FIELD: engines and pumps.
SUBSTANCE: rotary sector internal combustion engine includes stator frame with cavity of cylindrical shape. Stator frame is a part of airborne vehicle. Disc of airborne vehicle is installed in stator frame on hollow shaft installed on hollow axis. Stator frame and disc of airborne vehicle are divided into the main and filling sectors consisting of parts of primary and secondary movable working chambers. Elements of primary and secondary movable working chambers with inlet channels, ignition plugs and parts of nozzle assemblies are provided in cavity of stator frame. Parts of nozzle assemblies form movable nozzle assemblies during rotation of airborne vehicle disc, via which the product is supplied to front walls of movable combustion chambers and exhaust gas leaves the outlet nozzles. Complete rotation of engine shaft is performed at actuation of the number of movable combustion chambers, which is equal to the product of squared number of the main sectors accepted on the engine times the number of filling sectors in the main sector and times the number of primary and secondary movable combustion chambers in the main sector, which participate simultaneously in the cycle (operating stroke), at provision of application of kinetic energy of the product from movable combustion chambers to disc of the airborne device of rotor at several points in circumferential direction of cavity of stator frame and multiple participation in the operation of one and the same movable combustion chambers at one revolution of engine rotor.
EFFECT: creation of engine for disc-type airborne vehicle.
3 cl, 15 dwg
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Authors
Dates
2012-10-20—Published
2010-09-14—Filed