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 |
|