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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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