PL447528A1 - Metal-carbon laminate and its producing method - Google Patents
Metal-carbon laminate and its producing methodInfo
- Publication number
- PL447528A1 PL447528A1 PL447528A PL44752824A PL447528A1 PL 447528 A1 PL447528 A1 PL 447528A1 PL 447528 A PL447528 A PL 447528A PL 44752824 A PL44752824 A PL 44752824A PL 447528 A1 PL447528 A1 PL 447528A1
- Authority
- PL
- Poland
- Prior art keywords
- thickness
- self
- carbon
- weight
- thick
- Prior art date
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
- 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
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
-
- 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
-
- 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
-
- 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
-
- 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
-
- 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 włókniny poliestrowej (1) o gramaturze 339 g/m<sup>2</sup> i o grubości od 4 mm do 8 mm, do której obu powierzchni przylega adhezyjnie warstwa samonaprawiająca się pierwsza (2) o grubości od 1 mm do 2 mm, składająca się z włókien szklanych wypełnionych diizocyjanianem izoforonu i połączonych żywicą termoplastyczną. Warstwa samonaprawiająca się pierwsza (2) przylega adhezyjnie do dwóch warstw 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 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 też 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.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 a first self-healing layer (2) with a thickness of 1 mm to 2 mm, consisting of glass fibres filled with isophorone diisocyanate and bonded with a thermoplastic resin, is adhered by adhesive means. The first self-healing layer (2) is adhesively adhered to two layers of a carbon fiber-based thermoplastic composite (3) each 0.04 mm thick, which are adhesively adhered to a second self-healing layer (4) 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 application also covers a method of producing a metal-carbon laminate, which consists in applying on both sides to 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. Two layers of a thermoplastic composite based on carbon fibres (3), 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 thickness and a second self-healing layer (4) of 0.2 mm to 0.4 mm thickness.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL447528A PL248600B1 (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 |
|---|---|---|---|
| PL447528A PL248600B1 (en) | 2024-01-17 | 2024-01-17 | Metal-carbon laminate and method of producing it |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| PL447528A1 true PL447528A1 (en) | 2024-08-12 |
| PL248600B1 PL248600B1 (en) | 2026-01-05 |
Family
ID=92264408
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL447528A PL248600B1 (en) | 2024-01-17 | 2024-01-17 | Metal-carbon laminate and method of producing it |
Country Status (1)
| Country | Link |
|---|---|
| PL (1) | PL248600B1 (en) |
Citations (4)
| 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 |
-
2024
- 2024-01-17 PL PL447528A patent/PL248600B1/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 | 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)
| 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 |
|---|---|
| PL248600B1 (en) | 2026-01-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| PL447525A1 (en) | Metal-glass laminate and method of producing it | |
| PL447530A1 (en) | Metal-carbon laminate and its producing method | |
| PL441554A1 (en) | Aluminum-glass laminate and method of its production | |
| JP5898769B2 (en) | Elastic floor finish | |
| KR970701626A (en) | CUSHION-BACKED CARPET | |
| PL437402A1 (en) | Titanium-glass-carbon laminate and its producing method | |
| CN103108752A (en) | Solvent-free lamination adhesive for flexible packaging laminates and laminated structures prepared therefrom | |
| JP2013506575A (en) | Open cell rigid foam composites | |
| PL441552A1 (en) | Aluminum-glass laminate and method of its production | |
| JP4296763B2 (en) | Substrate coating method, substrate, coating apparatus, laminate manufacturing method and laminate | |
| KR100497727B1 (en) | Surface sheet and sandwich structure using the same | |
| PL447528A1 (en) | Metal-carbon laminate and its producing method | |
| PL447527A1 (en) | Metal-carbon laminate and its producing method | |
| PL447523A1 (en) | Metal-glass laminate and method of producing it | |
| PL447531A1 (en) | Metal-carbon-glass laminate and its producing method | |
| PL447524A1 (en) | Metal-glass laminate and method of producing it | |
| PL447526A1 (en) | Metal-glass-carbon laminate and its producing method | |
| PL447529A1 (en) | Metal-carbon laminate and its producing method | |
| PL447522A1 (en) | Metal-glass laminate and method of producing it | |
| US9616257B2 (en) | Multi-layer chemical and biological protection fabric for mobile shelters | |
| PL451053A1 (en) | Self-healing laminate and method for its production | |
| PL451052A1 (en) | Self-healing laminate and method for its production | |
| PL451051A1 (en) | Self-healing laminate and method for its production | |
| PL451055A1 (en) | Self-healing laminate and method for its production | |
| PL451054A1 (en) | Self-healing laminate and method of producing it |