发明名称 SANDWICH-STRUCTURAL COMPOSITE APPARATUS WITH CORE, AND JOINING AND SPLICING METHOD FOR RETENTION OF STRUCTURAL AND ACOUSTIC CAPABILITY
摘要 <p>PROBLEM TO BE SOLVED: To solve the problem in which, in manufacturing a sandwich-structural composite having a shock attenuation property, blockage of open cells along abutting edges of open cell core panels detracts from the shock attenuation property of the blocked cells.SOLUTION: A sandwich-structural composite is assembled from a front sheet and a back sheet. The front sheet and the back sheet have first and second open cell core panels sandwiched between the sheets. The first and second open cell core panels are spliced along intermeshing edges of the panels such that projections from the panels engage slots penetrating 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 structural and acoustic capability of the composite without the need for adhesives (e.g., film, foaming agents, paste, and potting compounds) between the intermeshing edges of the core panels.</p>
申请公布号 JP2015136938(A) 申请公布日期 2015.07.30
申请号 JP20140231409 申请日期 2014.11.14
申请人 BOEING CO 发明人 GEOFFREY E HARRISON;ADAM J SAWICKI;TORBEN SYBERG
分类号 B32B3/30;B64C1/00 主分类号 B32B3/30
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