Way to create a sum of forces thrust propulsion device USING TOROOBRAZUYUSCHEGO ICE TANDEM detonator ring vortex combustion chambers

摘要

A method for creating a sum thrust forces using reactive force toroobrazuyuschego ICE and tandem detonator annular swirl combustion chamber, wherein the vehicle body, the skirt having a through passage through the annular spherical vortex combustor with detonator, being the small combustion chamber, the inlet of which groove of the annular chamber combustion or with a detonator, which is a cyclic combustion chamber with the blind bore and the spool, wherein the frequency of cycles increases with the number of internal stems pits in the slide valve for supplying air to the detonator, with fuel injection, ignition, such as spark discharge, electric arc, laser and expanding gases energy transfer nozzle normally along the annular combustion chamber axis, whereby detonation waves move circularly annular combustion chamber with offset lightweight high temperature flame to the inner diameter, through which flows the energy of expanding gas to the annular slit nozzle with tangential short cylindrical inner n oskostyu with which exhaust breaks, forming the eversible torr where exhaust torus dual acceleration of eversible side draws air through the through passage, which is used for high-speed combustion of hydrogen, hydrogen fluoride, methanol or other fuels with the injection point extractor-fed through a check valve plane under the dome, under high temperature and shock mikrokupolom ignition torus exhaust, wherein the uneven supply allows smooth and fast maneuver in easy