发明名称 Fiber Composite Component, Adhesive Arrangement For Fiber Composite Components, And Method For Manufacturing A Fiber Composite Component And An Adhesive Arrangement
摘要 A fiber composite component includes a composite including cured matrix material and a fiber material embedded therein. At least one partial area of the fiber composite component is provided with at least one thread, which undulates as it extends along a surface area of the composite, so that sections of the thread alternately run inside of the composite and outside of the composite. An adhesive arrangement for such fiber composite components is also disclosed. Finally, methods for manufacturing such a fiber composite component or for manufacturing such an adhesive arrangement are disclosed.
申请公布号 US2016069009(A1) 申请公布日期 2016.03.10
申请号 US201514845468 申请日期 2015.09.04
申请人 Airbus Defence and Space GmbH 发明人 Meer Thomas
分类号 D05C15/16;B32B5/26;D06M17/04;B32B7/12 主分类号 D05C15/16
代理机构 代理人
主权项 1. A fiber composite component comprising a composite comprising cured matrix material and fiber material embedded therein, wherein at least one partial area of the fiber composite component includes at least one thread, the thread undulating as the thread extends along a surface area of the composite, so that sections of the thread alternately run inside of the composite and outside of the composite.
地址 Ottobrunn DE