发明名称 Impact resistant structure for the helicopter and energy absorber used for the same
摘要 An impact resistant structure of a helicopter having an energy absorber positioned under a floor of the helicopter and directly connected to a cabin frame of the helicopter. The energy absorber is arranged in accordance with a distribution of a ground reaction force on a general ground at a time of crash situation. The energy absorber also includes a plurality of independent hollow tubes of fiber reinforced composite material integrally formed by bundling only the hollow tubes. The hollow tubes are arranged so as to reduce a number of intersecting wall surfaces of the hollow tubes.
申请公布号 US6959894(B2) 申请公布日期 2005.11.01
申请号 US20030724186 申请日期 2003.12.01
申请人 KAWASAKI JUKOGYO KABUSHIKI KAISHA 发明人 HAYASHI TOHRU
分类号 B64C1/00;B64C1/06;B64C1/18;B64C27/00;B64C27/04;F16F7/12;(IPC1-7):B64C1/06 主分类号 B64C1/00
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