DE3561897D1 - Axial locking device for a rotor blade of a turbo machine - Google Patents

Axial locking device for a rotor blade of a turbo machine

Info

Publication number
DE3561897D1
DE3561897D1 DE8585401152T DE3561897T DE3561897D1 DE 3561897 D1 DE3561897 D1 DE 3561897D1 DE 8585401152 T DE8585401152 T DE 8585401152T DE 3561897 T DE3561897 T DE 3561897T DE 3561897 D1 DE3561897 D1 DE 3561897D1
Authority
DE
Germany
Prior art keywords
locking device
rotor blade
turbo machine
axial locking
axial
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
DE8585401152T
Other languages
English (en)
Inventor
Jean Marc Surdi
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 DE3561897D1 publication Critical patent/DE3561897D1/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
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE8585401152T 1984-06-14 1985-06-12 Axial locking device for a rotor blade of a turbo machine Expired DE3561897D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8409286A FR2566061B1 (fr) 1984-06-14 1984-06-14 Dispositif de verrouillage axial d'une aube de turbomachine

Publications (1)

Publication Number Publication Date
DE3561897D1 true DE3561897D1 (en) 1988-04-21

Family

ID=9304994

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8585401152T Expired DE3561897D1 (en) 1984-06-14 1985-06-12 Axial locking device for a rotor blade of a turbo machine

Country Status (5)

Country Link
US (1) US4604033A (de)
EP (1) EP0165860B1 (de)
JP (1) JPS6111404A (de)
DE (1) DE3561897D1 (de)
FR (1) FR2566061B1 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2585069B1 (fr) * 1985-07-16 1989-06-09 Snecma Dispositif de limitation du debattement angulaire d'aubes montees sur un disque de rotor de turbomachine
US4836750A (en) * 1988-06-15 1989-06-06 Pratt & Whitney Canada Inc. Rotor assembly
FR2681374B1 (fr) * 1991-09-18 1993-11-19 Snecma Fixation d'aube de souflante de turboreacteur.
US5318405A (en) * 1993-03-17 1994-06-07 General Electric Company Turbine disk interstage seal anti-rotation key through disk dovetail slot
FR2715975B1 (fr) * 1994-02-10 1996-03-29 Snecma Rotor de turbomachine à rainures d'aube débouchantes axiales ou inclinées.
US6634863B1 (en) * 2000-11-27 2003-10-21 General Electric Company Circular arc multi-bore fan disk assembly
FR2841933B1 (fr) * 2002-07-04 2004-12-03 Snecma Moteurs Cale autobloquante
JP4911286B2 (ja) * 2006-03-14 2012-04-04 株式会社Ｉｈｉ ファンのダブテール構造
JP4807113B2 (ja) * 2006-03-14 2011-11-02 株式会社Ｉｈｉ ファンのダブテール構造
US20090053064A1 (en) * 2006-09-01 2009-02-26 Ress Jr Robert A Fan blade retention system
FR2915495B1 (fr) 2007-04-30 2010-09-03 Snecma Procede de reparation d'une aube mobile de turbomachine
US9662721B2 (en) * 2008-02-26 2017-05-30 United Technologies Corporation Method of generating a curved blade retention slot in a turbine disk
FR2929660B1 (fr) 2008-04-07 2012-11-16 Snecma Dispositif anti-usure pour rotor de turbomachine, bouchon formant dispositif anti-usure et rotor de compresseur de moteur a turbine a gaz comportant un bouchon anti-usure
US8419370B2 (en) * 2009-06-25 2013-04-16 Rolls-Royce Corporation Retaining and sealing ring assembly
FR2948725B1 (fr) * 2009-07-28 2012-10-05 Snecma Dispositif anti-usure d'un rotor de turbomachine
FR2965843B1 (fr) * 2010-10-06 2012-11-09 Snecma Rotor pour turbomachine
FR2972759B1 (fr) * 2011-03-15 2015-09-18 Snecma Systeme d'etancheite et de retenue axiale des aubes pour une roue de turbine de turbomachine
FR2974863B1 (fr) * 2011-05-06 2015-10-23 Snecma Disque de soufflante de turbomachine
FR2986284B1 (fr) 2012-01-31 2014-03-28 Snecma Procede de reparation de marques d’usure.
FR3075284B1 (fr) * 2017-12-18 2020-09-04 Safran Aircraft Engines Dispositif amortisseur

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3378230A (en) * 1966-12-16 1968-04-16 Gen Electric Mounting of blades in turbomachine rotors
FR2492906A2 (fr) * 1976-03-25 1982-04-30 Snecma Dispositif de retenue pour aubes de soufflantes
FR2345605A1 (fr) * 1976-03-25 1977-10-21 Snecma Dispositif de retenue pour aubes de soufflantes
US4221542A (en) * 1977-12-27 1980-09-09 General Electric Company Segmented blade retainer
US4265595A (en) * 1979-01-02 1981-05-05 General Electric Company Turbomachinery blade retaining assembly
FR2507679A1 (fr) * 1981-06-12 1982-12-17 Snecma Dispositif de verrouillage d'une aube de rotor de turbomachine
US4453890A (en) * 1981-06-18 1984-06-12 General Electric Company Blading system for a gas turbine engine
FR2519072B1 (fr) * 1981-12-29 1986-05-30 Snecma Dispositif de retenue axiale et radiale d'aube de rotor de turboreacteur
US4451205A (en) * 1982-02-22 1984-05-29 United Technologies Corporation Rotor blade assembly
FR2524932A1 (fr) * 1982-04-08 1983-10-14 Snecma Dispositif de retenue axiale de pieds d'aube dans un disque de turbomachine
FR2535794A1 (fr) * 1982-11-08 1984-05-11 Snecma Dispositif de retenue axiale et radiale d'aubes de soufflante
FR2535793B1 (fr) * 1982-11-08 1987-04-10 Snecma Dispositif de verrouillage axial d'aubes de soufflante

Also Published As

Publication number Publication date
JPS6111404A (ja) 1986-01-18
EP0165860B1 (de) 1988-03-16
FR2566061A1 (fr) 1985-12-20
FR2566061B1 (fr) 1988-09-02
US4604033A (en) 1986-08-05
EP0165860A1 (de) 1985-12-27
JPH0340204B2 (de) 1991-06-18

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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