Method and assembly for manufacturing a single-piece hollow section component with fibrous compound material

摘要

The method involves providing an inner tool kernel (3). The inner tool kernel is covered with main layer (4) from GRP components material (2). The main layer is cured from the GRP components material such that the inner tool kernel is removed. Independent claims are included for the following: (1) aircraft construction material; and (2) arrangement for manufacturing one-piece GRP component.