发明名称 |
Connection arrangement to connect two flexible tanks of an aircraft |
摘要 |
A connection arrangement for detachably connecting a first flexible tank and a second flexible tank in an aircraft includes a latching device, a first tubular connecting element attached to the first tank, and a second tubular connecting element attached to the second tank. The first and the second connecting elements are detachably connected to each other using the latching device. In a connected state of the connecting elements, fluid exchange can take place between the first and the second tanks via the first and the second connecting elements, the latching device is disposed inside one of the first and second flexible tanks and is actuatable from outside the respective flexible tank.
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申请公布号 |
US2005034781(A1) |
申请公布日期 |
2005.02.17 |
申请号 |
US20030612108 |
申请日期 |
2003.07.02 |
申请人 |
EUROCOPTER DEUTSCHLAND GMBH |
发明人 |
RODOUSAKIS ELEFTHERIOS;KIOWSKY HARALD |
分类号 |
B64D37/06;(IPC1-7):B65B1/04 |
主分类号 |
B64D37/06 |
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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