JPS6111404A - タービンエンジンの羽根の回転軸方向鎖錠装置 - Google Patents

タービンエンジンの羽根の回転軸方向鎖錠装置

Info

Publication number
JPS6111404A
JPS6111404A JP60127904A JP12790485A JPS6111404A JP S6111404 A JPS6111404 A JP S6111404A JP 60127904 A JP60127904 A JP 60127904A JP 12790485 A JP12790485 A JP 12790485A JP S6111404 A JPS6111404 A JP S6111404A
Authority
JP
Japan
Prior art keywords
blade
locking ring
slot
notch
leg
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
JP60127904A
Other languages
English (en)
Japanese (ja)
Other versions
JPH0340204B2 (enExample
Inventor
ジヤン・マルク・シユルデイ
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.)
NASHIONARU DECHIYUUDO E DO CON
NASHIONARU DECHIYUUDO E DO KONSUTORIYUKUSHION DE MOTOORU DABIASHION SOC
Original Assignee
NASHIONARU DECHIYUUDO E DO CON
NASHIONARU DECHIYUUDO E DO KONSUTORIYUKUSHION DE MOTOORU DABIASHION SOC
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 NASHIONARU DECHIYUUDO E DO CON, NASHIONARU DECHIYUUDO E DO KONSUTORIYUKUSHION DE MOTOORU DABIASHION SOC filed Critical NASHIONARU DECHIYUUDO E DO CON
Publication of JPS6111404A publication Critical patent/JPS6111404A/ja
Publication of JPH0340204B2 publication Critical patent/JPH0340204B2/ja
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
    • F01D5/32—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)
JP60127904A 1984-06-14 1985-06-12 タービンエンジンの羽根の回転軸方向鎖錠装置 Granted JPS6111404A (ja)

Applications Claiming Priority (2)

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
FR8409286 1984-06-14

Publications (2)

Publication Number Publication Date
JPS6111404A true JPS6111404A (ja) 1986-01-18
JPH0340204B2 JPH0340204B2 (enExample) 1991-06-18

Family

ID=9304994

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60127904A Granted JPS6111404A (ja) 1984-06-14 1985-06-12 タービンエンジンの羽根の回転軸方向鎖錠装置

Country Status (5)

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

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
FR2345605A1 (fr) * 1976-03-25 1977-10-21 Snecma Dispositif de retenue pour aubes de soufflantes
FR2492906A2 (fr) * 1976-03-25 1982-04-30 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
JPH0340204B2 (enExample) 1991-06-18
EP0165860B1 (fr) 1988-03-16
FR2566061A1 (fr) 1985-12-20
DE3561897D1 (en) 1988-04-21
US4604033A (en) 1986-08-05
FR2566061B1 (fr) 1988-09-02
EP0165860A1 (fr) 1985-12-27

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Legal Events

Date Code Title Description
LAPS Cancellation because of no payment of annual fees