发明名称 A GYROSCOPIC AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING
摘要 PURPOSE: A vertical takeoff and landing aircraft using a gyroscopic principle is provided to rapidly and elaborately control and to stably keep the posture of an aircraft with a gyroscope. CONSTITUTION: A vertical takeoff and landing aircraft using a gyroscopic principle comprises a rotation body(40) and wings(30). A first engine(50) is mounted on the rotation body to rotate the rotation body through the first engine and served as a gyroscope. The wings are mounted on the rotation body to be rotated with the rotation body, thereby generating upward force.
申请公布号 KR20120038713(A) 申请公布日期 2012.04.24
申请号 KR20100100316 申请日期 2010.10.14
申请人 KOREA RESEARCH INSTITUTE OF STANDARDS AND SCIENCE 发明人 KOO, JA YONG
分类号 B64C29/00;A63H27/127;B64C27/20;B64C39/06 主分类号 B64C29/00
代理机构 代理人
主权项
地址