发明名称 Wall element for land-, aircraft- and space vehicle, comprises molded part made of fiber-reinforced plastic material and having outer surface, where plastic film is disposed on outer surface with high tensile strength in area-wise manner
摘要 The wall element (10) comprises a molded part (12) made of fiber-reinforced plastic material and having an outer surface (14), where a plastic film (18) is disposed on the outer surface with high tensile strength in an area-wise manner. The plastic film has tensile strength of 20 N/mm 2>or more, and a breaking elongation of 250% or more. A layer of the plastic film is formed on the basis of polyvinyl acetate and/or polyurethane, polyvinyl butyral (50-80 wt.%) and polyethylene. The plastic film is a single-layer film or a multi-layer film, and comprises several layers. The wall element (10) comprises a molded part (12) made of fiber-reinforced plastic material and having an outer surface (14), where a plastic film (18) is disposed on the outer surface with high tensile strength in an area-wise manner. The plastic film has tensile strength of 20 N/mm 2>or more, and a breaking elongation of 250% or more. A layer of the plastic film is formed on the basis of polyvinyl acetate and/or polyurethane, polyvinyl butyral (50-80 wt.%) and polyethylene. The plastic film is a single-layer film or a multi-layer film, and comprises several layers, where a layer formed on the basis of polyvinyl acetate and/or polyurethane is arranged between the two further layers, which are formed on the basis of polycarbonate and/or polyethylene terephthalate. The plastic film has a thickness of 300-500 mu m, is fixed on the outer surface of the molded part by self-adhesion and/or adhesive agent, and is formed in an UV-absorbing-, a flame retardant- and an electrically conducting manner. The layer of the plastic film comprises metallic nanoparticles. The plastic material of the molded part comprises duroplastic material. The plastic material of the molded part comprises thermoplastic high-capacity plastic material. The plastic material of the molded part is reinforced with glass fibers, carbon fibers and/or aramide fibers. The fibers in the plastic material have a length of more than 50 mm and are present as uni-, bi- or multi-directional fabric or knitted fabric. The wall element forms a part of the land-, aircraft- and space vehicle.
申请公布号 DE102009037171(A1) 申请公布日期 2011.02.10
申请号 DE20091037171 申请日期 2009.08.03
申请人 DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. 发明人 KINDERVATER, CHRISTOF;KECK, RUEDIGER;KOCIAN, FRANK;SEEGER, NIKO
分类号 B32B27/08;B32B27/18;B32B27/28;B32B27/30;B32B27/36;B32B27/38;B64C1/00;B64C1/12;B64C3/26;C08J5/04 主分类号 B32B27/08
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