发明名称 Fuel supply circuit for an aircraft engine
摘要 <p>The circuit has a fuel supply conduit (18) for supplying fuel to fuel injectors (16) of a combustion chamber, and a servo-valve (24) for controlling a hydraulic actuator (22) e.g. jack, with variable geometry. A load loss regulating element (20) constituted by a diaphragm is interposed between a high pressure outlet of a pump (10) and the fuel supply conduit. The servo-valve includes a high pressure admission inlet (HP) connected to the high pressure outlet of the pump upstream of the element, and a low pressure exhaust outlet (BP) connected to the supply conduit downstream of the element.</p>
申请公布号 EP2048337(B1) 申请公布日期 2013.06.26
申请号 EP20080166348 申请日期 2008.10.10
申请人 SNECMA 发明人 GALOZIO, PHILIPPE;MONTAROU, CEDRIC;MORIN, DENIS
分类号 F02C7/236;F02C7/232 主分类号 F02C7/236
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