发明名称 Aircraft engine cowl panel with closure default indicator
摘要 <p>The indicator, designed to show at a glance when engine fan nacelle panel (6) locks have been left unfastened, consists of a flap (16) that can be closed over the locks (14) only when they have been fastened. Otherwise the flap, which can be made for enhanced visibility by painting it in a bright colour or adding a flag, stays in the open position.</p>
申请公布号 EP1314839(B1) 申请公布日期 2006.01.25
申请号 EP20020292913 申请日期 2002.11.25
申请人 AIRBUS FRANCE 发明人 PORTE, ALAIN
分类号 E05B41/00;B64D29/06;B64D29/08;B64D45/00;E05C19/14 主分类号 E05B41/00
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