FR3096400B1 - Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir - Google Patents

Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir Download PDF

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Publication number
FR3096400B1
FR3096400B1 FR1905301A FR1905301A FR3096400B1 FR 3096400 B1 FR3096400 B1 FR 3096400B1 FR 1905301 A FR1905301 A FR 1905301A FR 1905301 A FR1905301 A FR 1905301A FR 3096400 B1 FR3096400 B1 FR 3096400B1
Authority
FR
France
Prior art keywords
blade
leading edge
wing
integrated metal
obtaining
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
FR1905301A
Other languages
English (en)
Other versions
FR3096400A1 (fr
Inventor
Sébastien Serge Francis Congratel
Cano Célia Iglesias
Antoine Hubert Marie Jean Masson
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 FR1905301A priority Critical patent/FR3096400B1/fr
Priority to US16/879,171 priority patent/US11333028B2/en
Publication of FR3096400A1 publication Critical patent/FR3096400A1/fr
Application granted granted Critical
Publication of FR3096400B1 publication Critical patent/FR3096400B1/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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/12—Moulds or cores; Details thereof or accessories therefor with incorporated means for positioning inserts, e.g. labels
    • 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
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/324—Blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • 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
    • F05D2230/50—Building or constructing in particular ways
    • F05D2230/53—Building or constructing in particular ways by integrally manufacturing a component, e.g. by milling from a billet or one piece construction
    • 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
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/121—Fluid guiding means, e.g. vanes related to the leading edge of a stator vane
    • 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
    • F05D2240/303—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 leading 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
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
    • 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
    • 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
    • F05D2300/70—Treatment or modification of materials
    • F05D2300/702—Reinforcement

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir . L’invention concerne une aube (20) de turbomachine comprenant un aubage (21) en matériau composite à renfort fibreux densifié par une matrice et un bord d’attaque (21a) métallique intégré, l’aubage s’étendant suivant une direction longitudinale (L), le bord d’attaque (21a) étant formé par un clinquant métallique (30) surmoulé sur l’aubage, ledit clinquant (30) ayant une aile intrados (31) et une aile extrados (32) qui s’étendent respectivement sur les faces intrados (24) et extrados (25) de l’aubage en épousant un profil aérodynamique de l’aube. L’une parmi l’aile intrados (31) et l’aile extrados (32) présente une portion de positionnement (40) s’étendant suivant la direction longitudinale (L), ladite portion ayant une face interne (41) plane et une épaisseur croissante en s’éloignant du bord d’attaque (21a), et étant logée dans une rainure de forme correspondante dans l’aubage. L’invention vise aussi un procédé de fabrication d’une telle aube. Figure pour l’abrégé : Fig. 3.
FR1905301A 2019-05-21 2019-05-21 Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir Active FR3096400B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1905301A FR3096400B1 (fr) 2019-05-21 2019-05-21 Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir
US16/879,171 US11333028B2 (en) 2019-05-21 2020-05-20 Turbomachine vane with integrated metal leading edge and method for obtaining it

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1905301A FR3096400B1 (fr) 2019-05-21 2019-05-21 Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir
FR1905301 2019-05-21

Publications (2)

Publication Number Publication Date
FR3096400A1 FR3096400A1 (fr) 2020-11-27
FR3096400B1 true FR3096400B1 (fr) 2021-05-28

Family

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Family Applications (1)

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FR1905301A Active FR3096400B1 (fr) 2019-05-21 2019-05-21 Aube de turbomachine à bord d’attaque métallique intégré et procédé pour l’obtenir

Country Status (2)

Country Link
US (1) US11333028B2 (fr)
FR (1) FR3096400B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114952523B (zh) * 2021-02-26 2023-12-05 中国航发商用航空发动机有限责任公司 航空发动机的叶片的加工方法和加工装置
FR3121953A1 (fr) * 2021-04-20 2022-10-21 Safran Aircraft Engines Procede de fabrication d’une aube composite de turbomachine
FR3125999B1 (fr) * 2021-08-03 2023-12-01 Safran Pale dégivrante d’hélice ou de soufflante de turbomachine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110294941A1 (en) * 2010-05-26 2011-12-01 Shin-Etsu Chemical Co., Ltd. Vinyl chloride-based resin composition, method of producing vinyl chloride-based polymer composition, and vinyl chloride-based polymer composition obtained thereby
FR2978931B1 (fr) * 2011-08-10 2014-05-09 Snecma Procede de realisation d'un renfort de protection du bord d'attaque d'une pale
FR3008920B1 (fr) * 2013-07-29 2015-12-25 Safran Procede de fabrication d'une aube en materiau composite a bord d'attaque metallique integre pour moteur aeronautique a turbine a gaz
FR3010132A1 (fr) * 2013-09-04 2015-03-06 Safran Bord d'attaque metallique d'aube en materiau composite pour moteur a turbine a gaz
DE102014226700A1 (de) 2014-12-19 2016-06-23 Rolls-Royce Deutschland Ltd & Co Kg Kompressorschaufel einer Gasturbine
GB201702698D0 (en) * 2017-02-20 2017-04-05 Rolls Royce Plc Fan

Also Published As

Publication number Publication date
FR3096400A1 (fr) 2020-11-27
US11333028B2 (en) 2022-05-17
US20200370438A1 (en) 2020-11-26

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