KR20140030224A - 등방성을 유지한 성형체의 제조 방법 - Google Patents
등방성을 유지한 성형체의 제조 방법 Download PDFInfo
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Abstract
Description
도 2는 실시예 2에서 사용한 입체 형상의 금형의 모식도이다.
도 3은 실시예 1 및 3에서 얻어진 성형품의 모식도(사시도)이다.
도 4는 실시예 2에 있어서의 금형에의 기재 배치의 모식도이다.
도 5는 실시예 2에서 얻어진 성형품의 모식도(사시도)이다.
도 6은 실시예 4에 있어서의 금형에의 기재 배치의 모식도이다.
도 7은 실시예 4에서 얻어진 성형품의 모식도(사시도)이다.
도 8은 금형의 단부(端部) 구조의 설명도이다.
도 9는 실시예 11에 있어서의 금형에의 기재 배치의 모식도이다.
2 금형 캐비티
3 금형 캐비티 엣지부
4 금형 캐비티 총면적
5 기재(프리프레그) 충전부
6 유동부
7 Vf의 계측점
8 인장 탄성율 계측점
9 보스형상부
10 리브형상부
11 금형 단부(端部)의 빼기구배(draft angle)
12 금형의 클리어런스
13 프리프레그의 오버랩부
Claims (10)
- 섬유강화 복합재료로 이루어지는 성형체의 제조 방법으로서,
1) 평균 섬유 길이 5∼100㎜의 강화섬유와 열가소성 수지를 포함하는 랜덤 매트를, 열가소성 수지가 결정성인 경우는 융점 이상, 열분해 온도 미만의 온도까지, 비결정성인 경우는 유리 전이 온도 이상, 열분해 온도 미만의 온도까지 가열하는 것에 의해 열가소성 수지를 함침시켜 프리프레그를 얻는 프리프레그 제작 공정과,
2) 열가소성 수지가 결정성인 경우는 융점 이상, 열분해 온도 미만의 온도, 비결정성인 경우는 유리 전이 온도 이상, 열분해 온도 미만의 온도로 한 상기 프리프레그를, 열가소성 수지가 결정성인 경우에는 융점 온도 미만, 비결정성인 경우에는 유리 전이 온도 미만이 되도록 온도 조절된 금형에, 아래 식 (3)으로 나타내는 충전율이 50% 이상 100% 이하가 되도록 배치하는 프리프레그 배치 공정과,
3) 상기 금형 내에서, 상기 프리프레그를 가압함과 아울러, 열가소성 수지가 결정성인 경우는 융점 미만, 비결정성인 경우는 유리 전이 온도 미만의 온도로 성형을 완결시켜 성형체를 얻는 성형 공정을 포함하고,
상기 랜덤 매트는, 25∼10000g/㎡의 단위면적당 중량으로 상기 강화섬유가 실질적으로 2차원 랜덤하게 배향되어 있고,
식 (1)에서 정의되는 임계 단사 수 이상으로 구성되는 강화섬유 다발(A)이, 상기 랜덤 매트에 있어서의 섬유 전량에 대해 20Vol% 이상 99Vol% 미만 포함되어 있고,
또한, 상기 강화섬유 다발(A)에 있어서의 평균 섬유 수(N)가, 아래 식 (2)을 만족하는 것을 특징으로 하는, 섬유강화 복합재료로 이루어지는 성형체의 제조 방법.
임계 단사 수 = 600/D (1)
0.7×104/D2 < N < 1×105/D2 (2)
(식 (1) 및 식 (2) 중, D는 강화섬유의 평균 섬유 지름(㎛)이다)
충전율(%) = 100×[기재 면적(㎟)/금형 캐비티 투영 면적(㎟)] (3)
(식 (3) 중, 기재 면적이란 배치된 모든 프리프레그를 빠짐 방향에의 투영 면적이며, 금형 캐비티 투영 면적이란 빠짐 방향에의 투영 면적이다)
- 제1항에 있어서,
상기 랜덤 매트에 있어서의 열가소성 수지의 함유량은, 상기 강화섬유 100 질량부에 대해 50∼1000 질량부인 성형체의 제조 방법.
- 제1항 또는 제2항에 있어서,
상기 프리프레그 배치 공정에서, 상기 금형의 온도를, 열가소성 수지가 결정성인 경우는 융점-200℃ 이상, 융점-10℃ 이하, 비결정성인 경우는 유리 전이 온도-200℃ 이상, 유리 전이 온도-10℃ 이하로 온도 조절하는 성형체의 제조 방법.
- 제1항 내지 제3항 중 어느 한 항에 있어서,
상기 프리프레그 배치 공정에서, 상기 프리프레그를, 아래 식 (4)으로 나타내는 총면적 충전율이 30% 이상 100% 이하가 되도록 배치하는 성형체의 제조 방법.
총면적 충전율(%) = 100×[기재 총면적(㎟)/금형 캐비티 총면적(㎟)] (4)
(식 (4) 중, 기재 총면적이란, 수평 전개한 모든 프리프레그의 투영 면적에서부터, 적층 및 오버랩부의 면적을 뺀 면적이며, 금형 캐비티 총면적이란, 금형 캐비티 표면의 면적의 합이다)
- 제1항 내지 제4항 중 어느 한 항에 있어서,
상기 프리프레그 배치 공정에서, 복수매의 프리프레그의 단부를 오버랩시키는 성형체의 제조 방법.
- 제1항 내지 제5항 중 어느 한 항에 있어서,
상기 강화섬유의 평균 섬유 길이는, 10∼30㎜인 성형체의 제조 방법.
- 제1항 내지 제6항 중 어느 한 항에 있어서,
상기 금형은, 단부(端部)의 클리어런스가 0.01∼0.1㎜이며, 밀폐하는 것이 가능한 것인 성형체의 제조 방법.
- 제1항 내지 제7항 중 어느 한 항에 있어서,
상기 프리프레그의 보이드율이, 0∼30%인 성형체의 제조 방법.
- 제1항 내지 제8항 중 어느 한 항에 있어서,
상기 성형 공정에서, 프리프레그를 가압하는 압력을 3㎫∼100㎫로 하는 성형체의 제조 방법.
- 제1항 내지 제9항 중 어느 한 항에 기재된 제조 방법에 의해 얻어지는 성형체로서,
임의의 방향에 대한 인장 탄성율 및 이와 직교하는 방향에 대한 인장 탄성율에 대해, 큰 쪽의 값을 작은 쪽의 값으로 나눈 비(Eδ)가 1.0 내지 1.3인 성형체.
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| PCT/JP2012/063731 WO2012165418A1 (ja) | 2011-05-31 | 2012-05-29 | 等方性を維持した成形体の製造方法 |
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| EP (1) | EP2716433B1 (ko) |
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| Publication number | Publication date |
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| JPWO2012165418A1 (ja) | 2015-02-23 |
| RU2553299C1 (ru) | 2015-06-10 |
| WO2012165418A1 (ja) | 2012-12-06 |
| CN103582556A (zh) | 2014-02-12 |
| BR112013030891A2 (pt) | 2016-12-06 |
| EP2716433A1 (en) | 2014-04-09 |
| EP2716433A4 (en) | 2014-11-26 |
| JP5606622B2 (ja) | 2014-10-15 |
| US20150064408A1 (en) | 2015-03-05 |
| JP2014205354A (ja) | 2014-10-30 |
| US20140077412A1 (en) | 2014-03-20 |
| US8900502B2 (en) | 2014-12-02 |
| MX2013013507A (es) | 2014-02-27 |
| EP2716433B1 (en) | 2018-04-18 |
| US10006677B2 (en) | 2018-06-26 |
| CN103582556B (zh) | 2016-03-02 |
| KR101452677B1 (ko) | 2014-10-22 |
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