发明名称 Stiffening structure for reinforcing planar structure, particularly skin field of fuselage of aircraft, comprises variety of struts with different geometries, where one strut has linear geometry
摘要 <p>The stiffening structure (2) comprises a variety of struts (6,8) with different geometries, where one strut has a linear geometry. The linear strut runs along the circumferential direction of a planar structure. Multiple closed loops (24) are formed between the struts. The linear struts are designed as frames, where the zigzag strut runs between the frames in the circumferential direction.</p>
申请公布号 DE102009056996(A1) 申请公布日期 2011.06.09
申请号 DE20091056996 申请日期 2009.12.04
申请人 EADS DEUTSCHLAND GMBH 发明人 JOERN, PAUL;WEBER, MARKUS J.;PROWE, JENS;MACHUNZE, WOLFGANG;MEYER, LARS
分类号 F16S3/08;B64C1/06;B64C1/08 主分类号 F16S3/08
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