DE60206282D1 - Verfahren zur herstellung von einer verbundstruktur aus einem schaumgefüllten wabenkern - Google Patents

Verfahren zur herstellung von einer verbundstruktur aus einem schaumgefüllten wabenkern

Info

Publication number
DE60206282D1
DE60206282D1 DE60206282T DE60206282T DE60206282D1 DE 60206282 D1 DE60206282 D1 DE 60206282D1 DE 60206282 T DE60206282 T DE 60206282T DE 60206282 T DE60206282 T DE 60206282T DE 60206282 D1 DE60206282 D1 DE 60206282D1
Authority
DE
Germany
Prior art keywords
foam
producing
composite structure
wave core
filled wave
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
DE60206282T
Other languages
English (en)
Other versions
DE60206282T2 (de
Inventor
D Webster
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.)
Lockheed Martin Corp
Original Assignee
Lockheed Corp
Lockheed Martin Corp
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 Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp
Publication of DE60206282D1 publication Critical patent/DE60206282D1/de
Application granted granted Critical
Publication of DE60206282T2 publication Critical patent/DE60206282T2/de
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
    • B29C69/00—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore
    • B29C69/001—Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore a shaping technique combined with cutting, e.g. in parts or slices combined with rearranging and joining the cut parts
    • 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
    • B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/34—Auxiliary operations
    • B29C44/56—After-treatment of articles, e.g. for altering the shape
    • B29C44/569—Shaping and joining components with different densities or hardness
    • 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/02—Bending or folding
    • B29C53/04—Bending or folding of plates or sheets
    • 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
    • B29C2793/00—Shaping techniques involving a cutting or machining operation
    • B29C2793/009—Shaping techniques involving a cutting or machining operation after shaping
    • 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
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001—Combinations of extrusion moulding with other shaping operations
    • B29C48/0012—Combinations of extrusion moulding with other shaping operations combined with shaping by internal pressure generated in the material, e.g. foaming
    • 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
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/12—Articles with an irregular circumference when viewed in cross-section, e.g. window profiles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/04—Condition, form or state of moulded material or of the material to be shaped cellular or porous
    • 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
    • B29L2031/3076—Aircrafts
    • 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
    • B29L2031/60—Multitubular or multicompartmented articles, e.g. honeycomb
    • B29L2031/608—Honeycomb structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
DE60206282T 2001-07-30 2002-07-26 Verfahren zur herstellung von einer verbundstruktur aus einem schaumgefüllten wabenkern Expired - Lifetime DE60206282T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US917850 2001-07-30
US09/917,850 US6649096B2 (en) 2001-07-30 2001-07-30 Method of making a filled honeycomb core composite structure
PCT/US2002/023935 WO2003011575A1 (en) 2001-07-30 2002-07-26 Method of making a filled honeycomb core composite structure

Publications (2)

Publication Number Publication Date
DE60206282D1 true DE60206282D1 (de) 2006-02-02
DE60206282T2 DE60206282T2 (de) 2006-06-22

Family

ID=25439412

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60206282T Expired - Lifetime DE60206282T2 (de) 2001-07-30 2002-07-26 Verfahren zur herstellung von einer verbundstruktur aus einem schaumgefüllten wabenkern

Country Status (5)

Country Link
US (1) US6649096B2 (de)
EP (1) EP1412162B1 (de)
CA (1) CA2453407C (de)
DE (1) DE60206282T2 (de)
WO (1) WO2003011575A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7842147B2 (en) * 2007-01-31 2010-11-30 M.C. Gill Corporation Composite panel having in-situ thermoset foamed core
DE202007003855U1 (de) * 2007-03-13 2008-07-17 Wolf-Dietrich Hannecke Kunststofftechnik Kunststoffformkörper
ITVR20100205A1 (it) * 2010-10-27 2012-04-28 Lasi Srl Sistema di trattamento di gas
US9597826B2 (en) 2012-10-30 2017-03-21 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US9149999B2 (en) 2012-10-30 2015-10-06 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
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
US9333684B2 (en) * 2012-10-30 2016-05-10 Bell Helicopter Textron Inc. Method of repairing, splicing, joining, machining, and stabilizing honeycomb core using pourable structural foam and a structure incorporating the same
US9015941B2 (en) 2012-10-30 2015-04-28 Bell Helicopter Textron Inc. Method of repairing honeycomb core using pourable structural foam
US9610561B2 (en) 2014-08-11 2017-04-04 Corning Incorporated Method of making a honeycomb having channels containing a porous adsorbent
RU2685743C1 (ru) * 2018-04-16 2019-04-23 Геннадий Алексеевич Павлов Подкильный обтекатель антенны судовой гидроакустической станции
CN111923313B (zh) * 2020-08-15 2022-10-25 东莞市粤丰新型建材有限公司 一种建筑预制复合砌块的制备方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3317074A (en) * 1963-06-17 1967-05-02 Douglas Aircraft Co Inc Cryogenic containers
US3879245A (en) * 1972-06-27 1975-04-22 Composite Structures Corp Method of making composite cored structures
US4584041A (en) * 1983-04-21 1986-04-22 Lear Siegler, Inc. Method of making a containment vessel
US4687691A (en) * 1986-04-28 1987-08-18 United Technologies Corporation Honeycomb spliced multilayer foam core aircraft composite parts and method for making same
US4964936A (en) * 1988-10-11 1990-10-23 Imi-Tech Corporation Method of making foam-filled cellular structures
US5188879A (en) * 1991-07-15 1993-02-23 Sorrento Engineering Corporation Polyimide foam filled structures
US5338594A (en) * 1992-02-07 1994-08-16 Hexcel Corporation Foam filled honeycomb and methods for their production
US5834082A (en) * 1992-05-04 1998-11-10 Webcore Technologies, Inc. Reinforced foam cores and method and apparatus of production
US5288538A (en) * 1992-12-16 1994-02-22 Reynolds Metals Company Expandable honeycomb core structural member
US5529480A (en) * 1994-10-28 1996-06-25 The Boeing Company Honeycomb core forming restricter
US5569508A (en) * 1995-01-03 1996-10-29 The Boeing Company Resin transfer molding with honeycomb core and core filler
US5580502A (en) * 1995-03-23 1996-12-03 Sikorsky Aircraft Corporation Method of fabricating a composite article having an integral, co-cured composite stiffening member
US5780074A (en) * 1995-10-16 1998-07-14 The Boeing Company Apparatus for shaping honeycomb core
US5654518A (en) * 1995-12-06 1997-08-05 Rockwell International Corporation Double truss structural armor component

Also Published As

Publication number Publication date
US6649096B2 (en) 2003-11-18
US20030020195A1 (en) 2003-01-30
CA2453407A1 (en) 2003-02-13
CA2453407C (en) 2009-11-24
DE60206282T2 (de) 2006-06-22
WO2003011575A1 (en) 2003-02-13
EP1412162B1 (de) 2005-09-21
EP1412162A1 (de) 2004-04-28

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