PL4010562T3 - Łopatka wirnika do wirnika maszyny wirowej statku powietrznego, wirnik do maszyny wirowej statku powietrznego oraz maszyna wirowa statku powietrznego - Google Patents

Łopatka wirnika do wirnika maszyny wirowej statku powietrznego, wirnik do maszyny wirowej statku powietrznego oraz maszyna wirowa statku powietrznego

Info

Publication number
PL4010562T3
PL4010562T3 PL20756934.4T PL20756934T PL4010562T3 PL 4010562 T3 PL4010562 T3 PL 4010562T3 PL 20756934 T PL20756934 T PL 20756934T PL 4010562 T3 PL4010562 T3 PL 4010562T3
Authority
PL
Poland
Prior art keywords
rotor
aircraft turbomachine
turbomachine
aircraft
blade
Prior art date
Application number
PL20756934.4T
Other languages
English (en)
Inventor
Bertrand Guillaume Robin PELLATON
Lucas BENASSIS
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 PL4010562T3 publication Critical patent/PL4010562T3/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
    • 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
    • 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/10—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator 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
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • F01D11/127—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 a deformable or crushable structure, e.g. honeycomb
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
PL20756934.4T 2019-08-07 2020-07-29 Łopatka wirnika do wirnika maszyny wirowej statku powietrznego, wirnik do maszyny wirowej statku powietrznego oraz maszyna wirowa statku powietrznego PL4010562T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1909053A FR3099786B1 (fr) 2019-08-07 2019-08-07 Aube mobile pour une roue d’une turbomachine
PCT/FR2020/051397 WO2021023927A1 (fr) 2019-08-07 2020-07-29 Aube mobile pour une roue d'une turbomachine

Publications (1)

Publication Number Publication Date
PL4010562T3 true PL4010562T3 (pl) 2023-12-11

Family

ID=68807056

Family Applications (1)

Application Number Title Priority Date Filing Date
PL20756934.4T PL4010562T3 (pl) 2019-08-07 2020-07-29 Łopatka wirnika do wirnika maszyny wirowej statku powietrznego, wirnik do maszyny wirowej statku powietrznego oraz maszyna wirowa statku powietrznego

Country Status (6)

Country Link
US (1) US12116904B2 (pl)
EP (2) EP4010562B1 (pl)
CN (1) CN114207253A (pl)
FR (1) FR3099786B1 (pl)
PL (1) PL4010562T3 (pl)
WO (1) WO2021023927A1 (pl)

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4752185A (en) * 1987-08-03 1988-06-21 General Electric Company Non-contacting flowpath seal
GB0324843D0 (en) * 2003-10-24 2003-11-26 Alstom Switzerland Ltd Improvements in or relating to axial flow turbines
GB2413160B (en) * 2004-04-17 2006-08-09 Rolls Royce Plc Turbine rotor blades
FR2893268B1 (fr) * 2005-11-15 2008-02-08 Snecma Sa Procede de realisation d'un rebord situe a l'extremite libre d'une aube, aube obtenue par ce procede et turbomachine equipee de cette aube
WO2012052740A1 (en) * 2010-10-18 2012-04-26 University Of Durham Sealing device for reducing fluid leakage in turbine apparatus
FR3001759B1 (fr) * 2013-02-07 2015-01-16 Snecma Rouge aubagee de turbomachine
US9856739B2 (en) * 2013-09-18 2018-01-02 Honeywell International Inc. Turbine blades with tip portions having converging cooling holes
US10301945B2 (en) 2015-12-18 2019-05-28 General Electric Company Interior cooling configurations in turbine rotor blades
FR3067405B1 (fr) * 2017-06-13 2020-08-14 Safran Aircraft Engines Turbomachine et procede d'etancheite par soufflage d'air
US10704406B2 (en) 2017-06-13 2020-07-07 General Electric Company Turbomachine blade cooling structure and related methods
US11015453B2 (en) * 2017-11-22 2021-05-25 General Electric Company Engine component with non-diffusing section
EP3728796A1 (fr) * 2017-12-19 2020-10-28 Safran Helicopter Engines Roue de turbine
BE1025961B1 (fr) * 2018-01-30 2019-08-28 Safran Aero Boosters S.A. Passage annulaire entre une virole et une plateforme rotorique de turbomachine

Also Published As

Publication number Publication date
US20220316346A1 (en) 2022-10-06
FR3099786B1 (fr) 2021-07-30
WO2021023927A1 (fr) 2021-02-11
CN114207253A (zh) 2022-03-18
EP4234886A3 (fr) 2023-11-08
US12116904B2 (en) 2024-10-15
FR3099786A1 (fr) 2021-02-12
EP4234886A2 (fr) 2023-08-30
EP4010562B1 (fr) 2023-08-30
EP4010562A1 (fr) 2022-06-15

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