发明名称 |
LEADING EDGE STRUCTURE, IN PARTICULAR FOR THE AIR INTAKE OF THE NACELLE OF AN AIRCRAFT ENGINE |
摘要 |
<p>The invention relates to a structure of a leading edge (1), in particular for the air intake of an aircraft nacelle, including a leading edge (2) and an inner partition wall (3) defining a longitudinal compartment (5) inside the leading edge (2). The leading edge (2) and said inner partition wall (3) are made of multiaxial composite materials.</p> |
申请公布号 |
EP2454154(A1) |
申请公布日期 |
2012.05.23 |
申请号 |
EP20100745376 |
申请日期 |
2010.06.29 |
申请人 |
AIRCELLE |
发明人 |
BOUILLON, FLORENT;RAVAILLER, FREDERIC |
分类号 |
B64D29/00;B64C3/28;B64D33/02 |
主分类号 |
B64D29/00 |
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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