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 |
The device has connection elements (46) e.g. bolts or rivets, housed in passage holes (38, 44) formed in cylindrical parts to be connected, respectively. Each element comprises a rod (48) having ends provided with supports (50, 52) for holding the parts in a plated manner. Each hole includes a reduced section adjusted to a section of the rod near the corresponding support, and another section with a large clearance at a junction plane (42), such that the rod is subjected to weak shearing forces at the junction plane during relative deformation of the connected parts. |
申请公布号 |
EP2481936(A1) |
申请公布日期 |
2012.08.01 |
申请号 |
EP20120305082 |
申请日期 |
2012.01.24 |
申请人 |
AIRBUS OPERATIONS SAS;ROLLS-ROYCE PLC |
发明人 |
PORTE, ALAIN;DIDA, STEPHANE;MARRO, MARTIAL;REED, JULIAN;WATTAM, DAVID;WOODWARD, COLIN;HALLIDAY, CAROLINE |
分类号 |
F16B5/02;F16L23/032 |
主分类号 |
F16B5/02 |
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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