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FR2968363B1 - Rotor de turbomachine avec une cale anti-usure entre un disque et un anneau - Google Patents

Rotor de turbomachine avec une cale anti-usure entre un disque et un anneau

Info

Publication number
FR2968363B1
FR2968363B1 FR1060087A FR1060087A FR2968363B1 FR 2968363 B1 FR2968363 B1 FR 2968363B1 FR 1060087 A FR1060087 A FR 1060087A FR 1060087 A FR1060087 A FR 1060087A FR 2968363 B1 FR2968363 B1 FR 2968363B1
Authority
FR
France
Prior art keywords
wear
bond
disc
ring
turbomachine 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.)
Active
Application number
FR1060087A
Other languages
English (en)
Other versions
FR2968363A1 (fr
Inventor
Michael Delapierre
Patrick Jean Louis Reghezza
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 FR1060087A priority Critical patent/FR2968363B1/fr
Priority to US13/310,073 priority patent/US8911212B2/en
Publication of FR2968363A1 publication Critical patent/FR2968363A1/fr
Application granted granted Critical
Publication of FR2968363B1 publication Critical patent/FR2968363B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/266—Rotors specially for elastic fluids mounting compressor rotors on shafts
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • 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
    • F01D5/326—Locking of axial insertion type blades by other means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1060087A 2010-12-03 2010-12-03 Rotor de turbomachine avec une cale anti-usure entre un disque et un anneau Active FR2968363B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1060087A FR2968363B1 (fr) 2010-12-03 2010-12-03 Rotor de turbomachine avec une cale anti-usure entre un disque et un anneau
US13/310,073 US8911212B2 (en) 2010-12-03 2011-12-02 Turbomachine rotor with anti-wear shim between a disk and an annulus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1060087A FR2968363B1 (fr) 2010-12-03 2010-12-03 Rotor de turbomachine avec une cale anti-usure entre un disque et un anneau

Publications (2)

Publication Number Publication Date
FR2968363A1 FR2968363A1 (fr) 2012-06-08
FR2968363B1 true FR2968363B1 (fr) 2014-12-05

Family

ID=44228008

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1060087A Active FR2968363B1 (fr) 2010-12-03 2010-12-03 Rotor de turbomachine avec une cale anti-usure entre un disque et un anneau

Country Status (2)

Country Link
US (1) US8911212B2 (fr)
FR (1) FR2968363B1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9200520B2 (en) * 2012-06-22 2015-12-01 General Electric Company Gas turbine conical flange bolted joint
FR3014151B1 (fr) * 2013-11-29 2015-12-04 Snecma Soufflante, en particulier pour une turbomachine
EP3073052B1 (fr) 2015-02-17 2018-01-24 Rolls-Royce Corporation Ensemble de soufflant
JP6650773B2 (ja) * 2016-02-04 2020-02-19 三菱重工航空エンジン株式会社 航空部品及び航空用ガスタービンエンジン
US20180045218A1 (en) * 2016-08-11 2018-02-15 United Technologies Corporation Shim for gas turbine engine
US11015483B2 (en) * 2018-03-09 2021-05-25 General Electric Company High pressure compressor flow path flanges with leak resistant plates for improved compressor efficiency and cyclic life
US10788087B2 (en) * 2019-01-22 2020-09-29 Schaeffler Technologies AG & Co. KG One-way clutch with support shim
US20200347568A1 (en) * 2019-04-30 2020-11-05 Deere & Company Loader parking stand

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2502690B1 (fr) * 1981-03-27 1985-09-13 Snecma Dispositif de verrouillage d'aubes de soufflante et de fixation de capot avant d'un turboreacteur
US5112193A (en) * 1990-09-11 1992-05-12 Pratt & Whitney Canada Fan blade axial retention device
US5123813A (en) * 1991-03-01 1992-06-23 General Electric Company Apparatus for preloading an airfoil blade in a gas turbine engine
US5282720A (en) * 1992-09-15 1994-02-01 General Electric Company Fan blade retainer
FR2723397B1 (fr) * 1994-08-03 1996-09-13 Snecma Disque de compresseur de turbomachine muni d'une gorge circulaire asymetrique
US5501575A (en) * 1995-03-01 1996-03-26 United Technologies Corporation Fan blade attachment for gas turbine engine
US6283712B1 (en) * 1999-09-07 2001-09-04 General Electric Company Cooling air supply through bolted flange assembly
FR2803623B1 (fr) * 2000-01-06 2002-03-01 Snecma Moteurs Agencement de retenue axiale d'aubes dans un disque
FR2867223B1 (fr) * 2004-03-03 2006-07-28 Snecma Moteurs Turbomachine comme par exemple un turboreacteur pour avion
FR2903154B1 (fr) * 2006-06-29 2011-10-28 Snecma Rotor de turbomachine et turbomachine comportant un tel rotor
FR2911632B1 (fr) 2007-01-18 2009-08-21 Snecma Sa Disque de rotor de soufflante de turbomachine
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
FR2948725B1 (fr) 2009-07-28 2012-10-05 Snecma Dispositif anti-usure d'un rotor de turbomachine

Also Published As

Publication number Publication date
FR2968363A1 (fr) 2012-06-08
US20120263597A1 (en) 2012-10-18
US8911212B2 (en) 2014-12-16

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