Abstract: Provided are a forming method of forming, with high efficiency, a tear line groove even with a layout of unsuitable for processing for drawing a locus in a unicursal manner, and an instrument panel formed by the forming method. The forming method is a method of forming a tear line groove in an airbag deployment portion, the tear line groove including: an airbag deployment portion forming step of applying, as one die of two dies constituting a cavity into which a molten resin is injected to form the airbag deployment portion, a die having a ridge protruding inwardly in the cavity to form a part of the tear line groove; and a post-processing step of processing the remaining tear line groove, which were not formed in the airbag deployment portion forming step.

Abstract: Interior material for vehicle including a foamed sheet layer having a foam surface opposing a first rear surface of the first sheet layer, a first sheet layer joined along the foam surface, and a second sheet layer joined to a part of a first surface of the first sheet layer, bonded together while a surface boundary of the first sheet layer and the second sheet layer is kept linear, in which a first surface of the first sheet layer has a joined portion having a width dimension substantially the same as that of the second sheet layer and formed linearly, and a surface treated layer formed excluding the joined portion, and the second sheet layer joined along the joined portion and bonded together by a pressing force with a second surface of the second sheet layer and a foam rear surface of the foamed sheet layer as pressure receiving surfaces.

Abstract: A fiber-reinforced composite material and a method for manufacturing the same. A first binder resin is applied to a first portion for forming a deformed part of a fiber base material, and a second binder resin is applied to a second portion excluding the first portion. The fiber base material is then heated so that the degree of melting of the first binder resin during shaping is less than the degree of melting of the second binder resin, and the second binder resin is softened. Shaping is then performed so that a deformed part is formed in the fiber base material, and a preform is obtained. A fiber-reinforced composite material is obtained using the preform as a molding precursor.

Abstract: A fiber-reinforced composite material and a method for manufacturing the same. A first binder resin is applied to a first portion for forming a deformed part of a fiber base material, and a second binder resin is applied to a second portion excluding the first portion. The fiber base material is then heated so that the degree of melting of the first binder resin during shaping is less than the degree of melting of the second binder resin, and the second binder resin is softened. Shaping is then performed so that a deformed part is formed in the fiber base material, and a preform is obtained. A fiber-reinforced composite material is obtained using the preform as a molding precursor.