JP2013528245A5 - - Google Patents

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JP2013528245A5
JP2013528245A5 JP2013514145A JP2013514145A JP2013528245A5 JP 2013528245 A5 JP2013528245 A5 JP 2013528245A5 JP 2013514145 A JP2013514145 A JP 2013514145A JP 2013514145 A JP2013514145 A JP 2013514145A JP 2013528245 A5 JP2013528245 A5 JP 2013528245A5
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resin composition
component
composite structure
fibrous material
matrix resin
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Priority claimed from PCT/US2010/038377 external-priority patent/WO2011155947A1/en
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本発明による複合構造およびオーバーオールド成形された複合構造(E1〜E2)は、耐クリープ性の改善が示されただけでなく、機械的性質、特に曲げ弾性率の大きな改善が示された。これら両方が、使用および経時による物品の耐久性および安全性に寄与する。
以下に、本発明の好ましい態様を示す。
[1] 表面を有する複合材料であって、前記複合材料は、不織構造、布地、繊維バット、およびそれらの組み合わせから選択される繊維状材料を含み、前記繊維状材料はマトリックス樹脂組成物で含浸され、前記表面は表面樹脂組成物でできた少なくとも一部を有し、
前記表面樹脂組成物および前記マトリックス樹脂組成物は、同一または異なるものであり、および
前記表面樹脂組成物および前記マトリックス樹脂組成物は、a)ポリエステル、ポリアミド、およびそれらの混合物から選択される1種または複数種の熱可塑性樹脂と;b)0.5または約0.5〜6.0または約6.0重量%のナノクレイとを含む熱可塑性組成物から選択され、
前記重量パーセントは前記熱可塑性組成物の全重量を基準する
ことを特徴とする複合構造。
[2] 前記繊維状材料が、ガラス繊維、炭素繊維、アラミド繊維、天然繊維、またはそれらの混合物で作成されていることを特徴とする[1]に記載の複合構造。
[3] 前記繊維状材料がガラス繊維で作成されていることを特徴とする[2]に記載の複合構造。
[4] 前記ナノクレイがセピオライト型クレイであることを特徴とする[1]から[3]のいずれかに記載の複合構造。
[5] 前記熱可塑性組成物がa)1種または複数種のポリエステルを含むことを特徴とする[1]から[4]のいずれかに記載の複合構造。
[6] 前記1種または複数種のポリエステルが、ポリ(エチレンテレフタレート)(PET)、ポリ(トリメチレンテレフタレート)(PTT)、ポリ(1,4−ブチレンテレフタレート)(PBT)、ポリ(エチレン2,6−ナフトエート)(PEN)、ポリ(1,4−シクロヘキシルジメチレンテレフタレート)(PCT)、ならびにそれらのコポリマーおよびブレンドから選択されることを特徴とする[5]に記載の複合構造。
[7] 前記熱可塑性組成物が、a)完全脂肪族ポリアミド、半芳香族ポリアミド、およびそれらのブレンドから選択される1種または複数種のポリアミドを含むことを特徴とする[1]から[4]のいずれかに記載の複合構造。
[8] 前記1種または複数種のポリアミドが半芳香族ポリアミドから選択されることを特徴とする[7]に記載の複合構造。
[9] 前記マトリックス樹脂組成物および/または前記表面樹脂組成物が、1種または複数種の衝撃改質剤、1種または複数種の熱安定剤、1種または複数種の酸化安定剤、補強剤、1種または複数種の紫外光安定剤、1種または複数種の難燃剤、またはそれらの混合物をさらに含むことを特徴とする[1]から[8]のいずれかに記載の複合構造。
[10] 前記マトリックス樹脂組成物および/または前記表面樹脂が、超分岐ポリエステルデンドリマーから選択される溶融レオロジー改質剤をさらに含むことを特徴とする[1]から[9]のいずれかに記載の複合構造。
[11] シート構造の形態にあることを特徴とする[1]から[10]のいずれかに記載の複合構造。
[12] 自動車、トラック、民間航空機、航空宇宙産業、鉄道、家庭用品、コンピュータハードウェア、携帯型デバイス、娯楽、およびスポーツの構成材料、機械の構造用部品、建造物の構造用部品、光起電力設備の構造用部品、または機械装置の構造用部品の形態にあることを特徴とする[1]から[11]のいずれかに記載の複合構造。
[13] 表面を有する複合構造の製造方法であって:
[1]、[4]〜[10]のいずれかに記載のマトリックス樹脂組成物を、[1]〜[3]のいずれか一項に記載の繊維状材料に含浸させる工程を含み、前記複合構造の表面の少なくとも一部が、[1]または[4]〜[10]のいずれかに記載の表面樹脂組成物で作成されることを特徴とする方法。
[14] オーバーモールド成形された複合構造であって:
i)表面を有する第1の構成要素であって、前記第1の構成要素は不織構造、布地、繊維バット、およびそれらの組み合わせから選択される繊維状材料を含み、前記繊維状材料にはマトリックス樹脂組成物が含浸され、前記表面は表面樹脂組成物でできた少なくとも一部を有する、第1の構成要素と、
ii)1種または複数種の熱可塑性樹脂を含むオーバーモールド成形用樹脂組成物を含む第2の構成要素と
を含み、
前記表面樹脂組成物および前記マトリックス樹脂組成物は、同一または異なるものであって、[1]または[4]〜[10]のいずれかに記載の熱可塑性組成物から選択され、
前記第1の構成要素の前記表面の少なくとも一部の上で、前記第2の構成要素が前記第1の構成要素に接着される
ことを特徴とするオーバーモールド成形された複合構造。
[15] 自動車、トラック、民間航空機、航空宇宙産業、鉄道、家庭用品、コンピュータハードウェア、携帯型デバイス、娯楽、およびスポーツの構成材料、機械の構造用部品、建造物の構造用部品、光起電力設備の構造用部品、または機械装置の構造用部品の形態にあることを特徴とする[14]に記載のオーバーモールド成形された複合構造。
The composite structure according to the present invention and the overmolded composite structure (E1 to E2) showed not only an improvement in creep resistance but also a great improvement in mechanical properties, in particular the flexural modulus. Both of these contribute to the durability and safety of the article over time and use.
Below, the preferable aspect of this invention is shown.
[1] A composite material having a surface, wherein the composite material includes a fibrous material selected from a non-woven structure, a fabric, a fiber vat, and a combination thereof, and the fibrous material is a matrix resin composition. Impregnated, the surface has at least a portion made of a surface resin composition;
The surface resin composition and the matrix resin composition are the same or different, and the surface resin composition and the matrix resin composition are selected from a) polyester, polyamide, and mixtures thereof Or a thermoplastic composition comprising a plurality of thermoplastic resins; and b) 0.5 or about 0.5 to 6.0 or about 6.0 wt% nanoclay,
The composite structure, wherein the weight percent is based on the total weight of the thermoplastic composition.
[2] The composite structure according to [1], wherein the fibrous material is made of glass fiber, carbon fiber, aramid fiber, natural fiber, or a mixture thereof.
[3] The composite structure according to [2], wherein the fibrous material is made of glass fiber.
[4] The composite structure according to any one of [1] to [3], wherein the nanoclay is a sepiolite type clay.
[5] The composite structure according to any one of [1] to [4], wherein the thermoplastic composition includes a) one or more kinds of polyesters.
[6] The one or more polyesters are poly (ethylene terephthalate) (PET), poly (trimethylene terephthalate) (PTT), poly (1,4-butylene terephthalate) (PBT), poly (ethylene 2, The composite structure according to [5], characterized in that it is selected from 6-naphthoate) (PEN), poly (1,4-cyclohexyldimethylene terephthalate) (PCT), and copolymers and blends thereof.
[7] The thermoplastic composition includes [1] to [4], wherein the thermoplastic composition includes one or more polyamides selected from a) fully aliphatic polyamides, semi-aromatic polyamides, and blends thereof. ] The composite structure in any one of.
[8] The composite structure according to [7], wherein the one or more polyamides are selected from semi-aromatic polyamides.
[9] The matrix resin composition and / or the surface resin composition includes one or more types of impact modifiers, one or more types of thermal stabilizers, one or more types of oxidation stabilizers, and reinforcement. The composite structure according to any one of [1] to [8], further comprising an agent, one or more ultraviolet light stabilizers, one or more flame retardants, or a mixture thereof.
[10] The matrix resin composition and / or the surface resin further includes a melt rheology modifier selected from hyperbranched polyester dendrimers, according to any one of [1] to [9] Composite structure.
[11] The composite structure according to any one of [1] to [10], which is in the form of a sheet structure.
[12] automobiles, trucks, civil aircraft, aerospace industry, railways, household goods, computer hardware, portable devices, entertainment and sports components, mechanical structural parts, building structural parts, photovoltaics The composite structure according to any one of [1] to [11], wherein the composite structure is in the form of a structural component for electric power equipment or a structural component for mechanical equipment.
[13] A method for producing a composite structure having a surface comprising:
Including impregnating the fibrous material according to any one of [1] to [3] with the matrix resin composition according to any one of [1] and [4] to [10], A method wherein at least a part of the surface of the structure is made of the surface resin composition according to any one of [1] or [4] to [10].
[14] An overmolded composite structure comprising:
i) a first component having a surface, the first component comprising a fibrous material selected from a nonwoven structure, a fabric, a fiber vat, and combinations thereof, wherein the fibrous material includes A first component impregnated with a matrix resin composition, the surface having at least a portion made of a surface resin composition;
ii) a second component comprising an overmolding resin composition comprising one or more thermoplastic resins;
The surface resin composition and the matrix resin composition are the same or different and are selected from the thermoplastic compositions according to any one of [1] or [4] to [10],
An overmolded composite structure wherein the second component is adhered to the first component over at least a portion of the surface of the first component.
[15] Automobiles, trucks, civil aircraft, aerospace industry, railways, household goods, computer hardware, portable devices, entertainment and sports components, mechanical structural parts, building structural parts, photovoltaics The overmolded composite structure according to [14], which is in the form of a structural component for electric power equipment or a structural component for mechanical equipment.

Claims (3)

表面を有する複合材料であって、前記複合材料は、不織構造、布地、繊維バット、およびそれらの組み合わせから選択される繊維状材料を含み、前記繊維状材料はマトリックス樹脂組成物で含浸され、前記表面は表面樹脂組成物でできた少なくとも一部を有し、
前記表面樹脂組成物および前記マトリックス樹脂組成物は、同一または異なるものであり、および
前記表面樹脂組成物および前記マトリックス樹脂組成物は、a)ポリエステル、ポリアミド、およびそれらの混合物から選択される1種または複数種の熱可塑性樹脂と;b)0.5または約0.5〜6.0または約6.0重量%のナノクレイとを含む熱可塑性組成物から選択され、
前記重量パーセントは前記熱可塑性組成物の全重量を基準する
ことを特徴とする複合構造。
A composite material having a surface, the composite material comprising a fibrous material selected from non-woven structures, fabrics, fiber vats, and combinations thereof, wherein the fibrous material is impregnated with a matrix resin composition; The surface has at least a portion made of a surface resin composition;
The surface resin composition and the matrix resin composition are the same or different, and the surface resin composition and the matrix resin composition are selected from a) polyester, polyamide, and mixtures thereof Or a thermoplastic composition comprising a plurality of thermoplastic resins; and b) 0.5 or about 0.5 to 6.0 or about 6.0 wt% nanoclay,
Composite structure wherein the weight percent, characterized in that based on the total weight of the thermoplastic composition.
表面を有する複合構造の製造方法であって:
マトリックス樹脂組成物を、繊維状材料に含浸させる工程を含み、前記複合構造の表面の少なくとも一部が、表面樹脂組成物で作成され、
前記表面樹脂組成物および前記マトリックス樹脂組成物は、同一または異なるものであって、a)ポリエステル、ポリアミド、およびそれらの混合物から選択される1種または複数種の熱可塑性樹脂と;b)0.5または約0.5〜6.0または約6.0重量%のナノクレイとを含む熱可塑性組成物から選択され、
前記重量パーセントは前記熱可塑性組成物の全重量を基準とし、
前記繊維状材料は、不織構造、布地、繊維バット、およびそれらの組み合わせから選択される
ことを特徴とする方法。
A method for producing a composite structure having a surface comprising:
Including impregnating a fibrous material with a matrix resin composition, wherein at least a portion of the surface of the composite structure is made of the surface resin composition;
The surface resin composition and the matrix resin composition are the same or different, and a) one or more thermoplastic resins selected from polyesters, polyamides, and mixtures thereof; and b) 0. Selected from 5 or about 0.5 to 6.0 or about 6.0% by weight of nanoclay;
The weight percent is based on the total weight of the thermoplastic composition;
The method wherein the fibrous material is selected from non-woven structures, fabrics, fiber batts, and combinations thereof .
オーバーモールド成形された複合構造であって:
i)表面を有する第1の構成要素であって、前記第1の構成要素は不織構造、布地、繊維バット、およびそれらの組み合わせから選択される繊維状材料を含み、前記繊維状材料にはマトリックス樹脂組成物が含浸され、前記表面は表面樹脂組成物でできた少なくとも一部を有する、第1の構成要素と、
ii)1種または複数種の熱可塑性樹脂を含むオーバーモールド成形用樹脂組成物を含む第2の構成要素と
を含み、
前記表面樹脂組成物および前記マトリックス樹脂組成物は、同一または異なるものであって、a)ポリエステル、ポリアミド、およびそれらの混合物から選択される1種または複数種の熱可塑性樹脂と;b)0.5または約0.5〜6.0または約6.0重量%のナノクレイとを含む熱可塑性組成物から選択され、
前記重量パーセントは前記熱可塑性組成物の全重量を基準とし、
前記第1の構成要素の前記表面の少なくとも一部の上で、前記第2の構成要素が前記第1の構成要素に接着される
ことを特徴とするオーバーモールド成形された複合構造。
Overmolded composite structure:
i) a first component having a surface, the first component comprising a fibrous material selected from a nonwoven structure, a fabric, a fiber vat, and combinations thereof, wherein the fibrous material includes A first component impregnated with a matrix resin composition, the surface having at least a portion made of a surface resin composition;
ii) a second component comprising an overmolding resin composition comprising one or more thermoplastic resins;
The surface resin composition and the matrix resin composition are the same or different, and a) one or more thermoplastic resins selected from polyesters, polyamides, and mixtures thereof; and b) 0. Selected from 5 or about 0.5 to 6.0 or about 6.0% by weight of nanoclay ;
The weight percent is based on the total weight of the thermoplastic composition;
An overmolded composite structure wherein the second component is adhered to the first component over at least a portion of the surface of the first component.
JP2013514145A 2010-06-11 2010-06-11 Creep-resistant composite structures and methods for their production Withdrawn JP2013528245A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2010/038377 WO2011155947A1 (en) 2010-06-11 2010-06-11 Creep-resistant composite structures and processes for their preparation

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JP2013528245A JP2013528245A (en) 2013-07-08
JP2013528245A5 true JP2013528245A5 (en) 2013-08-15

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EP (1) EP2580267A1 (en)
JP (1) JP2013528245A (en)
KR (1) KR20130118856A (en)
CN (1) CN102933640A (en)
BR (1) BR112012028645A2 (en)
CA (1) CA2799250A1 (en)
MX (1) MX2012014263A (en)
RU (1) RU2013101001A (en)
WO (1) WO2011155947A1 (en)

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KR102106548B1 (en) * 2018-12-12 2020-05-04 주식회사 세프라 Olefin elastomer composite resin composition for airbag chute containing dendrimer

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