发明名称 BYPASS TURBOJET NACELLE
摘要 FIELD: engines and pumps.SUBSTANCE: moving cowling can be displaced between closed position whereat it closed deflecting means and open position it opens nacelle channel and said deflecting means. Moving cowling has extension composed of nozzle section arranged at its downstream lower end. Said nozzle section comprises at least one panel arranged to pivot relative to axis perpendicular to nacelle lengthwise axis. Every panel is coupled with turbojet fixed coaling by transfer link arranged to turn around points of attachment to panel and fixed cowling. Moving cowling has extension composed of interflap fixed sections arranged on every side of every panel at moving nozzle section. Fixed section are designed to allow continuity of streamline of downstream section when nozzle section panel stays in flight position.EFFECT: higher reliability and simplified design.11 cl, 12 dwg
申请公布号 RU2499904(C2) 申请公布日期 2013.11.27
申请号 RU20100145242 申请日期 2009.04.09
申请人 AIRCELLE 发明人 VAUCHEL GUY BERNARD
分类号 F02K1/12;F02K1/72 主分类号 F02K1/12
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