发明名称 TAKING OFF AND LANDING AIRPLANE USING VARIABLE ROTARY WINGS
摘要 PURPOSE: A vertical take-off and landing aircraft using variable rotary wings is provided to create thrust by employing a propeller engine and creating backward thrust with the rotary wings, thereby enabling efficient aviation. CONSTITUTION: A vertical take-off and landing aircraft comprises rotary wings, a tilting drive unit, and a propeller engine. The rotary wings create a floating force for the aircraft to take off. The tilting drive unit receives a signal from a cockpit and tilts a drive shaft to turn the rotary wing 90° to the front of a flying wing when the aircraft flies at middle-high speed. The propeller engine generates thrust and advances with the rotary wings which rotate to the front of the flying wing and propel frontward. The tilting drive unit comprises a receiver receiving a signal from the cockpit, a control device, and a servo motor which generates a rotating force for driving a pinion.
申请公布号 KR20100026130(A) 申请公布日期 2010.03.10
申请号 KR20080085010 申请日期 2008.08.29
申请人 LIM, CHAE HO 发明人 LIM, CHAE HO
分类号 B64C29/02;B64C27/08;B64C27/22 主分类号 B64C29/02
代理机构 代理人
主权项
地址