发明名称 Producing sandwich panel to manufacture e.g. walls of aircraft cabin, comprises stacking different layers of sandwich structure on mold, and covering structure by layer of material suitable to allow vacuum evacuation of water
摘要 <p>#CMT# #/CMT# The method comprises: stacking different layers of a sandwich structure (1) on a mold (4), where the structure comprises a central core (3) or cellular foam, and the core is pre-impregnated with a resin material; and covering the sandwich structure by a layer of a material suitable to allow a uniform vacuum evacuation of the water produced during the polymerization step of the resin. The material layer is arranged on the side of the sandwich structure. The whole structure is covered with a cover capable of enabling the vacuum so as to keep the sandwich structure under pressure. #CMT# : #/CMT# The method comprises: stacking different layers of a sandwich structure (1) on a mold (4), where the structure comprises a central core (3) or cellular foam, and the core is pre-impregnated with a resin material; and covering the sandwich structure by a layer of a material suitable to allow a uniform vacuum evacuation of the water produced during the polymerization step of the resin. The material layer is arranged on the side of the sandwich structure. The whole structure is covered with a cover capable of enabling the vacuum so as to keep the sandwich structure under pressure. The polymerization step is carried out to obtain the sandwich panel. A set of transverse grooves (5) and/or a set of longitudinal grooves are formed at a face of the central core on the side of the mold. The grooves form a grid of the central core of the sandwich structure. An independent claim is included for a sandwich panel. #CMT#USE : #/CMT# The method is useful for producing a sandwich panel (claimed) that is useful to manufacture furniture, walls or shells of an aircraft cabin. #CMT#ADVANTAGE : #/CMT# The method is capable of producing sandwich panel with high mechanical strength and improved aesthetic properties. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The figure shows a front view of a core. 1 : Sandwich structure 2 : Fabric layer 3 : Central core 4 : Mold 5 : Transverse groove.</p>
申请公布号 FR2998212(A1) 申请公布日期 2014.05.23
申请号 FR20120060960 申请日期 2012.11.19
申请人 EA TECHNIQUE 发明人 THULLIEZ JEAN-PIERRE
分类号 B32B3/12;B32B3/30;B32B27/04;B64C1/00 主分类号 B32B3/12
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