FR2945329B1 - Rotor de soufflante d'un turboracteur d'avion - Google Patents

Rotor de soufflante d'un turboracteur d'avion

Info

Publication number
FR2945329B1
FR2945329B1 FR0953001A FR0953001A FR2945329B1 FR 2945329 B1 FR2945329 B1 FR 2945329B1 FR 0953001 A FR0953001 A FR 0953001A FR 0953001 A FR0953001 A FR 0953001A FR 2945329 B1 FR2945329 B1 FR 2945329B1
Authority
FR
France
Prior art keywords
turboractor
aircraft
blower rotor
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
FR0953001A
Other languages
English (en)
Other versions
FR2945329A1 (fr
Inventor
Herve Buisson
Jean Luc Goga
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
Priority to FR0953001A priority Critical patent/FR2945329B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to EP10723700.0A priority patent/EP2427658B1/fr
Priority to JP2012509073A priority patent/JP5497157B2/ja
Priority to BRPI1013848A priority patent/BRPI1013848A2/pt
Priority to US13/318,502 priority patent/US8899935B2/en
Priority to CN201080020196.0A priority patent/CN102422026B/zh
Priority to RU2011149487/06A priority patent/RU2525817C2/ru
Priority to CA2760470A priority patent/CA2760470A1/fr
Priority to PCT/FR2010/050747 priority patent/WO2010128229A1/fr
Publication of FR2945329A1 publication Critical patent/FR2945329A1/fr
Application granted granted Critical
Publication of FR2945329B1 publication Critical patent/FR2945329B1/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
    • F01D5/3015—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type with side plates

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0953001A 2009-05-06 2009-05-06 Rotor de soufflante d'un turboracteur d'avion Active FR2945329B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0953001A FR2945329B1 (fr) 2009-05-06 2009-05-06 Rotor de soufflante d'un turboracteur d'avion
JP2012509073A JP5497157B2 (ja) 2009-05-06 2010-04-19 航空機ターボジェット用のファンロータ
BRPI1013848A BRPI1013848A2 (pt) 2009-05-06 2010-04-19 rotor de ventilador, e, turborreator
US13/318,502 US8899935B2 (en) 2009-05-06 2010-04-19 Fan rotor for an airplane turbojet
EP10723700.0A EP2427658B1 (fr) 2009-05-06 2010-04-19 Rotor de soufflante d'un turboreacteur d'avion
CN201080020196.0A CN102422026B (zh) 2009-05-06 2010-04-19 用于飞机涡轮喷气发动机的风扇转子
RU2011149487/06A RU2525817C2 (ru) 2009-05-06 2010-04-19 Ротор вентилятора турбореактивного двигателя самолета
CA2760470A CA2760470A1 (fr) 2009-05-06 2010-04-19 Rotor de soufflante d'un turboreacteur d'avion
PCT/FR2010/050747 WO2010128229A1 (fr) 2009-05-06 2010-04-19 Rotor de soufflante d'un turboreacteur d'avion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0953001A FR2945329B1 (fr) 2009-05-06 2009-05-06 Rotor de soufflante d'un turboracteur d'avion

Publications (2)

Publication Number Publication Date
FR2945329A1 FR2945329A1 (fr) 2010-11-12
FR2945329B1 true FR2945329B1 (fr) 2011-06-03

Family

ID=41278266

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0953001A Active FR2945329B1 (fr) 2009-05-06 2009-05-06 Rotor de soufflante d'un turboracteur d'avion

Country Status (9)

Country Link
US (1) US8899935B2 (fr)
EP (1) EP2427658B1 (fr)
JP (1) JP5497157B2 (fr)
CN (1) CN102422026B (fr)
BR (1) BRPI1013848A2 (fr)
CA (1) CA2760470A1 (fr)
FR (1) FR2945329B1 (fr)
RU (1) RU2525817C2 (fr)
WO (1) WO2010128229A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8840375B2 (en) * 2011-03-21 2014-09-23 United Technologies Corporation Component lock for a gas turbine engine
GB201317161D0 (en) 2013-09-27 2013-11-06 Rolls Royce Plc Retainer plate
GB201318623D0 (en) 2013-10-22 2013-12-04 Rolls Royce Plc Retainer plate
FR3057908B1 (fr) * 2016-10-21 2019-11-22 Safran Aircraft Engines Ensemble rotatif d'une turbomachine muni d'un systeme de maintien axial d'une aube
RU2659416C1 (ru) * 2017-04-07 2018-07-02 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Рабочее колесо компрессора газотурбинного двигателя

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3395891A (en) * 1967-09-21 1968-08-06 Gen Electric Lock for turbomachinery blades
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
FR2535793B1 (fr) * 1982-11-08 1987-04-10 Snecma Dispositif de verrouillage axial d'aubes de soufflante
FR2535794A1 (fr) * 1982-11-08 1984-05-11 Snecma Dispositif de retenue axiale et radiale d'aubes de soufflante
SU1130693A1 (ru) * 1983-04-11 1984-12-23 Производственное объединение "Брянский машиностроительный завод" им.В.И.Ленина Устройство дл осевой фиксации рабочих лопаток турбомашины
US5259728A (en) * 1992-05-08 1993-11-09 General Electric Company Bladed disk assembly
US5350279A (en) * 1993-07-02 1994-09-27 General Electric Company Gas turbine engine blade retainer sub-assembly
US5984639A (en) * 1998-07-09 1999-11-16 Pratt & Whitney Canada Inc. Blade retention apparatus for gas turbine rotor
FR2886336B1 (fr) * 2005-05-26 2007-08-24 Snecma Moteurs Sa Perfectionnement a une roue aubagee de rotor pour renforcer le verrouillage des aubes
FR2889264B1 (fr) 2005-07-29 2007-11-02 Snecma Verrouillage des aubes dans un rotor de soufflante
FR2900437B1 (fr) 2006-04-27 2008-07-25 Snecma Sa Systeme de retention des aubes dans un rotor

Also Published As

Publication number Publication date
BRPI1013848A2 (pt) 2016-04-12
EP2427658A1 (fr) 2012-03-14
EP2427658B1 (fr) 2015-07-08
FR2945329A1 (fr) 2010-11-12
RU2525817C2 (ru) 2014-08-20
RU2011149487A (ru) 2013-06-20
JP5497157B2 (ja) 2014-05-21
CN102422026B (zh) 2014-08-20
US20120045341A1 (en) 2012-02-23
JP2012526231A (ja) 2012-10-25
CA2760470A1 (fr) 2010-11-11
US8899935B2 (en) 2014-12-02
CN102422026A (zh) 2012-04-18
WO2010128229A1 (fr) 2010-11-11

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