发明名称 |
Aircraft fuel transfer pump with auxiliary fuel line scavenge pump |
摘要 |
<p>An improved fuel transfer pump is provided for relatively high flow transfer of fuel from one aircraft to another during an inflight refueling procedure, wherein the fuel transfer pump includes a jet-type scavenge pump for evacuating residual fuel from a fuel line or manifold. The scavenge pump comprises a venturi element connected along a recirculation conduit through which a small fuel flow is diverted from the high pressure discharge side of the fuel transfer pump for return to the fuel tank. The recirculation fuel flow induces a vacuum in a suction throat of the venturi element, and this vacuum is coupled by a suction line to evacuate residual fuel from the fuel line or manifold to the fuel tank. A flow baffle is mounted along the recirculation conduit downstream from the venturi element to ensure flooding and priming of the scavenge pump.</p> |
申请公布号 |
IL129099(D0) |
申请公布日期 |
2000.02.17 |
申请号 |
IL19970129099 |
申请日期 |
1997.09.23 |
申请人 |
J.C. CARTER COMPANY, INC. |
发明人 |
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分类号 |
B64D39/00;F04D13/12;F04F5/46;F04F5/52;(IPC1-7):E03B |
主分类号 |
B64D39/00 |
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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