发明名称 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT |
摘要 |
A vertical take-off and landing aircraft comprises: a propeller (2) which generates lift and thrust; a main frame (4) which supports a seat (41) and ground contact legs (42); a sub frame (5) which supports the propeller (2) and is rotatably disposed in a front-back direction with respect to the main frame (4); a power supply means (3) which is supported by the main frame (4) and supplies power to the propeller (2); a control stick (6) which is connected to the sub frame (5); and a main wing (7) which is disposed in the propeller (2), the main wing (7) being configured to usually retreat to a position that does not interfere with an air current generated by the propeller (2), and when the thrust is lost, be able to move to a position at which the lift is generated. Consequently, gliding becomes possible even when the thrust is lost while an increase in the size of the body thereof is suppressed. |
申请公布号 |
WO2014185492(A1) |
申请公布日期 |
2014.11.20 |
申请号 |
WO2014JP62955 |
申请日期 |
2014.05.15 |
申请人 |
IHI CORPORATION |
发明人 |
TSUNEKAWA, MASAYOSHI;TAMURA, TETSUYA |
分类号 |
B64C29/00;B64C27/20;B64C27/22 |
主分类号 |
B64C29/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|