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FR3069185B1 - Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles - Google Patents

Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles Download PDF

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Publication number
FR3069185B1
FR3069185B1 FR1756807A FR1756807A FR3069185B1 FR 3069185 B1 FR3069185 B1 FR 3069185B1 FR 1756807 A FR1756807 A FR 1756807A FR 1756807 A FR1756807 A FR 1756807A FR 3069185 B1 FR3069185 B1 FR 3069185B1
Authority
FR
France
Prior art keywords
hollow core
profile
composite material
material reinforced
unidirectional fiber
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
FR1756807A
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English (en)
Other versions
FR3069185A1 (fr
Inventor
Rodolphe Trouve
Jean-Claude Lacombe
Julien Rodes
Thomas Schutz
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.)
Airbus Operations SAS
Airbus SAS
Original Assignee
Airbus Operations SAS
Airbus 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 Airbus Operations SAS, Airbus SAS filed Critical Airbus Operations SAS
Priority to FR1756807A priority Critical patent/FR3069185B1/fr
Priority to US16/037,269 priority patent/US11124285B2/en
Publication of FR3069185A1 publication Critical patent/FR3069185A1/fr
Application granted granted Critical
Publication of FR3069185B1 publication Critical patent/FR3069185B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/185—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3085—Wings
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

L'invention porte sur un profil aérodynamique, comportant une peau (6) définissant la surface extérieure dudit profil aérodynamique, un bord d'attaque (1), un bord de fuite (3) et une portion centrale (2) représentant au moins 50% de la corde du profil. Le profil comporte un noyau creux (5) en matériau composite renforcé par un textile à fibres unidirectionnelles. Le noyau creux présente en section une forme oblongue arrondie, notamment à chacune de ses extrémités. La peau (6) prend appui sur le noyau creux (5) sur la longueur de la portion centrale (2) dudit profil aérodynamique, tant à l'intrados qu'à l'extrados dudit profil. Le renfort par un textile à fibres unidirectionnelles permet une orientation adéquate de fibres de renfort pour optimiser des propriétés mécaniques dans certaines directions. La forme allongée le long de la corde du profil et arrondie du noyau creux (5) lui confère une grande résistance à la déformation.
FR1756807A 2017-07-18 2017-07-18 Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles Active FR3069185B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1756807A FR3069185B1 (fr) 2017-07-18 2017-07-18 Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles
US16/037,269 US11124285B2 (en) 2017-07-18 2018-07-17 Aerodynamic/hydrodynamic profile with a composite reinforced oblong foam core

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1756807 2017-07-18
FR1756807A FR3069185B1 (fr) 2017-07-18 2017-07-18 Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles

Publications (2)

Publication Number Publication Date
FR3069185A1 FR3069185A1 (fr) 2019-01-25
FR3069185B1 true FR3069185B1 (fr) 2020-07-24

Family

ID=59859346

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1756807A Active FR3069185B1 (fr) 2017-07-18 2017-07-18 Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles

Country Status (2)

Country Link
US (1) US11124285B2 (fr)
FR (1) FR3069185B1 (fr)

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US20230078701A1 (en) * 2021-09-13 2023-03-16 Rohr, Inc. Composite structure and method for forming same

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Also Published As

Publication number Publication date
FR3069185A1 (fr) 2019-01-25
US20190023372A1 (en) 2019-01-24
US11124285B2 (en) 2021-09-21

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