FR3090733B1 - Ensemble de turbomachine comprenant des aubes de soufflante à bord de fuite prolongé - Google Patents

Ensemble de turbomachine comprenant des aubes de soufflante à bord de fuite prolongé Download PDF

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Publication number
FR3090733B1
FR3090733B1 FR1873734A FR1873734A FR3090733B1 FR 3090733 B1 FR3090733 B1 FR 3090733B1 FR 1873734 A FR1873734 A FR 1873734A FR 1873734 A FR1873734 A FR 1873734A FR 3090733 B1 FR3090733 B1 FR 3090733B1
Authority
FR
France
Prior art keywords
trailing edge
fan
blade
assembly including
fan blades
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
FR1873734A
Other languages
English (en)
Other versions
FR3090733A1 (fr
Inventor
Paul Antoine Foresto
Vivien Mickaël Courtier
Stéphane Roger MAHIAS
William Henri Joseph Riera
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 FR1873734A priority Critical patent/FR3090733B1/fr
Priority to EP19848803.3A priority patent/EP3899207B1/fr
Priority to PCT/FR2019/053234 priority patent/WO2020128384A1/fr
Priority to CN201980091919.7A priority patent/CN113423921B/zh
Priority to US17/416,897 priority patent/US11473430B2/en
Publication of FR3090733A1 publication Critical patent/FR3090733A1/fr
Application granted granted Critical
Publication of FR3090733B1 publication Critical patent/FR3090733B1/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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan 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
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • 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
    • F05D2300/603—Composites; e.g. fibre-reinforced

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L’invention concerne un ensemble (1) d’une turbomachine comprenant une soufflante (2) et une pièce (3) du type tambour de booster, la soufflante (2) comprenant : des aubes (20) comportant une pale (23) et un prolongateur (30) rapporté et fixé sur le bord de fuite (25) de la pale (23), un disque (10) de soufflante (2) et une série de plateformes (16) inter-aubes, le prolongateur (30) de chaque aube (20) s’étendant au-delà de la face aval (14) du disque (10) de soufflante (2) en direction du bord amont (4) de la pièce (3) et recouvrant au moins partiellement la cavité (6) entre la soufflante (2) et la pièce (3). Figure pour l’abrégé : Fig. 3
FR1873734A 2018-12-21 2018-12-21 Ensemble de turbomachine comprenant des aubes de soufflante à bord de fuite prolongé Active FR3090733B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1873734A FR3090733B1 (fr) 2018-12-21 2018-12-21 Ensemble de turbomachine comprenant des aubes de soufflante à bord de fuite prolongé
EP19848803.3A EP3899207B1 (fr) 2018-12-21 2019-12-20 Ensemble de turbomachine comprenant des aubes de soufflante à bord de fuite prolongé
PCT/FR2019/053234 WO2020128384A1 (fr) 2018-12-21 2019-12-20 Ensemble de turbomachine comprenant des aubes de soufflante à bord de fuite prolongé
CN201980091919.7A CN113423921B (zh) 2018-12-21 2019-12-20 包括具有延伸的后缘的风扇叶片的涡轮机组件
US17/416,897 US11473430B2 (en) 2018-12-21 2019-12-20 Turbomachine assembly comprising fan blades with an extended trailing edge

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1873734A FR3090733B1 (fr) 2018-12-21 2018-12-21 Ensemble de turbomachine comprenant des aubes de soufflante à bord de fuite prolongé

Publications (2)

Publication Number Publication Date
FR3090733A1 FR3090733A1 (fr) 2020-06-26
FR3090733B1 true FR3090733B1 (fr) 2020-12-04

Family

ID=68281472

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1873734A Active FR3090733B1 (fr) 2018-12-21 2018-12-21 Ensemble de turbomachine comprenant des aubes de soufflante à bord de fuite prolongé

Country Status (5)

Country Link
US (1) US11473430B2 (fr)
EP (1) EP3899207B1 (fr)
CN (1) CN113423921B (fr)
FR (1) FR3090733B1 (fr)
WO (1) WO2020128384A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12435636B1 (en) 2024-05-23 2025-10-07 General Electric Company Composite airfoil for a turbine engine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7144221B2 (en) * 2004-07-30 2006-12-05 General Electric Company Method and apparatus for assembling gas turbine engines
US8016561B2 (en) * 2006-07-11 2011-09-13 General Electric Company Gas turbine engine fan assembly and method for assembling to same
JP5370046B2 (ja) * 2009-09-25 2013-12-18 株式会社Ｉｈｉ 航空機エンジン用ファン
US9121294B2 (en) * 2011-12-20 2015-09-01 General Electric Company Fan blade with composite core and wavy wall trailing edge cladding
US9399922B2 (en) * 2012-12-31 2016-07-26 General Electric Company Non-integral fan blade platform
EP2964895A4 (fr) * 2013-03-07 2016-12-28 United Technologies Corp Pale de soufflante hybride pour moteurs à réaction
GB201408824D0 (en) * 2014-05-19 2014-07-02 Rolls Royce Plc Fan disc
US10099434B2 (en) * 2014-09-16 2018-10-16 General Electric Company Composite airfoil structures
US9745851B2 (en) * 2015-01-15 2017-08-29 General Electric Company Metal leading edge on composite blade airfoil and shank
FR3038653B1 (fr) * 2015-07-08 2017-08-04 Snecma Assemblage d'une plateforme rapportee d'aube de soufflante sur un disque de soufflante
US10730112B2 (en) * 2016-08-02 2020-08-04 Raytheon Technologies Corporation Micro lattice hybrid composite fan blade
EP3409892B1 (fr) * 2017-05-31 2020-07-15 Ansaldo Energia Switzerland AG Pale de turbine à gaz comprenant des ailettes pour compenser des forces centrifugales

Also Published As

Publication number Publication date
CN113423921A (zh) 2021-09-21
WO2020128384A1 (fr) 2020-06-25
US20220056803A1 (en) 2022-02-24
FR3090733A1 (fr) 2020-06-26
US11473430B2 (en) 2022-10-18
EP3899207A1 (fr) 2021-10-27
EP3899207B1 (fr) 2022-07-27
CN113423921B (zh) 2023-03-24

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