FIELD: process engineering.
SUBSTANCE: invention covers method of producing structural component for aerospace aircraft. Proposed method comprises the following steps whereat: web with uniaxial reinforcing elements is fed that comprises glass fiber layer pre-impregnated with resin matrix, to coiling machine. Web with biaxial reinforcing elements is fed that comprises metal structure pre-impregnated with resin matrix, to coiling machine. Said coiling machine produces web with uniaxial or biaxial reinforced elements on laminator. Then, said web is cured to produce structural element.
EFFECT: invention allows automation of production process.
8 cl, 6 dwg
