发明名称 Gas turbine engine fuel return valve and system
摘要 <p>A fuel return valve (108) and system includes a flow-level select and shut-off valve and a servo control valve (102). The flow-level select and shut-off valve includes a first fuel inlet, a second fuel inlet, a return-to-tank fuel outlet, and a valve element movable between a shut-off position, a mid-flow position, and a max-flow position. The servo control valve is coupled to the flow-level select and shut-off valve and is configured to control relative fluid pressures therein to selectively move the valve element to the shut-off position, the mid-flow position, and the max-flow position.</p>
申请公布号 EP2623745(A2) 申请公布日期 2013.08.07
申请号 EP20130152110 申请日期 2013.01.21
申请人 HONEYWELL INTERNATIONAL INC. 发明人 FUTA, PAUL;LEWIS, STEVEN ALAN;PORTOLESE, LARRY
分类号 F02C7/232 主分类号 F02C7/232
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