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FR2519072B1 - Dispositif de retenue axiale et radiale d'aube de rotor de turboreacteur - Google Patents

Dispositif de retenue axiale et radiale d'aube de rotor de turboreacteur

Info

Publication number
FR2519072B1
FR2519072B1 FR8124355A FR8124355A FR2519072B1 FR 2519072 B1 FR2519072 B1 FR 2519072B1 FR 8124355 A FR8124355 A FR 8124355A FR 8124355 A FR8124355 A FR 8124355A FR 2519072 B1 FR2519072 B1 FR 2519072B1
Authority
FR
France
Prior art keywords
axial
rotor blade
radial retention
turbo jet
jet rotor
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
FR8124355A
Other languages
English (en)
Other versions
FR2519072A1 (fr
Inventor
Jean-Claude Dhuic
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 FR8124355A priority Critical patent/FR2519072B1/fr
Priority to US06/452,772 priority patent/US4474535A/en
Priority to JP57234910A priority patent/JPS58119904A/ja
Priority to DE8282402387T priority patent/DE3267199D1/de
Priority to EP82402387A priority patent/EP0083289B1/fr
Publication of FR2519072A1 publication Critical patent/FR2519072A1/fr
Application granted granted Critical
Publication of FR2519072B1 publication Critical patent/FR2519072B1/fr
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
    • F01D5/323—Locking of axial insertion type blades by means of a key or the like parallel to the axis of the rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR8124355A 1981-12-29 1981-12-29 Dispositif de retenue axiale et radiale d'aube de rotor de turboreacteur Expired FR2519072B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR8124355A FR2519072B1 (fr) 1981-12-29 1981-12-29 Dispositif de retenue axiale et radiale d'aube de rotor de turboreacteur
US06/452,772 US4474535A (en) 1981-12-29 1982-12-22 Axial and radial holding system for the rotor vane of a turbojet engine
JP57234910A JPS58119904A (ja) 1981-12-29 1982-12-27 タ−ボジエツトのロ−タ羽根の軸方向及び径方向固定装置
DE8282402387T DE3267199D1 (en) 1981-12-29 1982-12-28 Rotor wheel of a turbo jet engine comprising a device for axially and radially retaining the rotor blades on the rotor wheel
EP82402387A EP0083289B1 (fr) 1981-12-29 1982-12-28 Roue de rotor de turbomachine munie d'un dispositif de retenue axiale et radiale d'aubes sur le disque

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8124355A FR2519072B1 (fr) 1981-12-29 1981-12-29 Dispositif de retenue axiale et radiale d'aube de rotor de turboreacteur

Publications (2)

Publication Number Publication Date
FR2519072A1 FR2519072A1 (fr) 1983-07-01
FR2519072B1 true FR2519072B1 (fr) 1986-05-30

Family

ID=9265456

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8124355A Expired FR2519072B1 (fr) 1981-12-29 1981-12-29 Dispositif de retenue axiale et radiale d'aube de rotor de turboreacteur

Country Status (5)

Country Link
US (1) US4474535A (fr)
EP (1) EP0083289B1 (fr)
JP (1) JPS58119904A (fr)
DE (1) DE3267199D1 (fr)
FR (1) FR2519072B1 (fr)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2566061B1 (fr) * 1984-06-14 1988-09-02 Snecma Dispositif de verrouillage axial d'une aube de turbomachine
US4711007A (en) * 1986-09-29 1987-12-08 Westinghouse Electric Corp. Method and apparatus for installing free standing turbine blades
US5205714A (en) * 1990-07-30 1993-04-27 General Electric Company Aircraft fan blade damping apparatus
GB2262139A (en) * 1991-12-04 1993-06-09 Rolls Royce Plc Fan blade retainer
US5282720A (en) * 1992-09-15 1994-02-01 General Electric Company Fan blade retainer
FR2697285B1 (fr) * 1992-10-28 1994-11-25 Snecma Système de verrouillage d'extrémités d'aubes.
GB9223593D0 (en) * 1992-11-11 1992-12-23 Rolls Royce Plc Gas turbine engine fan blade assembly
US5318405A (en) * 1993-03-17 1994-06-07 General Electric Company Turbine disk interstage seal anti-rotation key through disk dovetail slot
GB9412963D0 (en) * 1994-06-28 1994-09-28 Rolls Royce Plc Gas turbine engine fan blade assembly
FR2728299B1 (fr) * 1994-12-14 1997-01-24 Snecma Dispositif de fixation axiale d'aubes de rotor de turboreacteur
US5720596A (en) * 1997-01-03 1998-02-24 Westinghouse Electric Corporation Apparatus and method for locking blades into a rotor
FR2807096B1 (fr) * 2000-03-30 2002-05-31 Abb Alstom Power Nv Disque rotorique de turbine equipe d'ailettes a pied de sapin et procede de montage d'une ailette sur un disque
US6457942B1 (en) * 2000-11-27 2002-10-01 General Electric Company Fan blade retainer
US6481971B1 (en) * 2000-11-27 2002-11-19 General Electric Company Blade spacer
US6520742B1 (en) * 2000-11-27 2003-02-18 General Electric Company Circular arc multi-bore fan disk
US6739837B2 (en) 2002-04-16 2004-05-25 United Technologies Corporation Bladed rotor with a tiered blade to hub interface
US6786696B2 (en) 2002-05-06 2004-09-07 General Electric Company Root notched turbine blade
GB0216951D0 (en) * 2002-07-20 2002-08-28 Rolls Royce Plc A fan blade assembly
US6736602B2 (en) * 2002-07-31 2004-05-18 United Technologies Corporation Hollow fan hub under blade bumper
FR2911632B1 (fr) * 2007-01-18 2009-08-21 Snecma Sa Disque de rotor de soufflante de turbomachine
US20080273982A1 (en) * 2007-03-12 2008-11-06 Honeywell International, Inc. Blade attachment retention device
US8485785B2 (en) 2007-07-19 2013-07-16 Siemens Energy, Inc. Wear prevention spring for turbine blade
WO2014113009A1 (fr) * 2013-01-17 2014-07-24 United Technologies Corporation Entretoise d'emplanture de pale de rotor équipée d'élément de prise
GB201503303D0 (en) 2015-02-27 2015-04-15 Rolls Royce Plc Retention device
FR3139597B1 (fr) * 2022-09-12 2024-10-25 Safran Aircraft Engines Ensemble de turbomachine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3383095A (en) * 1967-09-12 1968-05-14 Gen Electric Lock for turbomachinery blades
US3936234A (en) * 1975-02-10 1976-02-03 General Electric Company Device for locking turbomachinery blades
FR2345605A1 (fr) * 1976-03-25 1977-10-21 Snecma Dispositif de retenue pour aubes de soufflantes
DE2639200A1 (de) * 1976-08-31 1978-03-09 Volkswagenwerk Ag Laufrad fuer axialturbinen, insbesondere fuer gasturbinen
US4208170A (en) * 1978-05-18 1980-06-17 General Electric Company Blade retainer
US4265595A (en) * 1979-01-02 1981-05-05 General Electric Company Turbomachinery blade retaining assembly

Also Published As

Publication number Publication date
EP0083289B1 (fr) 1985-10-30
US4474535A (en) 1984-10-02
JPS58119904A (ja) 1983-07-16
JPH0131002B2 (fr) 1989-06-22
DE3267199D1 (en) 1985-12-05
EP0083289A1 (fr) 1983-07-06
FR2519072A1 (fr) 1983-07-01

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Legal Events

Date Code Title Description
ST Notification of lapse