FR3065483B1 - Dispositif d'etancheite entre rotor et stator de turbomachine - Google Patents

Dispositif d'etancheite entre rotor et stator de turbomachine Download PDF

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Publication number
FR3065483B1
FR3065483B1 FR1753535A FR1753535A FR3065483B1 FR 3065483 B1 FR3065483 B1 FR 3065483B1 FR 1753535 A FR1753535 A FR 1753535A FR 1753535 A FR1753535 A FR 1753535A FR 3065483 B1 FR3065483 B1 FR 3065483B1
Authority
FR
France
Prior art keywords
sealing device
upstream
rotor
turbomachine stator
wipers
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
FR1753535A
Other languages
English (en)
Other versions
FR3065483A1 (fr
Inventor
Baptiste Marie Aubin Pierre Jouy
Josselin Luc Florent Sicard
Mathieu Charles Jean Verdiere
Loic Fabien Francois Villard
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
Safran Aircraft Engines 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 FR1753535A priority Critical patent/FR3065483B1/fr
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to JP2020508084A priority patent/JP7175963B2/ja
Priority to EP18725281.2A priority patent/EP3615774B1/fr
Priority to US16/608,103 priority patent/US11441442B2/en
Priority to CN201880026978.1A priority patent/CN110546349B/zh
Priority to PCT/FR2018/051022 priority patent/WO2018197800A1/fr
Priority to CA3060182A priority patent/CA3060182A1/fr
Priority to BR112019022128-0A priority patent/BR112019022128B1/pt
Priority to RU2019133382A priority patent/RU2762016C2/ru
Publication of FR3065483A1 publication Critical patent/FR3065483A1/fr
Application granted granted Critical
Publication of FR3065483B1 publication Critical patent/FR3065483B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • 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
    • F05D2240/55—Seals
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/28—Three-dimensional patterned
    • F05D2250/283—Three-dimensional patterned honeycomb
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611—Coating

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)

Abstract

Est concerné un dispositif d'étanchéité entre une partie de rotor et une partie de stator, comprenant au moins un revêtement (46) abradable coopérant avec au moins deux léchettes amont et aval. Axialement en amont des léchettes, le dispositif d'étanchéité comprend une paroi (54) circonférentielle qui s'étend radialement, jusqu'au-delà de la surface axiale libre d'étanchéité amont (48a) du revêtement (46), pour créer, en extrémité libre de la léchette amont, un décollement du gaz en circulation.
FR1753535A 2017-04-24 2017-04-24 Dispositif d'etancheite entre rotor et stator de turbomachine Active FR3065483B1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR1753535A FR3065483B1 (fr) 2017-04-24 2017-04-24 Dispositif d'etancheite entre rotor et stator de turbomachine
EP18725281.2A EP3615774B1 (fr) 2017-04-24 2018-04-24 Dispositif d'étanchéité entre rotor et stator de turbomachine
US16/608,103 US11441442B2 (en) 2017-04-24 2018-04-24 Device for sealing between a rotor and a stator of a turbine engine
CN201880026978.1A CN110546349B (zh) 2017-04-24 2018-04-24 用于在涡轮发动机的转子和定子之间密封的装置
JP2020508084A JP7175963B2 (ja) 2017-04-24 2018-04-24 タービンエンジンのロータとステータとの間のシール装置
PCT/FR2018/051022 WO2018197800A1 (fr) 2017-04-24 2018-04-24 Dispositif d'étanchéité entre rotor et stator de turbomachine
CA3060182A CA3060182A1 (fr) 2017-04-24 2018-04-24 Dispositif d'etancheite entre rotor et stator de turbomachine
BR112019022128-0A BR112019022128B1 (pt) 2017-04-24 2018-04-24 Dispositivo de vedação e turbomáquina a gás
RU2019133382A RU2762016C2 (ru) 2017-04-24 2018-04-24 Уплотнительное устройство между ротором и статором газотурбинного двигателя

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1753535A FR3065483B1 (fr) 2017-04-24 2017-04-24 Dispositif d'etancheite entre rotor et stator de turbomachine
FR1753535 2017-04-24

Publications (2)

Publication Number Publication Date
FR3065483A1 FR3065483A1 (fr) 2018-10-26
FR3065483B1 true FR3065483B1 (fr) 2020-08-07

Family

ID=59297045

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1753535A Active FR3065483B1 (fr) 2017-04-24 2017-04-24 Dispositif d'etancheite entre rotor et stator de turbomachine

Country Status (8)

Country Link
US (1) US11441442B2 (fr)
EP (1) EP3615774B1 (fr)
JP (1) JP7175963B2 (fr)
CN (1) CN110546349B (fr)
CA (1) CA3060182A1 (fr)
FR (1) FR3065483B1 (fr)
RU (1) RU2762016C2 (fr)
WO (1) WO2018197800A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2021162084A (ja) * 2020-03-31 2021-10-11 川崎重工業株式会社 ラビリンスシール及びガスタービン
CN112065511B (zh) * 2020-08-31 2021-10-26 南京航空航天大学 引射式蜂窝衬套-篦齿封严结构

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4351532A (en) * 1975-10-01 1982-09-28 United Technologies Corporation Labyrinth seal
US5639095A (en) * 1988-01-04 1997-06-17 Twentieth Technology Low-leakage and low-instability labyrinth seal
FR2635562B1 (fr) * 1988-08-18 1993-12-24 Snecma Anneau de stator de turbine associe a un support de liaison au carter de turbine
US5218816A (en) * 1992-01-28 1993-06-15 General Electric Company Seal exit flow discourager
WO2005061854A1 (fr) * 2003-12-17 2005-07-07 Watson Cogeneration Company Lisses de coiffe d'extremite de turbine a gaz
US7281894B2 (en) * 2005-09-09 2007-10-16 General Electric Company Turbine airfoil curved squealer tip with tip shelf
US7686568B2 (en) * 2006-09-22 2010-03-30 General Electric Company Methods and apparatus for fabricating turbine engines
US8167547B2 (en) 2007-03-05 2012-05-01 United Technologies Corporation Gas turbine engine with canted pocket and canted knife edge seal
JP2009047043A (ja) * 2007-08-17 2009-03-05 Mitsubishi Heavy Ind Ltd 軸流タービン
DE102009042857A1 (de) * 2009-09-24 2011-03-31 Rolls-Royce Deutschland Ltd & Co Kg Gasturbine mit Deckband-Labyrinthdichtung
EP2390466B1 (fr) 2010-05-27 2018-04-25 Ansaldo Energia IP UK Limited Ensemble refroidissement d'une turbine à gaz
US8628092B2 (en) * 2010-11-30 2014-01-14 General Electric Company Method and apparatus for packing rings
US8807927B2 (en) * 2011-09-29 2014-08-19 General Electric Company Clearance flow control assembly having rail member
JP5374563B2 (ja) * 2011-10-03 2013-12-25 三菱重工業株式会社 軸流タービン
US9080459B2 (en) * 2012-01-03 2015-07-14 General Electric Company Forward step honeycomb seal for turbine shroud
FR2985759B1 (fr) 2012-01-17 2014-03-07 Snecma Aube mobile de turbomachine
US9151174B2 (en) * 2012-03-09 2015-10-06 General Electric Company Sealing assembly for use in a rotary machine and methods for assembling a rotary machine
US9291061B2 (en) * 2012-04-13 2016-03-22 General Electric Company Turbomachine blade tip shroud with parallel casing configuration
RU2509896C1 (ru) * 2012-08-01 2014-03-20 Общество с ограниченной ответственностью "Научно-производственное предприятие Вакууммаш" Надбандажное лабиринтное уплотнение для паровой турбины
EP2759676A1 (fr) * 2013-01-28 2014-07-30 Siemens Aktiengesellschaft Agencement de turbine présentant un meilleur effet d'étanchéité au niveau d'un joint étanche
FR3022944B1 (fr) * 2014-06-26 2020-02-14 Safran Aircraft Engines Ensemble rotatif pour turbomachine
CN105757257B (zh) * 2016-05-06 2018-04-17 亿昇(天津)科技有限公司 一种主动式迷宫密封结构

Also Published As

Publication number Publication date
CA3060182A1 (fr) 2018-11-01
JP2020517860A (ja) 2020-06-18
BR112019022128A2 (pt) 2020-05-12
FR3065483A1 (fr) 2018-10-26
CN110546349B (zh) 2022-08-30
EP3615774B1 (fr) 2022-12-28
US11441442B2 (en) 2022-09-13
RU2762016C2 (ru) 2021-12-14
RU2019133382A3 (fr) 2021-11-16
WO2018197800A1 (fr) 2018-11-01
US20200095882A1 (en) 2020-03-26
RU2019133382A (ru) 2021-05-25
EP3615774A1 (fr) 2020-03-04
CN110546349A (zh) 2019-12-06
JP7175963B2 (ja) 2022-11-21

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