FIELD: process engineering.
SUBSTANCE: invention relates to aircraft and space engineering, particularly, to reinforcement of component from fibrous composite and vacuum-mat. Vacuum-mat has, at least, one intake part for reproducible intake of, at least, one reinforcing component. This component is fitted in, at least, one intake part of vacuum-mat. Vacuum-mat with, at least, one reinforcing fitted-in component is arranged, in reproducible and tight manner, at component from fibrous composite to be reinforced so that part of the mould may be cooled down to bond, at least, one reinforcing element with component from fibrous composite. Then, vacuum-mat is removed from reinforced component. Said vacuum-mat may be reused.
EFFECT: higher efficiency and accuracy.
14 cl, 9 dwg
