FR2983261B1 - Aube de redressement de flux d'air pour moteur d'aeronef et structure de redressement de flux associee - Google Patents

Aube de redressement de flux d'air pour moteur d'aeronef et structure de redressement de flux associee

Info

Publication number
FR2983261B1
FR2983261B1 FR1103588A FR1103588A FR2983261B1 FR 2983261 B1 FR2983261 B1 FR 2983261B1 FR 1103588 A FR1103588 A FR 1103588A FR 1103588 A FR1103588 A FR 1103588A FR 2983261 B1 FR2983261 B1 FR 2983261B1
Authority
FR
France
Prior art keywords
draft
aircraft engine
relief structure
structure therefor
air flow
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
FR1103588A
Other languages
English (en)
Other versions
FR2983261A1 (fr
Inventor
Arnaud Oudin
Bertrand Desjoyeaux
Nicolas Dezeustre
Olivier Kerbler
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 Nacelles SAS
Original Assignee
Aircelle SA
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
Priority to FR1103588A priority Critical patent/FR2983261B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to RU2014124910/06A priority patent/RU2014124910A/ru
Priority to BR112014012131A priority patent/BR112014012131A2/pt
Priority to EP12795536.7A priority patent/EP2783079A1/fr
Priority to CA2856232A priority patent/CA2856232A1/fr
Priority to PCT/FR2012/052615 priority patent/WO2013093258A1/fr
Priority to CN201280057641.XA priority patent/CN103987924A/zh
Publication of FR2983261A1 publication Critical patent/FR2983261A1/fr
Priority to US14/286,666 priority patent/US9915157B2/en
Application granted granted Critical
Publication of FR2983261B1 publication Critical patent/FR2983261B1/fr
Active 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • F04D29/40—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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2225/00—Synthetic polymers, e.g. plastics; Rubber
    • F05C2225/08—Thermoplastics
    • 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
    • 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
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • 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
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • F05D2300/436—Polyetherketones, e.g. PEEK
    • 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
    • F05D2300/40—Organic materials
    • F05D2300/44—Resins
    • 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
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • F05D2300/6034—Orientation of fibres, weaving, ply angle
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
FR1103588A 2011-11-24 2011-11-24 Aube de redressement de flux d'air pour moteur d'aeronef et structure de redressement de flux associee Active FR2983261B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1103588A FR2983261B1 (fr) 2011-11-24 2011-11-24 Aube de redressement de flux d'air pour moteur d'aeronef et structure de redressement de flux associee
BR112014012131A BR112014012131A2 (pt) 2011-11-24 2012-11-13 palheta de passagem de fluxo de ar de motor de aeronave e estrutura de passagem do fluxo associada
EP12795536.7A EP2783079A1 (fr) 2011-11-24 2012-11-13 Aube de redressement de flux d'air pour moteur d'aéronef et structure de redressement de flux associée
CA2856232A CA2856232A1 (fr) 2011-11-24 2012-11-13 Aube de redressement de flux d'air pour moteur d'aeronef, et structure de redressement de flux associee
RU2014124910/06A RU2014124910A (ru) 2011-11-24 2012-11-13 Спрямляющая поток воздуха лопатка двигателя летательного аппарата и соответствующая спрямляющая поток конструкция
PCT/FR2012/052615 WO2013093258A1 (fr) 2011-11-24 2012-11-13 Aube de redressement de flux d'air pour moteur d'aéronef et structure de redressement de flux associée
CN201280057641.XA CN103987924A (zh) 2011-11-24 2012-11-13 飞机发动机气流矫直叶片以及相关气流矫直结构
US14/286,666 US9915157B2 (en) 2011-11-24 2014-05-23 Aircraft engine air flow straightening vane and associated flow straightening structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1103588A FR2983261B1 (fr) 2011-11-24 2011-11-24 Aube de redressement de flux d'air pour moteur d'aeronef et structure de redressement de flux associee

Publications (2)

Publication Number Publication Date
FR2983261A1 FR2983261A1 (fr) 2013-05-31
FR2983261B1 true FR2983261B1 (fr) 2014-11-28

Family

ID=47291130

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1103588A Active FR2983261B1 (fr) 2011-11-24 2011-11-24 Aube de redressement de flux d'air pour moteur d'aeronef et structure de redressement de flux associee

Country Status (8)

Country Link
US (1) US9915157B2 (fr)
EP (1) EP2783079A1 (fr)
CN (1) CN103987924A (fr)
BR (1) BR112014012131A2 (fr)
CA (1) CA2856232A1 (fr)
FR (1) FR2983261B1 (fr)
RU (1) RU2014124910A (fr)
WO (1) WO2013093258A1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3017650B1 (fr) * 2014-02-14 2019-06-28 Safran Aube de redresseur pour moteur a turbine a gaz a structure hybride
FR3023329B1 (fr) * 2014-07-03 2019-08-02 Safran Aircraft Engines Stator ondule pour diminuer le bruit cree par l'interaction avec un rotor
US10352273B2 (en) 2016-11-08 2019-07-16 Rohr, Inc. Track beam with composite lug
US10724387B2 (en) * 2018-11-08 2020-07-28 Raytheon Technologies Corporation Continuation of a shear tube through a vane platform for structural support
CN112814948A (zh) * 2020-12-31 2021-05-18 西安汇腾航空科技有限公司 一种航空发动机导流片及其制造方法
US12065003B2 (en) 2021-03-29 2024-08-20 The Goodyear Tire & Rubber Company Shear band construction
GB2606557B (en) * 2021-05-13 2024-07-24 Dyson Technology Ltd A compressor
GB2606558B (en) * 2021-05-13 2024-02-28 Dyson Technology Ltd A compressor

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1987001743A1 (fr) * 1984-03-13 1987-03-26 Shikishima Canvas Kabushiki Kaisha Structure de fibres de renforcement de materiaux de construction
FR2625528B1 (fr) * 1987-12-31 1993-06-04 Plastiremo Aube monobloc composite fibre-resine pour turbomachine et procede pour sa fabrication
JP4060981B2 (ja) * 1998-04-08 2008-03-12 本田技研工業株式会社 ガスタービンの静翼構造体及びそのユニット
FR2817906B1 (fr) * 2000-12-12 2003-03-28 Snecma Moteurs Volet redresseur de turbomachine et son procede de realisation
GB2402717B (en) * 2003-06-10 2006-05-10 Rolls Royce Plc A vane assembly for a gas turbine engine
GB0424481D0 (en) * 2004-11-05 2004-12-08 Rolls Royce Plc Composite aerofoil
AT503840B1 (de) * 2006-06-30 2010-09-15 Facc Ag Leitschaufelanordnung für ein triebwerk
US20080072569A1 (en) * 2006-09-27 2008-03-27 Thomas Ory Moniz Guide vane and method of fabricating the same
GB2458685B (en) * 2008-03-28 2010-05-12 Rolls Royce Plc An article formed from a composite material
US8419374B2 (en) * 2009-08-14 2013-04-16 Hamilton Sundstrand Corporation Gas turbine engine composite blade
US8499450B2 (en) * 2010-01-26 2013-08-06 United Technologies Corporation Three-dimensionally woven composite blade with spanwise weft yarns
FR2956876B1 (fr) * 2010-02-26 2012-10-19 Snecma Module structural et aerodynamique d'un carter de turbomachine et structure de carter comportant une pluralite d'un tel module

Also Published As

Publication number Publication date
EP2783079A1 (fr) 2014-10-01
BR112014012131A2 (pt) 2017-05-30
CA2856232A1 (fr) 2013-06-27
CN103987924A (zh) 2014-08-13
WO2013093258A1 (fr) 2013-06-27
US9915157B2 (en) 2018-03-13
US20140255178A1 (en) 2014-09-11
FR2983261A1 (fr) 2013-05-31
RU2014124910A (ru) 2015-12-27

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