PL447527A1 - Metal-carbon laminate and its producing method - Google Patents

Metal-carbon laminate and its producing method

Info

Publication number
PL447527A1
PL447527A1 PL447527A PL44752724A PL447527A1 PL 447527 A1 PL447527 A1 PL 447527A1 PL 447527 A PL447527 A PL 447527A PL 44752724 A PL44752724 A PL 44752724A PL 447527 A1 PL447527 A1 PL 447527A1
Authority
PL
Poland
Prior art keywords
thickness
self
carbon
weight
thick
Prior art date
Application number
PL447527A
Other languages
Polish (pl)
Other versions
PL248599B1 (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 PL447527A priority Critical patent/PL248599B1/en
Publication of PL447527A1 publication Critical patent/PL447527A1/en
Publication of PL248599B1 publication Critical patent/PL248599B1/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

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, który charakteryzuje się tym, że w części środkowej laminatu znajduje się warstwa włókniny poliestrowej (1) o gramaturze 339 g/m<sup>2</sup> i o grubości od 4 mm do 8 mm, do której obu powierzchni przylegają adhezyjnie dwie warstwy kompozytu termoplastycznego na bazie włókien węglowych (2) o grubości 0,04 mm każda, które przylegają adhezyjnie do warstwy samonaprawiającej się pierwszej (3) o grubości od  mm do 2 mm, składającej się z włókien szklanych wypełnionych diizocyjanianem izoforonu i połączonych żywicą termoplastyczną. Warstwa samonaprawiająca się pierwsza (3) przylega adhezyjnie do warstwy samonaprawiającej się drugiej (4) 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. Zgłoszenie obejmuje także sposób wytwarzania laminatu metal-węgiel, który polega na tym, że na dwa arkusze blachy (6) ze stopu niklu z tytanem o grubości 1 mm posiadające na obu powierzchniach warstwę ceramiczną (5) 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 (4) o grubości od 0,2 mm do 0,4 mm. Następnie na jeden z arkuszy blachy (6) ze stopu niklu z tytanem o grubości 1 mm posiadający na obu powierzchniach warstwę ceramiczną (5) o grubości od 5 µm do 12 µm i warstwę samonaprawiającą się drugą (4) o grubości od 0,2 mm do 0,4 mm nakłada się dwie warstwy kompozytu termoplastycznego na bazie włókien węglowych (2) o grubości 0,04 mm każda.The subject of the application is a metal-carbon laminate, which is characterized in that the central part of the laminate contains a layer of polyester nonwoven fabric (1) with a basis weight of 339 g/m<sup>2</sup> and a thickness of 4 mm to 8 mm, to both surfaces of which two layers of a thermoplastic composite based on carbon fibers (2) with a thickness of 0.04 mm each are adhesively adhered, which are adhesively adhered to a first self-healing layer (3) with a thickness of 1 mm to 2 mm, consisting of glass fibers filled with isophorone diisocyanate and bonded with a thermoplastic resin. The first self-healing layer (3) is adhesively adhered to a second self-healing layer (4) having a thickness of 0.2 mm to 0.4 mm and consisting of microcapsules having a size of 25 µm to 100 µm, each of which consists 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 having a size of 20 nm to 100 nm combined with a thermoplastic resin. The application also covers a method of producing a metal-carbon laminate, which comprises applying microcapsules of size from 25 µm to 100 µm on both sides of two 1 mm thick nickel-titanium alloy sheets (6) having a ceramic layer (5) of thickness from 5 µm to 12 µm on both surfaces, each consisting 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 size from 20 nm to 100 nm, wherein the microcapsules and carbon nanotubes are manually coated with a thermoplastic resin, and a second self-healing layer (4) of thickness from 0.2 mm to 0.4 mm is obtained. Then, two layers of a thermoplastic composite based on carbon fibres (2), each 0.04 mm thick, are applied to one of the sheets (6) made of a 1 mm thick nickel-titanium alloy having on both surfaces a ceramic layer (5) of 5 µm to 12 µm thick and a second self-healing layer (4) of 0.2 mm to 0.4 mm thick.

PL447527A 2024-01-17 2024-01-17 Metal-carbon laminate and method of producing it PL248599B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL447527A PL248599B1 (en) 2024-01-17 2024-01-17 Metal-carbon laminate and method of producing it

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL447527A PL248599B1 (en) 2024-01-17 2024-01-17 Metal-carbon laminate and method of producing it

Publications (2)

Publication Number Publication Date
PL447527A1 true PL447527A1 (en) 2024-08-12
PL248599B1 PL248599B1 (en) 2026-01-05

Family

ID=92264384

Family Applications (1)

Application Number Title Priority Date Filing Date
PL447527A PL248599B1 (en) 2024-01-17 2024-01-17 Metal-carbon laminate and method of producing it

Country Status (1)

Country Link
PL (1) PL248599B1 (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
PL248599B1 (en) 2026-01-05

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