发明名称 |
MULTI-AXIAL LAMINATE COMPOSITE STRUCTURES AND METHODS OF FORMING THE SAME |
摘要 |
<p>Composite laminate structures and methods of forming the same are disclosed. In one embodiment, the structure includes a first bidirectional layer (112) having a first portion (117) that includes parallel reinforcement fibers oriented at a first angle relative to a first direction and a second portion (114) that includes parallel reinforcement fibers oriented at a second angle relative to the first direction. The structure further includes a second bidirectional layer (118) having a first portion (119) that includes parallel reinforcement fibers oriented at a third angle relative to the first direction and a second portion (120) that includes parallel reinforcement fibers oriented at a fourth angle relative to the first direction. At least one unidirectional (116) layer having a plurality of parallel reinforcement fibers is coupled to at least one of the first bidirectional layer and the second bidirectional layer.</p> |
申请公布号 |
WO2006121505(A8) |
申请公布日期 |
2007.01.25 |
申请号 |
WO2006US09730 |
申请日期 |
2006.03.16 |
申请人 |
THE BOEING COMPANY;KISMARTON, MAX, U. |
发明人 |
KISMARTON, MAX, U. |
分类号 |
B29C70/08;B29C70/20;B29C70/22;B29C70/24;B64C1/00 |
主分类号 |
B29C70/08 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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