SE7411309L - - Google Patents

Info

Publication number
SE7411309L
SE7411309L SE7411309A SE7411309A SE7411309L SE 7411309 L SE7411309 L SE 7411309L SE 7411309 A SE7411309 A SE 7411309A SE 7411309 A SE7411309 A SE 7411309A SE 7411309 L SE7411309 L SE 7411309L
Authority
SE
Sweden
Prior art keywords
rotor
blade root
chamber
downstream
plate
Prior art date
Application number
SE7411309A
Other languages
Unknown language ( )
English (en)
Other versions
SE397382B (sv
Inventor
A J Scalzo
L D Mclaurin
Original Assignee
Westinghouse Electric 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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of SE7411309L publication Critical patent/SE7411309L/
Publication of SE397382B publication Critical patent/SE397382B/xx

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
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates
    • 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
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
SE7411309A 1973-09-07 1974-09-06 Rotor for axialgasturbin SE397382B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00395316A US3853425A (en) 1973-09-07 1973-09-07 Turbine rotor blade cooling and sealing system

Publications (2)

Publication Number Publication Date
SE7411309L true SE7411309L (ru) 1975-03-10
SE397382B SE397382B (sv) 1977-10-31

Family

ID=23562524

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7411309A SE397382B (sv) 1973-09-07 1974-09-06 Rotor for axialgasturbin

Country Status (10)

Country Link
US (1) US3853425A (ru)
JP (1) JPS5228169B2 (ru)
CA (1) CA975301A (ru)
CH (1) CH584345A5 (ru)
DE (1) DE2440430C2 (ru)
FR (1) FR2243331B1 (ru)
GB (1) GB1449415A (ru)
IT (1) IT1020433B (ru)
NL (1) NL7411052A (ru)
SE (1) SE397382B (ru)

Families Citing this family (76)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50155818A (ru) * 1974-06-07 1975-12-16
US4021138A (en) * 1975-11-03 1977-05-03 Westinghouse Electric Corporation Rotor disk, blade, and seal plate assembly for cooled turbine rotor blades
GB1512882A (en) * 1976-02-11 1978-06-01 Rolls Royce Bladed rotor assembly for a gas turbine engine
US4218189A (en) * 1977-08-09 1980-08-19 Rolls-Royce Limited Sealing means for bladed rotor for a gas turbine engine
US4275990A (en) * 1977-12-17 1981-06-30 Rolls-Royce Limited Disc channel for cooling rotor blade roots
US4685863A (en) * 1979-06-27 1987-08-11 United Technologies Corporation Turbine rotor assembly
FR2468727A1 (fr) * 1979-10-26 1981-05-08 Snecma Perfectionnement aux aubes de turbine refroidies
US4422827A (en) * 1982-02-18 1983-12-27 United Technologies Corporation Blade root seal
US4439107A (en) * 1982-09-16 1984-03-27 United Technologies Corporation Rotor blade cooling air chamber
US4507052A (en) * 1983-03-31 1985-03-26 General Motors Corporation End seal for turbine blade bases
US4523890A (en) * 1983-10-19 1985-06-18 General Motors Corporation End seal for turbine blade base
US4674955A (en) * 1984-12-21 1987-06-23 The Garrett Corporation Radial inboard preswirl system
US4759688A (en) * 1986-12-16 1988-07-26 Allied-Signal Inc. Cooling flow side entry for cooled turbine blading
US4898514A (en) * 1987-10-27 1990-02-06 United Technologies Corporation Turbine balance arrangement with integral air passage
FR2639063A1 (fr) * 1988-11-17 1990-05-18 Snecma Segment d'arret et d'etancheite d'un ensemble d'aubes monte sur un disque de rotor de turbomachine
US5018943A (en) * 1989-04-17 1991-05-28 General Electric Company Boltless balance weight for turbine rotors
US5112193A (en) * 1990-09-11 1992-05-12 Pratt & Whitney Canada Fan blade axial retention device
US5256035A (en) * 1992-06-01 1993-10-26 United Technologies Corporation Rotor blade retention and sealing construction
US5302086A (en) * 1992-08-18 1994-04-12 General Electric Company Apparatus for retaining rotor blades
CA2198225C (en) * 1994-08-24 2005-11-22 Leroy D. Mclaurin Gas turbine blade with cooled platform
ES2118638T3 (es) * 1994-10-31 1998-09-16 Westinghouse Electric Corp Alabe rotativo de turbina de gas con plataforma refrigerada.
US6059529A (en) * 1998-03-16 2000-05-09 Siemens Westinghouse Power Corporation Turbine blade assembly with cooling air handling device
US6273683B1 (en) 1999-02-05 2001-08-14 Siemens Westinghouse Power Corporation Turbine blade platform seal
WO2000075491A1 (de) * 1999-06-07 2000-12-14 Siemens Aktiengesellschaft Strömungsmaschine sowie dichtelement für einen rotor einer strömungsmaschine
JP3864157B2 (ja) * 2003-12-05 2006-12-27 本田技研工業株式会社 軸流型タービンホイール
US7192245B2 (en) * 2004-12-03 2007-03-20 Pratt & Whitney Canada Corp. Rotor assembly with cooling air deflectors and method
DE102005024932A1 (de) * 2005-05-31 2006-12-07 Rolls-Royce Deutschland Ltd & Co Kg Turbinenschaufelaxialsperre
US20060275107A1 (en) * 2005-06-07 2006-12-07 Ioannis Alvanos Combined blade attachment and disk lug fluid seal
CN101258305B (zh) * 2005-09-07 2011-06-15 西门子公司 用于对转子中的动叶片进行轴向固定的装置、用于一种这样的装置的密封件以及一种这样的装置的应用
US7484936B2 (en) * 2005-09-26 2009-02-03 Pratt & Whitney Canada Corp. Blades for a gas turbine engine with integrated sealing plate and method
US7500832B2 (en) * 2006-07-06 2009-03-10 Siemens Energy, Inc. Turbine blade self locking seal plate system
FR2905139B1 (fr) * 2006-08-25 2012-09-28 Snecma Aube de rotor d'une turbomachine
ES2321862T3 (es) * 2006-09-25 2009-06-12 Siemens Aktiengesellschaft Rotor de turbina con placas de bloqueo y correspondiente procedimiento de montaje.
US7762780B2 (en) * 2007-01-25 2010-07-27 Siemens Energy, Inc. Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies
US7566201B2 (en) * 2007-01-30 2009-07-28 Siemens Energy, Inc. Turbine seal plate locking system
US8128371B2 (en) * 2007-02-15 2012-03-06 General Electric Company Method and apparatus to facilitate increasing turbine rotor efficiency
FR2918106B1 (fr) * 2007-06-27 2011-05-06 Snecma Dispositif de retenue axiale d'aubes montees sur un disque de rotor de turbomachine.
MX2010001538A (es) * 2007-08-08 2010-03-15 Alstom Technology Ltd Dispositivo de rotor de una turbina.
US20090110561A1 (en) * 2007-10-29 2009-04-30 Honeywell International, Inc. Turbine engine components, turbine engine assemblies, and methods of manufacturing turbine engine components
US10544677B2 (en) 2017-09-01 2020-01-28 United Technologies Corporation Turbine disk
US7918265B2 (en) * 2008-02-14 2011-04-05 United Technologies Corporation Method and apparatus for as-cast seal on turbine blades
US8038405B2 (en) * 2008-07-08 2011-10-18 General Electric Company Spring seal for turbine dovetail
ATE523658T1 (de) * 2008-07-17 2011-09-15 Ansaldo Energia Spa Rotoranordnung für eine gasturbine, gasturbine mit der rotoranordnung und verfahren zum kühlen der rotoranordnung
EP2218873A1 (de) * 2009-02-17 2010-08-18 Siemens Aktiengesellschaft Rotorabschnitt für einen Rotor einer Turbomaschine, Laufschaufel für eine Turbomaschine und Blockierelement
US20100232939A1 (en) * 2009-03-12 2010-09-16 General Electric Company Machine Seal Assembly
US8696320B2 (en) * 2009-03-12 2014-04-15 General Electric Company Gas turbine having seal assembly with coverplate and seal
EP2236759A1 (de) * 2009-03-27 2010-10-06 Siemens Aktiengesellschaft Laufschaufelsystem
US9109457B2 (en) * 2010-09-03 2015-08-18 Siemens Energy, Inc. Axial locking seals for aft removable turbine blade
EP2964894B1 (en) 2013-03-05 2019-04-10 Rolls-Royce North American Technologies, Inc. Turbine segmented cover plate retention method
JP5358031B1 (ja) * 2013-03-22 2013-12-04 三菱重工業株式会社 タービンロータ、タービン、及びシール板の取外方法
FR3011032B1 (fr) * 2013-09-25 2017-12-29 Snecma Ensemble rotatif pour turbomachine
EP2860350A1 (de) * 2013-10-10 2015-04-15 Siemens Aktiengesellschaft Turbinenschaufel sowie Gasturbine
EP2933436A1 (de) * 2014-04-15 2015-10-21 Siemens Aktiengesellschaft Radscheibe mit wenigstens einem Dichtblech
GB201417038D0 (en) * 2014-09-26 2014-11-12 Rolls Royce Plc A bladed rotor arrangement
EP3048256A1 (de) * 2015-01-20 2016-07-27 Siemens Aktiengesellschaft Rotor umfassend eine Turbinenschaufel mit einer Sicherungseinrichtung
CN105065065A (zh) * 2015-08-07 2015-11-18 山东青能动力股份有限公司 一种枞树型叶根动叶片锁紧装置及其装配工艺
GB201516657D0 (en) 2015-09-21 2015-11-04 Rolls Royce Plc Seal-plate anti-rotation in a stage of a gas turbine engine
MX2019006639A (es) * 2016-12-13 2019-08-01 Mitsubishi Hitachi Power Sys Metodo para desmontar/montar turbina de gas, montaje de placa selladora y rotor de turbina de gas.
WO2018110584A1 (ja) 2016-12-13 2018-06-21 三菱日立パワーシステムズ株式会社 ガスタービンの分解組立方法、ガスタービンロータ及びガスタービン
MX2019006636A (es) * 2016-12-13 2019-08-01 Mitsubishi Hitachi Power Sys Metodo para desmontar/montar turbina de gas, montaje de placa selladora y rotor de turbina de gas.
KR101882109B1 (ko) * 2016-12-23 2018-07-25 두산중공업 주식회사 가스 터빈
FR3064667B1 (fr) * 2017-03-31 2020-05-15 Safran Aircraft Engines Dispositif de refroidissement d'un rotor de turbomachine
KR101878360B1 (ko) * 2017-04-12 2018-07-13 두산중공업 주식회사 리테이너 조립구조를 포함하는 가스터빈 블레이드 조립체 및 이를 포함하는 가스터빈
EP3438410B1 (en) 2017-08-01 2021-09-29 General Electric Company Sealing system for a rotary machine
US10472968B2 (en) 2017-09-01 2019-11-12 United Technologies Corporation Turbine disk
US10550702B2 (en) * 2017-09-01 2020-02-04 United Technologies Corporation Turbine disk
US10641110B2 (en) * 2017-09-01 2020-05-05 United Technologies Corporation Turbine disk
US10724374B2 (en) 2017-09-01 2020-07-28 Raytheon Technologies Corporation Turbine disk
EP3564489A1 (de) * 2018-05-03 2019-11-06 Siemens Aktiengesellschaft Rotor mit fliehkraft-optimierten kontaktflächen
KR102142141B1 (ko) * 2018-08-17 2020-08-06 두산중공업 주식회사 터빈, 가스 터빈, 및 터빈 블레이드 분리 방법
KR102134812B1 (ko) 2018-08-17 2020-07-16 두산중공업 주식회사 터빈, 이를 포함하는 가스 터빈, 터빈의 조립 방법, 및 터빈의 분해 방법
CN109707464A (zh) * 2018-12-14 2019-05-03 北京全四维动力科技有限公司 用于保护蒸汽轮机叶片叶根和轮槽的组合装置
KR102205571B1 (ko) * 2019-06-05 2021-01-20 두산중공업 주식회사 터빈 로터 디스크에 대한 터빈 블레이드의 고정 및 실링 구조
US11377967B2 (en) * 2019-12-06 2022-07-05 Raytheon Technologies Corporation Pre-formed faceted turbine blade damper seal
US11313240B2 (en) * 2020-02-05 2022-04-26 Raytheon Technologies Corporation Rounded radial snap configuration for a gas turbine engine cover plate
US11352892B2 (en) * 2020-04-17 2022-06-07 Raytheon Technologies Corporation Seal element for sealing a joint between a rotor blade and a rotor disk

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB905582A (en) * 1960-05-26 1962-09-12 Rolls Royce Improvements relating to the sealing of blades in a bladed rotor
US3490852A (en) * 1967-12-21 1970-01-20 Gen Electric Gas turbine rotor bucket cooling and sealing arrangement
US3644058A (en) * 1970-05-18 1972-02-22 Westinghouse Electric Corp Axial positioner and seal for turbine blades
US3728042A (en) * 1971-08-27 1973-04-17 Westinghouse Electric Corp Axial positioner and seal for cooled rotor blade
US3748060A (en) * 1971-09-14 1973-07-24 Westinghouse Electric Corp Sideplate for turbine blade

Also Published As

Publication number Publication date
IT1020433B (it) 1977-12-20
CH584345A5 (ru) 1977-01-31
JPS5228169B2 (ru) 1977-07-25
GB1449415A (en) 1976-09-15
JPS5054712A (ru) 1975-05-14
FR2243331B1 (ru) 1980-03-21
NL7411052A (nl) 1975-03-11
DE2440430A1 (de) 1975-03-13
US3853425A (en) 1974-12-10
FR2243331A1 (ru) 1975-04-04
SE397382B (sv) 1977-10-31
DE2440430C2 (de) 1983-07-21
CA975301A (en) 1975-09-30

Similar Documents

Publication Publication Date Title
SE7411309L (ru)
GB1012066A (en) Improvements in cover plate assembly for sealing spaces between turbine blades
GB1502549A (en) Gas turbine having cooled turbine rotor blades
US4218189A (en) Sealing means for bladed rotor for a gas turbine engine
GB1295025A (ru)
GB1277212A (en) A sealing device
GB1497619A (en) Turbine blade tip seal
GB1306575A (en) Segmented seal assembly for axial flow turbines
GB1317376A (en) Rotor for axial flow turbine
GB1461965A (en) Axial flow turbine structure
GB928349A (en) Improvements in or relating to bladed rotors of fluid flow machines
GB1441855A (en) Turbine diaphragm seal structure
GB1125920A (en) Turbomachine rotors
GB1318654A (en) Bladed rotors
GB1231450A (ru)
GB1528729A (en) Gas turbine cooling system
GB1109457A (en) Segmented diaphragm assembly for turbines
GB1160856A (en) Internally Cooled Inside Seal
GB1241358A (en) Static seal structure
US4177011A (en) Bar for sealing the gap between adjacent shroud plates in liquid-cooled gas turbine
US3552753A (en) High efficiency static seal assembly
KR920020054A (ko) 드럼 회전자를 갖는 충동 터어빈
GB933047A (en) Improvements in rotor assembly for gas turbine engines
GB988541A (en) Gas turbine rotor cooling
GB1161297A (en) Turbomachine Rotors

Legal Events

Date Code Title Description
NUG Patent has lapsed

Ref document number: 7411309-3

Effective date: 19920408

Format of ref document f/p: F