发明名称 FUEL INJECTION SYSTEM FOR TURBOJET ENGINE AND METHOD OF ASSEMBLING SUCH AN INJECTION SYSTEM
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 EP2598803(A2) 申请公布日期 2013.06.05
申请号 EP20110754695 申请日期 2011.07.18
申请人 SNECMA 发明人 BUNEL, JACQUES, MARCEL, ARTHUR;DE SOUSA, MARIO, CESAR;SEVI, GUILLAUME;DEMOULIN, BRICE, ARNAUD
分类号 F23R3/14;F23R3/00 主分类号 F23R3/14
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