公开(公告)号：WO2005014391A8

公开(公告)日：2005-04-14

申请号：PCT/RU2004000250

申请日：2004-06-29

Applicant: DEMIN ALEXSANDR PAVLOVICH ,  DEMIN SERGEI ALEXANDROVICH

Inventor： DEMIN ALEXSANDR PAVLOVICH ,  DEMIN SERGEI ALEXANDROVICH

IPC: B64C27/22 ,  B64C27/28 ,  B64C29/00 ,  B64C31/024 ,  B64D27/06

CPC classification number: B64C27/28 ,  B64C29/0033 ,  B64C31/024 ,  B64D27/06

Abstract: The invention relates to multipurpose heavier-than-air aircrafts which can be used in the form of an airplane, helicopter or a sailplane. The inventive multipurpose heavier-than-air aircraft consists of a body comprising a tail assembly which is provided with a rudder, a pitch control surface and a chassis. A lifting forwardswept wing is fixed to the centre wing section of the body. A slotted opening closed with shutters is embodied in the top section of the body, wherein a driving engine used for sailplane mode and provided with a thrust propeller fixed to the shaft thereof is arranged. Said driving engine is cinematically connected to a carriage displacement drive by means of a main strut displacing mechanism. The carriage is provided with the position lock thereof corresponding to airplane, helicopter and sailplane flight modes. The carriage displacement drive is connected to an asymmetrical lever displacement mechanism. The major arm of said asymmetrical lever and an auxiliary strut are pivotally connected to the driving engine. Said auxiliary strut is pivotally connected to the rockshaft of the asymmetrical lever my means of a mechanism.

Abstract translation: 本发明涉及可以以飞机，直升机或滑翔机的形式使用的多用途重型飞机。 本发明的多用途重型飞机由包括尾部组件的主体组成，尾部组件设置有方向舵，俯仰控制表面和底盘。 抬起的前卫翼固定在身体的中心翼部分。 具有快门的开槽开口体现在主体的顶部，其中设置有用于帆板模式的驱动引擎，并且设置有固定在其轴上的推力推进器。 所述驱动发动机通过主支柱移位机构电动连接到滑架移动驱动装置。 滑架具有对应于飞机，直升机和帆板飞行模式的位置锁定。 滑架位移驱动器连接到不对称的杠杆位移机构。 所述不对称杆和辅助支柱的主臂枢转地连接到驱动发动机。 所述辅助支柱枢转地连接到不对称杠杆的轴心，其机构的装置。