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 EP0934449(A1) 申请公布日期 1999.08.11
申请号 EP19970947827 申请日期 1997.09.23
申请人 J.C. CARTER COMPANY, INC. 发明人 BROWN, ALBERT, W.;PICKETT, JOHN;SCANDERBEG, DINO, C.
分类号 B64D39/00;F04D13/12;F04F5/46;F04F5/52;(IPC1-7):E03B5/00 主分类号 B64D39/00
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