发明名称 ROTOR BLADE, A ROTOR, AN AIRCRAFT, AND A METHOD
摘要 A blade (20) of a rotor (5), the blade (20) having a suction side (21) and a pressure side (22) extending transversely from a leading edge (23) towards a trailing edge (24) and extending spanwise from a root section (31) towards a free end section (41). The blade (40) comprises, going from the root section (31) towards said free end section (41): a root zone (30); followed by rounded zone (35); said rounded zone (35) presenting rounded pressure and suction sides (22'', 21'') departing from said main plane (P1) in a direction (Z) parallel to the axis of rotation (AXROT) of said blade.
申请公布号 US2013323043(A1) 申请公布日期 2013.12.05
申请号 US201313775418 申请日期 2013.02.25
申请人 EUROCOPTER;EUROCOPTER 发明人 FINCK SEBASTIEN;SUDRE LAURENT
分类号 B64C27/46 主分类号 B64C27/46
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