MX9401201A - Un metodo para fabricar una pieza de material compuesto, en particular un panel emparedado a partir de una pluralidad de preformas ensambladas entre si. - Google Patents

Un metodo para fabricar una pieza de material compuesto, en particular un panel emparedado a partir de una pluralidad de preformas ensambladas entre si.

Info

Publication number
MX9401201A
MX9401201A MX9401201A MX9401201A MX9401201A MX 9401201 A MX9401201 A MX 9401201A MX 9401201 A MX9401201 A MX 9401201A MX 9401201 A MX9401201 A MX 9401201A MX 9401201 A MX9401201 A MX 9401201A
Authority
MX
Mexico
Prior art keywords
composite material
preforms
preform
assembled
piece
Prior art date
Application number
MX9401201A
Other languages
English (en)
Inventor
Stephane Castagnos
Jean-Louis Limousin
Original Assignee
Europ Propulsion
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 Europ Propulsion filed Critical Europ Propulsion
Publication of MX9401201A publication Critical patent/MX9401201A/es

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B18/00Layered products essentially comprising ceramics, e.g. refractory products
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C37/00Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
    • B29C37/0078Measures or configurations for obtaining anchoring effects in the contact areas between layers
    • B29C37/0082Mechanical anchoring
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00Producing articles with hollow walls
    • B29D24/002Producing articles with hollow walls formed with structures, e.g. cores placed between two plates or sheets, e.g. partially filled
    • B29D24/005Producing 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
    • B29D24/007Producing 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 and a chamfered edge
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71Ceramic products containing macroscopic reinforcing agents
    • C04B35/78Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
    • C04B35/80Fibres, filaments, whiskers, platelets, or the like
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/71Ceramic products containing macroscopic reinforcing agents
    • C04B35/78Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
    • C04B35/80Fibres, filaments, whiskers, platelets, or the like
    • C04B35/83Carbon fibres in a carbon matrix
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/60Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608Honeycomb structures
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/02Composition of constituents of the starting material or of secondary phases of the final product
    • C04B2235/50Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
    • C04B2235/52Constituents or additives characterised by their shapes
    • C04B2235/5208Fibers
    • C04B2235/5216Inorganic
    • C04B2235/524Non-oxidic, e.g. borides, carbides, silicides or nitrides
    • C04B2235/5248Carbon, e.g. graphite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2235/00Aspects relating to ceramic starting mixtures or sintered ceramic products
    • C04B2235/60Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
    • C04B2235/614Gas infiltration of green bodies or pre-forms
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/38Fiber or whisker reinforced
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/32Ceramic
    • C04B2237/38Fiber or whisker reinforced
    • C04B2237/385Carbon or carbon composite
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/62Forming laminates or joined articles comprising holes, channels or other types of openings

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Structural Engineering (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Composite Materials (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Abstract

Un método para la fabricación de una pieza de material compuesto, comprendiendo el método: elaborar preformas distintas para diferentes porciones de la pieza, por lo menos una de las preformas es una preforma de fibra hilvanada y muestra fibrillas que se proyectan substancialmente en forma perpendicular desde una superficie de la preforma, formándose las fibrillas por los extremos de fibras que se han desplazado sobre el hilvanado de la preforma; ensamblar entre sí la preformas mientras que están en un estado no densificado o un estado que no se ha densificado totalmente, con las dos preformas ensamblandose entre sí por lo menos en parte por las superficies respectivas en contacto de las dos preformas que se unen por medio de las fibrillas que se proyectan desde la superficie de la por lo menos una de las dos preformas, y en donde la superficie de la otra preforma se acopla; y co-densificar las preformas ensambladas entre sí.
MX9401201A 1993-02-17 1994-02-16 Un metodo para fabricar una pieza de material compuesto, en particular un panel emparedado a partir de una pluralidad de preformas ensambladas entre si. MX9401201A (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9301767A FR2701665B1 (fr) 1993-02-17 1993-02-17 Procédé de fabrication d'une pièce en matériau composite, notamment un panneau sandwich, à partir de plusieurs préformes assemblées.

Publications (1)

Publication Number Publication Date
MX9401201A true MX9401201A (es) 1994-08-31

Family

ID=9444130

Family Applications (1)

Application Number Title Priority Date Filing Date
MX9401201A MX9401201A (es) 1993-02-17 1994-02-16 Un metodo para fabricar una pieza de material compuesto, en particular un panel emparedado a partir de una pluralidad de preformas ensambladas entre si.

Country Status (12)

Country Link
US (1) US5490892A (es)
EP (1) EP0611741B1 (es)
JP (1) JP3719721B2 (es)
AT (1) ATE160334T1 (es)
CA (1) CA2115473C (es)
DE (1) DE69406815T2 (es)
ES (1) ES2110190T3 (es)
FR (1) FR2701665B1 (es)
MX (1) MX9401201A (es)
NO (1) NO180287C (es)
RU (1) RU2119872C1 (es)
UA (1) UA26925C2 (es)

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US6261675B1 (en) 1999-03-23 2001-07-17 Hexcel Corporation Core-crush resistant fabric and prepreg for fiber reinforced composite sandwich structures
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US20050158171A1 (en) * 2004-01-15 2005-07-21 General Electric Company Hybrid ceramic matrix composite turbine blades for improved processibility and performance
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US20070036958A1 (en) * 2005-08-10 2007-02-15 Agvantage, Inc. Composite material with grain filler and method of making same
JP4795062B2 (ja) * 2006-03-15 2011-10-19 有限会社泰成電機工業 板状物及びその製造方法
FR2921076B1 (fr) * 2007-09-18 2010-04-02 Roy Guy Le Panneau a forte resistance structurelle, dispositif et procede pour fabriquer un tel panneau
US8372498B2 (en) 2007-12-17 2013-02-12 Sikorsky Aircraft Corporation Composite core densification
US20100196652A1 (en) * 2009-02-03 2010-08-05 Demien Jacquinet Quasi-isotropic sandwich structures
IT1393462B1 (it) * 2009-03-23 2012-04-20 Angelo Peruzza Di Paolo Peruzza & C S A S Ora A Peruzza S R L Pellicola per la produzione di manufatti in materiale composito, metodo di produzione di detta pellicola, e metodo per la produzione di manufatti in materiale composito impiegante tale pellicola
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FR2948693B1 (fr) * 2009-07-28 2014-01-17 Saertex France Procede de realisation d'une ame avec fibres de pontage integrees pour panneaux en materiaux composites, panneau obtenu et dispositif
FR2972448B1 (fr) * 2011-03-07 2013-04-19 Commissariat Energie Atomique Procede de fabrication d'un composite a matrice ceramique
FR2989921B1 (fr) * 2012-04-27 2015-05-15 Hexcel Reinforcements Utilisation, dans la fabrication d'une piece composite, d'une operation de penetration, pour ameliorer la conductivite electrique transverse de la piece composite
US9527262B2 (en) * 2012-09-28 2016-12-27 General Electric Company Layered arrangement, hot-gas path component, and process of producing a layered arrangement
US9833930B2 (en) * 2012-10-23 2017-12-05 Albany Engineered Composites, Inc. Circumferential stiffeners for composite fancases
RU2544043C2 (ru) * 2012-10-25 2015-03-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ изготовления сотовой конструкции
EP2922690B1 (en) * 2012-11-20 2017-04-19 Vestas Wind Systems A/S Wind turbine blades and method of manufacturing the same
FR3001452B1 (fr) * 2013-01-29 2015-02-13 Herakles Procede de fabrication d'un panneau d'attenuation acoustique de forme courbee
RU2537307C1 (ru) * 2013-07-22 2014-12-27 Анатолий Михайлович Мельников Способ изготовления сэндвич-панелей (варианты)
CN105531243B (zh) 2013-09-20 2018-01-16 通用电气公司 通过化学气相渗透制作的陶瓷基质复合物及其制造方法
GB201402732D0 (en) * 2014-02-17 2014-04-02 Rolls Royce Plc A honeycomb structure
DE102014215964A1 (de) * 2014-08-12 2016-02-18 Bayerische Motoren Werke Aktiengesellschaft Verfahren zum Herstellen eines mit einem unidirektionalen Fasergelege versehenen SMC-Bauteiles
FR3026675B1 (fr) * 2014-10-02 2016-11-11 Mbda France Procede pour la realisation d'une piece monolithique composite thermostructurale a double paroi et piece obtenue
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RU175034U1 (ru) * 2016-12-21 2017-11-16 федеральное государственное бюджетное образовательное учреждение высшего образования "Московский государственный технический университет имени Н.Э. Баумана (национальный исследовательский университет)" (МГТУ им. Н.Э. Баумана) Схема теплозащитного покрытия многоразового теплового щита спускаемого аппарата для возвращения после полета к Луне
RU173721U1 (ru) * 2016-12-21 2017-09-07 федеральное государственное бюджетное образовательное учреждение высшего образования "Московский государственный технический университет имени Н.Э. Баумана (национальный исследовательский университет)" (МГТУ им. Н.Э. Баумана) Схема теплозащитного покрытия многоразового теплового щита спускаемого аппарата для возвращения с низкой околоземной орбиты
FR3070623B1 (fr) * 2017-09-04 2020-10-09 Coriolis Composites Procede de realisation d’une piece en materiau composite par aiguilletage oriente d’une preforme
FR3084011B1 (fr) * 2018-07-17 2021-02-26 Safran Ceram Procede de fabrication d'un panneau accoustique
FR3086786B1 (fr) 2018-10-01 2020-12-18 Airbus Operations Sas Procede de fabrication d'une peau acoustique degivrante pour panneau acoustique d'aeronef, utilisant un dispositif d'ecartement de fibres
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Also Published As

Publication number Publication date
RU2119872C1 (ru) 1998-10-10
EP0611741A1 (fr) 1994-08-24
NO940541D0 (no) 1994-02-16
EP0611741B1 (fr) 1997-11-19
ES2110190T3 (es) 1998-02-01
NO180287C (no) 1997-03-26
FR2701665A1 (fr) 1994-08-26
CA2115473C (en) 2001-05-01
JPH06246890A (ja) 1994-09-06
CA2115473A1 (en) 1994-08-18
DE69406815T2 (de) 1998-03-12
DE69406815D1 (de) 1998-01-02
US5490892A (en) 1996-02-13
UA26925C2 (uk) 1999-12-29
JP3719721B2 (ja) 2005-11-24
NO180287B (no) 1996-12-16
ATE160334T1 (de) 1997-12-15
FR2701665B1 (fr) 1995-05-19
NO940541L (es) 1994-08-18

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HC Change of company name or juridical status

Owner name: SANOFI-SYNTHELABO

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