Abstract: A sound-absorbing panel to be used affixed to a jet engine of an aircraft, provided with: a resin core layer having a first surface, a second surface disposed on the side opposite from the first surface, and multiple partitions extending between the first surface and second surface so as to partition multiple cells; a resin first skin layer laminated on the first surface of the core layer; and a resin second skin layer laminated on the second surface of the core layer. The first skin layer is disposed so as to face the external space while in use, and has multiple through-holes for providing communication between internal spaces of the multiple cells and external space faced by the first skin layer. The core layer has openings for providing communication between the internal spaces of the multiple cells and external space of the core layer.

Abstract: A sound-absorbing panel to be used affixed to a jet engine of an aircraft, provided with: a resin core layer having a first surface, a second surface disposed on the side opposite from the first surface, and multiple partitions extending between the first surface and second surface so as to partition multiple cells; a resin first skin layer laminated on the first surface of the core layer; and a resin second skin layer laminated on the second surface of the core layer. The first skin layer is disposed so as to face the external space while in use, and has multiple through-holes for providing communication between internal spaces of the multiple cells and external space faced by the first skin layer. The core layer has openings for providing communication between the internal spaces of the multiple cells and external space of the core layer.

Abstract: A multilayer structure (4) of the present invention includes a hollow plate-like body (1) made of a thermoplastic resin, and a fiber sheet (2) and a thermoplastic resin film (3) that are laminated on at least one principal surface of the hollow plate-like body. Even if this multilayer structure (4) is curved, raised wrinkles (6) are not formed or not likely to be formed on the inner surface due to buckling or bending, so that the strength is not likely to be reduced. Thus, the multilayer structure can satisfy both flexural rigidity and flexural strength while maintaining the light weight. The fiber sheet (2) is preferably a multiaxial fiber sheet and/or a woven fabric. The lamination is preferably thermal lamination using an adhesive film interposed between the layers.