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1. 发明申请

US20140284431A1 AIRCRAFT STRUCTURE WITH STRUCTURAL NON-FIBER REINFORCING BONDING RESIN LAYER 审中-公开
标题翻译：结构非纤维增强粘结层结构的飞机结构
公开(公告)号：US20140284431A1
公开(公告)日：2014-09-25
申请号：US14355502
申请日：2011-12-12
申请人： Tommy Grankaell , Per Hallander , Mikael Petersson , Bjoern Weidmann
发明人： Tommy Grankaell , Per Hallander , Mikael Petersson , Bjoern Weidmann
IPC分类号： B64C1/00
CPC分类号： B64C1/00 , B29C65/4835 , B29C65/488 , B29C65/54 , B29C66/112 , B29C66/1122 , B29C66/131 , B29C66/545 , B29C66/63 , B29C66/721 , B29C66/7212 , B29C66/7311 , B29C66/73752 , B29C66/7392 , B29C66/7394 , B29C66/81455 , B29C66/9141 , B29C66/91441 , B29C66/91921 , B29D99/0028 , B29L2031/3085 , B64C3/187 , B64C3/20 , B64C3/24 , Y02T50/43 , Y10T428/24521 , B29K2307/04 , B29K2309/08
摘要： The present invention regards an aircraft structure comprising an aerodynamic composite shell (7), the interior face (9) of which in whole or in part is bonded with at least one two- or three-dimensional structural composite part (11) by means of a bonding material (15). It also regards a method of manufacture of the aircraft structure. The bonding material (15) comprises a non-structural fiber reinforced resin system, wherein at least one portion of the bonding material, which portion spatially corresponds with an interior face filling volume (21), is thicker than other portions of the bonding material (15), due to settlement of resin of the non-structural fiber reinforced resin system in said interior face filling volume (21) during the viscous phase of the curing of the non-structural fiber reinforced resin system.
摘要翻译：本发明涉及一种包括空气动力学复合材料壳体（7）的飞机结构，其内表面（9）全部或部分地通过至少一个二维或三维结构复合材料部件（11）与接合材料（15）。它还涉及飞机结构的制造方法。接合材料（15）包括非结构纤维增强树脂体系，其中在空间上对应于内表面填充体积（21）的部分的粘合材料的至少一部分比粘结材料的其它部分 15），由于在非结构纤维增强树脂体系的固化粘性相中，所述内表面填充体积（21）中的非结构纤维增强树脂体系的树脂沉降。

2. 发明申请

US20140147619A1 COMPOSITE ARTICLE AND A METHOD OF FORMING A COMPOSITE ARTICLE 审中-公开
标题翻译：复合材料和形成复合材料的方法
公开(公告)号：US20140147619A1
公开(公告)日：2014-05-29
申请号：US13978681
申请日：2011-01-21
申请人： Tommy Grankaell , Per Hallander , Anders Lundberg , Tonny Nyman , Bjoern Weidmann , Mikael Petersson
发明人： Tommy Grankaell , Per Hallander , Anders Lundberg , Tonny Nyman , Bjoern Weidmann , Mikael Petersson
IPC分类号： B32B5/26 , B29C70/30
CPC分类号： B32B5/26 , B29C70/222 , B29C70/30 , B29C70/342 , B29C70/46 , B32B2250/05 , B32B2250/20 , B32B2260/023 , Y10T428/24124
摘要： The present invention relates to a composite article 801, wherein the article has a longitudinal direction L and a transversal direction T, the article 80 comprises a stack of plies wherein one ply is a bottom ply and one ply is a top ply, most of or all of the plies comprise fibres, and the article comprises a plurality of plies having fibres substantially in the orthogonal direction 810 to the longitudinal direction L of the article 801 and the stack further comprises a plurality of plies having fibres substantially in the same direction 811 as the longitudinally direction L of the article 801 and/or a plurality of plies having fibres in the diagonal direction (812, 813, 815, 816, 817, 818) of the longitudinal direction (L) of the article (801), wherein at least one of the ply/plies having fibres substantially in the orthogonal direction 810 to the longitudinal direction L of the article 801 comprise fibres that are stiffer than the fibres in the other plies which have less stiff fibres. The present invention also relates to a method of forming an article on a tool, the tool having one longitudinal direction L and one transversal direction T.
摘要翻译：本发明涉及一种复合制品801，其中制品具有纵向方向L和横向方向T，制品80包括一叠层，其中一层是底层，一层是顶层，大多数或所有的帘布层都包含纤维，并且制品包括多个帘布层，其具有基本上在与制品801的纵向方向L相关的正交方向810上的纤维，并且该堆叠还包括多个帘布层，其具有基本上沿相同方向811的纤维物品801的纵向方向L和/或具有在物品（801）的纵向方向（L）上的对角线方向（812,813,815,816,817,818）上的纤维的多个帘布层，其中在具有基本上在与制品801的纵向方向L相关的正交方向810上的纤维的帘布层/帘布层中的至少一个包括比其他帘布层中具有较低刚性纤维的纤维更硬的纤维 res。本发明还涉及一种在工具上形成物品的方法，该工具具有一个纵向方向L和一个横向方向T.

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