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FR2393931A1 - Dispositif de maintien des aubes d'un rotor - Google Patents

Dispositif de maintien des aubes d'un rotor

Info

Publication number
FR2393931A1
FR2393931A1 FR777718254A FR7718254A FR2393931A1 FR 2393931 A1 FR2393931 A1 FR 2393931A1 FR 777718254 A FR777718254 A FR 777718254A FR 7718254 A FR7718254 A FR 7718254A FR 2393931 A1 FR2393931 A1 FR 2393931A1
Authority
FR
France
Prior art keywords
hooks
nipples
teeth
housing
cooperate
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.)
Granted
Application number
FR777718254A
Other languages
English (en)
Other versions
FR2393931B1 (fr
Inventor
Josette Benoist
Pierre Antoine Glowacki
Gerard Marcel Francois Mandet
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR777718254A priority Critical patent/FR2393931A1/fr
Priority to GB25506/78A priority patent/GB1575500A/en
Priority to US05/912,862 priority patent/US4189282A/en
Priority to DE2824853A priority patent/DE2824853C2/de
Publication of FR2393931A1 publication Critical patent/FR2393931A1/fr
Application granted granted Critical
Publication of FR2393931B1 publication Critical patent/FR2393931B1/fr
Granted 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
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Dispositif de maintien et d'étanchéité d'aubes de turbine. Une plaque annulaire porte d'un même côté vers son bord extérieur des tétons et vers son bord intérieur des crochets. Le disque de rotor porte sur son bord inférieur une dentelure, le sommet des dents étant conformé pour coopérer avec la surfacè interne des crochets. Les aubes portent sur leur rebord des logements. Deux aubes voisines forment un logement dans lequel vient se placer les tétons lorsque les crochets coopèrent avec les dents. Les tétons sont portés par des languettes découpées radialement dans la plaque annulaire. Application au maintien des aubes de turbine.
FR777718254A 1977-06-08 1977-06-08 Dispositif de maintien des aubes d'un rotor Granted FR2393931A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR777718254A FR2393931A1 (fr) 1977-06-08 1977-06-08 Dispositif de maintien des aubes d'un rotor
GB25506/78A GB1575500A (en) 1977-06-08 1978-05-31 Device for securing blades of a turbine rotor
US05/912,862 US4189282A (en) 1977-06-08 1978-06-05 Device to secure vanes to a rotor
DE2824853A DE2824853C2 (de) 1977-06-08 1978-06-06 Vorrichtung zur Halterung der Schaufeln eines Turbinenläufers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR777718254A FR2393931A1 (fr) 1977-06-08 1977-06-08 Dispositif de maintien des aubes d'un rotor

Publications (2)

Publication Number Publication Date
FR2393931A1 true FR2393931A1 (fr) 1979-01-05
FR2393931B1 FR2393931B1 (fr) 1980-03-21

Family

ID=9192085

Family Applications (1)

Application Number Title Priority Date Filing Date
FR777718254A Granted FR2393931A1 (fr) 1977-06-08 1977-06-08 Dispositif de maintien des aubes d'un rotor

Country Status (4)

Country Link
US (1) US4189282A (fr)
DE (1) DE2824853C2 (fr)
FR (1) FR2393931A1 (fr)
GB (1) GB1575500A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2710103A1 (fr) * 1993-09-16 1995-03-24 Snecma Flasque de rotor de turbomachine et assemblage de ce flasque avec un rotor.
WO2012136917A1 (fr) * 2011-04-05 2012-10-11 Snecma Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant des tenons anti-rotation fendus

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2419389A1 (fr) * 1978-03-08 1979-10-05 Snecma Perfectionnements aux flasques de rotors de turbomachines
US4502809A (en) * 1981-08-31 1985-03-05 Carrier Corporation Method and apparatus for controlling thermal growth
US4688992A (en) * 1985-01-25 1987-08-25 General Electric Company Blade platform
US4767276A (en) * 1986-12-19 1988-08-30 General Electric Company Retainer ring
US4741205A (en) * 1986-12-22 1988-05-03 Westinghouse Electric Corp. "V" notched integrally shrouded turbine blade and method for determining shroud tightness and wear of a circular array of rotating blades disposed in a rotor
GB8705216D0 (en) * 1987-03-06 1987-04-08 Rolls Royce Plc Rotor assembly
US4895490A (en) * 1988-11-28 1990-01-23 The United States Of America As Represented By The Secretary Of The Air Force Internal blade retention system for rotary engines
DE4432999C2 (de) * 1994-09-16 1998-07-30 Mtu Muenchen Gmbh Laufrad einer Turbomaschine, insbesondere einer axial durchströmten Turbine eines Gasturbinentriebwerks
FR2814495B1 (fr) * 2000-09-28 2003-01-17 Snecma Moteurs Systeme de retention amont pour aubes et plates-formes de soufflante
US6827554B2 (en) * 2003-02-25 2004-12-07 General Electric Company Axial entry turbine bucket dovetail with integral anti-rotation key
KR101070904B1 (ko) * 2004-08-20 2011-10-06 삼성테크윈 주식회사 레이디얼 터빈 휠
GB2429498A (en) * 2005-08-26 2007-02-28 Rolls Royce Plc A blade mounting arrangement
DE502006008991D1 (de) * 2006-01-10 2011-04-14 Siemens Ag Verfahren zur Vorbereitung von Turbinenschaufeln mit einer Abdeckleiste mit Steckverbindung für eine anschließende Behandlung, sowie Turbinenschaufel dafür
FR2903154B1 (fr) * 2006-06-29 2011-10-28 Snecma Rotor de turbomachine et turbomachine comportant un tel rotor
EP1916389A1 (fr) * 2006-10-26 2008-04-30 Siemens Aktiengesellschaft Assemblage d'aubes de turbine
US9840931B2 (en) * 2008-11-25 2017-12-12 Ansaldo Energia Ip Uk Limited Axial retention of a platform seal
US10662793B2 (en) * 2014-12-01 2020-05-26 General Electric Company Turbine wheel cover-plate mounted gas turbine interstage seal
GB2547906B (en) * 2016-03-02 2019-07-03 Rolls Royce Plc A bladed rotor arrangement
GB201604473D0 (en) * 2016-03-16 2016-04-27 Rolls Royce Plc A bladed rotor arrangement and a lock plate for a bladed rotor arrangement
US10907491B2 (en) * 2017-11-30 2021-02-02 General Electric Company Sealing system for a rotary machine and method of assembling same

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB779059A (en) * 1954-07-15 1957-07-17 Rolls Royce Improvements in or relating to axial-flow fluid machines, for example compressors orturbines of gas-turbine engines
GB928349A (en) * 1960-12-06 1963-06-12 Rolls Royce Improvements in or relating to bladed rotors of fluid flow machines
US3295825A (en) * 1965-03-10 1967-01-03 Gen Motors Corp Multi-stage turbine rotor
GB1479332A (en) * 1974-11-06 1977-07-13 Rolls Royce Means for retaining blades to a disc or like structure
FR2324873A1 (fr) * 1975-09-17 1977-04-15 Snecma Perfectionnements aux flasques de rotors de turbomachines

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2710103A1 (fr) * 1993-09-16 1995-03-24 Snecma Flasque de rotor de turbomachine et assemblage de ce flasque avec un rotor.
WO2012136917A1 (fr) * 2011-04-05 2012-10-11 Snecma Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant des tenons anti-rotation fendus
FR2973829A1 (fr) * 2011-04-05 2012-10-12 Snecma Flasque d'etancheite pour etage de turbine de turbomachine d'aeronef, comprenant des tenons anti-rotation fendus
CN103459777A (zh) * 2011-04-05 2013-12-18 斯奈克玛 用于航空器涡轮机组的涡轮机级的密封圈，包括开狭槽的防旋转栓
CN103459777B (zh) * 2011-04-05 2015-04-15 斯奈克玛 用于航空器涡轮机组的涡轮机级的密封圈,包括开狭槽的防旋转栓
US9494042B2 (en) 2011-04-05 2016-11-15 Snecma Sealing ring for a turbine stage of an aircraft turbomachine, comprising slotted anti-rotation pegs

Also Published As

Publication number Publication date
FR2393931B1 (fr) 1980-03-21
DE2824853A1 (de) 1978-12-21
DE2824853C2 (de) 1986-08-14
US4189282A (en) 1980-02-19
GB1575500A (en) 1980-09-24

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Legal Events

Date Code Title Description
ST Notification of lapse