| 摘要 |
An aircraft component includes a composite laminate structure, the composite laminate structure including an end surface at which a multiplicity of the layers of the laminate structure terminate. The aircraft component further includes a deflecting surface mounted to the composite laminate structure for protecting the end surface from direct impacts. In one embodiment, the end surface of the composite laminate structure has a convex cross-section and the deflecting surface includes laminate material laid over the end surface. In a further embodiment, the deflecting surface includes an inert strip. |
