发明名称 FLYING WING ROTATION MECHANISM OF MICRO AIR VEHICLE
摘要 A flying wing rotation mechanism of a micro air vehicle is driven under a control of a power module and a detent member. The flying wing rotation mechanism of a micro air vehicle includes a flapping arm and a flying wing. The flapping arm is connected to the detent member, and swings as the power module drives the detent member. An end of the flying wing is pivoted to the flapping arm. When the flapping arm swings, the flying wing swings with the flapping arm in sync. When swing direction of the flapping arm changes, the flying wing rotates relative to an axial direction of the flapping arm.
申请公布号 US2007210207(A1) 申请公布日期 2007.09.13
申请号 US20070748635 申请日期 2007.05.15
申请人 发明人 LIAO WEI-HSIANG
分类号 B64C33/00 主分类号 B64C33/00
代理机构 代理人
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