FR2987086B1 - Joint lineaire de plateforme inter-aubes - Google Patents

Joint lineaire de plateforme inter-aubes

Info

Publication number
FR2987086B1
FR2987086B1 FR1251611A FR1251611A FR2987086B1 FR 2987086 B1 FR2987086 B1 FR 2987086B1 FR 1251611 A FR1251611 A FR 1251611A FR 1251611 A FR1251611 A FR 1251611A FR 2987086 B1 FR2987086 B1 FR 2987086B1
Authority
FR
France
Prior art keywords
aubes
linear joint
platform inter
inter
platform
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
FR1251611A
Other languages
English (en)
Other versions
FR2987086A1 (fr
Inventor
Anne-Laure Ravier
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 FR1251611A priority Critical patent/FR2987086B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to CA2864536A priority patent/CA2864536C/fr
Priority to EP13710460.0A priority patent/EP2817491B1/fr
Priority to BR112014020359-8A priority patent/BR112014020359B1/pt
Priority to PCT/FR2013/050310 priority patent/WO2013124570A1/fr
Priority to RU2014138113A priority patent/RU2617635C2/ru
Priority to US14/378,788 priority patent/US9869323B2/en
Priority to JP2014558178A priority patent/JP6199319B2/ja
Priority to CN201380010535.0A priority patent/CN104145087B/zh
Publication of FR2987086A1 publication Critical patent/FR2987086A1/fr
Application granted granted Critical
Publication of FR2987086B1 publication Critical patent/FR2987086B1/fr
Priority to IN6758DEN2014 priority patent/IN2014DN06758A/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/16Sealings between pressure and suction sides
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • F01D11/008Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms

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)
  • Gasket Seals (AREA)
FR1251611A 2012-02-22 2012-02-22 Joint lineaire de plateforme inter-aubes Active FR2987086B1 (fr)

Priority Applications (10)

Application Number Priority Date Filing Date Title
FR1251611A FR2987086B1 (fr) 2012-02-22 2012-02-22 Joint lineaire de plateforme inter-aubes
CN201380010535.0A CN104145087B (zh) 2012-02-22 2013-02-15 用于叶片间平台的线性衬垫
BR112014020359-8A BR112014020359B1 (pt) 2012-02-22 2013-02-15 Gaxeta linear de plataforma interpás, plataforma interpás, rotor, e, turborreator
PCT/FR2013/050310 WO2013124570A1 (fr) 2012-02-22 2013-02-15 Joint linéaire de plateforme inter- aubes, plateforme inter- aubes, rotor et turboréacteur associés
RU2014138113A RU2617635C2 (ru) 2012-02-22 2013-02-15 Линейная прокладка для межлопаточной полки
US14/378,788 US9869323B2 (en) 2012-02-22 2013-02-15 Linear gasket for an inter-blade platform
CA2864536A CA2864536C (fr) 2012-02-22 2013-02-15 Joint lineaire de plateforme inter-aubes, plateforme inter-aubes, rotor et turboreacteur associes
EP13710460.0A EP2817491B1 (fr) 2012-02-22 2013-02-15 Joint linéaire de plateforme inter- aubes, plateforme inter- aubes, rotor et turboréacteur associés
JP2014558178A JP6199319B2 (ja) 2012-02-22 2013-02-15 ブレード間プラットフォーム用線形ガスケット
IN6758DEN2014 IN2014DN06758A (fr) 2012-02-22 2014-08-12

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1251611A FR2987086B1 (fr) 2012-02-22 2012-02-22 Joint lineaire de plateforme inter-aubes

Publications (2)

Publication Number Publication Date
FR2987086A1 FR2987086A1 (fr) 2013-08-23
FR2987086B1 true FR2987086B1 (fr) 2014-03-21

Family

ID=47901174

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1251611A Active FR2987086B1 (fr) 2012-02-22 2012-02-22 Joint lineaire de plateforme inter-aubes

Country Status (10)

Country Link
US (1) US9869323B2 (fr)
EP (1) EP2817491B1 (fr)
JP (1) JP6199319B2 (fr)
CN (1) CN104145087B (fr)
BR (1) BR112014020359B1 (fr)
CA (1) CA2864536C (fr)
FR (1) FR2987086B1 (fr)
IN (1) IN2014DN06758A (fr)
RU (1) RU2617635C2 (fr)
WO (1) WO2013124570A1 (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160305439A1 (en) * 2013-12-13 2016-10-20 United Technologies Corporation Fan platform edge seal
US9988920B2 (en) * 2015-04-08 2018-06-05 United Technologies Corporation Fan blade platform seal with leading edge winglet
FR3035676B1 (fr) * 2015-04-29 2017-05-12 Snecma Aube munie de plateformes possedant un raidisseur
FR3048997B1 (fr) * 2016-03-21 2020-03-27 Safran Aircraft Engines Plateforme d'aube et disque de soufflante de turbomachine aeronautique
FR3053083B1 (fr) 2016-06-22 2019-11-01 Safran Aircraft Engines Anneau de carenage de roue a aubes
BR112019021687A2 (pt) * 2017-04-21 2020-05-12 Zenimax Media Inc. Sistemas e métodos para renderização de qualidade adaptativa guiada por codificador
EP3438410B1 (fr) 2017-08-01 2021-09-29 General Electric Company Système d'étanchéité pour machine rotative
US10738630B2 (en) * 2018-02-19 2020-08-11 General Electric Company Platform apparatus for propulsion rotor
US11028714B2 (en) * 2018-07-16 2021-06-08 Raytheon Technologies Corporation Fan platform wedge seal
FR3091563B1 (fr) 2019-01-04 2023-01-20 Safran Aircraft Engines Joint d’étanchéité amélioré de plateforme inter-aubes
FR3097904B1 (fr) * 2019-06-26 2021-06-11 Safran Aircraft Engines Plateforme inter-aube avec caisson sacrificiel
FR3099201B1 (fr) * 2019-07-25 2021-08-20 Safran Aircraft Engines Rotor de soufflante comportant des moyens d'etancheite ameliores

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU881354A2 (ru) * 1980-01-04 1981-11-15 Предприятие П/Я В-2285 Устройство дл уплотнени рабочих лопаток турбины
DE19501724C1 (de) * 1995-01-20 1996-10-10 Bruss Dichtungstechnik Wellendichtring sowie Verfahren und Vorrichtung zu seiner Herstellung
JP3684620B2 (ja) * 1995-06-19 2005-08-17 石川島播磨重工業株式会社 翼間スペーサのシール構造
GB9602129D0 (en) * 1996-02-02 1996-04-03 Rolls Royce Plc Rotors for gas turbine engines
GB9915637D0 (en) * 1999-07-06 1999-09-01 Rolls Royce Plc A rotor seal
EP1124038A1 (fr) * 2000-02-09 2001-08-16 Siemens Aktiengesellschaft Aubage de turbine
US6447250B1 (en) * 2000-11-27 2002-09-10 General Electric Company Non-integral fan platform
US6705617B2 (en) * 2001-11-28 2004-03-16 Federal-Mogul World Wide, Inc. Hydrodynamic seal and method of making the same
FR2858351B1 (fr) * 2003-07-31 2006-01-13 Snecma Moteurs Plate-forme inter-aubes a flechissement lateral, pour un support d'aubes de turboreacteur
GB2420162A (en) * 2004-11-16 2006-05-17 Cross Mfg Company A seal arrangement for sealing between turbine blades
GB0611031D0 (en) * 2006-06-06 2006-07-12 Rolls Royce Plc An aerofoil stage and a seal for use therein
US7891670B2 (en) * 2008-02-01 2011-02-22 Freudenberg-Nok General Partnership Multi-directional shaft seal
FR2939835B1 (fr) * 2008-12-12 2017-06-09 Snecma Joint d'etancheite de plateforme dans un rotor de turbomachine, methode pour ameliorer l'etancheite entre une plateforme et une aube de turbomachine.
GB0910752D0 (en) 2009-06-23 2009-08-05 Rolls Royce Plc An annulus filler for a gas turbine engine
US8066479B2 (en) * 2010-04-05 2011-11-29 Pratt & Whitney Rocketdyne, Inc. Non-integral platform and damper for an airfoil

Also Published As

Publication number Publication date
CN104145087B (zh) 2016-03-02
WO2013124570A1 (fr) 2013-08-29
RU2617635C2 (ru) 2017-04-25
JP2015510077A (ja) 2015-04-02
US20150016960A1 (en) 2015-01-15
RU2014138113A (ru) 2016-04-10
US9869323B2 (en) 2018-01-16
BR112014020359B1 (pt) 2021-10-19
CA2864536C (fr) 2019-06-11
IN2014DN06758A (fr) 2015-05-22
CA2864536A1 (fr) 2013-08-29
JP6199319B2 (ja) 2017-09-20
BR112014020359A2 (fr) 2017-06-20
CN104145087A (zh) 2014-11-12
FR2987086A1 (fr) 2013-08-23
EP2817491B1 (fr) 2016-07-20
EP2817491A1 (fr) 2014-12-31

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