| 摘要 |
There are disclosed herein laminated materials often used as facing materials in aircraft interiors, and the use of phenolic resins and unidirectional carbon fibers (14) to form a prepreg, which ultimately comprises all of the layers of the laminated materials. Disclosed herein is a novel method for manufacturing such a prepreg and the product of that method. The final laminated material product formed has superior strength and impact resistance properties while exhibiting favorable smoke and burn characteristics. |
