| 发明名称 |
Impact resistant structure for the helicopter and energy absorber used for the same |
| 摘要 |
The present invention provides an impact resistant structure of a helicopter, which includes an energy absorber (1) positioned under a floor of the helicopter and directly connected to a cabin frame of the helicopter. The energy absorber includes a plurality of independent hollow tubes (10) of fiber reinforced composite material formed by bundling the hollow tubes. <IMAGE> <IMAGE> |
| 申请公布号 |
EP1426289(A1) |
申请公布日期 |
2004.06.09 |
| 申请号 |
EP20030257598 |
申请日期 |
2003.12.03 |
| 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):B64C1/00 |
主分类号 |
B64C1/00 |
| 代理机构 |
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