发明名称 Convertible aircraft with tilting rotors
摘要 To provide aerodynamic continuity between the front part, pivoting with the rotor, and the stationary rear part of a pod housing an engine for driving the rotor, a curved cowl curved about the pivot axis extends the rear edge of the bottom cowling of the front part to join this rear edge to the front edge of a bottom cowling of the stationary rear part, in helicopter mode, and a flap swivel-mounted on the top cowling of the front part joins this latter to the top cowling of the stationary rear part, onto which this flap is folded, in helicopter mode.
申请公布号 US6260793(B1) 申请公布日期 2001.07.17
申请号 US19990411558 申请日期 1999.10.01
申请人 EUROCOPTER 发明人 BALAYN FRéDéRIC;MAGRE ERIC
分类号 B64C7/00;B64C29/00;(IPC1-7):B64C27/22;B64C1/38;B64C27/52;B64D27/00;B64D29/00 主分类号 B64C7/00
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