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WO2002040264A3 - Method for producing composite elements - Google Patents

Method for producing composite elements Download PDF

Info

Publication number
WO2002040264A3
WO2002040264A3 PCT/EP2001/013021 EP0113021W WO0240264A3 WO 2002040264 A3 WO2002040264 A3 WO 2002040264A3 EP 0113021 W EP0113021 W EP 0113021W WO 0240264 A3 WO0240264 A3 WO 0240264A3
Authority
WO
WIPO (PCT)
Prior art keywords
opening
composite elements
iii
producing composite
metal
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.)
Ceased
Application number
PCT/EP2001/013021
Other languages
German (de)
French (fr)
Other versions
WO2002040264A2 (en
Inventor
Matthias Hefner
Heinz Forster
Gerhard Bernard
Georg Riess
Georg Knoblauch
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.)
BASF SE
Original Assignee
BASF SE
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 BASF SE filed Critical BASF SE
Priority to AU2002218293A priority Critical patent/AU2002218293A1/en
Publication of WO2002040264A2 publication Critical patent/WO2002040264A2/en
Publication of WO2002040264A3 publication Critical patent/WO2002040264A3/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/24Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with at least one layer not being coherent before laminating, e.g. made up from granular material sprinkled onto a substrate
    • 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
    • B29C44/00Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/12Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
    • B29C44/1228Joining preformed parts by the expanding material
    • B29C44/1233Joining preformed parts by the expanding material the preformed parts being supported during expanding
    • 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
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/04Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic 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
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/34Layered products comprising a layer of synthetic resin comprising polyamides
    • 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
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/40Layered products comprising a layer of synthetic resin comprising polyurethanes
    • 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
    • B32B38/0012Mechanical treatment, e.g. roughening, deforming, stretching
    • B32B2038/0016Abrading
    • 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
    • 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
    • B32B2311/00Metals, their alloys or their compounds
    • 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
    • B32B2605/00Vehicles
    • B32B2605/12Ships
    • 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
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/14Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/16Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating
    • B32B37/18Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating involving the assembly of discrete sheets or panels only
    • 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
    • B32B38/16Drying; Softening; Cleaning
    • B32B38/162Cleaning

Landscapes

  • Polyurethanes Or Polyureas (AREA)
  • Laminated Bodies (AREA)

Abstract

The invention relates to composite elements having a structure comprising the following layers: (i) between 2 and 20 mm of metal, (ii) between 10 and 300 mm of polyisocyanate polyaddition products which can be obtained by reacting (a) isocyanates with (b) polymer polyols, as compounds which react with ioscyanates, and (iii) between 2 and 20 mm of metal. The invention is characterised in that the metallic layers (i) and (iii) are fixed in such a way that area (R) is formed between the same for layer (ii), (R) is sealed, with the exception of at least one opening for filling (R) and at least one other opening, and the sealing of (R) is checked by measuring the pressure difference on the opening(s), before filling (R) with the starting components for producing (ii).
PCT/EP2001/013021 2000-11-14 2001-11-10 Method for producing composite elements Ceased WO2002040264A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2002218293A AU2002218293A1 (en) 2000-11-14 2001-11-10 Method for producing composite elements

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10056377.5 2000-11-14
DE2000156377 DE10056377A1 (en) 2000-11-14 2000-11-14 Production of metal-polyurethane-metal sandwich elements, for use e.g. in ships, bridges and buildings, involves feeding isocyanate and polymer-polyol starting materials into a sealed space formed between two metal layers

Publications (2)

Publication Number Publication Date
WO2002040264A2 WO2002040264A2 (en) 2002-05-23
WO2002040264A3 true WO2002040264A3 (en) 2002-09-19

Family

ID=7663245

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2001/013021 Ceased WO2002040264A2 (en) 2000-11-14 2001-11-10 Method for producing composite elements

Country Status (3)

Country Link
AU (1) AU2002218293A1 (en)
DE (1) DE10056377A1 (en)
WO (1) WO2002040264A2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10306892A1 (en) * 2003-02-18 2004-08-26 Basf Ag Layered composite structure manufacture, particularly in marine applications, involves bonding sidewalls onto outer layers before forming plastic layer between them
DE102004027417A1 (en) * 2004-06-04 2005-12-22 Basf Ag composite element
DE102008003560A1 (en) * 2008-01-09 2009-07-23 Voestalpine Polynorm Van Niftrik Bv Metal hybrid layer composite part with at least one metallic outer layer and method for its production
US8413485B2 (en) 2009-07-17 2013-04-09 Airbus Operations Gmbh Detection method and detection device for detecting core defects and delaminations in sandwich structures
DE102009027807A1 (en) * 2009-07-17 2011-03-10 Airbus Operations Gmbh Method for detecting defective sandwich component at aircraft construction, involves loading measuring chamber with predetermined pressure, and detecting and evaluating pressure adjusted in measuring chamber

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6050208A (en) * 1996-11-13 2000-04-18 Fern Investments Limited Composite structural laminate
WO2000059718A1 (en) * 1999-03-30 2000-10-12 Basf Aktiengesellschaft Composite elements containing polyisocyanate-polyaddition products

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6050208A (en) * 1996-11-13 2000-04-18 Fern Investments Limited Composite structural laminate
WO2000059718A1 (en) * 1999-03-30 2000-10-12 Basf Aktiengesellschaft Composite elements containing polyisocyanate-polyaddition products

Also Published As

Publication number Publication date
WO2002040264A2 (en) 2002-05-23
AU2002218293A1 (en) 2002-05-27
DE10056377A1 (en) 2002-05-23

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