PL447529A1 - Metal-carbon laminate and its producing method - Google Patents
Metal-carbon laminate and its producing methodInfo
- Publication number
- PL447529A1 PL447529A1 PL447529A PL44752924A PL447529A1 PL 447529 A1 PL447529 A1 PL 447529A1 PL 447529 A PL447529 A PL 447529A PL 44752924 A PL44752924 A PL 44752924A PL 447529 A1 PL447529 A1 PL 447529A1
- Authority
- PL
- Poland
- Prior art keywords
- thickness
- layer
- carbon
- weight
- sup
- Prior art date
Links
- 229910052799 carbon Inorganic materials 0.000 title abstract 4
- 238000000034 method Methods 0.000 title abstract 2
- XEKOWRVHYACXOJ-UHFFFAOYSA-N Ethyl acetate Chemical compound CCOC(C)=O XEKOWRVHYACXOJ-UHFFFAOYSA-N 0.000 abstract 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract 4
- 239000002041 carbon nanotube Substances 0.000 abstract 3
- 229910021393 carbon nanotube Inorganic materials 0.000 abstract 3
- 239000003094 microcapsule Substances 0.000 abstract 3
- 239000004745 nonwoven fabric Substances 0.000 abstract 3
- 229920000728 polyester Polymers 0.000 abstract 3
- 229920005992 thermoplastic resin Polymers 0.000 abstract 3
- 239000005058 Isophorone diisocyanate Substances 0.000 abstract 2
- 239000000919 ceramic Substances 0.000 abstract 2
- 239000002131 composite material Substances 0.000 abstract 2
- 239000000945 filler Substances 0.000 abstract 2
- NIMLQBUJDJZYEJ-UHFFFAOYSA-N isophorone diisocyanate Chemical compound CC1(C)CC(N=C=O)CC(C)(CN=C=O)C1 NIMLQBUJDJZYEJ-UHFFFAOYSA-N 0.000 abstract 2
- 229910001000 nickel titanium Inorganic materials 0.000 abstract 2
- 229920000582 polyisocyanurate Polymers 0.000 abstract 2
- 239000011495 polyisocyanurate Substances 0.000 abstract 2
- 239000011527 polyurethane coating Substances 0.000 abstract 2
- 229920001169 thermoplastic Polymers 0.000 abstract 2
- 239000004416 thermosoftening plastic Substances 0.000 abstract 2
- DVKJHBMWWAPEIU-UHFFFAOYSA-N toluene 2,4-diisocyanate Chemical compound CC1=CC=C(N=C=O)C=C1N=C=O DVKJHBMWWAPEIU-UHFFFAOYSA-N 0.000 abstract 2
- UPSFTMARMOEBKQ-UHFFFAOYSA-N 5-isocyanato-1-(isocyanatomethyl)-1,3,3-trimethylcyclohexane;isocyanic acid Chemical compound N=C=O.CC1(C)CC(N=C=O)CC(C)(CN=C=O)C1 UPSFTMARMOEBKQ-UHFFFAOYSA-N 0.000 abstract 1
- 229920000049 Carbon (fiber) Polymers 0.000 abstract 1
- 239000004917 carbon fiber Substances 0.000 abstract 1
- 239000003365 glass fiber Substances 0.000 abstract 1
Classifications
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- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered 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
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- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered 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
- B32B15/08—Layered 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
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- 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
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- 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
- B32B17/00—Layered products essentially comprising sheet glass, or glass, slag, or like fibres
- B32B17/02—Layered products essentially comprising sheet glass, or glass, slag, or like fibres in the form of fibres or filaments
-
- 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
- B32B18/00—Layered products essentially comprising ceramics, e.g. refractory products
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- 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
- B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
- B32B37/10—Methods 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
- B32B37/1018—Methods 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
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- 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
- B32B5/22—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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K9/00—Use of pretreated ingredients
- C08K9/10—Encapsulated ingredients
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- 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
- B32B2250/00—Layers arrangement
- B32B2250/05—5 or more layers
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- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—Fibrous or filamentary layer
- B32B2260/023—Two or more layers
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- 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
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
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- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/762—Self-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, 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 przylega adhezyjnie warstwa włókniny poliestrowej (2) o gramaturze 339 g/m<sup>2</sup> i o grubości od 4 mm do 8 mm. Do warstwy włókniny poliestrowej (2) przylegają adhezyjnie dwie warstwy kompozytu termoplastycznego na bazie włókien węglowych (3) o grubości 0,04 mm każda, które przylegają 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 100m, 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 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. 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 (3) o grubości 0,04 mm każda. Następnie nakłada się warstwę włókniny poliestrowej (2) 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 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 a layer of polyester nonwoven fabric (2) 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 thermoplastic composite based on carbon fibers (3) each 0.04 mm thick are adhesively adhered to the polyester nonwoven fabric layer (2), which are adhesively adhered to a second self-healing layer (4) 0.2 mm to 0.4 mm thick, consisting of microcapsules ranging in size from 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 in an amount of 51.2% by weight and carbon nanotubes ranging in size from 20 nm to 100 nm combined with a thermoplastic resin. The subject of the application is also a method of producing a metal-carbon laminate, which consists in applying on both sides of two sheets (6) of a 1 mm thick nickel-titanium alloy having on both surfaces a ceramic layer (5) of thickness from 5 µm to 12 µm microcapsules of size from 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 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. On one of the sheets (6) of a 1 mm thick nickel-titanium alloy having on both surfaces a ceramic layer (5) of 5 µm to 12 µm thickness and a second self-healing layer (4) of 0.2 mm to 0.4 mm thickness, two layers of a thermoplastic composite based on carbon fibres (3) of 0.04 mm thickness each are applied. Then a layer of polyester non-woven fabric (2) of 339 g/m<sup>2</sup> and 4 mm to 8 mm thickness is applied.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL447529A PL447529A1 (en) | 2024-01-17 | 2024-01-17 | Metal-carbon laminate and its producing method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL447529A PL447529A1 (en) | 2024-01-17 | 2024-01-17 | Metal-carbon laminate and its producing method |
Publications (1)
Publication Number | Publication Date |
---|---|
PL447529A1 true PL447529A1 (en) | 2024-08-12 |
Family
ID=92264403
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL447529A PL447529A1 (en) | 2024-01-17 | 2024-01-17 | Metal-carbon laminate and its producing method |
Country Status (1)
Country | Link |
---|---|
PL (1) | PL447529A1 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101215407A (en) * | 2008-01-18 | 2008-07-09 | 中山大学 | High temperature self-restoring fibre enhancement epoxy composite material and preparation method thereof |
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 |
-
2024
- 2024-01-17 PL PL447529A patent/PL447529A1/en unknown
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101215407A (en) * | 2008-01-18 | 2008-07-09 | 中山大学 | High temperature self-restoring fibre enhancement epoxy composite material and preparation method thereof |
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)
Title |
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TOMASZ SZMECHTYK, NATALIA SIENKIEWICZ: "ELIKSIR nr 11, 2015 rok, str.26-27", „ŻYWICE EPOKSYDOWE JAKO MATERIAŁY SAMONAPRAWIAJĄCE SIĘ" * |
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