公开(公告)号：WO2011056082A3

公开(公告)日：2011-08-25

申请号：PCT/PL2010000110

申请日：2010-11-05

Applicant: MARGANSKI EDWARD

Inventor： MARGANSKI EDWARD

IPC: B64C39/12

CPC classification number: B64C5/04 ,  B64C9/10 ,  B64C39/12

Abstract: The object of the invention is an aircraft provided with a device for creating a constant moment in relation to the axis of rotation of an additional control surface placed at the front of the aircraft at an as large as possible distance from the centre of gravity of the aircraft. The aircraft is characterised in that the control of the aerodynamic vertical force (7) is effected by deflecting control elements (3) pivotably mounted on the rotation axis (4), the deflection of said control elements causing rotation of a balance and control surface (1) mounted rotatably on axis (2), wherein the axis (2) is mounted perpendicularly to the plane of symmetry (5) of aircraft (6) forward of the resultant aerodynamic vertical force (7) generated by the balance and control surface (1).

Abstract translation: 本发明的目的是提供一种飞行器，该飞行器用于相对于放置在飞机前部的附加控制表面的旋转轴线产生恒定的力矩，该力矩与飞行器的重心距离尽可能大 飞机。 该飞行器的特征在于，通过偏转枢转地安装在旋转轴线（4）上的控制元件（3）来实现气动垂直力（7）的控制，所述控制元件的偏转导致平衡和控制表面（ 其中轴（2）垂直于飞机（6）的对称面（5）安装在由平衡和控制表面（7）产生的合成气动垂直力（7） 1）。