| 发明名称 |
LEADING EDGE STRUCTURE, IN PARTICULAR FOR AN AIR INLET OF AN AIRCRAFT ENGINE NACELLE |
| 摘要 |
<p>A leading edge structure for an air inlet of an aircraft nacelle includes a leading edge and an inner partition defining a longitudinal compartment that is located inside the leading edge and accommodates a de-icing and/or anti-icing mat. The leading edge structure includes a multi-axial composite structure placed on top of a heating element for anti-icing and/or de-icing.</p> |
| 申请公布号 |
EP2632797(A2) |
申请公布日期 |
2013.09.04 |
| 申请号 |
EP20110785743 |
申请日期 |
2011.10.24 |
| 申请人 |
AIRCELLE |
发明人 |
BOUILLON, FLORENT;COAT, CAROLINE |
| 分类号 |
B64D33/02;B29C70/24;B29C70/48;B29C70/88;B64C3/28;B64D15/12;B64D29/00;F01D25/02 |
主分类号 |
B64D33/02 |
| 代理机构 |
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代理人 |
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| 主权项 |
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