发明名称 |
LEADING EDGE STRUCTURE, IN PARTICULAR FOR AN AIR INLET OF AN AIRCRAFT ENGINE NACELLE |
摘要 |
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.
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申请公布号 |
US2013230390(A1) |
申请公布日期 |
2013.09.05 |
申请号 |
US201313872325 |
申请日期 |
2013.04.29 |
申请人 |
AIRCELLE |
发明人 |
BOUILLON FLORENT;COAT CAROLINE |
分类号 |
F01D25/02 |
主分类号 |
F01D25/02 |
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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