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FR2913735B1 - Disque de rotor d'une turbomachine - Google Patents

Disque de rotor d'une turbomachine

Info

Publication number
FR2913735B1
FR2913735B1 FR0701906A FR0701906A FR2913735B1 FR 2913735 B1 FR2913735 B1 FR 2913735B1 FR 0701906 A FR0701906 A FR 0701906A FR 0701906 A FR0701906 A FR 0701906A FR 2913735 B1 FR2913735 B1 FR 2913735B1
Authority
FR
France
Prior art keywords
turbomachine
rotor disc
rotor
disc
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
FR0701906A
Other languages
English (en)
Other versions
FR2913735A1 (fr
Inventor
Olivier Belmonte
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 FR0701906A priority Critical patent/FR2913735B1/fr
Priority to EP08152232A priority patent/EP1970538B1/fr
Priority to DE602008001269T priority patent/DE602008001269D1/de
Priority to CA2625317A priority patent/CA2625317C/fr
Priority to RU2008109760/06A priority patent/RU2487249C2/ru
Priority to US12/048,726 priority patent/US8277188B2/en
Priority to JP2008065685A priority patent/JP5152755B2/ja
Publication of FR2913735A1 publication Critical patent/FR2913735A1/fr
Application granted granted Critical
Publication of FR2913735B1 publication Critical patent/FR2913735B1/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
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/322—Blade mountings
    • 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
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • 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
    • 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
    • F04D29/60—Mounting; Assembling; Disassembling
    • F04D29/64—Mounting; Assembling; Disassembling of axial pumps
    • F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0701906A 2007-03-16 2007-03-16 Disque de rotor d'une turbomachine Active FR2913735B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR0701906A FR2913735B1 (fr) 2007-03-16 2007-03-16 Disque de rotor d'une turbomachine
EP08152232A EP1970538B1 (fr) 2007-03-16 2008-03-04 Disque de rotor d'une turbomachine
DE602008001269T DE602008001269D1 (de) 2007-03-16 2008-03-04 Rotorscheibe einer Strömungsmaschine
CA2625317A CA2625317C (fr) 2007-03-16 2008-03-12 Disque de rotor d'une turbomachine
RU2008109760/06A RU2487249C2 (ru) 2007-03-16 2008-03-13 Диск ротора газотурбинного двигателя, газотурбинный двигатель, содержащий такой диск, и защитная накладка ножек лопаток
US12/048,726 US8277188B2 (en) 2007-03-16 2008-03-14 Turbomachine rotor disk
JP2008065685A JP5152755B2 (ja) 2007-03-16 2008-03-14 ロータディスク

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0701906A FR2913735B1 (fr) 2007-03-16 2007-03-16 Disque de rotor d'une turbomachine

Publications (2)

Publication Number Publication Date
FR2913735A1 FR2913735A1 (fr) 2008-09-19
FR2913735B1 true FR2913735B1 (fr) 2013-04-19

Family

ID=38657112

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0701906A Active FR2913735B1 (fr) 2007-03-16 2007-03-16 Disque de rotor d'une turbomachine

Country Status (7)

Country Link
US (1) US8277188B2 (fr)
EP (1) EP1970538B1 (fr)
JP (1) JP5152755B2 (fr)
CA (1) CA2625317C (fr)
DE (1) DE602008001269D1 (fr)
FR (1) FR2913735B1 (fr)
RU (1) RU2487249C2 (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2913735B1 (fr) * 2007-03-16 2013-04-19 Snecma Disque de rotor d'une turbomachine
FR2933887B1 (fr) * 2008-07-18 2010-09-17 Snecma Procede de reparation ou de reprise d'un disque de turbomachine et disque de turbomachine repare ou repris
FR2955904B1 (fr) * 2010-02-04 2012-07-20 Snecma Soufflante de turbomachine
US8573947B2 (en) * 2010-03-10 2013-11-05 United Technologies Corporation Composite fan blade dovetail root
US8708656B2 (en) * 2010-05-25 2014-04-29 Pratt & Whitney Canada Corp. Blade fixing design for protecting against low speed rotation induced wear
GB201104994D0 (en) * 2011-03-25 2011-05-11 Rolls Royce Plc a rotor having an annulus filler
FR2995003B1 (fr) * 2012-09-03 2014-08-15 Snecma Rotor de turbine pour une turbomachine
US10145268B2 (en) 2013-03-15 2018-12-04 United Technologies Corporation Injection molded composite fan platform
WO2014197105A2 (fr) * 2013-03-25 2014-12-11 United Technologies Corporation Segment de plate-forme et pale non solidaire pour un rotor
EP3058180B1 (fr) * 2013-10-11 2018-12-12 United Technologies Corporation Rotor de soufflante ayant une fixation de plate-forme intégrée
FR3037367B1 (fr) * 2015-06-15 2017-06-30 Snecma Ensemble rotatif de turbomachine a garnitures de protection bombees
FR3052485B1 (fr) * 2016-06-08 2019-05-10 Safran Aircraft Engines Rotor a element de dissipation d'energie
GB201612288D0 (en) * 2016-07-15 2016-08-31 Rolls-Royce Ltd A rotor assembly for a turbomachine and a method of manufacturing the same
FR3082232B1 (fr) * 2018-06-12 2020-08-28 Safran Aircraft Engines Systeme de maintien pour le demontage d'une roue a aubes
FR3085711B1 (fr) * 2018-09-06 2021-07-23 Safran Aircraft Engines Roue a aubes de turbomachine pour aeronef
FR3089258B1 (fr) * 2018-12-03 2020-11-06 Safran Aircraft Engines Soufflante comprenant une plateforme inter-aubes fixée radialement par une tôle de protection sacrificielle
JP7269029B2 (ja) * 2019-02-27 2023-05-08 三菱重工業株式会社 動翼及び回転機械
CN113914999B (zh) * 2021-12-14 2022-03-18 成都中科翼能科技有限公司 一种燃气轮机压气机装配方法

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US322493A (en) * 1885-07-21 Philippe sorgue
US323642A (en) * 1885-08-04 Cotton-planter
US323072A (en) * 1885-07-28 William k
GB928349A (en) * 1960-12-06 1963-06-12 Rolls Royce Improvements in or relating to bladed rotors of fluid flow machines
GB1276106A (en) * 1969-12-19 1972-06-01 Rolls Royce FLUID FLOW MACHINE, e.g. GAS TURBINE ENGINE COMPRESSOR
US3640640A (en) * 1970-12-04 1972-02-08 Rolls Royce Fluid flow machine
US3801222A (en) * 1972-02-28 1974-04-02 United Aircraft Corp Platform for compressor or fan blade
US4621979A (en) * 1979-11-30 1986-11-11 United Technologies Corporation Fan rotor blades of turbofan engines
FR2608674B1 (fr) * 1986-12-17 1991-04-19 Snecma Roue de turbine a aubes ceramique
US5240375A (en) * 1992-01-10 1993-08-31 General Electric Company Wear protection system for turbine engine rotor and blade
US6290466B1 (en) * 1999-09-17 2001-09-18 General Electric Company Composite blade root attachment
EP1124038A1 (fr) * 2000-02-09 2001-08-16 Siemens Aktiengesellschaft Aubage de turbine
US6431835B1 (en) * 2000-10-17 2002-08-13 Honeywell International, Inc. Fan blade compliant shim
US6520742B1 (en) * 2000-11-27 2003-02-18 General Electric Company Circular arc multi-bore fan disk
FR2819289B1 (fr) * 2001-01-11 2003-07-11 Snecma Moteurs Systeme de retention des aubes de type combine ou cascade
FR2831207B1 (fr) * 2001-10-24 2004-06-04 Snecma Moteurs Plates-formes pour aubes d'un ensemble rotatif
US6860722B2 (en) * 2003-01-31 2005-03-01 General Electric Company Snap on blade shim
US7284958B2 (en) * 2003-03-22 2007-10-23 Allison Advanced Development Company Separable blade platform
FR2913735B1 (fr) * 2007-03-16 2013-04-19 Snecma Disque de rotor d'une turbomachine

Also Published As

Publication number Publication date
RU2008109760A (ru) 2009-09-20
EP1970538A1 (fr) 2008-09-17
CA2625317A1 (fr) 2008-09-16
FR2913735A1 (fr) 2008-09-19
JP5152755B2 (ja) 2013-02-27
US8277188B2 (en) 2012-10-02
EP1970538B1 (fr) 2010-05-19
DE602008001269D1 (de) 2010-07-01
US20080226457A1 (en) 2008-09-18
RU2487249C2 (ru) 2013-07-10
CA2625317C (fr) 2015-04-28
JP2008232146A (ja) 2008-10-02

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