| 发明名称 |
Closure flap for monocoque helicopter fuselage |
| 摘要 |
The helicopter fuselage closure hatch has load bearing pins (2,3) between the periphery of the flap and the periphery of the fuselage opening. A pivot axis pin is positioned in the area of one edge of the hatch. A link for the hatch to the fuselage is height adjustable.
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| 申请公布号 |
DE19840595(C1) |
申请公布日期 |
1999.12.09 |
| 申请号 |
DE19981040595 |
申请日期 |
1998.09.05 |
| 申请人 |
EUROCOPTER DEUTSCHLAND GMBH |
发明人 |
GREISINGER, MICHAEL;HAFFSTEIN, CLAUS-JUERGEN |
| 分类号 |
B64C1/14;(IPC1-7):B64C1/14 |
主分类号 |
B64C1/14 |
| 代理机构 |
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代理人 |
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