FIELD: engines and pumps.
SUBSTANCE: rotary-bladed internal combustion engine includes chamber with closed volume, inlet and outlet openings of waste gases, insulation mechanism of suction cavity from exhaust cavity and carrier concentrically fixed on power takeoff shaft. Chamber is formed with surfaces of fixed housing and plate-like rotor blades dividing the inner volume of chamber into cavities. Shaft is eccentrically located relative to fixed rotor axis. Insulation mechanism is kinematically connected to shaft by means of pinions and includes cylindrical separating element with opposite located slots on one end for interaction with plate-like blades, which is arranged in the pocket provided in the chamber, and support element. Power takeoff shaft is mounted on supports in the cover and partition separating the chamber from mounting cavity formed with the cover. Carrier is made in the form of a shell with longitudinal slots as per the number of plate-like blades. Some ends of blades are mounted with possibility of rotation on fixed axis of rotor, and other ends are arranged in longitudinal slots with possibility of interaction with insulation mechanism of cavities and carrier. Support element is arranged in mounting cavity. Electric power supply mechanism of spark plug is mounted on the end of support element. Flywheel is installed on power takeoff shaft end.
EFFECT: improving efficiency and simplifying the engine design.
1 cl, 2 dwg
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Authors
Dates
2011-06-27—Published
2009-03-30—Filed