The invention relates to: a body (2); a rotor (3) positioned to extend outwardly from inside the body (2) and to rotate about its axis; at least one blade (4) extending outwardly from the rotor (2) and providing lift and/or thrust to the body (2) by its movement; at least one outer blade (401) positioned in the blade (4) and providing lift and/or thrust for the body (2); at least one mechanism (5) enabling the outer blade (401) to be switched from a contracted first position, in which the outer blade is approximately completely located in the blade (4), to a second position, in which the outer blade extends outwardly from the blade (4), by means of a linear movement under the influence of a centrifugal force generated during the movement of the rotor (2).
本发明涉及:本体(2);旋翼(3),定位成从本体(2)内向外延伸并围绕其轴线旋转;至少一个叶片(4),从旋翼(2)向外延伸并通过其运动为本体(2)提供升力和/或推力;至少一个外部叶片(401),定位在叶片(4)中并为本体(2)提供升力和/或推力;至少一个机构(5),使得外部叶片(401)能够通过在旋翼(2)的运动期间所产生的离心力的影响下进行线性移动而从收缩的第一位置切换到第二位置,在第一位置中,外部叶片近乎完全位于叶片(4)中,在第二位置中,外部叶片从叶片(4)向外延伸。
Rotor craft
旋翼飞行器
2023-09-22
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |