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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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