[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

FR3023581B1 - Montage d'aubes en peripherie d'un disque de turbomachine - Google Patents

Montage d'aubes en peripherie d'un disque de turbomachine

Info

Publication number
FR3023581B1
FR3023581B1 FR1456554A FR1456554A FR3023581B1 FR 3023581 B1 FR3023581 B1 FR 3023581B1 FR 1456554 A FR1456554 A FR 1456554A FR 1456554 A FR1456554 A FR 1456554A FR 3023581 B1 FR3023581 B1 FR 3023581B1
Authority
FR
France
Prior art keywords
aubes
periphery
mounting
turbomachine disk
turbomachine
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
FR1456554A
Other languages
English (en)
Other versions
FR3023581A1 (fr
Inventor
Sebastien Congratel
Christian Bariaud
Dominique Jean Andre Bousquet
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 FR1456554A priority Critical patent/FR3023581B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to PCT/FR2015/051840 priority patent/WO2016005687A1/fr
Priority to RU2017101545A priority patent/RU2701925C2/ru
Priority to BR112017000302-3A priority patent/BR112017000302B1/pt
Priority to CA2954105A priority patent/CA2954105C/fr
Priority to CN201580036951.7A priority patent/CN106471217B/zh
Priority to EP15748279.5A priority patent/EP3167162B1/fr
Priority to US15/323,902 priority patent/US10787919B2/en
Publication of FR3023581A1 publication Critical patent/FR3023581A1/fr
Application granted granted Critical
Publication of FR3023581B1 publication Critical patent/FR3023581B1/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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/125—Fluid guiding means, e.g. vanes related to the tip of a stator vane

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1456554A 2014-07-08 2014-07-08 Montage d'aubes en peripherie d'un disque de turbomachine Active FR3023581B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1456554A FR3023581B1 (fr) 2014-07-08 2014-07-08 Montage d'aubes en peripherie d'un disque de turbomachine
RU2017101545A RU2701925C2 (ru) 2014-07-08 2015-07-02 Способ установки лопаток по периферии диска турбинного двигателя и инструмент для монтажа лопатки
BR112017000302-3A BR112017000302B1 (pt) 2014-07-08 2015-07-02 Método de montagem de palhetas e ferramenta de montagem de palheta
CA2954105A CA2954105C (fr) 2014-07-08 2015-07-02 Montage d'aubes en peripherie d'un disque de turbomachine
PCT/FR2015/051840 WO2016005687A1 (fr) 2014-07-08 2015-07-02 Montage d'aubes en peripherie d'un disque de turbomachine
CN201580036951.7A CN106471217B (zh) 2014-07-08 2015-07-02 在涡轮发动机圆盘周边桨叶的安装方法
EP15748279.5A EP3167162B1 (fr) 2014-07-08 2015-07-02 Montage d'aubes en peripherie d'un disque de turbomachine
US15/323,902 US10787919B2 (en) 2014-07-08 2015-07-02 Mounting of vanes at the periphery of a turbine engine disc

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1456554A FR3023581B1 (fr) 2014-07-08 2014-07-08 Montage d'aubes en peripherie d'un disque de turbomachine

Publications (2)

Publication Number Publication Date
FR3023581A1 FR3023581A1 (fr) 2016-01-15
FR3023581B1 true FR3023581B1 (fr) 2016-07-15

Family

ID=51519075

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1456554A Active FR3023581B1 (fr) 2014-07-08 2014-07-08 Montage d'aubes en peripherie d'un disque de turbomachine

Country Status (8)

Country Link
US (1) US10787919B2 (fr)
EP (1) EP3167162B1 (fr)
CN (1) CN106471217B (fr)
BR (1) BR112017000302B1 (fr)
CA (1) CA2954105C (fr)
FR (1) FR3023581B1 (fr)
RU (1) RU2701925C2 (fr)
WO (1) WO2016005687A1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3156603A1 (fr) * 2015-10-13 2017-04-19 Siemens Aktiengesellschaft Dispositif d'assemblage pour monter/démonter des aubes sur un disque
US10883386B2 (en) * 2017-06-21 2021-01-05 Mitsubishi Hitachi Power Systems Americas, Inc. Methods and devices for turbine blade installation alignment
US10830756B2 (en) 2017-09-22 2020-11-10 Applied Materials, Inc. Method to create a free-standing membrane for biological applications
US11084150B2 (en) * 2018-01-31 2021-08-10 Raytheon Technologies Corporation Wear liner installation tool
FR3090030B1 (fr) 2018-12-12 2020-11-20 Safran Aircraft Engines Dispositif de maintien pour le démontage d’une roue à aubes de turbomachine et procédé l’utilisant
CN109931112A (zh) * 2019-04-28 2019-06-25 杭州汽轮机股份有限公司 一种汽轮机自由叶片结构及其装配方法
DE102019215220A1 (de) 2019-10-02 2021-04-08 MTU Aero Engines AG System mit einer Laufschaufel für eine Gasturbine mit einem einen Dichtungsabschnitt aufweisenden Schaufelfußschutzblech
FR3127018A1 (fr) * 2021-09-14 2023-03-17 Safran Aircraft Engines Aube mobile pour turbine de turbomachine, présentant une conception améliorant l’étanchéité des cavités inter-aubes

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1009689A1 (ru) 1981-07-17 1983-04-07 Lavrov Vladimir V Способ сборки лопаток с диском
US6416286B1 (en) * 2000-12-28 2002-07-09 General Electric Company System and method for securing a radially inserted integral closure bucket to a turbine rotor wheel assembly having axially inserted buckets
GB0406889D0 (en) * 2004-03-26 2004-04-28 Alstom Technology Ltd Turbine and turbine blade
EP1916389A1 (fr) * 2006-10-26 2008-04-30 Siemens Aktiengesellschaft Assemblage d'aubes de turbine
US7975354B2 (en) * 2007-02-08 2011-07-12 United Technologies Corporation Bladed disk assembly method and impact device
US20120034086A1 (en) 2010-08-04 2012-02-09 General Electric Company Swing axial entry dovetail for steam turbine buckets
DE102010048732B3 (de) * 2010-10-16 2012-03-15 Mtu Aero Engines Gmbh Verfahren zum Herstellen eines integral beschaufelten Rotors

Also Published As

Publication number Publication date
CA2954105A1 (fr) 2016-01-14
US20170145841A1 (en) 2017-05-25
BR112017000302B1 (pt) 2022-11-16
CA2954105C (fr) 2022-04-26
BR112017000302A2 (pt) 2017-11-07
EP3167162B1 (fr) 2018-09-12
CN106471217B (zh) 2019-03-15
US10787919B2 (en) 2020-09-29
EP3167162A1 (fr) 2017-05-17
WO2016005687A1 (fr) 2016-01-14
CN106471217A (zh) 2017-03-01
RU2017101545A3 (fr) 2019-01-25
RU2701925C2 (ru) 2019-10-02
RU2017101545A (ru) 2018-08-08
FR3023581A1 (fr) 2016-01-15

Similar Documents

Publication Publication Date Title
IT201600097744A1 (it) Assieme di mozzo di bicicletta
FR3023581B1 (fr) Montage d'aubes en peripherie d'un disque de turbomachine
PL3792465T3 (pl) Architektura wielowirnikowego silnika turbinowego
FR3024883B1 (fr) Module de turbomachine
DK3073631T3 (da) Vindmølle med subsynkron svingningsundertrykkelse
FR3030446B1 (fr) Turbomachine a helice multi-diametres
DK3042084T3 (da) Flertrins centrifugalkompressor
DK2962965T3 (da) Vibrationstransportør
HUE050519T2 (hu) Radiális turbógép
DE112016005315A5 (de) Filterscheibe
FR2993599B1 (fr) Disque labyrinthe de turbomachine
FR3028575B1 (fr) Secteur d'aubage de stator d'une turbomachine
FR3012539B1 (fr) Compresseur radial
GB2567103B (en) Turbo engine rotor disc
DE112015002702T8 (de) Turbolader
GB201514212D0 (en) Turbine disc assembly
FR3021742B1 (fr) Veine instrumentee de turbomachine
DK3473901T3 (da) Skiveanordning
ES1180309Y (es) Sudario
DE112018002506A5 (de) Lamellenpaket
TH1501007056B (th) คอมเพรสเซอร์แบบก้นหอย
TH1501007051B (th) คอมเพรสเซอร์แบบก้นหอย
UA33671S (uk) Кришка гриль-установки
ITUA20163402A1 (it) Turbina pulitrice
ES1137208Y (es) Disector atraumatico

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20160115

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

CD Change of name or company name

Owner name: SAFRAN AIRCRAFT ENGINES, FR

Effective date: 20170719

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11