发明名称 Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle
摘要 <p>The nacelle has a connecting device comprising an annular flange (46) that is connected to an air inlet (42), and another annular flange (50) connected to a motor (44) that is pressed against the former flange. The flanges extend in a plane perpendicular to a longitudinal axis of the nacelle. Connecting elements i.e. bolts, are placed in respective bolt holes (48, 54) for connecting the flanges. One of the flanges comprises a U- or V-shaped opening (72) located between the bolt hole and a junction zone (68) of the flange and/or between the bolt hole and an outer edge (74) of the flange.</p>
申请公布号 EP2554822(A2) 申请公布日期 2013.02.06
申请号 EP20120305930 申请日期 2012.07.30
申请人 AIRBUS OPERATIONS SAS 发明人 PORTE, ALAIN;DIDA, STEPHANE;FARGUES, MATTHIEU;MARRO, MARTIAL;CHANCERELLE, EMERIC
分类号 F02C7/04;B64D33/02;F01D21/04;F01D25/24 主分类号 F02C7/04
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