ES2019134B3 - Pala de material compuesto, con nucleo estructural y revestimiento perfilado, y su procedimiento de fabricacion. - Google Patents

Pala de material compuesto, con nucleo estructural y revestimiento perfilado, y su procedimiento de fabricacion.

Info

Publication number
ES2019134B3
ES2019134B3 ES88401560T ES88401560T ES2019134B3 ES 2019134 B3 ES2019134 B3 ES 2019134B3 ES 88401560 T ES88401560 T ES 88401560T ES 88401560 T ES88401560 T ES 88401560T ES 2019134 B3 ES2019134 B3 ES 2019134B3
Authority
ES
Spain
Prior art keywords
shovel
composite material
manufacturing procedure
structural nucleus
profiled lining
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 - Lifetime
Application number
ES88401560T
Other languages
English (en)
Inventor
Balc'h Maurice Yves Marie Le
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 Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2019134B3 publication Critical patent/ES2019134B3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/473—Constructional features
    • B64C2027/4733—Rotor blades substantially made from particular materials
    • B64C2027/4736—Rotor blades substantially made from particular materials from composite materials
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/23—Sheet including cover or casing
    • Y10T428/233—Foamed or expanded material encased
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/23—Sheet including cover or casing
    • Y10T428/234—Sheet including cover or casing including elements cooperating to form cells
    • Y10T428/236—Honeycomb type cells extend perpendicularly to nonthickness layer
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24488—Differential nonuniformity at margin
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24496—Foamed or cellular component
    • Y10T428/24504—Component comprises a polymer [e.g., rubber, etc.]
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24496—Foamed or cellular component
    • Y10T428/24504—Component comprises a polymer [e.g., rubber, etc.]
    • Y10T428/24512—Polyurethane
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component
    • Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249981—Plural void-containing components
ES88401560T 1987-06-26 1988-06-21 Pala de material compuesto, con nucleo estructural y revestimiento perfilado, y su procedimiento de fabricacion. Expired - Lifetime ES2019134B3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8709078A FR2617119B1 (fr) 1987-06-26 1987-06-26 Pale en materiaux composites, a noyau structural et revetement d'habillage profile, et son procede de fabrication

Publications (1)

Publication Number Publication Date
ES2019134B3 true ES2019134B3 (es) 1991-06-01

Family

ID=9352586

Family Applications (1)

Application Number Title Priority Date Filing Date
ES88401560T Expired - Lifetime ES2019134B3 (es) 1987-06-26 1988-06-21 Pala de material compuesto, con nucleo estructural y revestimiento perfilado, y su procedimiento de fabricacion.

Country Status (7)

Country Link
US (1) US4935277A (es)
EP (1) EP0296964B1 (es)
JP (1) JPS6428097A (es)
CA (1) CA1316517C (es)
DE (1) DE3861266D1 (es)
ES (1) ES2019134B3 (es)
FR (1) FR2617119B1 (es)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5193736A (en) * 1991-03-01 1993-03-16 Interturbine Corporation Method for repairing turbine vanes
US5486096A (en) * 1994-06-30 1996-01-23 United Technologies Corporation Erosion resistant surface protection
US5720597A (en) * 1996-01-29 1998-02-24 General Electric Company Multi-component blade for a gas turbine
US5876651A (en) * 1996-05-29 1999-03-02 United Technologies Corporation Method for forming a composite structure
US6715992B2 (en) * 2001-04-04 2004-04-06 R & M Technology, Llc Helicopter blade and method of manufacture
US7059129B2 (en) * 2003-09-25 2006-06-13 Honeywell International, Inc. Variable geometry turbocharger
US7959412B2 (en) * 2006-09-29 2011-06-14 General Electric Company Wind turbine rotor blade with acoustic lining
FR2912990B1 (fr) * 2007-02-23 2009-04-24 Eurocopter France Pale de giravion pourvue d'un troncon radial et d'au moins un troncon en fleche avant et/ou arriere
GB2450139B (en) 2007-06-14 2010-05-05 Rolls Royce Plc An aerofoil for a gas turbine engine
GB0715303D0 (en) * 2007-08-08 2007-09-19 Airbus Uk Ltd Composite laminate structure
FR2926785B1 (fr) 2008-01-25 2010-02-19 Eurocopter France Pale de giravion munie d'un longeron integrant une attache de fixation,et procede de fabrication d'un tel longeron.
JP2011032988A (ja) * 2009-08-05 2011-02-17 Nitto Denko Corp 風力発電機ブレード用発泡充填材、風力発電機ブレード用発泡充填部品、風力発電機ブレード、風力発電機、および、風力発電機ブレードの製造方法
JP5308323B2 (ja) * 2009-12-22 2013-10-09 三菱重工業株式会社 風車翼及びそれを用いた風力発電装置
FR2964941B1 (fr) * 2010-09-16 2013-03-08 Eurocopter France Pale a vulnerabilite minimisee
WO2012064335A1 (en) * 2010-11-12 2012-05-18 Bell Helicopter Textron Inc. Composite rotor blade having weighted material for mass balancing
US8596570B1 (en) * 2011-02-22 2013-12-03 David Carambat Aircraft vehicle centrifugal fan apparatus
US10339228B2 (en) 2012-01-24 2019-07-02 Bell Helicopter Textron Inc. Aerodynamic analysis for quality assurance of manufactured parts
EP2660143B1 (en) * 2012-04-30 2021-07-07 Ratier-Figeac Propeller blade with lightweight insert and bulkheads
EP2669192B8 (en) * 2012-05-29 2017-03-01 Ratier-Figeac SAS Propeller blade
DE102012109226A1 (de) * 2012-09-28 2014-04-03 Rheinisch-Westfälische Technische Hochschule (Rwth) Aachen Vorrichtung zur Ableitung von Wärme
FR3000464B1 (fr) 2012-12-27 2016-01-15 Eads Europ Aeronautic Defence Dispositif d'absorption d'energie pour element de structure d'aeronef
FR3007737B1 (fr) 2013-06-26 2017-07-14 Eurocopter France Pale a rigidite en torsion reduite et rotor muni d'une telle pale
GB2523370B (en) * 2014-02-24 2016-08-10 Marine Current Turbines Ltd Blade manufacturing method
US9970303B2 (en) 2014-05-13 2018-05-15 Entrotech, Inc. Erosion protection sleeve
RU2616465C2 (ru) * 2015-04-16 2017-04-17 Борис Анатольевич Губарев Способ изготовления лопасти из композиционного материала
CN105252003B (zh) * 2015-11-09 2017-05-10 华中科技大学 一种飞机翼梁类零件的增材制造方法
BE1023299B1 (fr) * 2016-01-21 2017-01-26 Safran Aero Boosters S.A. Aube statorique
CN106672231A (zh) * 2016-10-19 2017-05-17 吴瑞霞 无人驾驶飞行器
NL2018263B1 (nl) * 2017-01-31 2018-08-16 Fibercore Ip Bv Aerodynamisch of hydrodynamisch blad uit gelaagd materiaal
FR3069185B1 (fr) 2017-07-18 2020-07-24 Airbus Operations Sas Profil aerodynamique a noyau creux oblong arrondi en materiau composite renforce par un textile a fibres unidirectionnelles
FR3070369B1 (fr) * 2017-08-30 2019-08-23 Airbus Operations Procede de fabrication d'un panneau d'un bord d'attaque d'aeronef permettant d'obtenir un ecoulement laminaire etendu, bord d'attaque comprenant au moins un panneau obtenu a partir dudit procede
JP6672233B2 (ja) * 2017-09-25 2020-03-25 三菱重工業株式会社 複合材翼の成形方法、複合材翼及び複合材翼の成形型
ES2936471T3 (es) * 2018-01-17 2023-03-17 Airbus Operations Slu Método para fabricar una estructura aeronáutica
CN111231369B (zh) * 2020-02-18 2022-11-01 中材科技风电叶片股份有限公司 防护壳体及其制备方法、风电叶片的制造方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3028292A (en) * 1957-05-27 1962-04-03 Parsons Corp Method of manufacturing plastic rotor blades
JPS5090098A (es) * 1973-12-14 1975-07-18
DE2558882C3 (de) * 1975-12-27 1979-10-11 Walter 5300 Bonn Schoenball Aufbau eines Rotors, insbesondere für Windkraftmaschinen
GB2032832B (en) * 1978-09-16 1982-07-28 Dowty Rotol Ltd Foam-containing structures
DE2944359A1 (de) * 1979-02-14 1980-08-21 Composite Tech Corp Verbundkoerper
DE3002584C2 (de) * 1980-01-25 1982-02-11 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zum Herstellen eines Formkörpers aus einem Grundkörper und einer Deckschicht
US4335174A (en) * 1980-09-04 1982-06-15 The Boeing Company Honeycomb structure end closure
US4664974A (en) * 1982-08-19 1987-05-12 Kent Sherwood Surface-reinforced foam article
FR2542695B1 (fr) * 1983-03-18 1985-07-26 Aerospatiale Helice multipale a pas variable a pale s en materiaux composites demontables individuellement, procede de fabrication de telles pales et pales ainsi realisees
US4753836A (en) * 1987-05-22 1988-06-28 Mizell James A Surfboard construction

Also Published As

Publication number Publication date
DE3861266D1 (de) 1991-01-24
FR2617119B1 (fr) 1989-12-01
EP0296964A1 (fr) 1988-12-28
JPS6428097A (en) 1989-01-30
CA1316517C (fr) 1993-04-20
FR2617119A1 (fr) 1988-12-30
US4935277A (en) 1990-06-19
EP0296964B1 (fr) 1990-12-12

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