发明名称 |
ENGINE MOUNTING STRUCTURE UNDER AN AIRCRAFT WING |
摘要 |
This invention relates to a mounting structure (1) for mounting an engine (2) under an aircraft wing (4), the structure comprising a rigid structure (8) and means (10) of fastening this rigid structure under the wing, the mounting means comprising a forward fastener (14), an intermediate fastener (15) and an aft fastener (16). According to the invention, the forward fastener has at least one triangular shackle on each side of a vertical plane passing through a longitudinal axis (5) of the engine (2), placed in a vertical plane oriented along a longitudinal direction (X) of the aircraft. Furthermore, the intermediate fastener comprises a connecting rod capable of transferring forces applied in a direction (Y) transverse to the aircraft, and the aft fastener comprises at least one shackle oriented along a vertical direction (Z) of the aircraft.
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申请公布号 |
CA2487800(C) |
申请公布日期 |
2012.10.23 |
申请号 |
CA20042487800 |
申请日期 |
2004.11.17 |
申请人 |
AIRBUS FRANCE |
发明人 |
MACHADO, STEPHANE;CASSAGNE, JEROME;DEL BLANCO, ANTHONY;MARTIN, YVON;CHAMBREUIL, ARNAUD |
分类号 |
F02C7/20;B64C3/32;B64D27/12;B64D27/26 |
主分类号 |
F02C7/20 |
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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