发明名称 Jointing of fuselage skin around aircraft windows
摘要 A joint is arranged in the vicinity of a row of windows (4-7), such that the course of the joint is not interrupted by the windows. The frames (10-13) are included as rip-stoppers to prevent propagation of cracks. The skin sections in the remaining regions of the joint are connected directly to each other. This connection can also take the form of butt-joints or overlapping joints.
申请公布号 DE4408476(A1) 申请公布日期 1995.09.21
申请号 DE19944408476 申请日期 1994.03.14
申请人 DAIMLER-BENZ AEROSPACE AIRBUS GMBH, 21129 HAMBURG, DE 发明人 HEMPEL, JOACHIM, 21224 ROSENGARTEN, DE
分类号 B64C1/14;(IPC1-7):B64C1/14 主分类号 B64C1/14
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