发明名称 Light high load capacity support for aircraft
摘要 The support has node points consisting of a basic shell (1) with recesses (15,16) to receive longitudinal straps (5) and cross bars (6). The node point also has a sleeve-like cover shell (2) enclosing the straps and cross bars together with the base shell. The straps and cross bars lie in the recesses and are glued flat with the surface of the recesses. The shell parts (1,2) have flanges (4) at their contact points to facilitate gluing together.
申请公布号 DE19613090(A1) 申请公布日期 1996.10.10
申请号 DE1996113090 申请日期 1996.04.02
申请人 LUFTSCHIFFBAU ZEPPELIN GMBH, 88046 FRIEDRICHSHAFEN, DE 发明人
分类号 B64B1/08;E04C3/04;E04C3/08;E04C3/28;(IPC1-7):B64B1/08;E04C3/02;F16S3/08 主分类号 B64B1/08
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