ITMI20041804A1 - Pala di un rutore di un primo stadio di una turbina a gas - Google Patents

Pala di un rutore di un primo stadio di una turbina a gas

Info

Publication number
ITMI20041804A1
ITMI20041804A1 IT001804A ITMI20041804A ITMI20041804A1 IT MI20041804 A1 ITMI20041804 A1 IT MI20041804A1 IT 001804 A IT001804 A IT 001804A IT MI20041804 A ITMI20041804 A IT MI20041804A IT MI20041804 A1 ITMI20041804 A1 IT MI20041804A1
Authority
IT
Italy
Prior art keywords
rutor
shovel
stage
gas turbine
turbine
Prior art date
Application number
IT001804A
Other languages
English (en)
Inventor
Marco Boncinelli
Giuseppe Sassanelli
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
Application filed by Nuovo Pignone Spa filed Critical Nuovo Pignone Spa
Priority to IT001804A priority Critical patent/ITMI20041804A1/it
Publication of ITMI20041804A1 publication Critical patent/ITMI20041804A1/it
Priority to EP05255496A priority patent/EP1637698A1/en
Priority to CA2518558A priority patent/CA2518558C/en
Priority to JP2005266308A priority patent/JP2006090314A/ja
Priority to US11/226,264 priority patent/US7530794B2/en
Priority to NO20054322A priority patent/NO20054322L/no
Priority to CN200510109741A priority patent/CN100585129C/zh

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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/321—Application in turbines in gas turbines for a special turbine stage
    • F05D2220/3212—Application in turbines in gas turbines for a special turbine stage the first stage of a turbine
    • 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
    • F05D2250/74—Shape given by a set or table of xyz-coordinates
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/02—Formulas of curves

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials For Photolithography (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Medicinal Preparation (AREA)
IT001804A 2004-09-21 2004-09-21 Pala di un rutore di un primo stadio di una turbina a gas ITMI20041804A1 (it)

Priority Applications (7)

Application Number Priority Date Filing Date Title
IT001804A ITMI20041804A1 (it) 2004-09-21 2004-09-21 Pala di un rutore di un primo stadio di una turbina a gas
EP05255496A EP1637698A1 (en) 2004-09-21 2005-09-08 Rotor blade for a first phase of a gas turbine
CA2518558A CA2518558C (en) 2004-09-21 2005-09-08 Rotor blade for a first phase of a gas turbine
JP2005266308A JP2006090314A (ja) 2004-09-21 2005-09-14 ガスタービンの第１フェーズ用のロータブレード
US11/226,264 US7530794B2 (en) 2004-09-21 2005-09-15 Rotor blade for a first phase of a gas turbine
NO20054322A NO20054322L (no) 2004-09-21 2005-09-20 Rotorblad for forste trinn i en gassturbin
CN200510109741A CN100585129C (zh) 2004-09-21 2005-09-21 用于燃气轮机的第一阶段的转子叶片

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT001804A ITMI20041804A1 (it) 2004-09-21 2004-09-21 Pala di un rutore di un primo stadio di una turbina a gas

Publications (1)

Publication Number Publication Date
ITMI20041804A1 true ITMI20041804A1 (it) 2004-12-21

Family

ID=35335622

Family Applications (1)

Application Number Title Priority Date Filing Date
IT001804A ITMI20041804A1 (it) 2004-09-21 2004-09-21 Pala di un rutore di un primo stadio di una turbina a gas

Country Status (7)

Country Link
US (1) US7530794B2 (it)
EP (1) EP1637698A1 (it)
JP (1) JP2006090314A (it)
CN (1) CN100585129C (it)
CA (1) CA2518558C (it)
IT (1) ITMI20041804A1 (it)
NO (1) NO20054322L (it)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7396211B2 (en) * 2006-03-30 2008-07-08 General Electric Company Stator blade airfoil profile for a compressor
US7467926B2 (en) * 2006-06-09 2008-12-23 General Electric Company Stator blade airfoil profile for a compressor
GB0704426D0 (en) 2007-03-08 2007-04-18 Rolls Royce Plc Aerofoil members for a turbomachine
US8007245B2 (en) * 2007-11-29 2011-08-30 General Electric Company Shank shape for a turbine blade and turbine incorporating the same
US8647069B2 (en) * 2010-07-26 2014-02-11 Snecma Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the fourth stage of a turbine
IT1401661B1 (it) * 2010-08-25 2013-08-02 Nuova Pignone S R L Forma di profilo areodinamico per compressore.
JP5358559B2 (ja) * 2010-12-28 2013-12-04 株式会社日立製作所 軸流圧縮機
CN102102544B (zh) * 2011-03-11 2013-10-02 北京华清燃气轮机与煤气化联合循环工程技术有限公司 燃气轮机的涡轮转子叶片
US8961119B2 (en) * 2012-06-19 2015-02-24 General Electric Company Airfoil shape for a compressor
WO2014120116A1 (en) * 2013-01-29 2014-08-07 United Technologies Corporation Blade rub material
US10301949B2 (en) 2013-01-29 2019-05-28 United Technologies Corporation Blade rub material
DE102013008145A1 (de) * 2013-05-14 2014-11-20 Man Diesel & Turbo Se Laufschaufel für einen Verdichter und Verdichter mit einer solchen Laufschaufel
US10443393B2 (en) * 2016-07-13 2019-10-15 Safran Aircraft Engines Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the seventh stage of a turbine
US10443392B2 (en) * 2016-07-13 2019-10-15 Safran Aircraft Engines Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5641268A (en) * 1991-09-17 1997-06-24 Rolls-Royce Plc Aerofoil members for gas turbine engines
JP2684936B2 (ja) * 1992-09-18 1997-12-03 株式会社日立製作所 ガスタービン及びガスタービン翼
US6095755A (en) * 1996-11-26 2000-08-01 United Technologies Corporation Gas turbine engine airfoils having increased fatigue strength
US5980209A (en) * 1997-06-27 1999-11-09 General Electric Co. Turbine blade with enhanced cooling and profile optimization
JP4086415B2 (ja) * 1999-06-03 2008-05-14 株式会社荏原製作所 タービン装置
US6461110B1 (en) * 2001-07-11 2002-10-08 General Electric Company First-stage high pressure turbine bucket airfoil
US6398489B1 (en) * 2001-02-08 2002-06-04 General Electric Company Airfoil shape for a turbine nozzle
US6457938B1 (en) * 2001-03-30 2002-10-01 General Electric Company Wide angle guide vane
US6474948B1 (en) * 2001-06-22 2002-11-05 General Electric Company Third-stage turbine bucket airfoil
US6450770B1 (en) * 2001-06-28 2002-09-17 General Electric Company Second-stage turbine bucket airfoil
US6503059B1 (en) * 2001-07-06 2003-01-07 General Electric Company Fourth-stage turbine bucket airfoil
US6503054B1 (en) * 2001-07-13 2003-01-07 General Electric Company Second-stage turbine nozzle airfoil
US6461109B1 (en) * 2001-07-13 2002-10-08 General Electric Company Third-stage turbine nozzle airfoil
US6558122B1 (en) * 2001-11-14 2003-05-06 General Electric Company Second-stage turbine bucket airfoil
US6685434B1 (en) * 2002-09-17 2004-02-03 General Electric Company Second stage turbine bucket airfoil
US6715990B1 (en) * 2002-09-19 2004-04-06 General Electric Company First stage turbine bucket airfoil
US6722853B1 (en) * 2002-11-22 2004-04-20 General Electric Company Airfoil shape for a turbine nozzle
US6722852B1 (en) * 2002-11-22 2004-04-20 General Electric Company Third stage turbine bucket airfoil
US6779977B2 (en) * 2002-12-17 2004-08-24 General Electric Company Airfoil shape for a turbine bucket
US6779980B1 (en) * 2003-03-13 2004-08-24 General Electric Company Airfoil shape for a turbine bucket
US6739838B1 (en) * 2003-03-17 2004-05-25 General Electric Company Airfoil shape for a turbine bucket
US6832897B2 (en) * 2003-05-07 2004-12-21 General Electric Company Second stage turbine bucket airfoil
US6769878B1 (en) * 2003-05-09 2004-08-03 Power Systems Mfg. Llc Turbine blade airfoil
US6854961B2 (en) * 2003-05-29 2005-02-15 General Electric Company Airfoil shape for a turbine bucket
US6808368B1 (en) * 2003-06-13 2004-10-26 General Electric Company Airfoil shape for a turbine bucket
US6769879B1 (en) * 2003-07-11 2004-08-03 General Electric Company Airfoil shape for a turbine bucket
US6884038B2 (en) * 2003-07-18 2005-04-26 General Electric Company Airfoil shape for a turbine bucket
US6910868B2 (en) * 2003-07-23 2005-06-28 General Electric Company Airfoil shape for a turbine bucket
US6866477B2 (en) * 2003-07-31 2005-03-15 General Electric Company Airfoil shape for a turbine nozzle
US6857855B1 (en) * 2003-08-04 2005-02-22 General Electric Company Airfoil shape for a turbine bucket
US6881038B1 (en) * 2003-10-09 2005-04-19 General Electric Company Airfoil shape for a turbine bucket

Also Published As

Publication number Publication date
EP1637698A1 (en) 2006-03-22
NO20054322L (no) 2006-03-22
CN100585129C (zh) 2010-01-27
CA2518558A1 (en) 2006-03-21
JP2006090314A (ja) 2006-04-06
CA2518558C (en) 2014-01-07
CN1769646A (zh) 2006-05-10
US7530794B2 (en) 2009-05-12
US20060059890A1 (en) 2006-03-23
NO20054322D0 (no) 2005-09-20

Similar Documents

Publication Publication Date Title
ITMI20041804A1 (it) Pala di un rutore di un primo stadio di una turbina a gas
DE602005025427D1 (de) Verstellbare Leitschaufelanordnung einer Gasturbine
DE602005007297D1 (de) Turbine eines Gasturbinentriebwerks
GB2428748B (en) Method Of Operating A Wind Turbine
DE50306044D1 (de) Schaufel einer Turbine
EP1865262A4 (en) GAS TURBINE COMBUSTION CHAMBER
GB2448087B (en) Second Stage Turbine Airfoil
DE502004003477D1 (de) Filmgekühlte Turbinenschaufel
DE602005012654D1 (de) Turbinenbauteil
DE602007001652D1 (de) Bewegliche Laufradschaufel einer Strömungsmaschine
EP1918549A4 (en) SEALING STRUCTURE OF GAS TURBINE COMBUSTION SYSTEM
ITMI20040709A1 (it) Statore ad elevata efficienzxa per primo stadio di una turbina a gas
GB0605896D0 (en) Turbine blade and diaphragm construction
ITMI20080164A1 (it) Metodo per l'avviamento di una turbina a gas
GB0504272D0 (en) A turbine engine and a method of operating a turbine engine
ITMI20040710A1 (it) Statore ad elevata efficienza per secondo stadio di una turbina a gas
ITTO20050208A1 (it) Gruppo bruciatore a gas per una turbina a gas
DE602006001806D1 (de) Brennkammer einer Gasturbine
DE602005005254D1 (de) Rotorscheibe einer Turbomaschine
ITTO20040309A1 (it) Metodo per controllare un combustore a gas di una turbina a gas
FR2877034B1 (fr) Aube de rotor d'une turbine a gaz
DE502005009070D1 (de) Gasturbinenrotor
DE502005002392D1 (de) Rotor einer Turbomaschine, insbesondere Gasturbinenrotor
ITMI20042167A1 (it) Pistola e metodo per assemblare una pistola
ITMI20040714A1 (it) Rotore ad elevata efficenza per primo stadio di una turbina a gas