DE3266872D1 - Compressor or turbine rotor, the wheel of which supports the hammer-type foot blades and method of assembling such a rotor - Google Patents

Compressor or turbine rotor, the wheel of which supports the hammer-type foot blades and method of assembling such a rotor

Info

Publication number
DE3266872D1
DE3266872D1 DE8282402242T DE3266872T DE3266872D1 DE 3266872 D1 DE3266872 D1 DE 3266872D1 DE 8282402242 T DE8282402242 T DE 8282402242T DE 3266872 T DE3266872 T DE 3266872T DE 3266872 D1 DE3266872 D1 DE 3266872D1
Authority
DE
Germany
Prior art keywords
rotor
hammer
compressor
assembling
supports
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
DE8282402242T
Other languages
English (en)
Inventor
Gerard Marcel Francois Mandet
Marc Roger Marchi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE3266872D1 publication Critical patent/DE3266872D1/de
Expired legal-status Critical Current

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
    • F01D5/32—Locking, e.g. by final locking blades or keys
    • 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
    • F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
    • 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
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic

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)
DE8282402242T 1981-12-09 1982-12-08 Compressor or turbine rotor, the wheel of which supports the hammer-type foot blades and method of assembling such a rotor Expired DE3266872D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8122982A FR2517739A1 (fr) 1981-12-09 1981-12-09 Dispositif de montage et de fixation d'aubes a pied marteau de compresseur et de turbine et procede de montage

Publications (1)

Publication Number Publication Date
DE3266872D1 true DE3266872D1 (en) 1985-11-14

Family

ID=9264819

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8282402242T Expired DE3266872D1 (en) 1981-12-09 1982-12-08 Compressor or turbine rotor, the wheel of which supports the hammer-type foot blades and method of assembling such a rotor

Country Status (5)

Country Link
US (1) US4465432A (de)
EP (1) EP0081436B1 (de)
JP (1) JPS58104304A (de)
DE (1) DE3266872D1 (de)
FR (1) FR2517739A1 (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2156908A (en) * 1984-03-30 1985-10-16 Rolls Royce Bladed rotor assembly for gas turbine engine
US4688992A (en) * 1985-01-25 1987-08-25 General Electric Company Blade platform
FR2616480B1 (fr) * 1987-06-10 1989-09-29 Snecma Dispositif de verrouillage d'aubes a pied marteau sur un disque de turbomachine et procedes de montage et de demontage
US4878811A (en) * 1988-11-14 1989-11-07 United Technologies Corporation Axial compressor blade assembly
US4859149A (en) * 1989-03-10 1989-08-22 General Motors Corporation Blade locking system
FR2644524A1 (fr) * 1989-03-15 1990-09-21 Snecma Aubes a pied marteau a positionnement angulaire ameliore
JPH0472685U (de) * 1990-10-31 1992-06-26
US5183389A (en) * 1992-01-30 1993-02-02 General Electric Company Anti-rock blade tang
GB2265671A (en) * 1992-03-24 1993-10-06 Rolls Royce Plc Bladed rotor for a gas turbine engine
DE4436729A1 (de) * 1994-10-14 1996-04-18 Abb Management Ag Beschaufelter Rotor
KR20020005034A (ko) * 1999-05-14 2002-01-16 칼 하인쯔 호르닝어 회전자용 밀봉 시스템을 갖는 터보 머신
US6508631B1 (en) * 1999-11-18 2003-01-21 Mks Instruments, Inc. Radial flow turbomolecular vacuum pump
FR2856728B1 (fr) * 2003-06-27 2005-10-28 Snecma Moteurs Aube de compresseur de turboreacteur
US8206116B2 (en) * 2005-07-14 2012-06-26 United Technologies Corporation Method for loading and locking tangential rotor blades and blade design
US8608446B2 (en) 2006-06-05 2013-12-17 United Technologies Corporation Rotor disk and blade arrangement
FR2907497B1 (fr) * 2006-10-24 2009-01-23 Snecma Sa Systeme d'equilibrage pour rotor de turbomachine
DE102010053141B4 (de) * 2009-12-07 2018-10-11 General Electric Technology Gmbh Turbinenaggregat mit möglicher Überdrehung des Fußes einer Schaufel bis zum Einbau einer letzten Schaufel
US8888459B2 (en) * 2011-08-23 2014-11-18 General Electric Company Coupled blade platforms and methods of sealing
EP2738356B1 (de) * 2012-11-29 2019-05-01 Safran Aero Boosters SA Statorschaufel einer Strömungsmaschine, Statorschaufelkranz einer Strömungsmaschine und zugehöriges Montageverfahren
CN102979763B (zh) * 2012-12-29 2015-09-16 成都成发科能动力工程有限公司 轴流式压缩机转子动叶片安装结构及动叶片安装方式
JP6190622B2 (ja) * 2013-05-15 2017-08-30 三菱日立パワーシステムズ株式会社 タービン
US10982555B2 (en) 2013-05-17 2021-04-20 Raytheon Technologies Corporation Tangential blade root neck conic
EP2918784A1 (de) * 2014-03-13 2015-09-16 Siemens Aktiengesellschaft Schaufelfuß für eine Turbinenschaufel
US10190595B2 (en) 2015-09-15 2019-01-29 General Electric Company Gas turbine engine blade platform modification
JP6785555B2 (ja) * 2016-01-15 2020-11-18 三菱パワー株式会社 動翼のタービンロータへの組付方法
RU2634507C1 (ru) * 2016-12-15 2017-10-31 Публичное Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Пао "Умпо") Рабочее колесо ротора компрессора высокого давления газотурбинного двигателя
CN112780351A (zh) * 2019-11-07 2021-05-11 中国航发商用航空发动机有限责任公司 航空发动机转子和航空发动机

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US843237A (en) * 1906-03-31 1907-02-05 Frank D Shepherd Steam-turbine.
US922581A (en) * 1908-01-22 1909-05-25 Gen Electric Elastic-fluid turbine.
US974496A (en) * 1910-01-13 1910-11-01 Duston Kemble Turbine vane and wheel.
US1601402A (en) * 1921-01-15 1926-09-28 Lorenzen Christian Gas turbine
DE691800C (de) * 1938-07-30 1940-06-06 Siemens Schuckertwerke Akt Ges Beschaufelung fuer insbesondere radial beaufschlagte Dampf- oder Gasturbinen
DE733419C (de) * 1940-06-13 1943-03-26 Siemens Ag Schaufelschloss fuer axial beaufschlagte Laufschaufelkraenze von Dampf- oder Gasturbinen
CH259204A (de) * 1942-12-24 1949-01-15 Sulzer Ag Verfahren zur Herstellung von Läufern für Turbomaschinen.
US2948505A (en) * 1956-12-26 1960-08-09 Gen Electric Gas turbine rotor
GB840820A (en) * 1957-03-22 1960-07-13 Vickers Electrical Co Ltd Locking means for axial flow turbo-machine blading
DE1085643B (de) * 1959-04-13 1960-07-21 Ehrhardt & Sehmer Ag Maschf Laufschaufelbefestigung bei Axialstroemungsmaschinen
US3042368A (en) * 1960-06-29 1962-07-03 Worthington Corp Removable lock for blade wheel assembly
NL295111A (de) * 1962-07-11
GB1358798A (en) * 1972-06-09 1974-07-10 Bbc Sulzer Turbomaschinen Sealing element for a turbo-machine

Also Published As

Publication number Publication date
JPS58104304A (ja) 1983-06-21
US4465432A (en) 1984-08-14
EP0081436B1 (de) 1985-10-09
FR2517739B1 (de) 1984-02-10
EP0081436A1 (de) 1983-06-15
FR2517739A1 (fr) 1983-06-10
JPS6215727B2 (de) 1987-04-09

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee