发明名称 Chevron for a nozzle, corresponding nozzle and turboreactor
摘要 According to the invention, the shape of each of said chevrons is defined: by two lateral sides (21, 22) having front ends (21A, 22A) that are connected to said nozzle (4, 10) and that, when moving away from the latter, converge towards each other without joining so that the rear ends (21R, 22R) of said lateral walls (21, 22) are spaced from each other; and by a curvilinear transverse line (23.1) connecting the rear ends (21R, 22R) of said lateral walls (21, 22) by forming two rounded side protrusions (24.1, 25.1) separated by an intermediate rounded recess (26.1).
申请公布号 EP2179163(A1) 申请公布日期 2010.04.28
申请号 EP20080841996 申请日期 2008.08.04
申请人 AIRBUS OPERATIONS (SAS) 发明人 SYLLA, AMADOU, ANDRE;HUBERT, JEROME;PELAGATTI, OLIVIER;PRAT, DAMIEN;DEBATIN, KLAUS
分类号 F02K1/38;F02K1/48 主分类号 F02K1/38
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