发明名称 Impact-absorbing component forming part of the structure of an aircraft
摘要 A shock-absorbing structure component has two cover layers and an intermediate layer that is arranged between them. The intermediate layer extends in an alternating form between the cover layers, with the material of the intermediate layer being selected such that it has a higher capacity elongation prior to breaking than that of the outer cover layer. The energy of an impact can thus be absorbed as the intermediate layer is stretched into a bag shape and the inner cover layer breaks off progressively.
申请公布号 GB2415237(B) 申请公布日期 2009.04.29
申请号 GB20050012090 申请日期 2005.06.14
申请人 EADS DEUTSCHLAND GMBH 发明人 PETER STARKE
分类号 F16F7/12;B32B3/12;B32B3/28;B32B7/02;B32B33/00;B64C3/28;F16F3/10 主分类号 F16F7/12
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