ATE470050T1 - Abstandhaltende scheibe für ein turbinentriebwerk - Google Patents

Abstandhaltende scheibe für ein turbinentriebwerk

Info

Publication number
ATE470050T1
ATE470050T1 AT05252294T AT05252294T ATE470050T1 AT E470050 T1 ATE470050 T1 AT E470050T1 AT 05252294 T AT05252294 T AT 05252294T AT 05252294 T AT05252294 T AT 05252294T AT E470050 T1 ATE470050 T1 AT E470050T1
Authority
AT
Austria
Prior art keywords
turbine engine
spacer washer
spacers
washer
spacer
Prior art date
Application number
AT05252294T
Other languages
English (en)
Inventor
Grabiel L Suciu
James W Norris
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of ATE470050T1 publication Critical patent/ATE470050T1/de

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49716—Converting

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AT05252294T 2004-04-15 2005-04-13 Abstandhaltende scheibe für ein turbinentriebwerk ATE470050T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/825,255 US7059831B2 (en) 2004-04-15 2004-04-15 Turbine engine disk spacers

Publications (1)

Publication Number Publication Date
ATE470050T1 true ATE470050T1 (de) 2010-06-15

Family

ID=34940795

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05252294T ATE470050T1 (de) 2004-04-15 2005-04-13 Abstandhaltende scheibe für ein turbinentriebwerk

Country Status (5)

Country Link
US (2) US7059831B2 (de)
EP (1) EP1591622B1 (de)
JP (1) JP4226566B2 (de)
AT (1) ATE470050T1 (de)
DE (1) DE602005021580D1 (de)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7186079B2 (en) 2004-11-10 2007-03-06 United Technologies Corporation Turbine engine disk spacers
US7448221B2 (en) 2004-12-17 2008-11-11 United Technologies Corporation Turbine engine rotor stack
US7309210B2 (en) 2004-12-17 2007-12-18 United Technologies Corporation Turbine engine rotor stack
US7726937B2 (en) 2006-09-12 2010-06-01 United Technologies Corporation Turbine engine compressor vanes
JP4935435B2 (ja) * 2007-03-09 2012-05-23 トヨタ自動車株式会社 ガスタービンの焼ばめ締結構造
JP4998023B2 (ja) * 2007-03-09 2012-08-15 トヨタ自動車株式会社 ガスタービンの焼ばめ締結構造
JP4835475B2 (ja) * 2007-03-09 2011-12-14 トヨタ自動車株式会社 ガスタービンの焼ばめ締結構造
US8303255B2 (en) * 2007-10-25 2012-11-06 United Technologies Corporation Shaft trim balancing devices, related systems and methods
FR2925106B1 (fr) * 2007-12-14 2010-01-22 Snecma Procede de conception d'une turbine multi-etages de turbomachine
US8317481B2 (en) * 2008-02-22 2012-11-27 General Electric Company Rotor of a turbomachine and method for replacing rotor blades of the rotor
US8287242B2 (en) 2008-11-17 2012-10-16 United Technologies Corporation Turbine engine rotor hub
FR2940768B1 (fr) * 2009-01-06 2013-07-05 Snecma Procede de fabrication d'un tambour de compresseur de turbomachine
US8177516B2 (en) * 2010-02-02 2012-05-15 General Electric Company Shaped rotor wheel capable of carrying multiple blade stages
US20110219781A1 (en) * 2010-03-10 2011-09-15 Daniel Benjamin Gas turbine engine with tie shaft for axial high pressure compressor rotor
US9145771B2 (en) * 2010-07-28 2015-09-29 United Technologies Corporation Rotor assembly disk spacer for a gas turbine engine
US8662845B2 (en) 2011-01-11 2014-03-04 United Technologies Corporation Multi-function heat shield for a gas turbine engine
US8740554B2 (en) 2011-01-11 2014-06-03 United Technologies Corporation Cover plate with interstage seal for a gas turbine engine
US8840375B2 (en) 2011-03-21 2014-09-23 United Technologies Corporation Component lock for a gas turbine engine
US8550784B2 (en) 2011-05-04 2013-10-08 United Technologies Corporation Gas turbine engine rotor construction
US9045990B2 (en) * 2011-05-26 2015-06-02 United Technologies Corporation Integrated ceramic matrix composite rotor disk geometry for a gas turbine engine
US20120301275A1 (en) * 2011-05-26 2012-11-29 Suciu Gabriel L Integrated ceramic matrix composite rotor module for a gas turbine engine
US8840373B2 (en) 2011-08-03 2014-09-23 United Technologies Corporation Gas turbine engine rotor construction
US10077663B2 (en) * 2011-09-29 2018-09-18 United Technologies Corporation Gas turbine engine rotor stack assembly
US9109608B2 (en) * 2011-12-15 2015-08-18 Siemens Energy, Inc. Compressor airfoil tip clearance optimization system
US9121280B2 (en) * 2012-04-09 2015-09-01 United Technologies Corporation Tie shaft arrangement for turbomachine
US20140064946A1 (en) * 2012-09-06 2014-03-06 Solar Turbines Incorporated Gas turbine engine compressor undercut spacer
GB2520203A (en) * 2012-09-06 2015-05-13 Solar Turbines Inc Gas turbine engine compressor undercut spacer
FR3015592B1 (fr) * 2013-12-19 2018-12-07 Safran Aircraft Engines Rotor comportant une virole amelioree et procede de realisation
US10669875B2 (en) * 2018-03-28 2020-06-02 Solar Turbines Incorporated Cross key anti-rotation spacer
DE102021123173A1 (de) * 2021-09-07 2023-03-09 MTU Aero Engines AG Rotorscheibe mit gekrümmtem Rotorarm für eine Fluggasturbine

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB595643A (en) * 1945-04-23 1947-12-11 Alan Arnold Griffith Improvements in or relating to fans, axial compressors and the like
US2213940A (en) * 1937-07-07 1940-09-03 Jendrassik George Rotor for gas turbines and rotary compressors
BE488226A (de) * 1947-02-17
US3056579A (en) * 1959-04-13 1962-10-02 Gen Electric Rotor construction
US3688371A (en) * 1970-04-30 1972-09-05 Gen Electric The method of manufacturing compositely formed rotors
US4470757A (en) * 1982-02-25 1984-09-11 United Technologies Corporation Sideplate retention for a turbine rotor
US4655683A (en) * 1984-12-24 1987-04-07 United Technologies Corporation Stator seal land structure
FR2607866B1 (fr) * 1986-12-03 1991-04-12 Snecma Axes de fixation de rotors de turbomachine, procede de montage et rotors ainsi montes
US5472313A (en) * 1991-10-30 1995-12-05 General Electric Company Turbine disk cooling system
US5660526A (en) * 1995-06-05 1997-08-26 Allison Engine Company, Inc. Gas turbine rotor with remote support rings
JP3621523B2 (ja) * 1996-09-25 2005-02-16 株式会社東芝 ガスタービンの動翼冷却装置
US6267553B1 (en) * 1999-06-01 2001-07-31 Joseph C. Burge Gas turbine compressor spool with structural and thermal upgrades
US6341419B1 (en) * 2000-02-29 2002-01-29 General Electric Company Loop stacked rotor assembly
US6375429B1 (en) * 2001-02-05 2002-04-23 General Electric Company Turbomachine blade-to-rotor sealing arrangement
US7147436B2 (en) * 2004-04-15 2006-12-12 United Technologies Corporation Turbine engine rotor retainer

Also Published As

Publication number Publication date
US7059831B2 (en) 2006-06-13
JP2005299673A (ja) 2005-10-27
US20050232773A1 (en) 2005-10-20
EP1591622B1 (de) 2010-06-02
US20070065287A1 (en) 2007-03-22
EP1591622A2 (de) 2005-11-02
EP1591622A3 (de) 2006-11-15
US7322101B2 (en) 2008-01-29
DE602005021580D1 (de) 2010-07-15
JP4226566B2 (ja) 2009-02-18

Similar Documents

Publication Publication Date Title
ATE470050T1 (de) Abstandhaltende scheibe für ein turbinentriebwerk
ATE438034T1 (de) Windenergieanlage mit halteeinrichtung für eine rotorwelle
FR2905983B1 (fr) Dispositif d'insonorisation d'un moteur d'helicoptere a turbine a gaz, et moteur ainsi obtenu
DE60141500D1 (de) Lageranordnung für Gasturbinentriebwerk
WO2005085649A8 (en) A fan, especially a ceiling fan with a balanced single blade
SE0402441L (sv) Lagerstativstruktur och gasturbinmotor som innefattar lagerstativstrukturen
BRPI0307475A2 (pt) válvula de arranque de turbina a ar.
BR0300233B1 (pt) turbina de vento com nacela.
BR0203493B1 (pt) aerofólio de turbina para motor de turbina a gás.
DE10301755A8 (de) Fanschaufel für ein Gasturbinentriebwerk
DE602005003759D1 (de) Gegenläufiges Turbinentriebwerk
BR0306617B1 (pt) mecanismo de bocal variável, turbo carregador de exaustão equipado com o mesmo, e método de fabricação de turbo carregador de exaustão com mecanismo de bocal variável.
DE602005009084D1 (de) Bläseranordnung für eine Gasturbine
DE602004031986D1 (de) Gebläse-turbinen-rotoranordnung für einen spitzenturbinenmotor
DE602005000003D1 (de) Turbostrahltriebwerk mit doppeltgelagerter Gebläseantriebswelle
DE60313929D1 (de) Gehäuse, Verdichter, Turbine und Triebwerk mit einem solchen Gehäuse
DE10392111D2 (de) Rotorblatt für Windenergieanlagen
DE602005001528D1 (de) Gasturbinentriebwerk
DE60239120D1 (de) Bläserschaufelblatt für ein Gasturbinentriebwerk
DE602004025887D1 (de) Rotorschaufel und Gasturbinentriebwerk mit einer entsprechenden Rotoranordnung
DE502005000209D1 (de) Dichtungs- und Dämpfungssystem für Turbinenschaufeln
DE602004018045D1 (de) Gebläseschaufelanordnung für ein tip-turbinentriebwerk und montageverfahren
BR0203490B1 (pt) aerofólio de turbina para motor de turbina a gás.
DE502004004513D1 (de) Rotor für eine gasturbine
BR0304161B1 (pt) processo e dispositivo para impedir deslocamentos da posiÇço de referÊncia, devido a deslocamentos axiais entre um eixo de entrada da embreagem e um eixo de saÍda da embreagem, de uma embreagem acionada por um atuador.

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties