发明名称 LEADING EDGE FOR AN AIRFOIL
摘要 A leading edge for an airfoil comprising a torsion box, the leading edge comprising a leading plate and a first inflatable element suitable for being filled with air. The leading plate comprises a convex side and a concave side. The first inflatable element is in contact with at least part of the concave side, thus reinforcing the leading plate. An airfoil comprising such a leading edge is also provided.
申请公布号 US2017106969(A1) 申请公布日期 2017.04.20
申请号 US201615295099 申请日期 2016.10.17
申请人 Airbus Operations S.L. 发明人 Pereira Mosqueira Fernando;VÁZQUEZ CASTRO Jesús Javier
分类号 B64C3/30;B64C3/26;B64C3/28 主分类号 B64C3/30
代理机构 代理人
主权项 1. A leading edge for an airfoil comprising a torsion box, the leading edge comprising: a leading plate with a convex side and a concave side, a first inflatable element configured to be filled with air, the first inflatable element being in contact with at least part of the concave side, thus reinforcing the leading plate.
地址 Getafe ES