FR2718670B1 - Part comprising at least a cover plate of composite material and method for making said part. - Google Patents

Part comprising at least a cover plate of composite material and method for making said part.

Info

Publication number
FR2718670B1
FR2718670B1 FR9404586A FR9404586A FR2718670B1 FR 2718670 B1 FR2718670 B1 FR 2718670B1 FR 9404586 A FR9404586 A FR 9404586A FR 9404586 A FR9404586 A FR 9404586A FR 2718670 B1 FR2718670 B1 FR 2718670B1
Authority
FR
France
Prior art keywords
part
making
method
composite material
cover plate
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 - Fee Related
Application number
FR9404586A
Other languages
French (fr)
Other versions
FR2718670A1 (en
Inventor
Lucien Fantino
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 FR9404586A priority Critical patent/FR2718670B1/en
Publication of FR2718670A1 publication Critical patent/FR2718670A1/en
Application granted granted Critical
Publication of FR2718670B1 publication Critical patent/FR2718670B1/en
Anticipated expiration legal-status Critical
Application status is Expired - Fee Related legal-status Critical

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
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/02Physical, chemical or physicochemical properties
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24Fibrous 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
    • 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
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543Fixing the position or configuration of fibrous reinforcements before or during moulding
    • 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
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/08Impregnating
    • 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
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/08Interconnection of layers by mechanical means
    • 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
    • B29L2007/00Flat articles, e.g. films or sheets
    • B29L2007/002Panels; Plates; Sheets
    • 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
    • B29L2009/00Layered products
    • 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
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B2038/0052Other operations not otherwise provided for
    • B32B2038/0076Curing, vulcanising, cross-linking
    • 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
    • B32B2260/00Impregnation or embedding of a layer; Bonding a fibrous, filamentary or particulate layer by using a binder
    • B32B2260/04Impregnation material
    • B32B2260/046Synthetic resin
    • 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
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/306Resistant to heat
FR9404586A 1994-04-18 1994-04-18 Part comprising at least a cover plate of composite material and method for making said part. Expired - Fee Related FR2718670B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9404586A FR2718670B1 (en) 1994-04-18 1994-04-18 Part comprising at least a cover plate of composite material and method for making said part.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9404586A FR2718670B1 (en) 1994-04-18 1994-04-18 Part comprising at least a cover plate of composite material and method for making said part.

Publications (2)

Publication Number Publication Date
FR2718670A1 FR2718670A1 (en) 1995-10-20
FR2718670B1 true FR2718670B1 (en) 1996-06-14

Family

ID=9462202

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9404586A Expired - Fee Related FR2718670B1 (en) 1994-04-18 1994-04-18 Part comprising at least a cover plate of composite material and method for making said part.

Country Status (1)

Country Link
FR (1) FR2718670B1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6027798A (en) * 1995-11-01 2000-02-22 The Boeing Company Pin-reinforced sandwich structure
US5876652A (en) * 1996-04-05 1999-03-02 The Boeing Company Method for improving pulloff strength in pin-reinforced sandwich structure
NL1007281C2 (en) * 1997-10-15 1999-04-19 Syncoglas Sa Nv Three-dimensional strengthening material.
FR2836690B1 (en) * 2002-03-04 2004-08-27 Eads Launch Vehicles Method for producing a composite monolithic piece thermostructural double wall and piece obtained
DE102005024408A1 (en) 2005-05-27 2006-11-30 Airbus Deutschland Gmbh Producing fiber reinforced foam materials for aircraft involves engaging through hole from first surface to engage at least one fiber bundle and pulling bundle(s) into through hole in foam material
FR2918599B1 (en) * 2007-07-13 2009-08-14 Chomarat Composites Soc Par Ac textile sandwich structure and method of manufacture
DE102007055684A1 (en) 2007-11-21 2009-06-10 Airbus Deutschland Gmbh An apparatus for manufacturing a reinforced cellular material
ITMI20080971A1 (en) * 2008-05-26 2009-11-27 Nat Style Ltd Device and process for the production in continuous of a three-dimensional fabric for the production of panels.
FR3026675B1 (en) 2014-10-02 2016-11-11 Mbda France Method for producing a composite monolithic piece thermostructural double wall and piece obtained

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1082164A (en) * 1953-08-06 1954-12-27 Tech Du Verre Tisse A process for the surface reinforcement of a plastic part materials by means of a fabric
US4196251A (en) * 1979-04-16 1980-04-01 International Harvester Company Rigidized resinous foam core sandwich structure
US4416929A (en) * 1981-07-02 1983-11-22 Proform, Inc. Multilayer stitched knitted fiberglass composite
FR2602178B1 (en) * 1986-08-01 1989-04-07 Chomarat & Cie Material for reinforcing articles statifies
FR2606704A1 (en) * 1986-11-18 1988-05-20 Mecelec Sa Method for producing electrically conducting components by the compression moulding technique, sandwich sheets for implementing the said method and electrically conducting components obtained
FR2628448B1 (en) * 1988-03-14 1990-11-16 Chomarat & Cie Textile armature usable for the realization of complex and complex laminated laminates in form having such a frame
FR2646442B1 (en) * 1989-04-28 1993-04-02 Chomarat & Cie textile armature usable for the production of composite materials and shaped articles comprising such a frame
FR2678547B1 (en) * 1991-07-03 1995-03-10 Guy Leroy Method and apparatus for producing composite and composite webs obtained.
FR2684719B1 (en) * 1991-12-04 1994-02-11 Snecma turbomachine blade comprising composite material plies.
FR2687173B1 (en) * 1992-02-11 1995-09-08 Aerospatiale Method for producing a fiber reinforcement for a composite component, and composite piece comprising such a frame.

Also Published As

Publication number Publication date
FR2718670A1 (en) 1995-10-20

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20121228