发明名称 Composite laminated plate having reduced crossply angle
摘要 <p>COMPOSITE LAMINATED PLATE HAVING REDUCED CROSSPLY A composite laminated plate (110) comprising a first plurality of plies of reinforcing fibres (120) for lengthwise strength with respect to a dominant load direction, and a second plurality of reinforcing fibres (130) oriented at angles with respect to the dominant load direction, where 0 is between 15 and 35 degrees. x-axis</p>
申请公布号 AU2014200352(A1) 申请公布日期 2014.09.11
申请号 AU20140200352 申请日期 2014.01.21
申请人 THE BOEING COMPANY 发明人 KISMARTON, MAX U.
分类号 B29C70/22;B32B5/12;B32B5/26 主分类号 B29C70/22
代理机构 代理人
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