| 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 |
WO2011007074(A1) |
申请公布日期 |
2011.01.20 |
| 申请号 |
WO2010FR51366 |
申请日期 |
2010.06.29 |
| 申请人 |
AIRCELLE;BOUILLON, FLORENT;RAVAILLER, FREDERIC |
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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