FIELD: aviation.
SUBSTANCE: invention relates to a method for producing an aircraft component from fiber-metal layered material. The method includes using manipulation system (2) with terminal executive body (3) and control unit (4) connected to manipulation system (2). In the method, metal layer (5) and uncured fibrous layer (6) are superimposed on each other in mold (7) by manipulation system (2) in the superimposition sequence. Each superimposition cycle includes taking metal layer (5) or fibrous layer (6) from corresponding feeding stack (8, 9) in accordance with the superimposition sequence, transporting layer (5, 6) to mold (7), placing layer (5, 6) on deposition surface in mold (7) in accordance with the superimposition sequence and depositing layer (5, 6) placed in such a way on deposition surface (10). After taking from feeding stack (8, 9) and before depositing on deposition surface (10), superimposed layer (5, 6) is deformed by terminal executive body (3) so that to align layer (5, 6) shape with deposition surface (10) shape. Metal layer (5) and fibrous layer (6) are taken and deformed by means of one and the same terminal executive body (3).
EFFECT: simplifying the production system and increasing the stability of its automated operation.
15 cl, 3 dwg
