首页> 外国专利> SANDWICH-STRUCTURAL COMPOSITE APPARATUS WITH CORE JOINING AND SPLICING METHOD FOR RETENTION OF STRUCTURAL AND ACOUSTIC CAPABILITY

SANDWICH-STRUCTURAL COMPOSITE APPARATUS WITH CORE JOINING AND SPLICING METHOD FOR RETENTION OF STRUCTURAL AND ACOUSTIC CAPABILITY

机译:夹心结构的复合材料夹层组合装置及其结构和声学能力的保持

摘要

A sandwich-structural composite is assembled from a front sheet and a backsheet that sandwich between them first and second open cell core panels thatarespliced together along intermeshing edges of the panels with projections fromthepanels engaging into slots into the panels. There is no adhesive substanceemployedbetween the intermeshing edges of the two core panels. The joining andsplicing of theintermeshing core panel edges retains the structural and acoustic capabilityof thecomposite without the need for adhesives (film, foaming, paste, pottingcompound, etc.)between the intermeshing edges of the core panels.
机译:三明治结构复合材料由正面和背面组装而成夹在第一张和第二张开孔核心面板之间的床单是沿着面板相互啮合的边缘拼接在一起,并带有的面板插入面板上的插槽。没有粘性物质受雇在两个芯板的相互啮合的边缘之间。加入和的拼接相互啮合的核心面板边缘保留了结构和声学功能的无需粘合剂的复合材料(薄膜,发泡剂,糊剂,灌封剂)化合物等)在芯板的相互啮合的边缘之间。

著录项

  • 公开/公告号CA2866720A1

    专利类型

  • 公开/公告日2015-07-21

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号CA20142866720

  • 申请日2014-10-08

  • 分类号B32B3/18;B32B7/12;B32B37;B64C1;F16S1/02;B32B3/12;

  • 国家 CA

  • 入库时间 2022-08-21 15:11:25

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