发明名称 A fuel supply of a motor of a rotorcraft, comprising means for initiating a suction pump for fuel from a distributor
摘要 The network has a fuel suction pump (3) taking fuel from a feeder tank (5) and conveying the fuel at high pressure to an engine via a feed circuit (4). The feed circuit is provided with a feed ejector (15) immersed inside the feeder tank. The feed ejector includes a nozzle for admitting a primary stream of fuel into a main channel. A fuel transfer circuit (10) includes a branch connection for admitting the primary stream of fuel through the nozzle to the main channel, where admission of the primary stream of fuel fed by the transfer circuit is forced at low pressure by a transfer pump (12). An independent claim is also included for a method for implementing the fluid flow network.
申请公布号 EP2657134(B1) 申请公布日期 2016.08.31
申请号 EP20130001782 申请日期 2013.04.08
申请人 AIRBUS HELICOPTERS 发明人 LOLLINI, LIONEL
分类号 B64D37/00;F02C7/236;F02M59/00 主分类号 B64D37/00
代理机构 代理人
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