FR2975449B1 - Dispositif de fixation d'une piece annulaire sur un arbre de turbomachine - Google Patents

Dispositif de fixation d'une piece annulaire sur un arbre de turbomachine

Info

Publication number
FR2975449B1
FR2975449B1 FR1154304A FR1154304A FR2975449B1 FR 2975449 B1 FR2975449 B1 FR 2975449B1 FR 1154304 A FR1154304 A FR 1154304A FR 1154304 A FR1154304 A FR 1154304A FR 2975449 B1 FR2975449 B1 FR 2975449B1
Authority
FR
France
Prior art keywords
fastening
annular part
turbomachine shaft
turbomachine
shaft
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.)
Active
Application number
FR1154304A
Other languages
English (en)
Other versions
FR2975449A1 (fr
Inventor
Christophe Perdrigeon
Philippe Gerard Edmond Joly
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 FR1154304A priority Critical patent/FR2975449B1/fr
Publication of FR2975449A1 publication Critical patent/FR2975449A1/fr
Application granted granted Critical
Publication of FR2975449B1 publication Critical patent/FR2975449B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/026Shaft to shaft connections
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/053Shafts
    • F04D29/054Arrangements for joining or assembling shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/266Rotors specially for elastic fluids mounting compressor rotors on shafts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D1/00Couplings for rigidly connecting two coaxial shafts or other movable machine elements
    • F16D1/06Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
    • F16D1/076Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end by clamping together two faces perpendicular to the axis of rotation, e.g. with bolted flanges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/30Retaining components in desired mutual position
    • F05B2260/301Retaining bolts or nuts

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1154304A 2011-05-17 2011-05-17 Dispositif de fixation d'une piece annulaire sur un arbre de turbomachine Active FR2975449B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1154304A FR2975449B1 (fr) 2011-05-17 2011-05-17 Dispositif de fixation d'une piece annulaire sur un arbre de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1154304A FR2975449B1 (fr) 2011-05-17 2011-05-17 Dispositif de fixation d'une piece annulaire sur un arbre de turbomachine

Publications (2)

Publication Number Publication Date
FR2975449A1 FR2975449A1 (fr) 2012-11-23
FR2975449B1 true FR2975449B1 (fr) 2015-11-13

Family

ID=44549663

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1154304A Active FR2975449B1 (fr) 2011-05-17 2011-05-17 Dispositif de fixation d'une piece annulaire sur un arbre de turbomachine

Country Status (1)

Country Link
FR (1) FR2975449B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112534118A (zh) * 2018-08-06 2021-03-19 赛峰飞机发动机公司 用于在涡轮机的至少两个转子部件之间传递轴向力的机械组件以及制造用于这种组件的可变螺纹的方法

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3007809B1 (fr) * 2013-07-01 2016-12-23 Snecma Ecrou pour turbomachine comportant des moyens de protection contre l'usure
FR3014150B1 (fr) * 2013-11-29 2018-03-02 Safran Aircraft Engines Soufflante, en particulier pour une turbomachine
FR3033890B1 (fr) * 2015-03-20 2019-08-23 Safran Aircraft Engines Fixation d'un disque fan a un arbre d'entrainement
FR3058757B1 (fr) * 2016-11-14 2018-11-02 Safran Aircraft Engines Dispositif de decouplage de premiere et seconde pieces d'une turbomachine
GB201800513D0 (en) * 2018-01-12 2018-02-28 Rolls Royce Plc Fan disc assembly
FR3087224B1 (fr) * 2018-10-10 2021-05-21 Safran Aircraft Engines Systeme de fixation d'un arbre d'une turbine contrarotative pour une turbomachine d'aeronef
FR3101114B1 (fr) * 2019-09-23 2021-08-27 Safran Aircraft Engines Ensemble pour une turbomachine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT112883B (de) * 1927-06-20 1929-04-10 Bbc Brown Boveri & Cie Einrichtung zur Befestigung einer Scheibe auf der durch die Nabe hindurchgehenden Welle.
US3900270A (en) * 1973-09-22 1975-08-19 Rolls Royce 1971 Ltd Shaft couplings
US4201513A (en) * 1976-12-07 1980-05-06 Rolls-Royce (1971) Limited Gas turbine engines
US5533863A (en) * 1993-03-26 1996-07-09 Allied Signal Inc Self positioning nut
FR2896827B1 (fr) * 2006-01-27 2008-04-25 Snecma Sa Assemblage a encombrement radial reduit entre un arbre de turbine et un tourillon d'arbre de compresseur de turbomachine
US20090034896A1 (en) * 2007-08-03 2009-02-05 Kenneth Lee Fisher Bearing retainer

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112534118A (zh) * 2018-08-06 2021-03-19 赛峰飞机发动机公司 用于在涡轮机的至少两个转子部件之间传递轴向力的机械组件以及制造用于这种组件的可变螺纹的方法

Also Published As

Publication number Publication date
FR2975449A1 (fr) 2012-11-23

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