FR2911632B1 - Disque de rotor de soufflante de turbomachine - Google Patents

Disque de rotor de soufflante de turbomachine

Info

Publication number
FR2911632B1
FR2911632B1 FR0700326A FR0700326A FR2911632B1 FR 2911632 B1 FR2911632 B1 FR 2911632B1 FR 0700326 A FR0700326 A FR 0700326A FR 0700326 A FR0700326 A FR 0700326A FR 2911632 B1 FR2911632 B1 FR 2911632B1
Authority
FR
France
Prior art keywords
rotor disc
turbomachine blower
turbomachine
blower
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
FR0700326A
Other languages
English (en)
Other versions
FR2911632A1 (fr
Inventor
Hong Son Le
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 FR0700326A priority Critical patent/FR2911632B1/fr
Priority to EP07291632.3A priority patent/EP1950381B1/fr
Priority to CA2619299A priority patent/CA2619299C/fr
Priority to JP2008007636A priority patent/JP5283388B2/ja
Priority to RU2008101906/06A priority patent/RU2454572C2/ru
Priority to US12/016,517 priority patent/US8246309B2/en
Publication of FR2911632A1 publication Critical patent/FR2911632A1/fr
Application granted granted Critical
Publication of FR2911632B1 publication Critical patent/FR2911632B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D5/3007—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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of 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
    • F04D29/26—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

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)
FR0700326A 2007-01-18 2007-01-18 Disque de rotor de soufflante de turbomachine Active FR2911632B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR0700326A FR2911632B1 (fr) 2007-01-18 2007-01-18 Disque de rotor de soufflante de turbomachine
EP07291632.3A EP1950381B1 (fr) 2007-01-18 2007-12-27 Disque de rotor de soufflante de turbomachine
CA2619299A CA2619299C (fr) 2007-01-18 2008-01-16 Disque de rotor de soufflante de turbomachine
JP2008007636A JP5283388B2 (ja) 2007-01-18 2008-01-17 ターボ機械ファン用のロータディスク
RU2008101906/06A RU2454572C2 (ru) 2007-01-18 2008-01-17 Диск ротора вентилятора газотурбинного двигателя и газотурбинный двигатель
US12/016,517 US8246309B2 (en) 2007-01-18 2008-01-18 Rotor disk for turbomachine fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0700326A FR2911632B1 (fr) 2007-01-18 2007-01-18 Disque de rotor de soufflante de turbomachine

Publications (2)

Publication Number Publication Date
FR2911632A1 FR2911632A1 (fr) 2008-07-25
FR2911632B1 true FR2911632B1 (fr) 2009-08-21

Family

ID=38421439

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0700326A Active FR2911632B1 (fr) 2007-01-18 2007-01-18 Disque de rotor de soufflante de turbomachine

Country Status (6)

Country Link
US (1) US8246309B2 (fr)
EP (1) EP1950381B1 (fr)
JP (1) JP5283388B2 (fr)
CA (1) CA2619299C (fr)
FR (1) FR2911632B1 (fr)
RU (1) RU2454572C2 (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWM334886U (en) * 2007-12-12 2008-06-21 Taiwei Fan Technology Co Ltd Combination type miniature axial-flow fan
DE102009007468A1 (de) * 2009-02-04 2010-08-19 Mtu Aero Engines Gmbh Integral beschaufelte Rotorscheibe für eine Turbine
US8485784B2 (en) * 2009-07-14 2013-07-16 General Electric Company Turbine bucket lockwire rotation prevention
EP2299056A1 (fr) * 2009-09-02 2011-03-23 Siemens Aktiengesellschaft Refroidissement d'un composant de turbine à gaz sous la forme d'un disque de rotor ou d'une aube
FR2955904B1 (fr) * 2010-02-04 2012-07-20 Snecma Soufflante de turbomachine
FR2968363B1 (fr) * 2010-12-03 2014-12-05 Snecma Rotor de turbomachine avec une cale anti-usure entre un disque et un anneau
EP2546465A1 (fr) 2011-07-14 2013-01-16 Siemens Aktiengesellschaft Pied d'aube, aube, disque de rotor et ensemble de turbomachine associés
JP2013249756A (ja) * 2012-05-31 2013-12-12 Hitachi Ltd 圧縮機
EP2971568B1 (fr) * 2013-03-15 2021-11-03 Raytheon Technologies Corporation Joint plat pour une soufflante d'un moteur à turbine à gaz
CA2918320C (fr) 2013-07-26 2018-05-15 Mra Systems, Inc. Mat d'accrochage de moteur pour aeronef
FR3014151B1 (fr) * 2013-11-29 2015-12-04 Snecma Soufflante, en particulier pour une turbomachine
FR3064667B1 (fr) * 2017-03-31 2020-05-15 Safran Aircraft Engines Dispositif de refroidissement d'un rotor de turbomachine
CN107100894A (zh) * 2017-07-05 2017-08-29 陕西金翼通风科技有限公司 一种通风机用叶片、叶轮及叶轮的安装方法
US10830048B2 (en) 2019-02-01 2020-11-10 Raytheon Technologies Corporation Gas turbine rotor disk having scallop shield feature
EP3862571A1 (fr) * 2020-02-06 2021-08-11 ABB Schweiz AG Ventilateur, machine synchrone et procédé de fabrication d'un ventilateur

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2965355A (en) * 1956-01-17 1960-12-20 United Aircraft Corp Turbine disc burst inhibitor
SU387128A1 (ru) * 1971-05-24 1973-06-21 Рабочее колесо турбомашины
US4344740A (en) * 1979-09-28 1982-08-17 United Technologies Corporation Rotor assembly
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
FR2695433B1 (fr) * 1992-09-09 1994-10-21 Snecma Joint annulaire d'étanchéité disposé à une extrémité axiale d'un rotor et recouvrant des brochages d'aubes.
US5281098A (en) * 1992-10-28 1994-01-25 General Electric Company Single ring blade retaining assembly
US5443365A (en) * 1993-12-02 1995-08-22 General Electric Company Fan blade for blade-out protection
WO1997049921A1 (fr) * 1996-06-21 1997-12-31 Siemens Aktiengesellschaft Rotor pour une turbomachine avec des pales a monter dans des rainures et pales pour un rotor
RU2173390C2 (ru) * 1996-06-21 2001-09-10 Сименс Акциенгезелльшафт Ротор для турбомашины с устанавливаемыми в пазы лопатками, а также лопатка для ротора
US6183202B1 (en) * 1999-04-30 2001-02-06 General Electric Company Stress relieved blade support
GB9925261D0 (en) * 1999-10-27 1999-12-29 Rolls Royce Plc Locking devices
FR2803623B1 (fr) * 2000-01-06 2002-03-01 Snecma Moteurs Agencement de retenue axiale d'aubes dans un disque
US6481971B1 (en) * 2000-11-27 2002-11-19 General Electric Company Blade spacer
US6634863B1 (en) * 2000-11-27 2003-10-21 General Electric Company Circular arc multi-bore fan disk assembly
GB2380770B (en) * 2001-10-13 2005-09-07 Rolls Royce Plc Indentor arrangement
GB2409240B (en) * 2003-12-18 2007-04-11 Rolls Royce Plc A gas turbine rotor
JP2005273646A (ja) * 2004-02-25 2005-10-06 Mitsubishi Heavy Ind Ltd 動翼体及びこの動翼体を有する回転機械
EP1703079A1 (fr) * 2005-08-26 2006-09-20 Siemens Aktiengesellschaft Solide de rotation pour la fixation d'une aube d'une turbo-machine

Also Published As

Publication number Publication date
CA2619299A1 (fr) 2008-07-18
EP1950381B1 (fr) 2016-03-02
JP5283388B2 (ja) 2013-09-04
JP2008180219A (ja) 2008-08-07
FR2911632A1 (fr) 2008-07-25
US20080298972A1 (en) 2008-12-04
EP1950381A1 (fr) 2008-07-30
RU2454572C2 (ru) 2012-06-27
RU2008101906A (ru) 2009-07-27
US8246309B2 (en) 2012-08-21
CA2619299C (fr) 2015-06-09

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