RU2012143742A

RU2012143742A - VERTICAL TAKEOFF AND LANDING DEVICE

Info

Publication number: RU2012143742A
Application number: RU2012143742/11A
Authority: RU
Inventors: Пётр Иванович Дуров
Original assignee: Пётр Иванович Дуров
Priority date: 2012-10-15
Filing date: 2012-10-15
Publication date: 2014-04-20
Also published as: WO2014062091A1; RU2520821C2

Abstract

Летательный аппарат вертикального взлета и посадки, содержащий корпус круглой формы или в форме эллипса с выпуклой верхней поверхностью и плоской нижней поверхностью с выступающей вниз его центральной частью, где расположены кабина с системой управления и силовой отсек, вертикальные сквозные отверстия, оси из труб с поворотными механизмами и угловыми редукторами и опорами, лобовой и кормовой поворотные механизмы, выдвижные шасси, гидравлическую систему, автопилот, парашюты с пиропатроном, откидной обтекаемый прозрачный купол, систему видеообзора, пороховые аварийные двигатели, отличающийся тем, что четыре вертикальные сквозные отверстия выполнены в форме овалов, малые оси симметрии двух из которых расположены вдоль продольной оси симметрии корпуса и двух других расположены вдоль поперечной оси симметрии корпуса, а внутри этих отверстий вдоль их малых осей симметрии установлены поворотные оси из труб, и также тем, что силовая установка состоит из не менее четырех двигателей, а вращение от двигателей передается через трансмиссии на не менее чем шесть воздушных винтовентиляторов, способных изменять общий шаг как совместно, так и раздельно.A vertical take-off and landing aircraft containing a round or elliptical body with a convex upper surface and a flat lower surface with its central part protruding downwards, where a cabin with a control system and a power compartment, vertical through holes, axles made of pipes with rotating mechanisms are located and angular gearboxes and supports, frontal and stern turning mechanisms, retractable landing gear, hydraulic system, autopilot, parachutes with squib, folding streamlined transparent dome, video viewing system, powder emergency engines, characterized in that four vertical through holes are made in the shape of ovals, small the axes of symmetry of two of which are located along the longitudinal axis of symmetry of the body and the other two are located along the transverse axis of symmetry of the body, and inside these holes along their small axes of symmetry there are rotary axes made of pipes, and also because the power plant consists of at least four engines, and the rotation from the engines is transmitted through transmissions to no less than six air propfans, capable of changing the overall pitch both jointly and separately.

Claims

Aircraft of vertical take-off and landing, comprising a round or elliptical hull with a convex upper surface and a flat lower surface with its central part protruding downward, where the cockpit with the control system and power compartment, vertical through holes, pipe axles with rotary mechanisms are located and angular gears and bearings, frontal and stern swivel mechanisms, retractable landing gears, hydraulic system, autopilot, parachutes with a squib, hinged streamlined transparent dome, system video review, powder emergency engines, characterized in that the four vertical through holes are made in the form of ovals, the small axis of symmetry of two of which are located along the longitudinal axis of symmetry of the shell and the other two are located along the transverse axis of symmetry of the shell, and inside these holes along their small axis of symmetry rotary axes made of pipes are installed, and also because the power plant consists of at least four engines, and rotation from the engines is transmitted through the transmissions to at least six propellers ntilyatorov capable of changing the collective pitch both together and separately.