发明名称 ターボジェットエンジンのための燃料噴射システムおよびそのような噴射システムを組み立てる方法
摘要 <p>A fuel injection system for a turbojet engine including a fixed part and a sliding lead-through, the fixed part and the sliding lead-through extending along a reference axis, the fixed part including a cavity that has a bottom and a closure cup, the sliding lead-through being provided with a sole plate contained inside the cavity. The injection system has increased resistance to wearing of the injector on which it is mounted. To achieve this it further includes a spring arranged in such a way as to apply to the sole plate a force capable of preventing the vibration-induced micro-movements of the sliding lead-through with respect to the fixed part in the absence of thermal expansion.</p>
申请公布号 JP5764208(B2) 申请公布日期 2015.08.12
申请号 JP20130521185 申请日期 2011.07.18
申请人 发明人
分类号 F23R3/28;F01D25/04;F02C7/00;F02C7/20;F23R3/60 主分类号 F23R3/28
代理机构 代理人
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