Fiber composite component producing method for e.g. spacecraft, involves hardening component together with multiple packed reinforcement elements subjected to vacuum for forming fiber composite component

摘要

The method involves positioning multiple reinforcement elements exhibiting a non-hardened fiber composite material on a component (1). The reinforcement elements are packed in separate attached vacuum bags. Vacuum is provided to the bags for separate application of pressure of the reinforcement elements by an ambient pressure prevalent outside the bags. The component together with the packed reinforcement elements that are subjected to the vacuum is hardened for forming a fiber composite component, where the reinforcement elements are made of CFK-prepreg-material.