FR2797212B1 - Procede de fabrication d'un objet en materiau composite renforce par des fibres, tel qu'une portion d'une pale de rotor pour un aeronef, et objet obtenu par ce procede - Google Patents

Procede de fabrication d'un objet en materiau composite renforce par des fibres, tel qu'une portion d'une pale de rotor pour un aeronef, et objet obtenu par ce procede

Info

Publication number
FR2797212B1
FR2797212B1 FR0010304A FR0010304A FR2797212B1 FR 2797212 B1 FR2797212 B1 FR 2797212B1 FR 0010304 A FR0010304 A FR 0010304A FR 0010304 A FR0010304 A FR 0010304A FR 2797212 B1 FR2797212 B1 FR 2797212B1
Authority
FR
France
Prior art keywords
aircraft
fiber
manufacturing
composite material
rotor blade
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
FR0010304A
Other languages
English (en)
French (fr)
Other versions
FR2797212A1 (fr
Inventor
Robert A Moore
Ronald J Measom
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.)
Bell Helicopter Textron Inc
Original Assignee
Bell Helicopter Textron Inc
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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of FR2797212A1 publication Critical patent/FR2797212A1/fr
Application granted granted Critical
Publication of FR2797212B1 publication Critical patent/FR2797212B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • 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
    • 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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/386—Automated tape laying [ATL]
    • 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
    • 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Inorganic Fibers (AREA)
FR0010304A 1999-08-06 2000-08-04 Procede de fabrication d'un objet en materiau composite renforce par des fibres, tel qu'une portion d'une pale de rotor pour un aeronef, et objet obtenu par ce procede Expired - Lifetime FR2797212B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/370,392 US6263936B1 (en) 1999-08-06 1999-08-06 Technique for making fiber composite object

Publications (2)

Publication Number Publication Date
FR2797212A1 FR2797212A1 (fr) 2001-02-09
FR2797212B1 true FR2797212B1 (fr) 2006-07-28

Family

ID=23459444

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0010304A Expired - Lifetime FR2797212B1 (fr) 1999-08-06 2000-08-04 Procede de fabrication d'un objet en materiau composite renforce par des fibres, tel qu'une portion d'une pale de rotor pour un aeronef, et objet obtenu par ce procede

Country Status (8)

Country Link
US (1) US6263936B1 (enExample)
JP (1) JP2001097287A (enExample)
KR (1) KR100645342B1 (enExample)
CA (1) CA2314833A1 (enExample)
DE (1) DE10037540B4 (enExample)
FR (1) FR2797212B1 (enExample)
GB (1) GB2352737B (enExample)
IT (1) IT1318725B1 (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020124029A1 (en) * 2001-03-02 2002-09-05 Gwinn John Glen Method and apparatus for creating, embedding and using a searchable font
US6659722B2 (en) * 2001-05-07 2003-12-09 Bell Helicopter Textron, Inc. Composite rotor blade and method of manufacture
US7165945B2 (en) * 2003-08-22 2007-01-23 Sikorsky Aircraft Corporation Braided spar for a rotor blade and method of manufacture thereof
US20050186081A1 (en) * 2004-02-24 2005-08-25 Mohamed Mansour H. Wind blade spar cap and method of making
CN100457994C (zh) * 2004-11-30 2009-02-04 中材科技股份有限公司 复合材料用三维多向编织物净尺寸仿形减纱编织方法
US9090027B2 (en) 2012-10-23 2015-07-28 Bell Helicopter Textron Inc. System and method of constructing composite structures
FR3023748B1 (fr) 2014-07-18 2016-08-26 Airbus Helicopters Procede de fabrication d'un longeron d'une pale, de fabrication d'une pale, et une pale
WO2016025386A1 (en) 2014-08-15 2016-02-18 Sikorsky Aircraft Corporation Rotor blade spar formation with automated fiber placement
DE102016118791A1 (de) * 2016-06-29 2018-01-04 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zum Konfektionieren und/oder Ablegen eines Materials an einer Formwerkzeugoberfläche und Computerprogrammprodukt

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4123212A (en) 1977-06-27 1978-10-31 Maso-Therm Corporation Apparatus for uniformly distributing glass fibers
US4273601A (en) * 1977-10-31 1981-06-16 Structural Composites Industries, Inc. Method for the production of elongated resin impregnated filament composite structures
DE2856661C2 (de) * 1978-12-29 1986-03-20 M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 8000 München Verfahren und Vorrichtung zur Herstellung von Kunststoff-Flügeln, insbesondere für Wind-Kraftanlagen in einer Form
US4351688A (en) * 1979-12-10 1982-09-28 General Dynamics Corporation Composite tape laying machine
GB2100835B (en) * 1981-06-15 1985-09-25 Budd Co Non-metallic leaf spring
GB2101519B (en) * 1981-06-22 1986-03-19 Vought Corp Apparatus for tape laying and manufacture of composite structures
GB2124130B (en) * 1982-07-24 1985-11-27 Rolls Royce Vacuum moulding fibre reinforced resin
GB8305749D0 (en) * 1983-03-02 1983-04-07 British Aerospace Tape laying apparatus
US4491493A (en) * 1983-04-08 1985-01-01 Eaton Homer L Composite tape preparation and application
FR2568167B1 (fr) * 1984-07-25 1986-08-29 Renault Procede de moulage de preimpregnes a fibres orientees
US4696707A (en) * 1987-08-18 1987-09-29 The Ingersoll Milling Machine Company Composite tape placement apparatus with natural path generation means
US5022952A (en) 1985-12-13 1991-06-11 Cincinnati Milacron Inc. Fiber placement machine
US4750965A (en) 1986-03-28 1988-06-14 The Ingersoll Milling Machine Company Adaptive control for tape laying head having natural path generation
DE3614365A1 (de) * 1986-04-28 1987-10-29 Messerschmitt Boelkow Blohm Vorrichtung zum ablegen eines vorimpraegnierten faserbandes
US5641366A (en) 1988-01-20 1997-06-24 Loral Vought Systems Corporation Method for forming fiber-reinforced composite
US4799981A (en) * 1988-03-15 1989-01-24 Cincinnati Milacron Inc. Spool servo control for tape web positioning
US5841892A (en) 1995-05-31 1998-11-24 Board Of Trustees Operating Michigan State University System for automated analysis of 3D fiber orientation in short fiber composites
DE19604275C2 (de) * 1996-02-06 1998-03-19 Deutsch Zentr Luft & Raumfahrt Verfahren zur Herstellung eines Bauteils

Also Published As

Publication number Publication date
IT1318725B1 (it) 2003-09-10
JP2001097287A (ja) 2001-04-10
GB0018819D0 (en) 2000-09-20
ITMI20001821A1 (it) 2002-02-04
FR2797212A1 (fr) 2001-02-09
KR100645342B1 (ko) 2006-11-14
US6263936B1 (en) 2001-07-24
DE10037540B4 (de) 2014-10-30
KR20010049996A (ko) 2001-06-15
CA2314833A1 (en) 2001-02-06
ITMI20001821A0 (it) 2000-08-04
DE10037540A1 (de) 2001-07-19
GB2352737B (en) 2003-05-14
GB2352737A (en) 2001-02-07

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