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Vertical Take-off Devices with Jet-Vortex Lift Generators

https://doi.org/10.30932/1992-3252-2019-17-1-46-57

Abstract

A theoretical and calculational substantiation of a possibility of implementing a qualitatively new design scheme of an aircraft of vertical take-off, in which the lifting force is initiated by a single vortex, artificially created over the aircraft, and the resulting static pressure drop above and below the device is presented. Decisions on vortex flows generated by a rotating disk and tornado-like vortexes arising in the atmosphere are analyzed. Layout schemes of an apparatus for vertical take-off of two types are proposed - with vortex and jet-vortex lift generators. In both schemes, it is supposed to use vertically mounted bi-rotor drive motors, in which both the rotor and the stator rotate, but in mutually opposite directions.

About the Authors

N. N. Ostroukhov
Moscow Aviation Institute (National Research University) (MAI)
Russian Federation

Ostroukhov, Nikolai N. - Ph.D. (Physics and Mathematics), senior lecturer, associate professor of the department of Theoretical Electrical Engineering



E. V. Chumakova
Moscow Aviation Institute (National Research University) (MAI)
Russian Federation

Chumakova, Ekaterina V. - Ph.D. (Physics and Mathematics), associate professor of the department of Computer mathematics MAI



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Review

For citations:


Ostroukhov N.N., Chumakova E.V. Vertical Take-off Devices with Jet-Vortex Lift Generators. World of Transport and Transportation. 2019;17(1):46-57. https://doi.org/10.30932/1992-3252-2019-17-1-46-57

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ISSN 1992-3252 (Print)