ZOLOTNIKOVY INTERNAL COMBUSTION ENGINE AND FUEL COMBUSTION METHOD

摘要

A spool internal combustion engine, including a housing in which a combustion chamber with blind channels is located, a rotating spool with a recess through which the working fluid is supplied and removed through the first or second blind channel, tangentially, characterized in that a universal device is used - a generator, kinematically connected with a compressor and a consumer for converting compressed air, fuel, energy spent on ignition into the energy of expanding gases, in a spherical loop vortex combustion chamber with its two blind channels located in series along the direction of rotation of the spool and cyclically overlapping by a spool with an internal recess deployed in the side of the combustion chamber with the use of channels, where the first is transferred compressed air from the compressor, the second channel removes the energy of the expanding gases from the combustion chamber, including multifunctional, or into the main combustion chamber of the power ICE with the ability to burn steam fuel Lleno or sequentially in two combustion chambers, or in one of them, or on an actuator blade and a working stroke within 300 degrees of rotation of the rotor, or on an actuator blade with its own charge of compressed air, or without it, or using it as a detonator for detonation ignition and swirling of vortex flows in an annular vortex loop combustion chamber with a tangential exhaust torus, where a distinctive feature of the combustion chamber (detonator) is that one blind duct is used for supplying compressed air, the third production duct