PL3853445T3 - Uszczelnienie turbiny - Google Patents

Uszczelnienie turbiny

Info

Publication number
PL3853445T3
PL3853445T3 PL19791320.5T PL19791320T PL3853445T3 PL 3853445 T3 PL3853445 T3 PL 3853445T3 PL 19791320 T PL19791320 T PL 19791320T PL 3853445 T3 PL3853445 T3 PL 3853445T3
Authority
PL
Poland
Prior art keywords
turbine seal
turbine
seal
Prior art date
Application number
PL19791320.5T
Other languages
English (en)
Inventor
Frédéric Philippe Jean-Jacques PARDO
Original Assignee
Safran Helicopter Engines
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 Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL3853445T3 publication Critical patent/PL3853445T3/pl

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
PL19791320.5T 2018-09-20 2019-09-20 Uszczelnienie turbiny PL3853445T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1858527A FR3086324B1 (fr) 2018-09-20 2018-09-20 Etancheite d'une turbine
PCT/FR2019/052206 WO2020058648A1 (fr) 2018-09-20 2019-09-20 Etancheite d'une turbine

Publications (1)

Publication Number Publication Date
PL3853445T3 true PL3853445T3 (pl) 2024-08-05

Family

ID=64049423

Family Applications (1)

Application Number Title Priority Date Filing Date
PL19791320.5T PL3853445T3 (pl) 2018-09-20 2019-09-20 Uszczelnienie turbiny

Country Status (7)

Country Link
US (1) US11408298B2 (pl)
EP (1) EP3853445B1 (pl)
CN (1) CN112840105B (pl)
CA (1) CA3113137A1 (pl)
FR (1) FR3086324B1 (pl)
PL (1) PL3853445T3 (pl)
WO (1) WO2020058648A1 (pl)

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6916154B2 (en) * 2003-04-29 2005-07-12 Pratt & Whitney Canada Corp. Diametrically energized piston ring
JP5045304B2 (ja) * 2007-08-16 2012-10-10 株式会社Ｉｈｉ ターボチャージャ
FR2949810B1 (fr) * 2009-09-04 2013-06-28 Turbomeca Dispositif de support d'un anneau de turbine, turbine avec un tel dispositif et turbomoteur avec une telle turbine
US8596969B2 (en) * 2010-12-22 2013-12-03 United Technologies Corporation Axial retention feature for gas turbine engine vanes
FR2989724B1 (fr) * 2012-04-20 2015-12-25 Snecma Etage de turbine pour une turbomachine
US9797515B2 (en) * 2012-09-28 2017-10-24 United Technologies Corporation Radially coacting ring seal
EP3458220B1 (fr) * 2016-05-18 2020-07-29 Safran Aircraft Engines Procédé de fabrication d'une structure alvéolaire
ES2758187T3 (es) 2017-02-17 2020-05-04 MTU Aero Engines AG Disposición de sellado para una turbina de gas

Also Published As

Publication number Publication date
CN112840105B (zh) 2023-06-09
WO2020058648A1 (fr) 2020-03-26
CN112840105A (zh) 2021-05-25
FR3086324B1 (fr) 2020-11-06
EP3853445A1 (fr) 2021-07-28
US20210348518A1 (en) 2021-11-11
EP3853445B1 (fr) 2024-04-17
US11408298B2 (en) 2022-08-09
FR3086324A1 (fr) 2020-03-27
CA3113137A1 (fr) 2020-03-26

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