Method for manufacturing composite material part for aircraft, involves integrating protecting portion in extension part of another protection portion, which is simultaneously realized with former portion in single manufacturing device

摘要

The method involves integrating a protecting portion (22) integrating in an extension part of another protection portion (24), which is simultaneously realized with the former protection portion in a single manufacturing device during a single continuous cycle. The former protecting portion is made of composite material by pultrusion. The latter protecting portion is carried out in a composite material containing aramide fibers identical to fibers used in composite material of the former protecting portion.