| 发明名称 |
Jet aircraft engine nacelle has air intake de-icing and anti-icing system created by resistive heating elements embedded in electrical insulating material |
| 摘要 |
<p>The air intake (2) lip (3) and tube (4) de-icing and anti-icing system (6a, 6b, 6c, 6d) consists of at least one set of resistive heating elements embedded in an electrical insulating material in the form of a mat within the air intake. The mat can be in two sections inside the air intake lip and in the joining zone (7c) between the lip and the first acoustic attenuation panel (5) of the engine nacelle tube.</p> |
| 申请公布号 |
FR2887518(A1) |
申请公布日期 |
2006.12.29 |
| 申请号 |
FR20050051711 |
申请日期 |
2005.06.22 |
| 申请人 |
AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE |
发明人 |
PORTE ALAIN |
| 分类号 |
B64D15/12;F02C7/045;F02C7/047 |
主分类号 |
B64D15/12 |
| 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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