发明名称 SURFACE AERODYNAMIQUE PORTANTE D'AERONEF, ET AERONEF MUNI DE LADITE SURFACE AERODYNAMIQUE PORTANTE
摘要 <p>The airfoil (10) has a main structure (15) including a spar (16), and a front structure (20) forming a leading edge (21), where an empty space (25) is formed between the main structure and the front structure. A rigid deflector element (30) is provided in the empty space, where the deflector element is fastened to the main structure. The deflector element includes a sharp edge (31) facing towards the front structure, so as to deflect an external obstacle i.e. bird impacting against the front structure, where the deflector element is not in contact with the front structure.</p>
申请公布号 FR2989666(B1) 申请公布日期 2014.12.05
申请号 FR20120001151 申请日期 2012.04.19
申请人 EUROCOPTER 发明人 LECERF LUC;MOREAU VINCENT;MARANINCHI XAVIER;SICARD JEAN CHARLES
分类号 B64C3/26;B64C5/00 主分类号 B64C3/26
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