RU2008111037A - DISC-like FLIGHT VEHICLE WITH VERTICAL TAKE-OFF AND LANDING, WITH INERTIAL MOTORS AND WAYS OF ITS WORK - Google Patents
DISC-like FLIGHT VEHICLE WITH VERTICAL TAKE-OFF AND LANDING, WITH INERTIAL MOTORS AND WAYS OF ITS WORK Download PDFInfo
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- RU2008111037A RU2008111037A RU2008111037/11A RU2008111037A RU2008111037A RU 2008111037 A RU2008111037 A RU 2008111037A RU 2008111037/11 A RU2008111037/11 A RU 2008111037/11A RU 2008111037 A RU2008111037 A RU 2008111037A RU 2008111037 A RU2008111037 A RU 2008111037A
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- vertical
- propulsion
- thrust
- aircraft
- landing
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Abstract
1. Дискообразный летательный аппарат с вертикальным взлетом и посадкой, содержащий корпус, поршневой двигатель внутреннего сгорания или газотурбинный двигатель, спаренный с электрогенератором постоянного тока, отличающийся тем, что вертикальный взлет и мягкую вертикальную посадку обеспечивает мощный инерционный движитель вертикальной тяги, а горизонтальный полет в любом направлении обеспечивают четыре инерционных движителя горизонтальной тяги, при этом все движители приводят в действие электродвигатели, присоединенные к электрогенератору, и направления всех сил тяги проходят через центр инерции летательного аппарата. ! 2. Способ работы летательного аппарата по п.1, отличающийся тем, что первоначально запускают двигатель внутреннего сгорания, спаренный с электрогенератором, и, включив электродвигатель постоянного тока с регулируемым числом оборотов в единицу времени, запускают движитель вертикальной тяги и плавно увеличивают число оборотов электродвигателя и величину силы вертикальной тяги, которая поднимает летательный аппарат на заданную высоту, а затем включают один или два движителя горизонтальной тяги для полета в заданном направлении. ! 3. Способ работы летательного аппарата по п.1 при посадке, отличающийся тем, что после достижения цели полета отключают один или два инерционных движителя, обеспечивающих полет, и включают один или два движителя горизонтальной тяги с противоположным направлением силы горизонтальной тяги, что позволяет затормозить летательный аппарат над местом посадки, после чего постепенно снижают число оборотов электродвигателя движителя вертикальной тяги и так плавно 1. A disk-shaped aircraft with vertical take-off and landing, comprising a hull, a piston internal combustion engine or a gas turbine engine paired with a direct current electric generator, characterized in that the vertical take-off and soft vertical landing provides a powerful inertial propulsion of vertical thrust, and horizontal flight in any four inertial horizontal thrust propulsors provide direction, with all propulsion motors driving electric motors connected to the electrog nerator, and the directions of all thrust forces pass through the center of inertia of the aircraft. ! 2. The method of operation of the aircraft according to claim 1, characterized in that the internal combustion engine is paired with an electric generator, and by turning on a direct current electric motor with an adjustable speed per unit time, the vertical thrust propulsion is started and the electric motor speed is gradually increased and the magnitude of the vertical thrust force that raises the aircraft to a predetermined height, and then include one or two horizontal thrust propulsion devices for flying in a given direction. ! 3. The method of operation of the aircraft according to claim 1 during landing, characterized in that after reaching the flight objective, one or two inertial propulsion engines providing flight are turned off and one or two horizontal thrust propulsion devices with opposite direction of horizontal thrust force are used, which allows the aircraft to brake the device above the landing site, after which they gradually reduce the number of revolutions of the electric motor of the vertical thrust propulsion device and so smoothly
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008111037/11A RU2008111037A (en) | 2008-03-25 | 2008-03-25 | DISC-like FLIGHT VEHICLE WITH VERTICAL TAKE-OFF AND LANDING, WITH INERTIAL MOTORS AND WAYS OF ITS WORK |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008111037/11A RU2008111037A (en) | 2008-03-25 | 2008-03-25 | DISC-like FLIGHT VEHICLE WITH VERTICAL TAKE-OFF AND LANDING, WITH INERTIAL MOTORS AND WAYS OF ITS WORK |
Publications (1)
Publication Number | Publication Date |
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RU2008111037A true RU2008111037A (en) | 2009-09-27 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2008111037/11A RU2008111037A (en) | 2008-03-25 | 2008-03-25 | DISC-like FLIGHT VEHICLE WITH VERTICAL TAKE-OFF AND LANDING, WITH INERTIAL MOTORS AND WAYS OF ITS WORK |
Country Status (1)
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RU (1) | RU2008111037A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10407178B2 (en) | 2014-08-04 | 2019-09-10 | Israel Aerospace Industries Ltd. | Propulsion system assembly |
-
2008
- 2008-03-25 RU RU2008111037/11A patent/RU2008111037A/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10407178B2 (en) | 2014-08-04 | 2019-09-10 | Israel Aerospace Industries Ltd. | Propulsion system assembly |
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