RU2019100991A - Препрег и способ его производства - Google Patents
Препрег и способ его производства Download PDFInfo
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- RU2019100991A RU2019100991A RU2019100991A RU2019100991A RU2019100991A RU 2019100991 A RU2019100991 A RU 2019100991A RU 2019100991 A RU2019100991 A RU 2019100991A RU 2019100991 A RU2019100991 A RU 2019100991A RU 2019100991 A RU2019100991 A RU 2019100991A
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- RU
- Russia
- Prior art keywords
- prepreg
- resin
- coefficient
- temperature
- thermosetting resin
- Prior art date
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- 238000004519 manufacturing process Methods 0.000 title claims 2
- 238000000034 method Methods 0.000 title claims 2
- 229920005989 resin Polymers 0.000 claims 16
- 239000011347 resin Substances 0.000 claims 16
- 239000010410 layer Substances 0.000 claims 14
- 239000011229 interlayer Substances 0.000 claims 9
- 229920001187 thermosetting polymer Polymers 0.000 claims 9
- 239000000835 fiber Substances 0.000 claims 6
- 229920000049 Carbon (fiber) Polymers 0.000 claims 5
- 239000004917 carbon fiber Substances 0.000 claims 5
- 229920005992 thermoplastic resin Polymers 0.000 claims 5
- 239000007787 solid Substances 0.000 claims 2
- 230000004888 barrier function Effects 0.000 claims 1
- 239000002245 particle Substances 0.000 claims 1
- 238000003825 pressing Methods 0.000 claims 1
Classifications
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- B32B5/02—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 structural features of a fibrous or filamentary layer
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- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/12—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat
- B29C70/14—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of short length, e.g. in the form of a mat oriented
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- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
- B29C70/205—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration
- B29C70/207—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration arranged in parallel planes of fibres crossing at substantial angles
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- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Textile Engineering (AREA)
- Inorganic Chemistry (AREA)
- Reinforced Plastic Materials (AREA)
Claims (14)
1. Препрег, включающий
слой волокна, содержащий однонаправленно скомпонованные дискретные углеродные волокна и термоотверждающуюся смолу; и
слой смолы, присутствующий на, по меньшей мере, одной стороне упомянутого слоя волокна и содержащий термоотверждающуюся смолу и термопластичную смолу;
где упомянутый препрег содержит углеродные волокна, характеризующиеся поверхностной массой волокон в диапазоне от 120 до 300 г/м2, и характеризуется массовой долей смолы в диапазоне от 25 до 50% по отношению к полной массе упомянутого препрега; и
где температура, при которой коэффициент межслоевого трения составляет 0,05 и менее, находится в температурном диапазоне от 40 до 80°С, при этом коэффициент межслоевого трения обуславливается контактной поверхностью раздела между слоями упомянутого препрега при вытягивании среднего слоя из трех слоев, каждый из которых изготовлен из упомянутого препрега и уложен, причем упомянутый коэффициент межслоевого трения измеряют с интервалами в 10°С в температурном диапазоне от 40°С до 80°С в условиях, включающих скорость вытягивания 0,2 мм/мин, перпендикулярное напряжение 0,08 МПа и длину вытягивания 1 мм.
2. Препрег по п. 1, где упомянутый слой смолы содержит твердую термопластичную смолу, растворимую в термоотверждающейся смоле.
3. Препрег по п. 2, где упомянутая твердая термопластичная смола, растворимая в упомянутой термоотверждающейся смоле, имеет форму частиц.
4. Препрег по любому из пп. 1-3, где упомянутый слой смолы содержит термопластичную смолу, нерастворимую в упомянутой термоотверждающейся смоле.
5. Препрег по п. 4, где упомянутая термопластичная смола, нерастворимая в упомянутой термоотверждающейся смоле, имеет форму частиц.
6. Препрег по любому из пп. 1-5, где при измерении упомянутого коэффициента межслоевого трения температурная область, в которой упомянутый коэффициент межслоевого трения составляет 0,05 и менее, существует в виде температурной области, имеющей в ширину 20°С и более.
7. Препрег по любому из пп. 1-6, где при измерении упомянутого коэффициента межслоевого трения температура, при которой степень увеличения упомянутого коэффициента межслоевого трения при длине вытягивания 2 мм по отношению к упомянутому коэффициенту межслоевого трения при длине вытягивания 1 мм заключена в пределах 40%, находится в диапазоне от температуры, на 10°С меньшей, до температуры, на 10°С большей, чем температура, при которой упомянутый коэффициент межслоевого трения является наименьшим при длине вытягивания 1 мм.
8. Препрег по любому из пп. 1-7, где листы упомянутого препрега, которые подвергают квазиизотропной укладке и прессованию, характеризуются пределом прочности при сжатии после удара, составляющим 250 МПа и более, согласно измерению в соответствии с ASTM D7137/7137M-07.
9. Препрег по любому из пп. 1-8, где на границе между упомянутым слоем смолы и упомянутым слоем волокна присутствует барьерный слой, образованный из смолы, вязкость которой является большей, чем вязкость упомянутой термоотверждающейся смолы в упомянутом слое смолы в температурной области от 40°С до 80°С.
10. Способ производства упомянутого препрега по любому из пп. 1-9, включающий стадию формования слоя волокна, содержащего однонаправленно скомпонованные дискретные углеродные волокна и термоотверждающуюся смолу, посредством введения рассечений в однонаправленно скомпонованные непрерывные углеродные волокна в слое волокна, содержащем упомянутые однонаправленно скомпонованные непрерывные углеродные волокна и упомянутую термоотверждающуюся смолу.
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| US10921859B2 (en) * | 2017-04-10 | 2021-02-16 | Securaplane Technologies, Inc. | Composite electronics cases and methods of making and using the same |
| EP3835343A4 (en) * | 2018-09-18 | 2022-05-25 | Toray Industries, Inc. | PREPREG, PREPREG LAMINATE AND FIBER REINFORCED COMPOSITE |
| WO2020235486A1 (ja) * | 2019-05-23 | 2020-11-26 | 東レ株式会社 | プリプレグ、積層体および成形品 |
| JP7521182B2 (ja) * | 2019-09-24 | 2024-07-24 | 株式会社明電舎 | 覆い部材 |
| WO2021117465A1 (ja) * | 2019-12-11 | 2021-06-17 | 東レ株式会社 | プリプレグ、積層体および一体化成形品 |
| CN111453523A (zh) * | 2020-04-28 | 2020-07-28 | 山东省东平县华东纸业有限责任公司 | 韧性强度优良的三层抽纸及其制备方法 |
| WO2022075265A1 (ja) * | 2020-10-06 | 2022-04-14 | 倉敷紡績株式会社 | 繊維補強樹脂引抜成形体及びその製造方法 |
| JP7577965B2 (ja) * | 2020-10-15 | 2024-11-06 | 東レ株式会社 | トウプレグ、および繊維強化複合材料 |
| WO2022145005A1 (ja) * | 2020-12-28 | 2022-07-07 | 三菱重工業株式会社 | 繊維強化シート積層体並びに繊維強化シート積層体の製造方法及び構造体の製造方法 |
| CN113561519B (zh) * | 2021-09-26 | 2021-12-28 | 昌亚新材料科技有限公司 | 纤维增韧的多层塑料型材及其制备方法、可降解食物餐盒 |
| JP2023049610A (ja) * | 2021-09-29 | 2023-04-10 | 三菱ケミカル株式会社 | フィルム付きプリプレグ、およびフィルム付きプリプレグの製造方法 |
| WO2024204522A1 (ja) * | 2023-03-30 | 2024-10-03 | 東レ株式会社 | 離型シ-ト付き樹脂フィルム |
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| US5772950A (en) | 1994-08-31 | 1998-06-30 | The Boeing Company | Method of vacuum forming a composite |
| JP4671890B2 (ja) * | 1996-12-18 | 2011-04-20 | 東レ株式会社 | プリプレグ |
| JP2003026768A (ja) * | 2001-07-13 | 2003-01-29 | Toray Ind Inc | エポキシ樹脂組成物、プリプレグおよび繊維強化複合材料 |
| JP2007217665A (ja) * | 2006-01-19 | 2007-08-30 | Toray Ind Inc | プリプレグおよび炭素繊維強化複合材料 |
| TWI447009B (zh) * | 2006-09-28 | 2014-08-01 | 東麗股份有限公司 | 複合預浸漬基材之製法、積層基材及纖維強化塑膠 |
| EP2134764B1 (en) * | 2007-04-17 | 2013-02-13 | Hexcel Corporation | Composite material with blend of thermoplastic particles |
| US8686069B2 (en) * | 2010-10-12 | 2014-04-01 | Hexcel Corporation | Solvent resistance of epoxy resins toughened with polyethersulfone |
| JP5900327B2 (ja) * | 2011-03-17 | 2016-04-06 | 東レ株式会社 | プリプレグ、プリプレグの製造方法および炭素繊維強化複合材料の製造方法 |
| US9187636B2 (en) * | 2012-08-26 | 2015-11-17 | Hexcel Corporation | Composite material with polyamide particle mixtures |
| US9200125B2 (en) * | 2012-08-26 | 2015-12-01 | Hexcel Corporation | Composite material with polyamide particles |
| JP5967323B1 (ja) * | 2015-01-07 | 2016-08-10 | 東レ株式会社 | プリプレグ |
| WO2017110991A1 (ja) * | 2015-12-25 | 2017-06-29 | 東レ株式会社 | プリプレグおよびその製造方法 |
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| JPWO2018003694A1 (ja) | 2019-04-18 |
| EP3476886A1 (en) | 2019-05-01 |
| EP3476886A4 (en) | 2020-01-08 |
| JP7003662B2 (ja) | 2022-02-10 |
| TW201819489A (zh) | 2018-06-01 |
| AU2017287341A1 (en) | 2018-10-25 |
| TWI723188B (zh) | 2021-04-01 |
| CA3020078C (en) | 2024-01-16 |
| KR102309912B1 (ko) | 2021-10-07 |
| CN109196026B (zh) | 2021-04-23 |
| CA3020078A1 (en) | 2018-01-04 |
| WO2018003694A1 (ja) | 2018-01-04 |
| BR112018071500A2 (pt) | 2019-02-19 |
| CN109196026A (zh) | 2019-01-11 |
| US20190210301A1 (en) | 2019-07-11 |
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