CN102941703A - 超级复合材料迭层板 - Google Patents

超级复合材料迭层板 Download PDF

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Publication number
CN102941703A
CN102941703A CN2012104420169A CN201210442016A CN102941703A CN 102941703 A CN102941703 A CN 102941703A CN 2012104420169 A CN2012104420169 A CN 2012104420169A CN 201210442016 A CN201210442016 A CN 201210442016A CN 102941703 A CN102941703 A CN 102941703A
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composite material
super
laminated plate
material laminated
super composite
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CN2012104420169A
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刘君才
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Abstract

本发明是一种大尺寸的超级复合材料迭层板，其由不同材料的(多孔)板材错缝交叉重迭而成，可做成各种大型物体，例如：三体舰船超大甲板，不沉的船壳，水上建筑的大型浮箱，重负荷机翼，楔形大跨度厂房及不用箱梁的桥面等。

Description

超级复合材料迭层板
技术领域
本发明是一种复合材料迭层板，特指一种超级复合材料迭层板。 
背景技术
实用新型200920141580金属复合夹层板，以及其它复合迭层板，虽然它们的强度较高，重量较轻，但它们都难以做成超大面积或超厚的大型物体。 
发明内容
本发明是一种可做大型物体的超级复合材料迭层板。 
其技术方案是，由多层不同材料的(多孔)板材，错缝交叉重迭成大尺寸的超级复合材料迭层板，其优点是，可做大型多体舰船的超大甲板，军民两用的不沉船壳，超长浮桥，水上建筑的大尺寸浮箱，重负荷机翼。甚至可做流线型单壳体潜水艇，楔形大跨度厂房顶，无箱梁的高架桥面等大型物体。其进一步的改进是，用胶粘剂联接各迭层板时，加用膨胀销钉或平头铆钉等紧固件，既方便施工又能提高超级复合材料迭层板抗损坏的性能。 
具体实施方案
本发明的超级复合材料迭层板，由不同材料的(多孔)板材，逐层粘接加钉固以错缝重迭各板材成大尺寸的超级复合材料迭层 板，或做成大型物体。例如：三体舰船要求重量尽可能轻，又有足够强度的超大甲板，即可用SiO2气凝胶薄板+铝合金蜂窝板+硬质泡沫酚醛塑料厚板+钢纤维增强铝合金板+SiO2气凝胶板＝复合材料大尺寸芯板，其整个表面再用碳纤增强环氧树脂缠绕成玻璃钢内蒙皮，再加上镀铟高强度钢的外蒙皮，即成三体舰船用超大甲板。 
现代新型潜水艇多采用隐蔽性好的单壳体结构做耐压艇体，但其浮力较双壳体结构的潜水艇小，如用超级复合材料迭层板做单壳体结构的潜水艇，就具有两者的优点，即在复合迭层板做的艇体框架上，先铺一层约10mm厚的高强度钢板作内壁，其上再胶粘一层铁氧体硬质泡沫陶瓷片→玻璃钢蜂窝板→SiO2气凝胶板→最后用碳纤维或玻璃布增强环氧树脂缠绕成整体外壳。当然，各层芯板之间应错缝重迭，逐层粘固+铆钉和膨胀销等钉固。 

Claims (2)

1.一种超级复合材料迭层板，由不同材料的(多孔)板材重迭成，其特征是：各板材之间错缝交叉重迭成大尺寸超级复合材料迭层板或大型物体。
2.如权利要求1所述的超级复合材料迭层板，其特征是：用胶粘剂加紧固件联接各层板材。
CN2012104420169A 2012-10-21 2012-10-21 超级复合材料迭层板 Pending CN102941703A (zh)

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CN2012104420169A CN102941703A (zh) 2012-10-21 2012-10-21 超级复合材料迭层板

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CN2012104420169A CN102941703A (zh) 2012-10-21 2012-10-21 超级复合材料迭层板

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CN102941703A true CN102941703A (zh) 2013-02-27

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106494027A (zh) * 2016-12-12 2017-03-15 苏州兹安金属制品有限公司 一种气凝胶蜂窝芯体

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012024023A1 (en) * 2010-08-17 2012-02-23 The Boeing Company Composite structures having composite-to-metal joints and method for making the same

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012024023A1 (en) * 2010-08-17 2012-02-23 The Boeing Company Composite structures having composite-to-metal joints and method for making the same

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106494027A (zh) * 2016-12-12 2017-03-15 苏州兹安金属制品有限公司 一种气凝胶蜂窝芯体

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Application publication date: 20130227