PL4010565T3 - Pierścień do turbiny maszyny wirowej lub silnika turbinowego - Google Patents

Pierścień do turbiny maszyny wirowej lub silnika turbinowego

Info

Publication number
PL4010565T3
PL4010565T3 PL20760497.6T PL20760497T PL4010565T3 PL 4010565 T3 PL4010565 T3 PL 4010565T3 PL 20760497 T PL20760497 T PL 20760497T PL 4010565 T3 PL4010565 T3 PL 4010565T3
Authority
PL
Poland
Prior art keywords
turboengine
turbomachine
turbine
seal ring
seal
Prior art date
Application number
PL20760497.6T
Other languages
English (en)
Inventor
Bertrand Guillaume Robin PELLATON
Mathieu Laurent HERRAN
Yohan Smith
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 PL4010565T3 publication Critical patent/PL4010565T3/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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
    • 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
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • 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
    • 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
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition
    • 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
    • F05D2240/11—Shroud seal segments

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)
PL20760497.6T 2019-08-05 2020-08-04 Pierścień do turbiny maszyny wirowej lub silnika turbinowego PL4010565T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1908957A FR3099787B1 (fr) 2019-08-05 2019-08-05 Anneau pour une turbine de turbomachine ou de turbomoteur
PCT/FR2020/051433 WO2021023945A1 (fr) 2019-08-05 2020-08-04 Anneau pour une turbine de turbomachine ou de turbomoteur

Publications (1)

Publication Number Publication Date
PL4010565T3 true PL4010565T3 (pl) 2024-02-19

Family

ID=69375409

Family Applications (1)

Application Number Title Priority Date Filing Date
PL20760497.6T PL4010565T3 (pl) 2019-08-05 2020-08-04 Pierścień do turbiny maszyny wirowej lub silnika turbinowego

Country Status (6)

Country Link
US (1) US20220251963A1 (pl)
EP (1) EP4010565B1 (pl)
CN (1) CN114207254B (pl)
FR (1) FR3099787B1 (pl)
PL (1) PL4010565T3 (pl)
WO (1) WO2021023945A1 (pl)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12529316B2 (en) 2021-06-18 2026-01-20 Rtx Corporation Bonding method for repair of superalloy article
US12055056B2 (en) 2021-06-18 2024-08-06 Rtx Corporation Hybrid superalloy article and method of manufacture thereof
US12392252B2 (en) 2021-06-18 2025-08-19 Rtx Corporation Hybrid bonded configuration for blade outer air seal (BOAS)
US12037912B2 (en) 2021-06-18 2024-07-16 Rtx Corporation Advanced passive clearance control (APCC) control ring produced by field assisted sintering technology (FAST)

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2659950B2 (ja) * 1987-03-27 1997-09-30 株式会社東芝 ガスタービンシユラウド
US5456576A (en) * 1994-08-31 1995-10-10 United Technologies Corporation Dynamic control of tip clearance
GB9725623D0 (en) * 1997-12-03 2006-09-20 Rolls Royce Plc Improvements in or relating to a blade tip clearance system
US6116852A (en) * 1997-12-11 2000-09-12 Pratt & Whitney Canada Corp. Turbine passive thermal valve for improved tip clearance control
GB0228748D0 (en) * 2002-12-10 2003-01-15 Alstom Switzerland Ltd Sealing arrangement
FR2891300A1 (fr) * 2005-09-23 2007-03-30 Snecma Sa Dispositif de controle de jeu dans une turbine a gaz
GB0703827D0 (en) * 2007-02-28 2007-04-11 Rolls Royce Plc Rotor seal segment
DE102009016260A1 (de) * 2009-04-03 2010-10-07 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Verfahren beim Schweißen und Bauteil
US8753073B2 (en) * 2010-06-23 2014-06-17 General Electric Company Turbine shroud sealing apparatus
ES2705532T3 (es) * 2012-10-30 2019-03-25 MTU Aero Engines AG Anillo de turbina y turbomáquina
US10060288B2 (en) * 2015-10-09 2018-08-28 United Technologies Corporation Multi-flow cooling passage chamber for gas turbine engine
US10100654B2 (en) * 2015-11-24 2018-10-16 Rolls-Royce North American Technologies Inc. Impingement tubes for CMC seal segment cooling
FR3055146B1 (fr) * 2016-08-19 2020-05-29 Safran Aircraft Engines Ensemble d'anneau de turbine
US10480337B2 (en) * 2017-04-18 2019-11-19 Rolls-Royce North American Technologies Inc. Turbine shroud assembly with multi-piece seals

Also Published As

Publication number Publication date
CN114207254A (zh) 2022-03-18
US20220251963A1 (en) 2022-08-11
FR3099787A1 (fr) 2021-02-12
WO2021023945A1 (fr) 2021-02-11
EP4010565A1 (fr) 2022-06-15
EP4010565B1 (fr) 2023-10-18
FR3099787B1 (fr) 2021-09-17
CN114207254B (zh) 2024-09-27

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