ATE539235T1 - Konfiguration von aufnahmenuten für turbinenschaufeln - Google Patents

Konfiguration von aufnahmenuten für turbinenschaufeln

Info

Publication number
ATE539235T1
ATE539235T1 AT06252765T AT06252765T ATE539235T1 AT E539235 T1 ATE539235 T1 AT E539235T1 AT 06252765 T AT06252765 T AT 06252765T AT 06252765 T AT06252765 T AT 06252765T AT E539235 T1 ATE539235 T1 AT E539235T1
Authority
AT
Austria
Prior art keywords
turbine
section
configuration
turbine blades
mounting grooves
Prior art date
Application number
AT06252765T
Other languages
English (en)
Inventor
Lon M Stevens
Kevin Mccusker
Moon-Kyoo Brian Kang
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 ATE539235T1 publication Critical patent/ATE539235T1/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
    • 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
    • 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
    • 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
    • F05D2250/71—Shape curved
    • 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
    • F05D2260/00—Function
    • F05D2260/94—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF]
    • F05D2260/941—Functionality given by mechanical stress related aspects such as low cycle fatigue [LCF] of high cycle fatigue [HCF] particularly aimed at mechanical or thermal stress reduction

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)
AT06252765T 2005-05-27 2006-05-26 Konfiguration von aufnahmenuten für turbinenschaufeln ATE539235T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/140,632 US7690896B2 (en) 2005-05-27 2005-05-27 Gas turbine disk slots and gas turbine engine using same

Publications (1)

Publication Number Publication Date
ATE539235T1 true ATE539235T1 (de) 2012-01-15

Family

ID=36649457

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06252765T ATE539235T1 (de) 2005-05-27 2006-05-26 Konfiguration von aufnahmenuten für turbinenschaufeln

Country Status (4)

Country Link
US (1) US7690896B2 (de)
EP (1) EP1726784B1 (de)
JP (1) JP2006329203A (de)
AT (1) ATE539235T1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090110561A1 (en) * 2007-10-29 2009-04-30 Honeywell International, Inc. Turbine engine components, turbine engine assemblies, and methods of manufacturing turbine engine components
US8162615B2 (en) * 2009-03-17 2012-04-24 United Technologies Corporation Split disk assembly for a gas turbine engine
JP5922370B2 (ja) * 2011-10-20 2016-05-24 三菱日立パワーシステムズ株式会社 動翼支持構造
US8689441B2 (en) 2011-12-07 2014-04-08 United Technologies Corporation Method for machining a slot in a turbine engine rotor disk
US10309232B2 (en) * 2012-02-29 2019-06-04 United Technologies Corporation Gas turbine engine with stage dependent material selection for blades and disk
US8959738B2 (en) 2012-03-21 2015-02-24 General Electric Company Process of repairing a component, a repair tool for a component, and a component
US9091173B2 (en) 2012-05-31 2015-07-28 United Technologies Corporation Turbine coolant supply system
US9366145B2 (en) 2012-08-24 2016-06-14 United Technologies Corporation Turbine engine rotor assembly
US9803647B2 (en) 2015-07-21 2017-10-31 General Electric Company Method and system for repairing turbomachine dovetail slots
US10047611B2 (en) 2016-01-28 2018-08-14 United Technologies Corporation Turbine blade attachment curved rib stiffeners
US10077665B2 (en) * 2016-01-28 2018-09-18 United Technologies Corporation Turbine blade attachment rails for attachment fillet stress reduction
FR3064667B1 (fr) * 2017-03-31 2020-05-15 Safran Aircraft Engines Dispositif de refroidissement d'un rotor de turbomachine
US10982557B2 (en) * 2018-11-15 2021-04-20 General Electric Company Turbine blade with radial support, shim and related turbine rotor
US11203944B2 (en) 2019-09-05 2021-12-21 Raytheon Technologies Corporation Flared fan hub slot

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3565547A (en) * 1969-02-24 1971-02-23 Carrier Corp Turbomachine rotor construction
US3936222A (en) * 1974-03-28 1976-02-03 United Technologies Corporation Gas turbine construction
US4203705A (en) * 1975-12-22 1980-05-20 United Technologies Corporation Bonded turbine disk for improved low cycle fatigue life
US4191509A (en) * 1977-12-27 1980-03-04 United Technologies Corporation Rotor blade attachment
JPS58167807A (ja) * 1982-03-29 1983-10-04 Hitachi Ltd タ−ボ機械のブレ−ド取付構造
US4813848A (en) * 1987-10-14 1989-03-21 United Technologies Corporation Turbine rotor disk and blade assembly
DE4323705A1 (de) 1993-07-15 1995-01-19 Abb Management Ag Turbine
US5415526A (en) * 1993-11-19 1995-05-16 Mercadante; Anthony J. Coolable rotor assembly
US5430936A (en) * 1993-12-27 1995-07-11 United Technologies Corporation Method for making gas turbine engine blade attachment slots
US5846054A (en) * 1994-10-06 1998-12-08 General Electric Company Laser shock peened dovetails for disks and blades
US5511945A (en) * 1994-10-31 1996-04-30 Solar Turbines Incorporated Turbine motor and blade interface cooling system
US5800124A (en) * 1996-04-12 1998-09-01 United Technologies Corporation Cooled rotor assembly for a turbine engine
EP1041246A1 (de) * 1999-03-29 2000-10-04 Siemens Aktiengesellschaft Kühlmitteldurchströmte, gegossene Gasturbinenschaufel sowie Vorrichtung und Verfahren zur Herstellung eines Verteilerraums der Gasturbinenschaufel
US6254333B1 (en) * 1999-08-02 2001-07-03 United Technologies Corporation Method for forming a cooling passage and for cooling a turbine section of a rotary machine
US6315298B1 (en) * 1999-11-22 2001-11-13 United Technologies Corporation Turbine disk and blade assembly seal
US6302651B1 (en) * 1999-12-29 2001-10-16 United Technologies Corporation Blade attachment configuration
US6837685B2 (en) * 2002-12-13 2005-01-04 General Electric Company Methods and apparatus for repairing a rotor assembly of a turbine
US20090110561A1 (en) * 2007-10-29 2009-04-30 Honeywell International, Inc. Turbine engine components, turbine engine assemblies, and methods of manufacturing turbine engine components

Also Published As

Publication number Publication date
JP2006329203A (ja) 2006-12-07
EP1726784A2 (de) 2006-11-29
EP1726784A3 (de) 2010-06-16
US7690896B2 (en) 2010-04-06
EP1726784B1 (de) 2011-12-28
US20060266050A1 (en) 2006-11-30

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