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Sandwich-structural composite apparatus with core joining and splicing method for retention of structural and acoustic capability

机译:具有芯部接合和拼接方法的三明治结构复合装置,用于保持结构和声学性能

摘要

A sandwich-structural composite is assembled from a front sheet and a back sheet that sandwich between them first and second open cell core panels that are spliced together along intermeshing edges of the panels with projections from the panels engaging into slots into the panels. There is no adhesive substance employed between the intermeshing edges of the two core panels. The joining and splicing of the intermeshing core panel edges retains the structural and acoustic capability of the composite without the need for adhesives (film, foaming, paste, potting compound, etc.) between the intermeshing edges of the core panels.
机译:三明治结构复合材料由前片和后片组装而成,前片和后片将第一和第二开孔芯板夹在它们之间,沿着板的相互啮合的边缘拼接在一起,并且板的突出部接合到板的槽中。在两个芯板的互相啮合的边缘之间没有使用粘性物质。相互啮合的芯板边缘的连接和拼接保持了复合材料的结构和声学性能,而在芯板的相互啮合的边缘之间不需要粘合剂(薄膜,泡沫,糊剂,灌封胶等)。

著录项

  • 公开/公告号EP2896498A1

    专利类型

  • 公开/公告日2015-07-22

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号EP20150150289

  • 申请日2015-01-07

  • 分类号B32B7/12;B32B3/06;B32B3/12;B32B3/20;F16B5;B64C3/20;

  • 国家 EP

  • 入库时间 2022-08-21 15:02:23

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