FR2890684B1 - Clinquant pour aube de turboreacteur - Google Patents

Clinquant pour aube de turboreacteur

Info

Publication number
FR2890684B1
FR2890684B1 FR0509420A FR0509420A FR2890684B1 FR 2890684 B1 FR2890684 B1 FR 2890684B1 FR 0509420 A FR0509420 A FR 0509420A FR 0509420 A FR0509420 A FR 0509420A FR 2890684 B1 FR2890684 B1 FR 2890684B1
Authority
FR
France
Prior art keywords
turboreactor
clinking
blade
turboreactor blade
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.)
Expired - Fee Related
Application number
FR0509420A
Other languages
English (en)
Other versions
FR2890684A1 (fr
Inventor
Jean Bernard Forgue
Jack Pierre Lauvergnat
Thierry Nitre
Patrick 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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR0509420A priority Critical patent/FR2890684B1/fr
Priority to CA2558759A priority patent/CA2558759C/fr
Priority to US11/519,015 priority patent/US7938626B2/en
Priority to EP06120645A priority patent/EP1764480B1/fr
Priority to JP2006248977A priority patent/JP5068049B2/ja
Priority to RU2006133128/06A priority patent/RU2413072C2/ru
Priority to DE602006003493T priority patent/DE602006003493D1/de
Priority to ES06120645T priority patent/ES2317437T3/es
Priority to CN2006101541611A priority patent/CN1932251B/zh
Publication of FR2890684A1 publication Critical patent/FR2890684A1/fr
Application granted granted Critical
Publication of FR2890684B1 publication Critical patent/FR2890684B1/fr
Expired - Fee Related 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
    • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers

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)
FR0509420A 2005-09-15 2005-09-15 Clinquant pour aube de turboreacteur Expired - Fee Related FR2890684B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR0509420A FR2890684B1 (fr) 2005-09-15 2005-09-15 Clinquant pour aube de turboreacteur
US11/519,015 US7938626B2 (en) 2005-09-15 2006-09-12 Shim for a turbojet blade
CA2558759A CA2558759C (fr) 2005-09-15 2006-09-12 Clinquant pour aube de turboreacteur
JP2006248977A JP5068049B2 (ja) 2005-09-15 2006-09-14 ターボジェットブレードのためのシム
EP06120645A EP1764480B1 (fr) 2005-09-15 2006-09-14 Clinquant pour aube de turboréacteur
RU2006133128/06A RU2413072C2 (ru) 2005-09-15 2006-09-14 Прокладка из фольги для лопатки турбореактивного двигателя, лопатка вентилятора, содержащая такую прокладку из фольги, и турбореактивный двигатель, содержащий такую лопатку вентилятора
DE602006003493T DE602006003493D1 (de) 2005-09-15 2006-09-14 Zwischenstück für eine Schaufel eines Turbinentriebwerks
ES06120645T ES2317437T3 (es) 2005-09-15 2006-09-14 Calzo para alabe de turborreactor.
CN2006101541611A CN1932251B (zh) 2005-09-15 2006-09-15 涡轮喷气发动机叶片的填隙片

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0509420A FR2890684B1 (fr) 2005-09-15 2005-09-15 Clinquant pour aube de turboreacteur

Publications (2)

Publication Number Publication Date
FR2890684A1 FR2890684A1 (fr) 2007-03-16
FR2890684B1 true FR2890684B1 (fr) 2007-12-07

Family

ID=36577386

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0509420A Expired - Fee Related FR2890684B1 (fr) 2005-09-15 2005-09-15 Clinquant pour aube de turboreacteur

Country Status (9)

Country Link
US (1) US7938626B2 (fr)
EP (1) EP1764480B1 (fr)
JP (1) JP5068049B2 (fr)
CN (1) CN1932251B (fr)
CA (1) CA2558759C (fr)
DE (1) DE602006003493D1 (fr)
ES (1) ES2317437T3 (fr)
FR (1) FR2890684B1 (fr)
RU (1) RU2413072C2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2660985C1 (ru) * 2013-12-06 2018-07-11 Турбомека Ротор с лопатками

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FR2918702B1 (fr) * 2007-07-13 2009-10-16 Snecma Sa Clinquant pour aube de turbomachine
FR2918703B1 (fr) 2007-07-13 2009-10-16 Snecma Sa Ensemble de rotor de turbomachine
FR2921409B1 (fr) * 2007-09-25 2009-12-18 Snecma Clinquant pour aube de turbomachine.
US8206118B2 (en) * 2008-01-04 2012-06-26 United Technologies Corporation Airfoil attachment
FR2934873B1 (fr) * 2008-08-06 2011-07-08 Snecma Dispositif amortisseur de vibrations pour attaches d'aubes.
US8047778B2 (en) * 2009-01-06 2011-11-01 General Electric Company Method and apparatus for insuring proper installation of stators in a compressor case
FR2945074B1 (fr) 2009-04-29 2011-06-03 Snecma Cale d'aube de soufflante renforcee
DE102009024845A1 (de) * 2009-06-09 2010-12-16 Howaldtswerke-Deutsche Werft Gmbh Propeller
JP5444932B2 (ja) * 2009-08-19 2014-03-19 株式会社Ｉｈｉ 動翼の固定装置、翼回転装置及び翼回転装置の組立方法
FR2951494B1 (fr) * 2009-10-15 2011-12-09 Snecma Clinquant pour aube de turbomachine.
FR2955904B1 (fr) * 2010-02-04 2012-07-20 Snecma Soufflante de turbomachine
FR2959527B1 (fr) * 2010-04-28 2012-07-20 Snecma Piece anti-usure pour echasse d'aube de soufflante de turboreacteur
FR2963383B1 (fr) * 2010-07-27 2016-09-09 Snecma Aube de turbomachine, rotor, turbine basse pression et turbomachine equipes d'une telle aube
GB2477825B (en) * 2010-09-23 2015-04-01 Rolls Royce Plc Anti fret liner assembly
US8225614B2 (en) * 2010-10-07 2012-07-24 General Electric Company Shim for sealing transition pieces
FR2981132B1 (fr) * 2011-10-10 2013-12-06 Snecma Ensemble pour turbomachine a refroidissement de disque
US9246372B2 (en) * 2012-01-20 2016-01-26 Fluor Technologies Corporation Rotor pole support ribs in gearless drives
US10273816B2 (en) 2013-02-12 2019-04-30 United Technologies Corporation Wear pad to prevent cracking of fan blade
EP2971559B1 (fr) * 2013-03-13 2019-10-23 United Technologies Corporation Agencement d'aubes avec patins d'usure, moteur à turbine à gaz et procédé de fabrication d'un agencement d'aubes
US10280771B2 (en) * 2013-10-11 2019-05-07 United Technologies Corporation Compressible fan blade with root spacer
US9464531B2 (en) * 2013-10-16 2016-10-11 General Electric Company Locking spacer assembly
FR3027071B1 (fr) * 2014-10-13 2019-08-23 Safran Aircraft Engines Procede d'intervention sur un rotor et clinquant associe
CN104500447A (zh) * 2014-12-14 2015-04-08 惠阳航空螺旋桨有限责任公司 风洞轴流压缩机风扇
CN104500446A (zh) * 2014-12-14 2015-04-08 惠阳航空螺旋桨有限责任公司 风洞轴流压缩机转子复合材料叶片根部连接结构
US10378371B2 (en) 2014-12-18 2019-08-13 United Technologies Corporation Anti-rotation vane
US10087948B2 (en) * 2015-03-30 2018-10-02 United Technologies Corporation Fan blade and method of covering a fan blade root portion
EP3075961A1 (fr) * 2015-04-02 2016-10-05 Siemens Aktiengesellschaft Ensemble d'aube directrice
US9772313B2 (en) * 2015-04-21 2017-09-26 The Boeing Company Method and apparatus for identifying shim geometries
US10738626B2 (en) * 2017-10-24 2020-08-11 General Electric Company Connection assemblies between turbine rotor blades and rotor wheels
US11555407B2 (en) 2020-05-19 2023-01-17 General Electric Company Turbomachine rotor assembly
FR3120911A1 (fr) 2021-03-16 2022-09-23 Safran Aircraft Engines Aube comprenant un membre d’attache résistant au frottement et roue mobile comprenant une telle aube d’une turbine axiale de turbomachine
FR3124218A1 (fr) 2021-06-21 2022-12-23 Safran Aircraft Engines Clinquant a languette longue pour pied d’aube de rotor de turbomachine
FR3124824B1 (fr) 2021-07-01 2023-12-15 Safran Aircraft Engines Clinquant a languette nervurée
FR3124823B1 (fr) 2021-07-02 2023-11-17 Safran Aircraft Engines Encoche de verouillage de clinquant d’aube
FR3127522A1 (fr) 2021-09-24 2023-03-31 Safran Aircraft Engines Procede de preparation d’un pied d’une aube de turbomachine
FR3127986A1 (fr) 2021-10-11 2023-04-14 Safran Aircraft Engines Aube de turbine avec un pied comprenant un bloquage du clinquant
FR3129976A1 (fr) 2021-12-03 2023-06-09 Safran Aircraft Engines Ensemble comprenant un clinquant monte sur un disque d’une roue mobile
CN114042695B (zh) * 2022-01-13 2022-04-29 中国民航大学 一种飞机发动机风扇叶片清洗润滑设备
FR3136507A1 (fr) * 2022-06-13 2023-12-15 Safran Aircraft Engines Dispositif de retenue axiale des aubes mobiles d’une turbine BP dans les alvéoles d’un disque de rotor de la turbine BP et procédé de montage de ces aubes mobiles

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US5423831A (en) * 1991-01-24 1995-06-13 Nates; Colin Clamp
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JPH10317907A (ja) * 1997-05-22 1998-12-02 Hitachi Ltd 圧縮機翼固定構造
US6212742B1 (en) * 1999-01-29 2001-04-10 Abb Power T & D Company Inc. Drip tray clamps for transformer fuse holders
CN2378627Y (zh) * 1999-02-04 2000-05-17 珠海市南产业电器有限公司 一种用于圣诞灯串的线夹
US6431835B1 (en) * 2000-10-17 2002-08-13 Honeywell International, Inc. Fan blade compliant shim
US6513767B1 (en) * 2001-09-04 2003-02-04 J. Linn Rodgers Ergonomic encirclement
JP2003314369A (ja) * 2002-04-26 2003-11-06 Ishikawajima Harima Heavy Ind Co Ltd ダブテールシム
US6860722B2 (en) * 2003-01-31 2005-03-01 General Electric Company Snap on blade shim

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2660985C1 (ru) * 2013-12-06 2018-07-11 Турбомека Ротор с лопатками
US10858946B2 (en) 2013-12-06 2020-12-08 Safran Helicopter Engines Bladed rotor

Also Published As

Publication number Publication date
ES2317437T3 (es) 2009-04-16
DE602006003493D1 (de) 2008-12-18
RU2006133128A (ru) 2008-03-20
JP5068049B2 (ja) 2012-11-07
RU2413072C2 (ru) 2011-02-27
CA2558759A1 (fr) 2007-03-15
EP1764480A1 (fr) 2007-03-21
US7938626B2 (en) 2011-05-10
JP2007077993A (ja) 2007-03-29
CA2558759C (fr) 2013-03-05
CN1932251B (zh) 2010-09-29
US20100226777A1 (en) 2010-09-09
EP1764480B1 (fr) 2008-11-05
CN1932251A (zh) 2007-03-21
FR2890684A1 (fr) 2007-03-16

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20110531