A VERTICAL TAKE-OFF AND LANDING AIRPLANE
A vertical takeoff and landing aircraft is provided to prevent unbalance of a lift force appearing in a pulsator when the air plane straightly flies by rotating a blade in a case. A vertical takeoff and landing aircraft includes a body(120), at least two rotation section(130), and a case(201). The r...
Saved in:
Main Author | |
---|---|
Format | Patent |
Language | English |
Published |
25.10.2006
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Summary: | A vertical takeoff and landing aircraft is provided to prevent unbalance of a lift force appearing in a pulsator when the air plane straightly flies by rotating a blade in a case. A vertical takeoff and landing aircraft includes a body(120), at least two rotation section(130), and a case(201). The rotation section includes a rotational shaft and a blade. The rotation section is connected to the body. The case covers the body and the rotation section. An opening is formed in the case. The case has a duct-like shape in which the opening is formed so as to surround the rotation section. The case includes a side wall at the circumference of the blade of the rotation section. |
---|---|
Bibliography: | Application Number: KR20050032736 |