The invention provides a flexible
composite skin and a manufacturing method and a tool structure thereof, and belongs to the technical field of
aviation, thereby solving a problem that an existing flexible
skin is poor in stability and bearing performance. The
composite skin comprises a flexible rubber base body, an embedded supporting structure and a
fiber reinforcement body. The embedded supporting structure and the
fiber reinforcement body are shaped in the flexible rubber base body in parallel, the embedded supporting structure and the
fiber reinforcement body are arranged in a mutually perpendicular and overlapped mode, and uniform and independent grid units are formed in the flexible rubber base body. The manufacturing tool structure comprises a
metal bottom plate,
fiber bundle moldplates, a supporting rod mold plate, a gland plate and a sliding block mold. The
metal bottom plate is fixedly connected with a pair of
fiber bundle mold plates, the supporting rod mold plate is fixedly installed on the upper surface of the
metal bottom plate, the supporting rod mold plate is connected with the pair of
fiber bundle mold plates to form a rectangular rail, and the sliding block moldslides along the rectangular rail. The flexible
composite skin and the manufacturing method and the tool structure thereof are mainly used for variable sweepback wing
quadrilateral shearing module units.