FR2252916A1 - - Google Patents

Info

Publication number
FR2252916A1
FR2252916A1 FR7342730A FR7342730A FR2252916A1 FR 2252916 A1 FR2252916 A1 FR 2252916A1 FR 7342730 A FR7342730 A FR 7342730A FR 7342730 A FR7342730 A FR 7342730A FR 2252916 A1 FR2252916 A1 FR 2252916A1
Authority
FR
France
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.)
Granted
Application number
FR7342730A
Other versions
FR2252916B1 (fr
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
Priority to FR7342730A priority Critical patent/FR2252916B1/fr
Priority to DE2451860A priority patent/DE2451860C3/de
Priority to GB51213/74A priority patent/GB1484179A/en
Priority to US05/527,291 priority patent/US3950115A/en
Publication of FR2252916A1 publication Critical patent/FR2252916A1/fr
Application granted granted Critical
Publication of FR2252916B1 publication Critical patent/FR2252916B1/fr
Expired legal-status Critical Current

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
    • B29D99/0028—Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
    • 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
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/083—Combinations of continuous fibres or fibrous profiled structures oriented in one direction and reinforcements forming a two dimensional structure, e.g. mats
    • 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
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/347—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation combined with compressing after the winding of lay-ups having a non-circular cross-section, e.g. flat spiral windings
    • 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
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • 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
    • B29D24/00—Producing articles with hollow walls
    • B29D24/002—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005—Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled the structure having joined ribs, e.g. honeycomb
    • 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
    • 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
    • B29L2031/082—Blades, e.g. for helicopters
    • 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
    • B29L2031/3047—Steering wheels
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24149—Honeycomb-like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Mechanical Operated Clutches (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7342730A 1973-11-30 1973-11-30 Expired FR2252916B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7342730A FR2252916B1 (fr) 1973-11-30 1973-11-30
DE2451860A DE2451860C3 (de) 1973-11-30 1974-10-31 Rotorblatt für Drehflügelflugzeuge
GB51213/74A GB1484179A (en) 1973-11-30 1974-11-26 Helicopter rotor blade
US05/527,291 US3950115A (en) 1973-11-30 1974-11-26 Plastics rotor blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7342730A FR2252916B1 (fr) 1973-11-30 1973-11-30

Publications (2)

Publication Number Publication Date
FR2252916A1 true FR2252916A1 (fr) 1975-06-27
FR2252916B1 FR2252916B1 (fr) 1978-02-24

Family

ID=9128528

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7342730A Expired FR2252916B1 (fr) 1973-11-30 1973-11-30

Country Status (4)

Country Link
US (1) US3950115A (fr)
DE (1) DE2451860C3 (fr)
FR (1) FR2252916B1 (fr)
GB (1) GB1484179A (fr)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2390331A1 (fr) * 1977-05-13 1978-12-08 Messerschmitt Boelkow Blohm Jonction principale de voilure portante pour aeronefs et vehicules spatiaux
FR2429148A1 (fr) * 1978-06-19 1980-01-18 Messerschmitt Boelkow Blohm Dispositif d'absorption de forces longitudinales ou de flexion dans un objet en matiere plastique renforcee de fibres, notamment en forme de pale de rotor
FR2660619A1 (fr) * 1990-04-06 1991-10-11 Agusta Spa Pale d'helicoptere.
FR2664629A1 (fr) * 1990-07-13 1992-01-17 Samsung Heavy Ind Bras plongeur pour excavatrice en materiaux composites polymeres de resistance elevee et procede pour sa fabrication.
FR2740379A1 (fr) * 1995-10-30 1997-04-30 Eurocopter France Procede de fabrication d'une pale en materiau composite pour rotor d'helicoptere, et pale pouvant etre obtenue par un tel procede
US6035531A (en) * 1995-10-30 2000-03-14 Eurocopter France Method for manufacturing a variable-pitch composite blade for a helicopter rotor
US6056838A (en) * 1995-10-30 2000-05-02 Eurocopter Method for manufacturing a variable-pitch composite blade for a helicopter rotor
EP1961658A1 (fr) * 2007-02-23 2008-08-27 Eurocopter Pale de giravion pourvue d' un tronçon radial et d ' au moins un tronçon en fléche avant et/ou arrière
EP3090866A1 (fr) * 2015-05-07 2016-11-09 Airbus Operations Limited Structures composites
EP3501979A1 (fr) * 2017-12-22 2019-06-26 Airbus Helicopters Enveloppes aerodynamiques epaisses pour cols de pales et carenages de manchons de pales d'un rotor d'un aeronef
FR3120249A1 (fr) * 2021-03-01 2022-09-02 Safran Aircraft Engines Aube comprenant une structure en matériau composite et procédé de fabrication associé

Families Citing this family (55)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4012169A (en) * 1973-05-10 1977-03-15 Societe Nationale Industrielle Aerospatiale Rotor for rotating wing type aircraft
US4083656A (en) * 1975-03-21 1978-04-11 Textron, Inc. Composite rotor blade
DE2641114C3 (de) * 1976-09-13 1981-05-14 Metallgesellschaft Ag, 6000 Frankfurt Verfahren zur Herstellung eines Kunststoff-Elektrofilters in Wabenform
DE2657832C3 (de) * 1976-12-21 1981-07-09 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schäkel für die Flügelaufhängung im Rumpf eines Luft- oder Raumfahrzeuges
FR2381662A1 (fr) * 1977-02-28 1978-09-22 Aerospatiale Pale, notamment pour un rotor d'helicoptere, et son procede de fabrication
US4264278A (en) * 1977-10-31 1981-04-28 Oscar Weingart Blade or spar
US4304376A (en) * 1977-12-05 1981-12-08 The Boeing Company Composite honeycomb core structures and single stage hot bonding method of producing such structures
US4251309A (en) * 1978-10-05 1981-02-17 The United States Of America As Represented By The Secretary Of The Army Method of making rotor blade root end attachment
US4284443A (en) * 1979-02-05 1981-08-18 The Boeing Company Single stage hot bonding method for producing composite honeycomb core structures
US4247255A (en) * 1979-03-15 1981-01-27 The Boeing Company Composite rotor blade root end
US4452658A (en) * 1979-04-03 1984-06-05 Schramm Burford J Method for making a helicopter rotor blade
US4316700A (en) * 1979-04-03 1982-02-23 Schramm Burford J Unitary, bonded-together helicopter rotorblade
US4409050A (en) * 1979-05-10 1983-10-11 Carter Wind Power Method of making blade supports
US4366387A (en) * 1979-05-10 1982-12-28 Carter Wind Power Wind-driven generator apparatus and method of making blade supports _therefor
US4304694A (en) * 1979-12-03 1981-12-08 United Technologies Corporation High damping epoxy resin composite
DE3006088A1 (de) * 1980-02-19 1981-08-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor eines drehfluegelflugzeugs
DE3032443C2 (de) * 1980-08-28 1982-08-12 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Bauelement mit einem Anschlußbereich mit versetzt angeordneten Bolzenaugen
DE3103710C2 (de) * 1981-02-04 1983-03-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "Rotor in Schalenbauweise"
US4395450A (en) * 1981-09-30 1983-07-26 The Boeing Company Composite structural skin spar joint and method of making
JPS58501582A (ja) * 1981-09-30 1983-09-22 ザ　ボ−イング　コンパニ− 複合構造物における外板と桁部材とを接続する為の継ぎ手
US4466774A (en) * 1982-08-30 1984-08-21 United Technologies Corporation Composite flexbeam joint
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
SE446847B (sv) * 1984-02-14 1986-10-13 Harald Unden Laminerad konstruktionsdel
US4693435A (en) * 1984-09-10 1987-09-15 United Technologies Corporation High speed aircraft control surface
FR2574752B1 (fr) * 1984-12-19 1987-02-20 Aerospatiale Pale pour rotor d'helicoptere en materiau composite multilongeron a caissons de torsion et son procede de fabrication
US4860610A (en) * 1984-12-21 1989-08-29 E. I. Du Pont De Nemours And Company Wound rotor element and centrifuge fabricated therefrom
US4675001A (en) * 1985-07-23 1987-06-23 E. I. Du Pont De Nemours And Company Centrifuge rotor
DE3528134A1 (de) * 1985-08-06 1987-02-12 Messerschmitt Boelkow Blohm Gabelfoermiger hebel an einem bauteil aus faserverstaerktem kunststoff
DE3929719A1 (de) * 1989-09-07 1991-03-14 Berthold Dipl Ing Karrais Propeller fuer verkehrsmittel, insbesondere flugzeuge
US5074753A (en) * 1989-10-16 1991-12-24 Bell Helicopter Textron Inc. Rotor blade
US5314309A (en) * 1990-05-25 1994-05-24 Anthony Blakeley Turbine blade with metallic attachment and method of making the same
US5118257A (en) * 1990-05-25 1992-06-02 Sundstrand Corporation Boot attachment for composite turbine blade, turbine blade and method of making turbine blade
US5340280A (en) * 1991-09-30 1994-08-23 General Electric Company Dovetail attachment for composite blade and method for making
FR2682663B1 (fr) * 1991-10-16 1994-01-07 Aerospatiale Ste Nationale Indle Rotor multipale, notamment pour helice arriere anticouple d'helicoptere et procede pour sa realisation.
US5273401A (en) * 1992-07-01 1993-12-28 The United States Of America As Represented By The Secretary Of The Air Force Wrapped paired blade rotor
DE19529476C2 (de) * 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
DE19529706C2 (de) * 1995-08-11 2001-08-02 Deutsch Zentr Luft & Raumfahrt Flächentragwerk, insbesondere für ein Luftfahrzeug
US5868351A (en) * 1996-05-23 1999-02-09 Bell Helicopter Textron Inc. Rotor blade stowing system
FR2776264B1 (fr) * 1998-03-23 2000-06-02 Eurocopter France Pale a pas variable en materiau composite pour rotor d'helicoptere et procede de fabrication d'une telle pale
JP4115349B2 (ja) * 2002-07-12 2008-07-09 シャープ株式会社 羽ばたき浮上移動装置
AU2003302245A1 (en) * 2002-12-09 2004-07-29 University Of Florida Bendable wing for micro air vehicle
EP1666354B1 (fr) * 2004-12-01 2010-09-29 Airbus Operations GmbH Composant structurel, procédé de fabrication d'un composant structurel et utilisation d'un composant structurel dans le revêtement d'un aéronef
EP2246259B1 (fr) * 2009-04-29 2012-12-12 Eurocopter Deutschland GmbH Aile de rotor avec élément integral de transmission de tension et de couple et son procédé de fabrication
JP5503481B2 (ja) * 2010-09-30 2014-05-28 一般社団法人日本航空宇宙工業会 繊維強化複合材料を用いた翼状構造体およびその製造方法
FR2977235B1 (fr) * 2011-06-30 2013-07-12 Eurocopter France Pale de rotor, et aeronef
PL2617555T3 (pl) * 2012-01-20 2014-11-28 Siemens Ag Łopatka wirnika turbiny wiatrowej z krawędzią spływu zawierającą niedoprzędy
PL2626298T3 (pl) * 2012-02-09 2015-03-31 Agustawestland Spa Łopata wirnika statku powietrznego i odpowiedni sposób jej wytwarzania
US9393745B2 (en) * 2012-05-15 2016-07-19 Hexcel Corporation Over-molding of load-bearing composite structures
US20140119930A1 (en) * 2012-10-30 2014-05-01 Bell Helicopter Textron Inc. Method of Repairing, Splicing, Joining, Machining, and Stabilizing Honeycomb Core Using Pourable Structural Foam and a Structure Incorporating the Same
FR3023747B1 (fr) * 2014-07-18 2017-03-10 Airbus Helicopters Procede de fabrication d'un longeron d'une pale, et de fabrication d'une pale
US10576699B2 (en) * 2016-08-09 2020-03-03 Sikorsky Aircraft Corporation Bond fixture for root end laminate or rotor blade
US11572162B2 (en) * 2019-05-29 2023-02-07 Lockheed Martin Corporation Securing assembly for a rotor blade
US11541995B2 (en) 2020-07-14 2023-01-03 Lockheed Martin Corporation Rotor blade assembly for bearingless rotor
FR3116560B1 (fr) * 2020-11-23 2023-06-16 Safran Aircraft Engines Aube composite pour une turbomachine d’aéronef et son procédé de fabrication
US20240110577A1 (en) * 2022-09-29 2024-04-04 Kuo-Tsun Lin Plastic ceiling fan blade with a safety structure

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US2690810A (en) * 1947-07-31 1954-10-05 Onera (Off Nat Aerospatiale) Aircraft propeller
US2868439A (en) * 1954-05-07 1959-01-13 Goodyear Aircraft Corp Plastic axial-flow compressor for gas turbines
US3000446A (en) * 1958-08-25 1961-09-19 Studebaker Packard Corp Helicopter rotor blades
DE1506573B1 (de) * 1967-06-30 1969-09-25 Messerschmitt Boelkow Blohm Verankerung eines aus glasfaserverstaerktem Kunststoff bestehenden Bauteiles,insbesondere eines Rotorblattes
FR1544344A (fr) * 1967-06-30 1968-10-31 Bolkow Gmbh Dispositif d'ancrage pour pieds de pales de rotors
GB1235508A (en) * 1967-09-12 1971-06-16 Messerschmitt Boelkow Blohm A rotor blade for a rotor craft
DE1531374A1 (de) * 1967-09-12 1970-01-29 Messerschmitt Boelkow Blohm Rotorblatt aus faserverstaerktem Kunststoff mit schlaufenartiger Blattwurzel
FR2041747A1 (fr) * 1969-05-20 1971-02-05 Sud Aviation
US3603701A (en) * 1969-08-28 1971-09-07 Tadeusz Tarcrynski Composite rotor blade retention
FR2125150B1 (fr) * 1971-02-15 1973-12-07 Aerospatiale
US3782856A (en) * 1972-05-31 1974-01-01 United Aircraft Corp Composite aerodynamic blade with twin-beam spar

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2390331A1 (fr) * 1977-05-13 1978-12-08 Messerschmitt Boelkow Blohm Jonction principale de voilure portante pour aeronefs et vehicules spatiaux
FR2429148A1 (fr) * 1978-06-19 1980-01-18 Messerschmitt Boelkow Blohm Dispositif d'absorption de forces longitudinales ou de flexion dans un objet en matiere plastique renforcee de fibres, notamment en forme de pale de rotor
FR2660619A1 (fr) * 1990-04-06 1991-10-11 Agusta Spa Pale d'helicoptere.
FR2664629A1 (fr) * 1990-07-13 1992-01-17 Samsung Heavy Ind Bras plongeur pour excavatrice en materiaux composites polymeres de resistance elevee et procede pour sa fabrication.
FR2740379A1 (fr) * 1995-10-30 1997-04-30 Eurocopter France Procede de fabrication d'une pale en materiau composite pour rotor d'helicoptere, et pale pouvant etre obtenue par un tel procede
US6035531A (en) * 1995-10-30 2000-03-14 Eurocopter France Method for manufacturing a variable-pitch composite blade for a helicopter rotor
US6056838A (en) * 1995-10-30 2000-05-02 Eurocopter Method for manufacturing a variable-pitch composite blade for a helicopter rotor
FR2912990A1 (fr) * 2007-02-23 2008-08-29 Eurocopter France Pale de giravion pourvue d'un troncon radial et d'au moins un troncon en fleche avant et/ou arriere
EP1961658A1 (fr) * 2007-02-23 2008-08-27 Eurocopter Pale de giravion pourvue d' un tronçon radial et d ' au moins un tronçon en fléche avant et/ou arrière
CN101249886B (zh) * 2007-02-23 2010-06-23 尤洛考普特公司 旋翼飞行器叶片
US8096779B2 (en) 2007-02-23 2012-01-17 Eurocopter Rotorcraft blade provided with a radial segment and with at least one forwardly- and/or rearwardly-swept segment
EP3090866A1 (fr) * 2015-05-07 2016-11-09 Airbus Operations Limited Structures composites
US10576698B2 (en) 2015-05-07 2020-03-03 Airbus Operations Limited Composite structures
EP3501979A1 (fr) * 2017-12-22 2019-06-26 Airbus Helicopters Enveloppes aerodynamiques epaisses pour cols de pales et carenages de manchons de pales d'un rotor d'un aeronef
FR3075757A1 (fr) * 2017-12-22 2019-06-28 Airbus Helicopters Enveloppes aerodynamiques epaisses pour cols de pales et carenages de manchons de pales d'un rotor d'un aeronef
US10858093B2 (en) 2017-12-22 2020-12-08 Airbus Helicopters Thick airfoil shapes for blade necks and for blade cuff fairings for an aircraft rotor
FR3120249A1 (fr) * 2021-03-01 2022-09-02 Safran Aircraft Engines Aube comprenant une structure en matériau composite et procédé de fabrication associé
WO2022184997A1 (fr) * 2021-03-01 2022-09-09 Safran Aircraft Engines Aube comprenant une structure en matériau composite et procédé de fabrication associé

Also Published As

Publication number Publication date
US3950115A (en) 1976-04-13
DE2451860A1 (de) 1975-07-10
GB1484179A (en) 1977-09-01
FR2252916B1 (fr) 1978-02-24
DE2451860B2 (de) 1980-10-09
DE2451860C3 (de) 1981-07-09

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