DE8915724U1 - - Google Patents

Info

Publication number
DE8915724U1
DE8915724U1 DE8915724U DE8915724U DE8915724U1 DE 8915724 U1 DE8915724 U1 DE 8915724U1 DE 8915724 U DE8915724 U DE 8915724U DE 8915724 U DE8915724 U DE 8915724U DE 8915724 U1 DE8915724 U1 DE 8915724U1
Authority
DE
Germany
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
DE8915724U
Other languages
German (de)
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to DE8915724U priority Critical patent/DE8915724U1/de
Publication of DE8915724U1 publication Critical patent/DE8915724U1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb 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
    • B29C67/00—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • B29C67/0044—Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 for shaping edges or extremities
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B31—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER; WORKING PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER
    • B31D—MAKING ARTICLES OF PAPER, CARDBOARD OR MATERIAL WORKED IN A MANNER ANALOGOUS TO PAPER, NOT PROVIDED FOR IN SUBCLASSES B31B OR B31C
    • B31D3/00—Making articles of cellular structure, e.g. insulating board
    • B31D3/02—Making articles of cellular structure, e.g. insulating board honeycombed structures, i.e. the cells having an essentially hexagonal section
    • B31D3/0284—Laminating honeycomb cores; applying cover sheets to core edges; working core edges
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered 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
    • B32B7/04—Interconnection of layers
    • B32B7/08—Interconnection of layers by mechanical means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B61—RAILWAYS
    • B61D—BODY DETAILS OR KINDS OF RAILWAY VEHICLES
    • B61D17/00—Construction details of vehicle bodies
    • B61D17/005—Construction details of vehicle bodies with bodies characterised by use of plastics materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62D—MOTOR VEHICLES; TRAILERS
    • B62D29/00—Superstructures, understructures, or sub-units thereof, characterised by the material thereof
    • B62D29/04—Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of synthetic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62D—MOTOR VEHICLES; TRAILERS
    • B62D29/00—Superstructures, understructures, or sub-units thereof, characterised by the material thereof
    • B62D29/04—Superstructures, understructures, or sub-units thereof, characterised by the material thereof predominantly of synthetic material
    • B62D29/048—Connections therefor, e.g. joints
    • 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
    • B29L2024/00—Articles with hollow walls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Architecture (AREA)
  • Structural Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
DE8915724U 1989-12-14 1989-12-14 Expired - Lifetime DE8915724U1 (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE8915724U DE8915724U1 (zh) 1989-12-14 1989-12-14

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE8915724U DE8915724U1 (zh) 1989-12-14 1989-12-14
DE3941248 1989-12-14

Publications (1)

Publication Number Publication Date
DE8915724U1 true DE8915724U1 (zh) 1991-05-16

Family

ID=25887960

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8915724U Expired - Lifetime DE8915724U1 (zh) 1989-12-14 1989-12-14

Country Status (1)

Country Link
DE (1) DE8915724U1 (zh)

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE9202774U1 (zh) * 1992-03-03 1992-07-02 Dethleffs Gmbh, 7972 Isny, De
DE9114757U1 (zh) * 1991-11-27 1992-12-24 Hymer Kg, 7967 Bad Waldsee, De
DE29503724U1 (de) * 1995-03-07 1995-05-11 Dreer Franz Möbelbauteil, insbesondere für Reisemobile und Caravans
EP0982212A1 (de) * 1998-08-27 2000-03-01 Inventio Ag Einrichtung zur Krafteinleitung in ein in Faserverbundbauweise hergestelltes Bauteil
DE102004010873A1 (de) * 2004-03-05 2005-09-22 Homag Holzbearbeitungssysteme Ag Verfahren und Vorrichtung zur Herstellung einer Leichtbauplatte
DE102004013145A1 (de) * 2004-03-17 2005-10-13 Airbus Deutschland Gmbh Verfahren zur Randabdichtung eines Kernverbundes
DE102004013146A1 (de) * 2004-03-17 2005-10-13 Airbus Deutschland Gmbh Verfahren zur Verstärkung von Kernstrukturen zur Bildung von beidseitig mit Deckschichten versehenen Kernverbunden sowie lokal verstärkter Kernverbund
DE102004013147A1 (de) * 2004-03-17 2005-10-13 Airbus Deutschland Gmbh Verfahren zur Integration von Verstärkungsbereichen in fertige Kernverbunde mit einer offenen dreidimensionalen Kernstruktur
DE102005023065A1 (de) * 2005-05-19 2006-11-30 Klebchemie, M.G. Becker Gmbh & Co Kg Leichtbauplatte
DE102005054608B3 (de) * 2005-11-11 2007-03-15 Innotech Holztechnologien Gmbh Verfahren zur Bearbeitung der Schmalflächen von Sandwichbauteilen in Leichtbauweise und eine Vorrichtung zur Durchführung des Verfahrens
DE202006004646U1 (de) * 2006-03-23 2007-08-09 Innovida Holdings Inc., Hallandale Beach Verbund von zwei Sandwichplatten
AT505767B1 (de) * 2008-03-07 2009-04-15 Blum Gmbh Julius Verfahren zum vorbereiten von leichtbauplatten fur die anschliessende befestigung von beschlagen
US7666493B2 (en) 2004-03-17 2010-02-23 Airbus Deutschland Gmbh Locally reinforced core structure for composite sandwich structure and method of producing the same
US7749420B2 (en) 2004-03-17 2010-07-06 Airbus Deutschland Gmbh Method and apparatus for processing open three-dimensional core structures such as folded honeycomb structures
DE102009060689A1 (de) 2009-12-29 2011-06-30 Airbus Operations GmbH, 21129 Verfahren zur Herstellung eines faserverstärkten Bauteils sowie Vorrichtung zur Durchführung des Verfahrens und faserverstärktes Bauteil
DE202010008964U1 (de) 2010-11-05 2012-02-06 Westfalia Presstechnik Gmbh & Co. Kg Hybridbauteil unter Verwendung von Wabenmaterial, insbesondere Wabenpappe
DE102011009871A1 (de) * 2011-01-31 2012-08-02 Elbe Flugzeugwerke Gmbh Stützkernverbundplatte
DE102011017353A1 (de) * 2011-04-16 2012-10-18 Daimler Ag Verfahren zur Herstellung einer Sandwichanordnung mit einer Kernlage und zumindest einer wölbstrukturierten Außenlage und Sandwichanordnung
US8506743B2 (en) 2004-03-17 2013-08-13 Airbus Deutschland Gmbh Composite sandwich structure with integrated reinforcement area and method of producing the same
ITPN20150013A1 (it) * 2015-05-12 2016-11-12 Indaf S A S Di Mauro Damiani & C Metodo di produzione per pannelli tamburati alveolari e pannelli ottenuti con tale metodo
DE10085095B3 (de) * 1999-10-08 2018-05-30 Milwaukee Composites, Inc. Platten mit einem vorgehärteten verstärkten Kern, Bodenanordnung enthaltend die Platten und deren Verwendung
DE102020132479A1 (de) 2020-12-07 2022-06-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verbundbauteil und Verfahren zu dessen Herstellung

Cited By (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE9114757U1 (zh) * 1991-11-27 1992-12-24 Hymer Kg, 7967 Bad Waldsee, De
DE9202774U1 (zh) * 1992-03-03 1992-07-02 Dethleffs Gmbh, 7972 Isny, De
DE29503724U1 (de) * 1995-03-07 1995-05-11 Dreer Franz Möbelbauteil, insbesondere für Reisemobile und Caravans
EP0982212A1 (de) * 1998-08-27 2000-03-01 Inventio Ag Einrichtung zur Krafteinleitung in ein in Faserverbundbauweise hergestelltes Bauteil
DE10085095B3 (de) * 1999-10-08 2018-05-30 Milwaukee Composites, Inc. Platten mit einem vorgehärteten verstärkten Kern, Bodenanordnung enthaltend die Platten und deren Verwendung
DE102004010873A1 (de) * 2004-03-05 2005-09-22 Homag Holzbearbeitungssysteme Ag Verfahren und Vorrichtung zur Herstellung einer Leichtbauplatte
US7658810B2 (en) 2004-03-17 2010-02-09 Airbus Deutschland Gmbh Method for sealing edges of a core of a composite sandwich structure
US7666493B2 (en) 2004-03-17 2010-02-23 Airbus Deutschland Gmbh Locally reinforced core structure for composite sandwich structure and method of producing the same
DE102004013145A1 (de) * 2004-03-17 2005-10-13 Airbus Deutschland Gmbh Verfahren zur Randabdichtung eines Kernverbundes
DE102004013147A1 (de) * 2004-03-17 2005-10-13 Airbus Deutschland Gmbh Verfahren zur Integration von Verstärkungsbereichen in fertige Kernverbunde mit einer offenen dreidimensionalen Kernstruktur
US7749420B2 (en) 2004-03-17 2010-07-06 Airbus Deutschland Gmbh Method and apparatus for processing open three-dimensional core structures such as folded honeycomb structures
DE102004013147B4 (de) * 2004-03-17 2008-01-03 Airbus Deutschland Gmbh Verfahren zur Integration von Verstärkungsbereichen in fertige Kernverbunde mit einer offenen dreidimensionalen Kernstruktur
DE102004013146B4 (de) * 2004-03-17 2008-01-24 Airbus Deutschland Gmbh Verfahren zur Verstärkung von Kernstrukturen zur Bildung von beidseitig mit Deckschichten versehenen Kernverbunden
DE102004013145B4 (de) * 2004-03-17 2010-04-01 Airbus Deutschland Gmbh Verfahren zur Randabdichtung eines Kernverbundes
DE102004013146A1 (de) * 2004-03-17 2005-10-13 Airbus Deutschland Gmbh Verfahren zur Verstärkung von Kernstrukturen zur Bildung von beidseitig mit Deckschichten versehenen Kernverbunden sowie lokal verstärkter Kernverbund
US8506743B2 (en) 2004-03-17 2013-08-13 Airbus Deutschland Gmbh Composite sandwich structure with integrated reinforcement area and method of producing the same
DE102005023065A1 (de) * 2005-05-19 2006-11-30 Klebchemie, M.G. Becker Gmbh & Co Kg Leichtbauplatte
DE102005054608B3 (de) * 2005-11-11 2007-03-15 Innotech Holztechnologien Gmbh Verfahren zur Bearbeitung der Schmalflächen von Sandwichbauteilen in Leichtbauweise und eine Vorrichtung zur Durchführung des Verfahrens
DE202006004646U1 (de) * 2006-03-23 2007-08-09 Innovida Holdings Inc., Hallandale Beach Verbund von zwei Sandwichplatten
AT505767B1 (de) * 2008-03-07 2009-04-15 Blum Gmbh Julius Verfahren zum vorbereiten von leichtbauplatten fur die anschliessende befestigung von beschlagen
DE102009060689A1 (de) 2009-12-29 2011-06-30 Airbus Operations GmbH, 21129 Verfahren zur Herstellung eines faserverstärkten Bauteils sowie Vorrichtung zur Durchführung des Verfahrens und faserverstärktes Bauteil
DE102009060689B4 (de) * 2009-12-29 2015-12-03 Airbus Operations Gmbh Verfahren zur Herstellung eines faserverstärkten Bauteils sowie Vorrichtung zur Durchführung des Verfahrens
US8894903B2 (en) 2009-12-29 2014-11-25 Airbus Operations Gmbh Method for the manufacture of a fiber-reinforced component
DE202010008964U1 (de) 2010-11-05 2012-02-06 Westfalia Presstechnik Gmbh & Co. Kg Hybridbauteil unter Verwendung von Wabenmaterial, insbesondere Wabenpappe
DE102011055010B4 (de) * 2010-11-05 2015-08-06 Westfalia Presstechnik Gmbh & Co. Kg Hybridbauteil für den Fahrzeugbereich
DE102011055010A1 (de) 2010-11-05 2012-05-10 Westfalia Presstechnik Gmbh & Co. Kg Hybridbauteil für den Fahrzeugbereich unter Verwendung von Wabenmaterial, insbesondere Wabenpappe
DE102011009871A1 (de) * 2011-01-31 2012-08-02 Elbe Flugzeugwerke Gmbh Stützkernverbundplatte
DE102011017353A1 (de) * 2011-04-16 2012-10-18 Daimler Ag Verfahren zur Herstellung einer Sandwichanordnung mit einer Kernlage und zumindest einer wölbstrukturierten Außenlage und Sandwichanordnung
DE102011017353B4 (de) * 2011-04-16 2016-01-14 Daimler Ag Verfahren zur Herstellung einer Sandwichanordnung mit einer Kernlage und zumindest einer wölbstrukturierten Außenlage und Sandwichanordnung
ITPN20150013A1 (it) * 2015-05-12 2016-11-12 Indaf S A S Di Mauro Damiani & C Metodo di produzione per pannelli tamburati alveolari e pannelli ottenuti con tale metodo
DE102020132479A1 (de) 2020-12-07 2022-06-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verbundbauteil und Verfahren zu dessen Herstellung

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