaschinen Ag Device for sealing turbomachines
US6769865B2 (en) * 2002-03-22 2004-08-03 General Electric Company Band cooled turbine nozzle
ITMI20021465A1 (it) * 2002-07-03 2004-01-05 Nuovo Pignone Spa Dispositivo di schermatura termica di facile montaggio per un accoppiamento tra una tubazione di raffreddamento ed una foratura passante rea
US6884023B2 (en) * 2002-09-27 2005-04-26 United Technologies Corporation Integral swirl knife edge injection assembly
DE102004014117A1 (de) * 2004-03-23 2005-10-13 Alstom Technology Ltd Komponente einer Turbomaschine mit einer Kühlanordnung
US7278828B2 (en) * 2004-09-22 2007-10-09 General Electric Company Repair method for plenum cover in a gas turbine engine
US7448221B2 (en) * 2004-12-17 2008-11-11 United Technologies Corporation Turbine engine rotor stack
US20070041800A1 (en) * 2005-08-17 2007-02-22 Santos Jay P Door lock installation kit
CH698928B1 (de) * 2006-05-18 2009-12-15 Man Diesel Se Leitapparat für eine axial angeströmte Turbine eines Abgasturboladers.
US8182205B2 (en) * 2007-02-06 2012-05-22 General Electric Company Gas turbine engine with insulated cooling circuit
FR2930592B1 (fr) * 2008-04-24 2010-04-30 Snecma Distributeur de turbine pour une turbomachine
DE102008060847B4 (de) * 2008-12-06 2020-03-19 MTU Aero Engines AG Strömungsmaschine
US8596959B2 (en) * 2009-10-09 2013-12-03 Pratt & Whitney Canada Corp. Oil tube with integrated heat shield
EP2383435A1 (en) * 2010-04-29 2011-11-02 Siemens Aktiengesellschaft Turbine vane hollow inner rail
EP2405104A1 (de) * 2010-07-08 2012-01-11 Siemens Aktiengesellschaft Verdichter und zugehöriges Gasturbinenkraftwerk
US9145771B2 (en) 2010-07-28 2015-09-29 United Technologies Corporation Rotor assembly disk spacer for a gas turbine engine
US8690530B2 (en) * 2011-06-27 2014-04-08 General Electric Company System and method for supporting a nozzle assembly
US9017013B2 (en) * 2012-02-07 2015-04-28 Siemens Aktiengesellschaft Gas turbine engine with improved cooling between turbine rotor disk elements
US8863531B2 (en) * 2012-07-02 2014-10-21 United Technologies Corporation Cooling apparatus for a mid-turbine frame
EP2900968B1 (en) * 2012-09-28 2018-10-31 United Technologies Corporation Split-zone flow metering t-tube
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
US11033845B2 (en) * 2014-05-29 2021-06-15 General Electric Company Turbine engine and particle separators therefore
WO2016025056A2 (en) 2014-05-29 2016-02-18 General Electric Company Turbine engine and particle separators therefore
FR3024179B1 (fr) * 2014-07-25 2016-08-26 Snecma Systeme d'alimentation en air sous pression installe dans une turbomachine d'aeronef comportant des moyens d'etancheite
EP3009608B1 (en) * 2014-10-02 2019-10-30 United Technologies Corporation Vane assembly with trapped segmented vane structures
US10309308B2 (en) * 2015-01-16 2019-06-04 United Technologies Corporation Cooling passages for a mid-turbine frame
US9885254B2 (en) * 2015-04-24 2018-02-06 United Technologies Corporation Mid turbine frame including a sealed torque box
US9970299B2 (en) 2015-09-16 2018-05-15 General Electric Company Mixing chambers for turbine wheel space cooling
US10125632B2 (en) 2015-10-20 2018-11-13 General Electric Company Wheel space purge flow mixing chamber
US10132195B2 (en) 2015-10-20 2018-11-20 General Electric Company Wheel space purge flow mixing chamber
US10273812B2 (en) * 2015-12-18 2019-04-30 Pratt & Whitney Canada Corp. Turbine rotor coolant supply system
US10519873B2 (en) 2016-04-06 2019-12-31 General Electric Company Air bypass system for rotor shaft cooling
FR3066228B1 (fr) * 2017-05-12 2021-06-11 Safran Aircraft Engines Limitation du deplacement d'un tube de liaison par engagement d'une portion incurvee de paroi d'enceinte pour turbomachine
CN107725113B (zh) * 2017-10-31 2024-06-07 绵阳渝荣节能科技有限责任公司 两级悬臂式轴流膨胀机
DE102019217394A1 (de) * 2019-11-11 2021-05-12 MTU Aero Engines AG Leitschaufelanordnung für eine strömungsmaschine

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CA610668A (en) * 1960-12-13 M. Fiori Bruno Stator unit
DE1403024A1 (de) * 1959-06-04 1968-11-21 Daimler Benz Ag Befestigung der Leitschaufeln von Stroemungsmaschinen
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US5488825A (en) * 1994-10-31 1996-02-06 Westinghouse Electric Corporation Gas turbine vane with enhanced cooling
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JP3495554B2 (ja) * 1997-04-24 2004-02-09 三菱重工業株式会社 ガスタービン静翼の冷却シュラウド
WO1998058158A1 (fr) * 1997-06-19 1998-12-23 Mitsubishi Heavy Industries, Ltd. Dispositif d'etancheite pour aubes de stator de turbine a gaz
JP3477347B2 (ja) * 1997-07-30 2003-12-10 三菱重工業株式会社 ガスタービン段間部シール装置

Also Published As

Publication number Publication date
ITMI991208A1 (it) 2000-12-01
NO330493B1 (no) 2011-05-02
NO20002769D0 (no) 2000-05-30
ES2304233T3 (es) 2008-10-01
EG22666A (en) 2003-06-30
DZ3089A1 (fr) 2004-06-20
MXPA00005368A (es) 2002-04-24
DE60038653T2 (de) 2009-06-04
NO20002769L (no) 2000-12-01
EP1057974B1 (en) 2008-04-23
US6398485B1 (en) 2002-06-04
EP1057974A2 (en) 2000-12-06
EP1057974A3 (en) 2004-01-21
RU2224895C2 (ru) 2004-02-27
AR024170A1 (es) 2002-09-04
DE60038653D1 (de) 2008-06-05
BR0002535A (pt) 2001-01-02

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