Fiber-reinforced composite component e.g. wing, manufacturing method for aircraft, involves removing body-shell component by blowing lifting pad, and controlling blowing of lifting pad by arithmetic unit

摘要

The method involves positioning a place-holder in a recess in a forming tool, and providing a body-shell component. The place-holder is removed, and a lifting pad is placed in the recess. The body-shell component is removed by blowing the lifting pad. The blowing of the lifting pad is controlled by an arithmetic unit by utilizing a valve in depending upon a deflection line of the body-shell component. The lifting pad is blown such that a deflection line of the body-shell component does not exceed a permitted deflection line. An independent claim is also included for a system for manufacturing a component of fiber-reinforced composite.