PL447531A1 - Metal-carbon-glass laminate and its producing method - Google Patents

Metal-carbon-glass laminate and its producing method

Info

Publication number
PL447531A1
PL447531A1 PL447531A PL44753124A PL447531A1 PL 447531 A1 PL447531 A1 PL 447531A1 PL 447531 A PL447531 A PL 447531A PL 44753124 A PL44753124 A PL 44753124A PL 447531 A1 PL447531 A1 PL 447531A1
Authority
PL
Poland
Prior art keywords
thickness
layer
carbon
weight
sup
Prior art date
Application number
PL447531A
Other languages
Polish (pl)
Other versions
PL248763B1 (en
Inventor
Jarosław Bieniaś
Patryk Jakubczak
Monika Ostapiuk
Magda Droździel-Jurkiewicz
Piotr Podolak
Original Assignee
Politechnika Lubelska
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 Politechnika Lubelska filed Critical Politechnika Lubelska
Priority to PL447531A priority Critical patent/PL248763B1/en
Publication of PL447531A1 publication Critical patent/PL447531A1/en
Publication of PL248763B1 publication Critical patent/PL248763B1/en

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
    • 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
    • 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
    • B32B15/00Layered products comprising a layer of metal
    • B32B15/14Layered products comprising a layer of metal next to a fibrous or filamentary layer
    • 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
    • B32B17/00Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/02Layered products essentially comprising sheet glass, or glass, slag, or like fibres in the form of fibres or filaments
    • 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
    • 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
    • B32B37/10Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • B32B37/1018Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure using only vacuum
    • 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
    • B32B5/00Layered 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
    • B32B5/22Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/20Integral or sandwich constructions
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K9/00Use of pretreated ingredients
    • C08K9/10Encapsulated ingredients
    • 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
    • B32B2250/00Layers arrangement
    • B32B2250/055 or more layers
    • 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
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/02Composition of the impregnated, bonded or embedded layer
    • B32B2260/021Fibrous or filamentary layer
    • B32B2260/023Two or more layers
    • 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
    • B32B2260/00Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • B32B2260/04Impregnation, embedding, or binder 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
    • B32B2307/70Other properties
    • B32B2307/762Self-repairing, self-healing

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Medicinal Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Mechanical Engineering (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Ceramic Engineering (AREA)
  • Laminated Bodies (AREA)

Abstract

Przedmiotem zgłoszenia jest laminat metal-węgiel-szkło, który charakteryzuje się tym, że w części środkowej laminatu znajduje się warstwa samonaprawiająca się pierwsza (1) o grubości od 1 mm do 2 mm, składająca się z włókien szklanych wypełnionych diizocyjanianem izoforonu i połączonych żywicą termoplastyczną, do której obu powierzchni przylegają adhezyjnie dwie warstwy kompozytu termoplastycznego na bazie włókien węglowych (2) o grubości 0,04 mm każda, do których przylega adhezyjnie warstwa włókniny poliestrowej (3) o gramaturze 339 g/m<sup>2</sup> i o grubości od 4 mm do 8 mm. Do warstwy włókniny poliestrowej (3) przylegają adhezyjnie dwie warstwy kompozytu termoplastycznego na bazie włókien szklanych (4) o grubości 0,04 mm każda, które przylegają adhezyjnie do warstwy samonaprawiającej się drugiej (5) o grubości od 0,2 mm do 0,4 mm, składającej się z mikrokapsułek o wielkości od 25 µm do 100 µm, z których każda składa się z powłoki poliuretanowej z poliizocyjanuranu diizocyjanianu toluenu w octanie etylu w ilości 48,8% wagowo i wypełnienia z izocjanatu diizocyjanianu izoforonu w ilości 51,2% wagowo i nanorurek węglowych o wielkości od 20 nm do 100 nm połączonych z żywicą termoplastyczną. Przedmiotem zgłoszenia jest też sposób wytwarzania laminatu metal-węgiel-szkło, który polega na tym, że na dwa arkusze blachy (7) ze stopu niklu z tytanem o grubości 1 mm posiadające na obu powierzchniach warstwę ceramiczną (6) o grubości od 5 µm do 12 µm nanosi się obustronnie mikrokapsułki o wielkości od 25 µm do 100 µm, z których każda składa się z powłoki poliuretanowej z poliizocyjanuranu diizocyjanianu toluenu w octanie etylu w ilości 48,8% wagowo i wypełnienia z izocjanatu diizocyjanianu izoforonu w ilości 51,2% wagowo i nanorurki węglowe o wielkości od 20 nm do 100 nm, przy czym mikrokapsułki i nanorurki węglowe powleka się ręcznie żywicą termoplastyczną i otrzymuje się warstwę samonaprawiającą się drugą (5) o grubości od 0,2 mm do 0,4 mm. Na jeden z arkuszy blachy (7) ze stopu niklu z tytanem o grubości 1 mm posiadający na obu powierzchniach warstwę ceramiczną (6) o grubości od 5 µm do 12 µm i warstwę samonaprawiającą się drugą (5) o grubości od 0,2 mm do 0,4 mm nakłada się dwie warstwy kompozytu termoplastycznego na bazie włókien szklanych (4) o grubości 0,04 mm każda. Następnie nakłada się warstwę włókniny poliestrowej (3) o gramaturze 339 g/m<sup>2</sup> i o grubości od 4 mm do 8 mm.The subject of the application is a metal-carbon-glass laminate, which is characterized in that the central part of the laminate contains a first self-healing layer (1) with a thickness of 1 mm to 2 mm, consisting of glass fibres filled with isophorone diisocyanate and bonded with a thermoplastic resin, to both surfaces of which two layers of a thermoplastic composite based on carbon fibres (2) with a thickness of 0.04 mm each are adhesively adhered, to which a layer of polyester non-woven fabric (3) with a basis weight of 339 g/m<sup>2</sup> and a thickness of 4 mm to 8 mm is adhesively adhered. Two layers of a glass fiber-based thermoplastic composite (4) each 0.04 mm thick are adhesively adhered to the polyester nonwoven fabric layer (3), which are adhesively adhered to a second self-healing layer (5) 0.2 mm to 0.4 mm thick, consisting of microcapsules 25 µm to 100 µm in size, each consisting of a polyurethane coating of toluene diisocyanate polyisocyanurate in ethyl acetate in an amount of 48.8% by weight and a filler of isophorone diisocyanate isocyanate in an amount of 51.2% by weight and carbon nanotubes 20 nm to 100 nm in size combined with a thermoplastic resin. The subject of the application is also a method of producing a metal-carbon-glass laminate, which consists in applying on both sides of two sheets (7) of a 1 mm thick nickel-titanium alloy having on both surfaces a ceramic layer (6) of a thickness of 5 µm to 12 µm microcapsules of a size of 25 µm to 100 µm, each of which consists of a polyurethane coating of toluene diisocyanate polyisocyanurate in ethyl acetate in the amount of 48.8% by weight and a filler of isophorone diisocyanate isocyanate in the amount of 51.2% by weight and carbon nanotubes of a size of 20 nm to 100 nm, wherein the microcapsules and carbon nanotubes are manually coated with a thermoplastic resin, and a second self-healing layer (5) of a thickness of 0.2 mm to 100 nm is obtained. 0.4 mm. On one of the sheets (7) made of a nickel-titanium alloy with a thickness of 1 mm and having on both surfaces a ceramic layer (6) with a thickness of 5 µm to 12 µm and a second self-healing layer (5) with a thickness of 0.2 mm to 0.4 mm, two layers of a thermoplastic composite based on glass fibres (4) with a thickness of 0.04 mm each are applied. Then a layer of polyester non-woven fabric (3) with a basis weight of 339 g/m<sup>2</sup> and a thickness of 4 mm to 8 mm is applied.

PL447531A 2024-01-17 2024-01-17 Metal-carbon-glass laminate and method of producing it PL248763B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL447531A PL248763B1 (en) 2024-01-17 2024-01-17 Metal-carbon-glass laminate and method of producing it

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL447531A PL248763B1 (en) 2024-01-17 2024-01-17 Metal-carbon-glass laminate and method of producing it

Publications (2)

Publication Number Publication Date
PL447531A1 true PL447531A1 (en) 2024-08-12
PL248763B1 PL248763B1 (en) 2026-01-26

Family

ID=92264396

Family Applications (1)

Application Number Title Priority Date Filing Date
PL447531A PL248763B1 (en) 2024-01-17 2024-01-17 Metal-carbon-glass laminate and method of producing it

Country Status (1)

Country Link
PL (1) PL248763B1 (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101215407A (en) * 2008-01-18 2008-07-09 中山大学 A high-temperature self-repairing fiber-reinforced epoxy composite material and its preparation method
EP2285563A1 (en) * 2008-04-16 2011-02-23 Airbus Operations Limited Composite laminate with self-healing layer
PL240800B1 (en) * 2021-03-25 2022-06-06 Lubelska Polt Titanium-glass-carbon laminate and its producing method
PL243177B1 (en) * 2022-06-27 2023-07-10 Lubelska Polt Magnesium-glass laminate and method of its production

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101215407A (en) * 2008-01-18 2008-07-09 中山大学 A high-temperature self-repairing fiber-reinforced epoxy composite material and its preparation method
EP2285563A1 (en) * 2008-04-16 2011-02-23 Airbus Operations Limited Composite laminate with self-healing layer
PL240800B1 (en) * 2021-03-25 2022-06-06 Lubelska Polt Titanium-glass-carbon laminate and its producing method
PL243177B1 (en) * 2022-06-27 2023-07-10 Lubelska Polt Magnesium-glass laminate and method of its production

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
TOMASZ SZMECHTYK, NATALIA SIENKIEWICZ: "ELIKSIR nr 11, 2015 rok, str.26-27", „ŻYWICE EPOKSYDOWE JAKO MATERIAŁY SAMONAPRAWIAJĄCE SIĘ" *

Also Published As

Publication number Publication date
PL248763B1 (en) 2026-01-26

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