FR3093536B1 - Rotor pour une turbine contrarotative de turbomachine - Google Patents

Rotor pour une turbine contrarotative de turbomachine Download PDF

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Publication number
FR3093536B1
FR3093536B1 FR1902389A FR1902389A FR3093536B1 FR 3093536 B1 FR3093536 B1 FR 3093536B1 FR 1902389 A FR1902389 A FR 1902389A FR 1902389 A FR1902389 A FR 1902389A FR 3093536 B1 FR3093536 B1 FR 3093536B1
Authority
FR
France
Prior art keywords
wing
spoiler
rotor
wall
external
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.)
Expired - Fee Related
Application number
FR1902389A
Other languages
English (en)
Other versions
FR3093536A1 (fr
Inventor
Patrick Jean Laurent Sultana
Olivier Renon
Laurent Cédric Zamai
Clément Charles Jérémy Coiffier
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
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1902389A priority Critical patent/FR3093536B1/fr
Priority to EP20161551.5A priority patent/EP3705684B1/fr
Priority to US16/811,341 priority patent/US11454117B2/en
Priority to CN202010157104.9A priority patent/CN111663962A/zh
Publication of FR3093536A1 publication Critical patent/FR3093536A1/fr
Application granted granted Critical
Publication of FR3093536B1 publication Critical patent/FR3093536B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • F01D1/26—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like traversed by the working-fluid substantially axially
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/03—Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted rotors
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/10—Anti- vibration means
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • 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
    • 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
    • F05D2240/20—Rotors
    • F05D2240/24—Rotors for turbines
    • 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
    • F05D2250/40—Movement of components
    • F05D2250/44—Movement of components by counter rotation
    • 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/38—Retaining components in desired mutual position by a spring, i.e. spring loaded or biased towards a certain position

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)

Abstract

Rotor (4) pour une turbine contrarotative (1) comprenant un tambour (9) et un aubage (10) monté à l’intérieur, ledit tambour (9) comprenant un crochet (11) délimitant un logement (12) présentant une paroi externe et une paroi interne, ledit aubage (10) comprenant une pale (15) et une plateforme externe (16) pourvue d’un becquet (17) placé à l’intérieur dudit logement (12),caractérisé en ce que le rotor (4) comprend un clinquant (18) comprenant une aile interne élastique et une aile externe, ladite aile externe étant disposée radialement entre ledit becquet (17) et ladite paroi externe, ladite aile interne présentant un premier appui avec ladite paroi interne et un second appui avec ledit becquet (17), ladite aile interne étant disposée dans le logement (12) de sorte à exercer une contrainte sur ledit becquet (17) de manière à plaquer ledit becquet (17) contre ladite paroi externe via ladite aile externe. Figure pour l'abrégé : Figure 2
FR1902389A 2019-03-08 2019-03-08 Rotor pour une turbine contrarotative de turbomachine Expired - Fee Related FR3093536B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1902389A FR3093536B1 (fr) 2019-03-08 2019-03-08 Rotor pour une turbine contrarotative de turbomachine
EP20161551.5A EP3705684B1 (fr) 2019-03-08 2020-03-06 Rotor pour une turbine contrarotative de turbomachine
US16/811,341 US11454117B2 (en) 2019-03-08 2020-03-06 Rotor for a contrarotating turbine of a turbine engine
CN202010157104.9A CN111663962A (zh) 2019-03-08 2020-03-09 涡轮发动机的反向旋转式涡轮的转子

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1902389 2019-03-08
FR1902389A FR3093536B1 (fr) 2019-03-08 2019-03-08 Rotor pour une turbine contrarotative de turbomachine

Publications (2)

Publication Number Publication Date
FR3093536A1 FR3093536A1 (fr) 2020-09-11
FR3093536B1 true FR3093536B1 (fr) 2021-02-19

Family

ID=67185392

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1902389A Expired - Fee Related FR3093536B1 (fr) 2019-03-08 2019-03-08 Rotor pour une turbine contrarotative de turbomachine

Country Status (4)

Country Link
US (1) US11454117B2 (fr)
EP (1) EP3705684B1 (fr)
CN (1) CN111663962A (fr)
FR (1) FR3093536B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11274557B2 (en) * 2019-11-27 2022-03-15 General Electric Company Damper assemblies for rotating drum rotors of gas turbine engines

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4171930A (en) * 1977-12-28 1979-10-23 General Electric Company U-clip for boltless blade retainer
US4159624A (en) * 1978-02-06 1979-07-03 Gruner George P Contra-rotating rotors with differential gearing
FR2641573B1 (fr) * 1989-01-11 1991-03-15 Snecma Rotor de turbomachine muni d'un dispositif de fixation des aubes
US5131813A (en) * 1990-04-03 1992-07-21 General Electric Company Turbine blade outer end attachment structure
US5131814A (en) * 1990-04-03 1992-07-21 General Electric Company Turbine blade inner end attachment structure
US5307622A (en) 1993-08-02 1994-05-03 General Electric Company Counterrotating turbine support assembly
US5333995A (en) * 1993-08-09 1994-08-02 General Electric Company Wear shim for a turbine engine
US7048496B2 (en) * 2002-10-31 2006-05-23 General Electric Company Turbine cooling, purge, and sealing system
FR2866073B1 (fr) * 2004-02-11 2006-07-28 Snecma Moteurs Turboreacteur ayant deux soufflantes contrarotatives solidaires d'un compresseur a basse pression contrarotatif
JP5334990B2 (ja) * 2007-12-20 2013-11-06 ボルボ エアロ コーポレイション ガスタービンエンジン
FR2942273B1 (fr) 2009-02-18 2011-06-10 Snecma Moteur double flux a roues de turbine contrarotatives
JP5646517B2 (ja) * 2009-03-09 2014-12-24 スネクマ タービンリング組立体
FR2986836B1 (fr) * 2012-02-09 2016-01-01 Snecma Tole annulaire anti-usure pour une turbomachine
US9103213B2 (en) * 2012-02-29 2015-08-11 General Electric Company Scalloped surface turbine stage with purge trough
FR3003301B1 (fr) * 2013-03-14 2018-01-05 Safran Helicopter Engines Anneau de turbine pour turbomachine
US20170167438A1 (en) * 2015-12-11 2017-06-15 General Electric Company Gas Turbine Engine

Also Published As

Publication number Publication date
EP3705684B1 (fr) 2021-08-18
FR3093536A1 (fr) 2020-09-11
US11454117B2 (en) 2022-09-27
EP3705684A1 (fr) 2020-09-09
US20200284150A1 (en) 2020-09-10
CN111663962A (zh) 2020-09-15

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