发明名称 |
COUNTERBALANCED REFUELING ARM ASSEMBLY |
摘要 |
. A rigid conduit refueling system for aircraft consisting of a wheeled support platform upon which swivel joints connected to a fuel supply source communicate with an arm conduit having a lower end pivotally mounted to the support platform and the upper end communicates with three elbow swivel couplings associated with a nozzle whereby the nozzle may be attached to the aircraft fuel tank inlet. Counterbalancing expansible chamber motors associated with the support platform and arm conduit bear the weight of the elevated components as controlled by a closed fluid circuit. |
申请公布号 |
CA1288742(C) |
申请公布日期 |
1991.09.10 |
申请号 |
CA19890610639 |
申请日期 |
1989.09.07 |
申请人 |
AEROQUIP CORPORATION |
发明人 |
FOURNIER, PAUL J.E.;REINKER, JOSEPH K. (JR.) |
分类号 |
F16L3/015 |
主分类号 |
F16L3/015 |
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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